DNVGL-ST-0377 Shipboard lifting appliancesStandard — DNVGL-ST-0377. Edition October 2018 Page 3...
Transcript of DNVGL-ST-0377 Shipboard lifting appliancesStandard — DNVGL-ST-0377. Edition October 2018 Page 3...
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DNV GL AS
STANDARD
DNVGL-ST-0377 Edition October 2018
Shipboard lifting appliances
FOREWORD
DNV GL standards contain requirements principles and acceptance criteria for objects personnelorganisations andor operations
copy DNV GL AS October 2018
Any comments may be sent by e-mail to rulesdnvglcom
This service document has been prepared based on available knowledge technology andor information at the time of issuance of thisdocument The use of this document by others than DNV GL is at the users sole risk DNV GL does not accept any liability or responsibilityfor loss or damages resulting from any use of this document
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CHANGES - CURRENT
This document supersedes the May 2016 edition Changes in this document are highlighted in red colour However if the changes involve a whole chaptersection or subsection normally only the title will be in red colour
Changes October 2018 entering into force as from date ofpublication
bull Sec1mdash Revision of definitionsmdash Topic Design temperature ([117] and [118]) deleted (shifted to and merged with [423])mdash Clarification on certification process
bull Sec2mdash Table 2-1 Documentation requirements revised and column Additional description completed
bull Sec3mdash This section has been aligned with DNVGL-ST-0378
bull Sec4mdash [423] Design temperature revised Previous [117] and [118] have been includedmdash See DNVGL-CG-0194 included in [492] Hydraulic cylinders
bull Sec7mdash Second paragraph in [73611] has been replaced completelymdash Revision of Table 7-4 Static test loads for interchangeable components concerning single-sheaved blocks
bull Sec8mdash Obsolete topic natural fibre ropes has been removed from this standardmdash [812] Certification requirements is a new paragraph Previous [812] Approval for manufacture has
been replaced completelymdash Requirements for metallic rope sheaves revised see [82422]mdash Table 8-3 Minimum diameter of rope sheaves and rope drums revised (increased values in column nominal
tensile strength of wire ropes)mdash Clarification on tensile tests of wire ropes (additional paragraph [85112] and additional Table 8-6)mdash Specification of dimensional check of wire ropes (additional paragraph [85113])mdash Specification of wire ropes identification colours see [85114]mdash Revision of discard criteria for wire ropes see [8533]
bull Sec9mdash Previous Table 9-1 deleted
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bull Sec11mdash Clarification on requirements concerning cold forming see [11233]mdash Clarification on requirements concerning corrosion protection of bolts and nuts see [112355]mdash Clarification on requirements concerning welding consumables see [112441]mdash Revision of the requirements for welding in cold-formed areas see [11327]mdash Revision of the requirements for non-destructive tests see [1158]
bull Sec12mdash Clarification concerning emergency exits see [122132]
bull Sec13mdash Clarification on certification and reporting of manufacturing surveys and tests see [1327]mdash Clarification on initial load tests see [133312]
Editorial correctionsIn addition to the above stated changes editorial corrections may have been made
Con
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DNV GL AS
CONTENTS
Changes - current3
Section 1 General information 911 Introduction912 Services 1813 Certification procedure 2014 Type of services22
Section 2 Documentation and certification 2421 Documentation to be submitted2422 Certification 27
Section 3 Materials3031 General 3032 Rolled structural steel for welding3133 Rolled steel not for welding3434 Steel forgings 3435 Steel castings 3836 Iron castings 3837 Steel tubes pipes and fittings 3938 Aluminium alloy structures3939 Composite materials 39310 Wires for ropes39
Section 4 Design and calculation principles 4241 General 4242 Design principles 4243 Calculation principles5044 Proof of structural safety 5545 Proof of safety against overturning 5846 Proof of fatigue strength 5947 Proof of suitability for use7348 Joints 7449 Special structural elements 82
Section 5 Cranes and supporting structures 9851 General 9852 Crane groups 99
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53 Design loads 10154 Hoist load coefficients 10755 Load combinations and partial safety factors 11256 Proofs 11657 Requirements for design and equipment 119
Section 6 Special lifting appliances and means of transport 12861 General 12862 Rope and chain hoists 12863 Ramps and car decks13264 Lifting appliances for research work13665 Industrial cargo-handling vehicles13766 Means of conveying persons or personnel 138
Section 7 Load-handling devices and interchangeable components 14171 General 14172 Load-handling devices 14173 Interchangeable components15174 Marking of load-handling devices and interchangeablecomponents 15975 Wear damage repair 162
Section 8 Ropes and rope accessories 16481 General 16482 Wire ropes 16483 Synthetic fibre ropes 17084 Rope-end attachments17285 Tests and examinations 17486 Documentation176
Section 9 Mechanical parts 17891 General 17892 Design criteria and operational requirements17993 Power drives18094 Slewing gears and slew rings 18095 Winches 18296 Hydraulic systems18597 Protective measures and safety devices 18798 Assessment of drawings and manufacturing survey 18799 Documentation189
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Section 10 Electrical equipment191101 General 191102 Design criteria and operational requirements192103 Drives and brakes192104 Cables and lines194105 Switches195106 Protective measures and safety devices 196107 Assessment of drawings and manufacturing survey 198108 Documentation199
Section 11 Construction of steel components 200111 General 200112 Requirements for manufacturers 200113 Design details 204114 Types of welds209115 Workmanship and testing of weld joints214116 Assessment of drawings and manufacturing survey 218117 Documentation219
Section 12 Technical and operational safety requirements 220121 General 220122 Design requirements220123 Equipment224124 Safety devices225125 Passive protective measures228126 Stowage and lashing devices228127 Operational requirements 229
Section 13 Testing and examination of shipboard lifting appliances 232131 General 232132 Manufacturing survey 233133 Initial test and examination 239134 Periodic tests and examinations 242135 Extraordinary tests and examinations 246136 Wear damage repair 248137 Lifting appliance documentation253
Appendix A Calculation of dynamic forces due to motions of the ship257A1 General 257
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A2 Dynamic forces generated by ships and similar floating bodies 257A3 Dynamic forces due to pontoons or barges260
Appendix B Detail classification for fatigue strength analysis (FAT classes) 261B1 261
Appendix C Wind loads form and sheltering coefficients275C1 General 275C2 Form coefficients cf 275C3 Sheltering coefficients η 276
Appendix D Rigging plan279
Changes ndash historic 280
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DNV GL AS
SECTION 1 GENERAL INFORMATION
11 Introduction
111 Objective
1111 This standard provides requirements for certification and verification of lifting appliances intended forload handling within and outside ship while in the harbour or in sheltered waters and within the ship while atsea
Guidance noteFor lifting appliances intended for load handling outside ship while at open sea and load handling onboard offshore unitsinstallations see DNVGL-ST-0378 Standard for offshore and platform lifting appliances
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112 Scope
1121 This standard covers the design materials fabrication installation testing and commissioning ofshipboard lifting appliances and industrial lifting appliancesThe categorization of lifting appliances is based on installation and intended function for the lifting appliance
a) Shipboard lifting appliances
mdash lifting appliances on board ships intended for load handling within and outside ships while in theharbour and within ships while at sea
b) Industrial lifting appliances
mdash lifting appliances onshore and offshore not covered by a) and DNVGL-ST-0378Guidance noteThe main purpose of the lifting appliance will define the category of the lifting appliance and relevant applicable standard
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1122 Each lifting appliance has its separate intended functions Examples of intended functions are butnot limited to
mdash loading and discharging of shipsmdash handling of provision store and spare parts cargo hoses gangways and ammunitionmdash handling of Suez canal boats and search lightsmdash conveyance of personspersonnelmdash handling of ramps and moveable cargo decks etc
1123 Requirements presented herein are minimum requirements to be satisfied although subject toacceptance by the Society other minimum requirements may be agreed eg based on new technologyavailable at the time of application for certification
1124 The requirements of this standard may be supplemented with additional requirements whereinstallation of specific design or assessment shows that standards that provide equivalent or higher level ofintegrity and safety are more appropriate
1125 The standard consists of a three level hierarchy of documents
mdash Sec1 and Sec2 provide principles and procedures of the Societys classification certification verificationand consultancy services
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mdash Sec3 through Sec13 provide technical provisions and acceptance criteria as well as the technical basis forthe services stated in the first two sections
mdash Appendices provide proven technology and sound engineering practice as well as guidance for the higherlevel documents mentioned in this document
1126 This standard distinguishes between
mdash information and description of servicesmdash requirements
Consequently these two subjects are separated and the standard is divided into three parts
mdash Sec1 to Sec2 General information application definitions and references Description of applicableservices and relations to rules and regulation from institutions other than the Society
mdash Sec3 to Sec13 Requirements and technical provisionsmdash Appendices
113 Application
1131 This standard shall be applied for certification of shipboard lifting appliances for ships with classnotation Crane This standard may also be applied as voluntary basis for verification and certification oflifting appliances and load-handling devices that are not classed with the Society
Guidance noteThe standard may also be applied to industrial cranes
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1132 The requirements presented herein should be applied consequently from concept design through thefinal construction including major modifications Alternatives to detailed requirements in this standard maybe accepted when the overall safety and reliability level is found to be equivalent or better than that of thisstandard Approval may be revoked if subsequent information indicates that the chosen alternative is notsatisfactory
1133 Specifications of the services provided by this standard are given in [12] and [14]
1134 The standard does not apply to launching appliances for LSA (except Sec3 and Sec11) launchinggear for diving equipment and ROVs structural parts of ramps and car decks dredging appliances whichare no loading gear personnel lifts (elevators) jacks overhead drilling equipment portable hoisting gearsuspensions (if not integral component of a load-handling device) etc
1135 Personnel lifting with cranes otherwise designed for lifting of loadscargo may be covered uponagreement
1136 Without prejudice to [1124] deviations from the requirements given in this standard may onlybe substituted where shown to provide an equivalent or higher level of integrity or safer than under thisstandard
1137 At the Societyrsquos discretion equivalent solutions and exemptions from the requirements given in thisstandard may be accepted
1138 In case of conflict between requirements given in this standard and a reference document therequirements given in this standard shall prevail
1139 Where reference is made to codes other than the Societys documents the valid revision shall betaken as the revision which was current at the date of issue of this standard unless otherwise noted
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114 Relation to the Societys other documents
1141 For lifting appliances covered by the class notation Crane see DNVGL-RU-SHIP Pt6 Ch5 Sec3Permanently installed cranes ndash Crane
115 Definitions abbreviations symbols and references1151 Active cable tensioning system (ACT)System keeping the tension of the hoisting wire to a given set point value
Guidance noteA supply of external energy is required
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1152 Active heave compensation system (AHC)System that maintains the position of the load to a given set point value
Guidance noteA supply of external energy is required
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1153 Class notationsReference is made to DNVGL-RU-SHIP Pt1 Ch1 Sec1
1154 Ship type notationCode used by the classification societies to define a type of vessel related to its most typical service (Multi-purpose dry cargo Bulk carrier Container ship and Crane vessel are typical examples) Reference ismade to DNVGL-RU-SHIP Pt1 Ch2 Sec3
1155 Automatic overload protection system (AOPS)A system that automatically safeguards and protects the crane against overload and ldquoover-momentrdquo duringoperation by allowing the hook to be pulled away from the crane in order to avoid significant damage
1156 Declaration of conformityA document attesting that a product or service is in conformity with specific standards or technicalspecifications (ISOIEC 17050 Conformity assessment - Suppliers declaration of conformity) Issued bymanufacturer or vendor
1157 Competent personbodyPerson or body possessing knowledge and experience required for performing thorough examination and testof lifting appliances and loose gear and who is acceptable to the competent authority
1158 Crane stiffnessCoefficient defined as the force applied on the hook necessary to obtain a unit deflection at the hook level
1159 CustomerAgreement (contract) holder with the Society Signifies the party who has requested the Societyrsquos service
11510 Dead loadsDead loads are the weights of all the fixed and mobile components of lifting appliances and loose gearpermanently present during operationFor the purpose of marking the dead loads of loose gear are designated as weight by the ILO The unit isspecified in tonnes (t) or kilograms (kg)
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11511 DesignerReference is made to DNVGL-RU-SHIP Pt1 Ch1 Sec1
11512 Design approvalVerifying that a design represented by a drawing or set of drawings is found to comply with all requirementgiven in a specified Society standard or Society regulation
Guidance noteIn the Societys business procedures design approvals are valid for one order only One order however may include a specifiednumber of units for specified locationsvessels
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11513 Design approval letterWritten confirmation of a design approval
11514 Design assessment for type approvalAssessment and acceptance of a design for type approval The type approval will be assigned first after aprototype test also has been successfully carried out
11515 Design verification report (DVR)Formalized report confirming the result of a completed design verification assignment
11516 Hoist load coefficientAlso referred to as dynamic amplification factor (DAF)A variable factor representing the vertical dynamic effects that the hoist load is exposed to
11517 Dynamic hoist loadThe hoist load when subjected to (multiplied with) a hoist load coefficient
11518 Dynamic working loadThe working load when subjected to (multiplied with) a hoist load coefficient
11519 Engineered liftSafe lift planned by qualified engineers with basis in thorough information with respect to crane capacitycrane functions and performance rigging crane support as well as weather and sea conditions
11520 Fixed load-lifting attachmentsAny equipment from which the working load for lifting appliance can be suspended and which is permanentlyfastened to the lower end of the hoist medium see Figure 1-1Fixed load-lifting attachments are part of the lifting appliance
11521 Heavy lift craneCrane with SWL above 250 t
11522 Hoist loadSum of a lifting appliances working load the weight of its fixed load-lifting attachment(s) and half ofthe weight of that part of hoist medium which is arranged between rope exit point and fixed load-liftingattachment(s) see Figure 1-1The hoist load is subjected to inertia forces
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Figure 1-1 Definitions
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11523 Hoist mediumWire rope(s) chain(s) or other equipment hanging down from the lifting appliance for example from thecrab or the jib head operated by a winch etc used to lift and lower loads suspended from the lower end(s)of the hoist medium(s) see Figure 1-1Hoist mediums are part of the lifting appliance
11524 ILOInternational labour organization
11525 Inertia forcesThe forces induced by change of velocity
11526 Inspection certificate 31A document issued by the manufacturer which contains the results of all the required tests It shall certifythat the tests have been carried out by the manufacturer on samples taken from the delivered productsdirect See EN 10204 and ISO 10474
11527 Inspection certificate 32A document prepared by both the manufacturers authorized inspection representative independent of themanufacturing department and either the purchasers authorized representative or the inspector designatedby the official regulations and in which they declare that the products supplied are in compliance with therequirements of the order and in which test results are supplied See EN 10204 and ISO 10474
11528 Interchangeable componentsLoad-bearing not rigidly attached interchangeable parts which may be integral components of liftingappliances and loose gear eg hooks blocks shackles swivels rings chains claws clamps pliers loadfastening ropes (slingsstrops) lifting straps etc
11529 Lifting applianceMachine or appliance used for the purpose of lifting goods and materials or in special modes personnel
11530 Lifting equipmentGeneral expression including lifting appliances loose gear and other lifting attachments used separately orin combination
11531 Load chartDiagram or table showing safe working load of a lifting appliance depending on radius or boom angle forspecified operational conditions
11532 Load-handling deviceDevice (hook grab electromagnet fork traverse spreader or other) for grabbing holding or handling theload which is not part of the lifting appliance see Figure 1-1Load-handling devices are part of the loose gear
11533 Loose gearAny equipment which connects the payload with the lifting appliance and which does not form an integralpart either of the lifting appliance or of the payload
Guidance noteLoose gear is easily detachable from the lifting appliance and from the payload
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11534 Machinery componentsRotating components transferring torque for drivingbraking purpose Examples are gearboxes wheels andshafts
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11535 Man riding winchWinch specially designed for hoistinglowering of a person
11536 Manual overload protection system (MOPS)System activated by the crane operator protecting the crane against overload and ldquoover-momentrdquo byreducing the load-carrying capacity and allowing the hook to be pulled away from the crane
11537 Mean time to failure (MTTF)The mean value of service time until failure occurs
11538 MechanismDevices needed to cause or to stop a relative motion between two rigid parts of a crane between the craneand its foundation or between the crane and the lifted load Thus motors brakes transmission systems andsimilar components are defined as mechanisms
11539 Mobile deck craneA mobile deck crane is a cable-controlled crane mounted on crawlers or rubber-tired carriers or a hydraulic-powered crane with a boom mounted on truck-type carriers or as self-propelled types
11540 OverloadLoad which exceeds the safe working load (SWL)
11541 Over-momentLoad moment which exceeds the maximum load moment (safe working load (SWL) multiplied by radius)
11542 Passive cable tensioning system (PCT)System keeping the tension of the hoisting wire between predefined limits using stored energy
11543 Passive heave compensation system (PHC)System that maintains the position of the load between predefined limits using stored energy
11544 PayloadLoad which is lifted by the lifting appliance and suspended from the loose gear or if such loose gear is notused directly from the fixed load-lifting attachment(s) see Figure 1-1
Guidance noteIf lifting appliances are used for lifting the load from water the payload may also include forces due to water flow suction or wateradhering by suction
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11545 Product certificate (general)Reference is made to DNVGL-RU-SHIP Pt1 Ch3 Sec5 [22]
11546 Product certificate (the Societyrsquos)Reference is made to DNVGL-RU-SHIP Pt1 Ch3 Sec5 [24]
11547 PurchaserCompany or person who orders the lifting equipment from a manufacturer This standard does not necessarilyrequire that the purchaser will need to have any direct relationship to or communication with the Society
11548 RemarkDefect in terms of the ILO model form 1 found in a shipboard lifting appliance or in an item of loose gearwhich are not part of classRemarks do not influence the validity of class
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11549 REPRope exit point Location on the lifting appliance where the rope is suspended - typically found at the outersheave in the crane boom tip
11550 RiskCombination of the probability of occurrence (frequency) of harm and the severity (consequence) of theharm
11551 Risk control measure (RCM)A means of controlling a single element of risk typically risk control is achieved by reducing either theconsequence or the frequencies
11552 ROVRemote operated vehicle
11553 Running riggingWire ropes passing over rope sheaves of guide rollers or wound on winches irrespective of whether or notthe ropes are moved under load
11554 Safe working load (SWL)Also referred to as working load limit rated capacity or nominal loadSafe working load is the designation for the maximum permissible working load of lifting appliances loosegear or interchangeable components The abbreviation SWL is used for marking the lifting appliance loosegear and interchangeable componentsThe unit of SWL is specified in tonnes (t) or kilograms (kg)
Guidance noteLifting appliances and loose gear can have different safe working loads depending on varying equipment conditions or operationalconditions cable tackle systems or load radii
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11555 Significant wave height (H13)Average height of the highest one third of the individual wave heights in a short-term constant sea statetypically three (3) hours
11556 The SocietyThe Society signifies DNV GL
11557 Standing riggingRopes that are not turned round or wound on to winches (eg guided wires pendants stays)
11558 Subsea cranesCranes intended for handling of unmanned submersibles for lowering to and retrieval from below sea level
11559 SuspensionGear which connects the payload with the load-handling device the load-handling device with the fixed load-lifting attachment or which connects the payload directly with the fixed load-lifting attachment if no load-handling device is used eg load fastening ropes (slingsstrops) or lifting straps (see Figure 1-1)Suspensions are part of the loose gear
Guidance noteSuspensions are no subject of this standard unless they are integral part of a load-handling device
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DNV GL AS
11560 Test reportA document signed by the manufacturer stating
mdash conformity with requirements given by a relevant standardmdash that tests are carried out on samples from the current production
Reference is made to DNVGL-RU-SHIP Pt1 Ch3 Sec5 [28]
11561 Type approvalA type approval of the Society confirms compliance with DNV GL rules for standard designs andor routinelymanufactured identical components See DNVGL-CP-0338 Type approval schemeType approval may be used as an alternative to a case by case design approval
11562 Type approval certificateA document issued by the Society confirming a type approval
11563 VerificationReference is made to DNVGL-RU-SHIP Pt1 Ch1 Sec1
11564 VesselReference is made to DNVGL-RU-SHIP Pt1 Ch1 Sec1
11565 Working load of lifting applianceAlso referred to as actual hook load useful load or suspended loadLoad which is lifted by the lifting appliance and suspended from the fixed load-lifting attachment(s) seeFigure 1-1
Guidance noteWorking load of lifting appliance is the sum of the payload and the loose gear
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11566 Working load of load-handling deviceLoad which is lifted by the load-handling device and suspended from it see Figure 1-1
Guidance noteWorking load of load-handling device is the sum of the payload and the lower suspensions
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11567 Works certificateReference is made to DNVGL-RU-SHIP Pt1 Ch3 Sec5 [25]
116 Crane design types1161 Winch luffing craneA crane where the boom is controlled by wire ropes through a winch
1162 Cylinder luffing craneA crane where the boom is controlled by hydraulic cylinder(s)
1163 Knuckle boom craneA crane where the boom is hinged and the boom and knuckle angles are controlled by a set of hydrauliccylinders
1164 Derrick craneA simple crane consisting of a vertical mast and a hinged jib The derrick crane is provided with devices forraising and lowering a load luffing the jib and slewing the jib about the mast
1165 Overhead travelling craneA crane which lifts the object by a trolley which normally moves horizontally along the crane beam The cranebeam ends have wheels running on rails at high level
1166 Gantry craneA crane which lifts the object by a trolley which normally moves horizontally along the crane beam The cranebeam is supported by vertical legs having wheels running on rails at ground level
1167 A-frame craneA hinged frame intended for lifting Hydraulic cylinders control the movement of the A-frame while a winch isfitted for hoisting and lowering the load
12 Services
121 Introduction
1211 This subsection describes possible combinations of the different services offered Furthermorevarious alternatives are described for confirmation of the various services by the Society
1212 Figure 1-2 describes the services offered and the associated documents issued by the Society toproof compliance
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Figure 1-2 Alternatives for documentation that may be issued to customers depending on typeand combination of services requested
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122 Regulatory basis
1221 This standard is based on the Societyrsquos understanding and interpretation of the ILO ConventionNo152 and Recommendation No160 of 1979
123 Acceptance by national authorities
1231 Regulatory bodies such as port authorities flag administrations shelf authorities and municipal orgovernmental health and safety authorities require that lifting appliances and loose gear shall be certifiedNormally the Societys certification in accordance with this standard will satisfy the authoritiesrsquo requirements
1232 In cases where requirements laid down by the pertinent body exceed the Societys requirementsdescribed in Sec3 through Sec13 The Society may as a voluntary service include the additionalrequirements in the design assessmentexamination and confirm whether or not they are found to befulfilled
13 Certification procedure
131 General
1311 The following parts components and systems are covered by this standard
mdash all load-carrying structural members and components of the lifting appliancemdash cargo hooks chains rings blocks sheaves shackles lifting beams swivels and ropesmdash structural integrity of grabs hydraulic dampers or other load transferring componentsmdash rope drumsmdash slewing bearing including fastenersmdash power systems (for hoisting derricking slewing and travelling)mdash brakes and braking systemsmdash safety equipmentmdash protection against firemdash seating and fasteners for prime movers winches and for bearings of power transmitting componentsmdash control and monitoring systemsmdash electrical installation
1312 The following activities are covered by this standard
mdash design assessmentmdash survey during fabrication and installationmdash witness testing and marking
132 Design assessment
1321 Load-carrying and other important components of a lifting appliance are subject to designassessment with respect to strength and suitability for its purpose A design approval is granted when thedesign assessment has been concluded without detection of non-compliancesThe design assessment may be substituted partly or completely by enhanced manufacturing survey andortesting In cases where the substitutions are applied for by the customer agreements shall be made betweenthe customer and the Society regarding possible reductions of documentation to be submitted for approvalinformation
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DNV GL AS
Upon special agreement the design assessment may be substituted by a strength evaluation based upontesting until failureStrength examination of components related to power supply and safety equipment is normally not carriedout by the Society
Guidance noteThe certification process includes the sequential steps design approval manufacturing survey (including installation survey) andtesting The Societyrsquos reports covering the separate phases are considered intermediate documents only and are documenting theprogress of the certification processThe Societyrsquos formal documentation of the certification to the customer will be
mdash Product certificate issued after completion of manufacturing process and full testing at the manufacturer
mdash CG2 issued after installation and full testing onboard in accordance with ILO152 requirements
For lifting appliances not subject to ILO 152 Form OLA201 may be issued after installation and full testing onboard
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1322 Each lifting appliance is normally given a separate design approval
1323 The design approval may be obtained either on a case-by-case basis or as a type approvalThe type approval means that the design as approved can be applied for identical units to be fabricated ierequested documents need not be submitted for each unitThe type approval will be based on certain conditions and its period of validity will be limitedSee DNVGL-CP-0338 Type approval scheme
133 Survey during fabrication and installation
1331 Normally a survey during manufacture of each separate lifting appliance shall be carried out by theSocietys surveyor in order to ascertain compliance with the approved drawings other requirements given inthis standard as well as general good workmanship
1332 As an alternative to survey during manufacture of each separate lifting appliance modified surveyprocedures and survey arrangements may be accepted provided the manufacturer operates a quality-assurance system approved and certified by the Society Acceptance shall be clearly formalized
1333 After a lifting appliance has been installed on its permanent foundation and before testing can takeplace it shall be subjected to a survey by a surveyor of the Society
134 Testing
1341 Components and each completed lifting appliance shall be subjected to functional testing and load-testing as specified in Sec13
135 Extension of scope of work
1351 Upon request from the customer the scope of work may be extended beyond the subjects andaspects covered in this standard
1352 Extensions shall be agreed in writing The Society may if found necessary require that the customerpresents reference documents for the extended scope of work such as authority regulations norms andstandards
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DNV GL AS
1353 In case of disputes regarding interpretations of requirements on which extended work is based thecustomer shall contact the publisherowner of the requirements and obtain their written interpretationIf the publisherowner is not willing to interpret the disputed requirement or an interpretation for otherreasons cannot be acquired the respective extension of the scope of work shall be omitted
136 Reduced scope of work
1361 For lifting appliances not to be installed on vessels classed by the Society upon request from andagreement with the customer parts of the scope of work components systems or specific aspects orrequirements may be excluded from the scope of work specified in the standard This will be annotated in thedocumentary evidence of the completed assignment (certificate)
1362 The Society will not agree to limit the scope of work or parts of the suggested services if this maylead to hazards or unacceptable lowering of the safety standard
14 Type of services
141 Basic certification
1411 The basic requirements presented in Sec3 through Sec13 are considered to cover the requirementsgiven in the ILO Convention No152 of 1979 specified in [1221] Lifting appliances and load-handlingdevices found to comply with these basic requirements are qualified for the Societys product certificationwhereupon the Societys product certificate may be issued based on FAT (factory acceptance test) andsurvey Following successful testing and survey after installation onboard a DNV GL CG2 certificate will beissued for cranes covered by the ILO regime (cargo cranes) For cranes not covered by the ILO regime aproduct certificate Form OLA 201 will be issued by the Society following successful onboard testing Thecargo gear register (CG1 if published by the Society) may be endorsed accordingly either as ILO crane or asother lifting appliances
1412 The basic requirement covers the two categories of lifting appliances a) and b) defined in [1121]as well as fixed load-lifting attachments and load-handling devices as well as personnel lifting as denoted in[1122]
1413 Some details of the basic requirements given in Sec3 through Sec13 are different for the differentcategory of lifting appliance a) and b) Furthermore some specific requirements are stated for cranes alsoused for personnel lifting
142 Cranes included in class scope
1421 On a voluntary basis cranes installed on board vessels and offshore units classed by the Societymay be included in the scope of work covered by classification In such cases the vesseloffshore unit will beassigned the additional class notation Crane see DNVGL-RU-SHIP Pt6 Ch5 Sec3
1422 Some of the requirements given in this standard have been extended with additional detailedrequirements for cranes to be covered by classification
143 Assignments completed before installation
1431 Assignments completed at the manufacturersrsquo premises can be agreed Such services shall normallybe completed with monitoring of tests at the manufacturer (FAT-tests) Applicable reports or certificates maybe issued See also [1432]
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 23Shipboard lifting appliances
DNV GL AS
1432 The reason for or purpose of such assignments may eg be
mdash completed certification of fixed load-lifting attachments load-handling devices or components TheSociety will normally issue the product certificate CG3 after completion of the tests
mdash provisional certification after FAT-test For instance if final destination is not decided or if themanufacturer is producing for stock Or the customer has requested FAT-tests and a documentaryconfirmation of the Societyrsquos service rendered until a certain point A Manufacturing survey report shouldbe issued
See also Figure 1-2
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 24Shipboard lifting appliances
DNV GL AS
SECTION 2 DOCUMENTATION AND CERTIFICATION
21 Documentation to be submitted
211 General
2111 The documentation necessary for verification assignments will depend on the scope of work agreedThe documentation and information requirements stated below are necessary for design approval andensuing certification
212 Documentation requirements
2121 Documentation shall be submitted as required by Table 2-1 as applicable for the lifting applianceCompleteness of submitted documentation is in the responsibility of the manufacturer of a lifting applianceIt may be partly or completely delegated to a sub-contractor (eg external designer or supplier ofcomponents) Where a sub-supplier provides components including DNVGL product certificate according toTables 2-2 to Table 2-4 no detail drawings of that component need to be resubmitted by the manufacturer ofthe lifting appliance
Table 2-1 Documentation requirements
Object Document type Additional description Shipboardcranes
Shipboardcranes
(if Cranenotation)
C010 - Design criteria
mdash load charts andor load tablesmdash dynamic factorsmdash fatigue load assumptionsmdash hoisting luffing and slewing speedsmdash operational and environmental
conditionsmdash variable rigging conditionsmdash rope lengths and hook heightsmdash categoty of crane see definitions
[112]mdash particulars of brake spring
performance
FI FI
General
C020 - Assembly or arrangementdrawing
mdash overview drawingsmdash additional rigging plans required for
cargo crane certification complyingwith ILO152
FI FI
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 25Shipboard lifting appliances
DNV GL AS
Object Document type Additional description Shipboardcranes
Shipboardcranes
(if Cranenotation)
Steel structures (general)
mdash crane booms crane housings cranecolumns supporting structures
mdash crane boom supports sea lashingmdash foundations and rigidly attached
fittingsmdash crane bridges trolleys gantries
bogies runways crane railsmdash stopper derailment guard devices to
prevent overturningmdash interchangeable components if not
standardized (hooks blocks shacklesetc)See Sec7 for requirements aboutdocumentation for CG3 certification
mdash rope sheaves which are notmanufactured in accordance with orgenerally in line with standards or typeapproved
AP AP
Steel structures (additional)
mdash platforms accesses laddersmdash design and fixing of cabinmdash steering stands if any
--- AP
Mechanical engineering (general)
mdash slew rings with bolting system andload limit diagram
mdash rotary bearings such as king pins androllers
mdash load-bearing hydraulic cylinders withtheir associated safeguard againstpressure loss
mdash spindles rack barsmdash winch drum with rope fixings and
winch bolting
AP AP
General(continuation)
C030 - Detailed drawing
Mechanical engineering (additional)
mdash complete winchesmdash complete slewing and swinging
mechanisms and travelling gearmdash swell compensator andor swell
absorbing systemsmdash hydraulic motors and pumps for
nominal power over 50 kWmdash ventilators and heat exchangers
--- AP
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 26Shipboard lifting appliances
DNV GL AS
Object Document type Additional description Shipboardcranes
Shipboardcranes
(if Cranenotation)
C030 - Detailed drawing(continuation)
Documents for information
mdash details of ropes (make strength) endconnections of ropes cable tacklesystem rope sheaves(Alternatively this information may beprovided on the assembly drawing)
mdash details of type tests and typeapprovals
mdash details of nominal sizes (SWL) andstandards on which standardizedinterchangeable components are based(Alternatively this information may beprovided on the assembly drawing)
FI FI
C040 - Design analysis mdash including fatigue analysis FI FI
M150 - Non-destructive testing (NDT)plan FI FI
Z060 - Functional description upon request FI FI
General(continuation)
Z161 - Operation manual upon request FI FI
mdash nominal data on electric main drivemotor for the electric load analysis ofthe ship
FI FI
Power supply Z030 - System arrangement plan mdash type and maker of prime moveror specification of other main andemergency power supply
mdash including mechanical components
--- FI
E170 - Electrical schematic drawing
mdash overview drawing of electricalinstallation (eg wiring diagram singleline diagram)
mdash circuit diagram including part listmdash lighting plan including emergency
power supplymdash type of protection of motors and
switch gearmdash complete information on explosion
protectionmdash control consoles and switch cabinets
--- APElectric powersystem
Z090 - Equipment list --- FI
S011 - System diagram (PampID) --- FI
S042 - Hydraulic control diagram AP AP
Z060 - Functional description FI FI
Hydraulicpower system
Z090 - Equipment list FI FI
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 27Shipboard lifting appliances
DNV GL AS
Object Document type Additional description Shipboardcranes
Shipboardcranes
(if Cranenotation)
Functional description of safety systemand the safety equipment to be included
mdash overview of security oriented devicesand controls
mdash flow chart of controlmdash functional description of safety system
and the safety equipment to beincluded (emergency shut-down limitswitch overload protection devicesetc)
--- APControl andmonitoring
I200 - Control and monitoring systemdocumentation
mdash details of protection devices to preventoverspeed
--- FI
2122 For general requirements for documentation including definition of the Info codes see DNVGL-RU-SHIP Pt1 Ch3 Sec2
2123 For a full definition of the documentation types see DNVGL-RU-SHIP Pt1 Ch3 Sec3
213 Design analysis
2131 For structural parts and components specified in [212] the drawings shall be supplemented withcalculations demonstrating that the structural strength complies with the requirements
2132 A complete listing of structural components and parts subjected to strength calculations shall besubmitted The list shall include information of
mdash types of failures considered (excessive yielding buckling fatigue fracture)mdash method of analysis performedmdash permissible stress or limit state method used
See also [43]
2133 The design calculations for hydraulic cylinders shall be based on the maximum obtainable pressure(safety valve setting) Alternatively if the maximum dynamic force applied on the crane is known this maybe used as basis for the design calculations In both cases different outreach positions shall be evaluated
22 Certification
221 Certificate requirements
2211 Certificates for components of shipboard lifting appliances shall be issued as required by Table 2-2 toTable 2-4Material certificates shall be issued as required in Sec3Certificates for entire lifting appliances shall be issued as required by [137]
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 28Shipboard lifting appliances
DNV GL AS
Table 2-2 Certificate requirements for shipboard lifting appliances
Object Certificatetype Issued by Certification
standard Additional description
Slewingbearings PC The Society
31 for crane group A31 for other crane groups if maker holds valid DNV GLapproval of manufacturer (AoM)
See Sec9 for requirements about certification
Hydrauliccylinders PC The Society
Applicable also for accumulatorsSee Sec9 for requirements about certification
Sheaves PC Manufacturer
Plastic sheaves to be delivered with the Societys TAPlastic sheaves not having valid type approval certificatemay be accepted on basis of a DNVGL productcertificate
Hoisting blocks PC The SocietyCG3 alternatively ILO form No 3 issued by IACS classor flag state administrationSee Sec7 for requirements about certification
Hooks PC The SocietyCG3 alternatively ILO form No 3 issued by IACS classor flag state administrationSee Sec7 for requirements about certification
Chains PC The SocietyCG3 alternatively ILO form No 3 issued by IACS classor flag state administrationSee Sec7 for requirements about certification
Swivels PC The SocietyCG3 alternatively ILO form No 3 issued by IACS classor flag state administrationSee Sec7 for requirements about certification
Shackles PC The SocietyCG3 alternatively ILO form No 3 issued by IACS classor flag state administrationSee Sec7 for requirements about certification
Wire ropes PC The SocietyCG4LA4 alternatively ILO form No 4 issued by IACSclass or flag state administrationSee Sec8 for requirements about certification
Winches PC Manufacturer See Sec9 for requirements about certification
Slewing gear PC ManufacturerWorks certificateSee Sec9 for requirements about certification
Transmissiongears andbrakes
PC Manufacturer
Works certificateApplicable when transmitting braking forces for hoistingand luffing For personnel handling the Societys PCrequired
See Sec9 for requirements about certification
Hydrauliccomponents TR Manufacturer
Except mountingsSee Sec9 for requirements about certification
Unless otherwise specified the certification standard is this standard
PC = Product Certificate TR = Test Report
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 29Shipboard lifting appliances
DNV GL AS
Table 2-3 Additional certificate requirements for Crane notations
Object Certificatetype Issued by Certification
standard Additional description
Winches PC The Society See Sec9 for requirements about certification
Control andmonitoring system PC The Society See Sec10 for requirements about certification
PC The SocietyRating 300 kW and aboveSee Sec10 for requirements about certification
Electric motors withrating 100 kW andabove TA The Society
Rating 100 kW and above but less than 300 kWSee Sec10 for requirements about certification
Equipment not having valid type approvalcertificate may be accepted on basis of a DNVGLproduct certificate reference is made to RU-SHIPPt4 Ch8 Sec1 [232]
Motor startersand frequencyconverters withrating 100 kW andabove
TA The Society
See Sec10 for requirements about certificationEquipment not having valid type approvalcertificate may be accepted on basis of a DNVGLproduct certificate reference is made to RU-SHIPPt4 Ch8 Sec1 [232]
Slip rings 100 kWand above PC The Society See Sec10 for requirements about certification
Unless otherwise specified the certification standard is this standard
PC = Product certificate TA = Type approval certificate TR = Test report
Table 2-4 Additional certificate requirements for ESV(Crane) notations
Object Certificatetype Issued by Certification
standard Additional description
Control andmonitoring systems PC The Society See Sec10 for requirements about certification
Unless otherwise specified the certification standard is this standard
PC = Product certificate
2212 For general certification requirements see DNVGL-RU-SHIP Pt1 Ch3 Sec4
2213 For a definition of the certification types see DNVGL-RU-SHIP Pt1 Ch1 Sec4 and DNVGL-RU-SHIPPt1 Ch3 Sec5
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 30Shipboard lifting appliances
DNV GL AS
SECTION 3 MATERIALS
31 General
311 Scope
3111 This section gives requirements for materials for structural members and equipment for liftingappliances with design temperature TD down to -30degCMaterials for lifting appliances with design temperature below -30degC will be especially considered Designtemperature is defined in [423]
3112 Materials with properties deviating from the requirements in this section may be accepted uponspecial consideration by the Society See also DNVGL-RU-SHIP Pt2 Ch1 Sec1 [34]
3113 For materials where no specific requirements are given generally recognised standards andengineering principles may be applied
3114 A traceability system that ensures correct installation and documentation of the material grades orstrength classes shall be established by the customer throughout the prefabrication and installation processProper care shall be exercised during handling and storage to preserve identification of such material
312 Structural category
3121 The following categorisation will be used for structural members
mdash Special highly stressed areas where no redundancy for total collapse exists
mdash Primary structures carrying main load as well as components with highly stressed areas
mdash Secondary structures other than primary and special members
Slewing bearings with flanges will normally be categorised as special other structure transmitting principleloads are normally categorised as primaryThe categories shall be agreed with the Society in each caseSee also detailed categorisation for bolt connections in [3441]
Guidance noteHighly stressed areas are considered to be areas utilised more than 85 of the allowable yield capacity
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
313 Steel manufacturing process
3131 Steel shall be made by the basic oxygen process electric furnace process or by other processespecially approved by the Society
314 Material manufacture survey certification and testing procedures
3141 Certificates covering specification of the chemical composition and mechanical properties shall bepresented for all materials for all load-carrying structures and mechanical components The test values shallshow conformity with the approved specification Test specimens shall be taken from the products delivered
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 31Shipboard lifting appliances
DNV GL AS
Requirements as per DNVGL-RU-SHIP Pt2 Ch1 General requirements for materials and fabrication to befulfilledApproved steel manufacturer will not be requiredMaterial certificates type 31 will suffice for special and primary structures except for slewing rings andslewing ring fasteners for shipboard cranes (class notation) in which case certificate type 32 is required Thematerial certificates for the shipboard crane (class notation) slewing rings shall be signed by the Societysrepresentative
Guidance noteThe document designation inspection certificate type 31 32 and 22 are in accordance with ISO 10474
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
3142 The materials shall be adequately marked for identification The marking shall at least comprisename or trade mark of the manufacturer material grade heat number and when referred to 32 certificatesthe stamp of the purchaserrsquos authorized representative
3143 Marking and identification of smaller items eg bolts and nuts shall be especially agreed uponbetween manufacturer and the Society but shall at least comply with fastener product standard
3144 Materials without proper identification will be rejected unless renewed testing verifies compliancewith approved specifications The number and type of tests will be decided in each case
315 Retesting
3151 Materials that prove unsatisfactory during delivery testing may be retested If the standard withwhich the materials shall comply gives no directive for retesting the retesting shall be carried out as given inDNVGL-RU-SHIP Pt2 Ch1 Provided the new test results are found to satisfy the prescribed specification thematerial may be accepted
32 Rolled structural steel for welding
321 General
3211 In addition to the requirements for structural steels set out in the following further requirementsmay be stipulated in special cases depending on the material application Thus testing for fracturemechanics analysis and through thickness ductility properties may be required Fracture mechanics testingin accordance with an approved procedure will be required for materials and welded joints when the cranemanufacturer cannot document satisfactory experience from previous similar material application
3212 Rolled structural steel for welded constructions may be carbon steel or carbon-manganese steel Thesteels are divided into three groups dependent on the specified yield strength(ReH) as follows
mdash normal strength steels 235 Nmm2 le ReH lt 265 Nmm2
mdash high strength steels 265 Nmm2 le ReH lt 420 Nmm2
mdash extra high strength steels
420 Nmm2 le ReH le 750 Nmm2
3213 Application of steel with specified minimum yield strength above 750 Nmm2 shall be especiallyagreed
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 32Shipboard lifting appliances
DNV GL AS
3214 Steels having through thickness ductility (ldquoZ-steelrdquo) may be required for members which will besignificantly strained in the thickness directionFor evaluation of required Z-grades reference is made to Eurocode 3 (EN 1993-1-10)
Guidance noteReduction of area after fracture (Z) is the mean value of three (3) tensile test samples to be taken with their longitudinal axisperpendicular to the surface of the product
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
3215 The requirements for chemical composition mechanical properties etc are given in DNVGL-RU-SHIPPt2 Ch2 Sec2 [3] for normal strength steels DNVGL-RU-SHIP Pt2 Ch2 Sec2 [4] for high-strength steelsand DNVGL-RU-SHIP Pt2 Ch2 Sec2 [5] for extra high strength steelsRequirements for impact energy are given in Table 3-1 for structural steel for special primary and secondaryapplications
Table 3-1 Required impact energy values for welded structural steel
Minimum impact energy KV 1) [J]Strength category Strength class
Longitudinal Transverse
Normal strength 235 27 20
High strength
265
315
355
390
27
31
34
41
20
22
24
27
Extra high strength 2)
420
460
500
550
620
690
750
42
46
50
55
62
69
69
28
31
33
37
41
46
46
1) Mean value for three (3) specimens There may be one lower value but not less than 70 of the mean value2) Up to 150 mm thickness larger thicknesses upon special agreement
3216 As an alternative to [3215] materials that comply with national or proprietary specificationsmay be accepted provided such specifications give reasonable equivalence to the requirements given in thissection or are approved for a specific application See also DNVGL-RU-SHIP Pt2 Ch1 Sec1 [34]
322 Impact test temperatures
3221 Required impact test temperatures are dependent on design temperature TD and the materialthickness Impact test temperatures are given in Table 3-2 for structural steel for special primary andsecondary applications For definition of design temperature see [423]For structural members subjected to compressive andor low tensile stresses modified requirements may beconsidered ie greater material thicknesses for the test temperatures specified
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 33Shipboard lifting appliances
DNV GL AS
3222 Impact test temperature for flanges for slewing bearings shall be as for special and primarymembers given in Table 3-2 based on actual thickness
3223 When welding a thinner plate to a thicker plate eg connecting a flange to the supporting structurefor the flange inserted reinforcement rings etc the following apply provided the thicker plate does notcontain butt welds
The impact test temperature shall be the lower of the temperatures according to Table 3-2 based on t = t1 ort = 025middott2 where
t1 = thickness of the thinner supporting platet2 = thickness of the flange
However the impact test temperature for the flange (thicker plate) shall not be higher than the required testtemperature based on t2 according to Table 3-2 plus 30deg C
Table 3-2 Impact test temperatures for welded structural steel
Impact test temperature in degC 1)Material
thickness t in mm Structural steel for special and primary members 2) Structural steel for secondary members 2)
t lt 6 No special provisions 3) No special provisions 3)
6 le t le 125 TD + 30 No special provisions 3)
125 lt t le 25 TD +10 TD + 30
25 lt t le 50 TD - 10 TD + 10
50 lt t le 70 TD - 20 TD + 10
t gt 70 TD - 30 TD - 10
1) For steel with yield strength below 500 MPa the test temperature need not be taken lower than -40degC For steelwith yield strength above 500 MPa the test temperature shall not be taken higher than 0degC and not lower than-60degC
2) See [3121] for definitions3) The requirements given in DNVGL-RU-SHIP Pt2 Ch2 or in the relevant material standard or approved material
specification apply
323 Testing3231 Test samplesUnless otherwise required the test samples shall be taken for positions as specified in DNVGL-RU-SHIP Pt2Ch2 or other recognised standards The sample of material from which test specimens are cut shall betreated together with and in the same way as the material presented The samples shall be suitably markedfor identification
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 34Shipboard lifting appliances
DNV GL AS
3232 Test specimensTest specimens shall be as specified in the approved standards The following additional requirements shallapply
mdash for impact testing of thin materials where the thickness makes it impossible to use an impact testspecimen of 10 times 10 mm the largest practicable of the following specimens shall be used10 times 75 mm or 10 times 5 mm
By this procedure the required impact values are reduced to 56 and 23 respectively of the value of thestandard 10 times 10 mm test specimen
33 Rolled steel not for welding
331 General
3311 Rolled steel for special and primary components other than those mentioned in [332] and [333](eg mechanisms) shall be specified with reference to a recognised standard see [3215] and [3216]The material shall be delivered in the following conditions
mdash carbon and carbonmanganese steel normalized condition
mdash alloy steel quenched and tempered condition
mdash as rolled (AR) condition when subjected to special consideration
For all materials impact toughness shall be documented by Charpy V-notch impact tests Test temperaturesshall be as required by Table 3-4 but in the case of low calculated stresses eg not exceeding 50 Nmm2
(characteristic value without partial safety factors) a test temperature of 20degC will be accepted Requiredminimum impact energy shall be as required for welded parts see [3215]
332 Bolts and nutsMaterials for bolts and nuts considered as important for the structural and operational safety of theassembly in question shall comply with the requirements given in [344] for bolts and nuts This includesrequirements for chemical composition and mechanical properties
333 Rolled rings
3331 Rolled rings for important components such as slewing rings toothed wheel rims etc shall complywith the requirements for steel forgings see [345]
34 Steel forgings
341 General
3411 Forgings shall generally be manufactured in accordance with the requirements given in DNVGL-RU-SHIP Pt2 Ch2 Sec6 Steel forgings
3412 As an alternative to [3411] materials that comply with national or proprietary specifications maybe accepted provided such specifications show reasonable equivalence to the requirements given in [3411]or are especially approved As a minimum the following particulars shall be specified manufacturing process
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 35Shipboard lifting appliances
DNV GL AS
chemical composition heat treatment mechanical properties and non-destructive testing See also DNVGL-RU-SHIP Pt 2 Ch1 Sec1 [34] For machinery components see DNVGL-RU-SHIP Pt4 Ch2 Sec1 [3]
342 Forgings for general application
3421 Forgings shall be specified with reference to DNVGL-RU-SHIP Pt2 Ch2 Sec6 Steel forgings or othernational or proprietary specification see [3412] As a minimum the standard shall require impact testingaccording to Table 3-3 Other mechanical properties shall minimum be according DNVGL-RU-SHIP Pt2 Ch2Sec6 Table 8 for unwelded forgings and according to DNVGL-RU-SHIP Pt2 Ch2 Sec6 Table 6 for weldedforgings For thicknesses over 100 mm smaller deviations from the specified mechanical properties maybe accepted based on specific approval by the Society For forged shackles cargo hooks swivels socketschains boltsnuts and slewing bearings the special requirements given in [343] to [345] apply
Table 3-3 Impact testing for steel forgings and steel castings
Design temperature TD Test temperature Minimum Charpy Value
TD ge -20degC 0degC 27 J
-20degC gt TD gt -30degC -20degC or (0degC) 27 J (48 J)
343 Forged shackles cargo hooks swivels sockets and chains
3431 Carbon and carbon-manganese steel forgings shall be made from killed and fine-grain treatednon-ageing steel It may be required that the non-ageing properties are verified by tests The chemicalcomposition and mechanical properties of the material with the exception of the impact test temperatureshall be as given in [3421] It may be required that the non-agening properties are verified by tests seeDNVGL-RU-SHIP Pt2 Ch1 Sec3 [38]Chemical composition and mechanical properties for alloy steels shall be specified with reference torecognised standard and are subject to individual consideration and approval by the Society The chemicalcomposition shall be suitable for the thickness in question Alloy steels shall be delivered in quenched andtempered conditionRequirements for impact test temperatures are specified in Table 3-4
Table 3-4 Impact test temperature for shackles cargo hooks chains sockets and swivels
Material thickness t (mm) Impact test temperature
t le 10 Impact test not required
10 lt t le 50 TD + 20 ordmC (1)
50 lt t le 100 TD + 10 ordmC (1)
t gt 100 TD (1)
1) TD = design temperature
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 36Shipboard lifting appliances
DNV GL AS
344 Bolts and nuts
3441 Bolt connections are normally considered to be in the following groups
mdash Special where it is part of a slewing ring connection
mdash Primary where the bolts or nuts are transferring principle loads
mdash Secondary where the bolts or nuts are transferring load not belonging in the category special orprimary Examples are bolt connections in driverrsquos cabin platforms stairs and ladders
3442 Bolts and nuts for use in connections categorised as special or primary shall conform with andbe tested in accordance with a recognised standard eg pertinent parts of ISO 898 or other recognisedstandard Charpy testing will generally not be required for nutsAdditional requirements for testing and inspection of slewing ring bolts are given in Table 3-5Bolt connections considered as secondary shall be made from suitable materials
3443 Nuts may be accepted to be in one strength class lower than the bolts of boltnut assemblies
3444 Bolts and nuts shall be delivered with the following certificates as per ISO 10474 verifyingcompliance with the material requirements and other test requirements
mdash inspection certificate type 32 for slewing ring bolts and nuts for shipboard cranes (Crane notation)mdash inspection certificate type 31 for slewing ring bolts and nuts for cranesmdash 22 test report for bolts and nuts in primary and secondary connections
3445 Fasteners (bolts nuts and washers) in marine environment shall normally be hot-dipped galvanizedor sherardized with coating thickness min 50 micrometer If special thread profiles or narrow tolerancesprohibit such coating thickness bolts-nuts may be supplied electro-plated or black provided properly coatedpainted after installation Pickling and electro-plating operations shall be followed by immediate hydrogen-relief (degassing) treatment to eliminate embrittling effects
3446 Galvanizing of bolts and nuts are acceptable provided additional loss of bolt load (pretension) of atleast 4 is compensated forUnless specific measures are taken against absorption of hydrogen galvanizing is not accepted for 129bolts
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 37Shipboard lifting appliances
DNV GL AS
Table 3-5 Testing and inspection of slewing ring bolts
Strength classISO 898 orequivalent
Diameterd in mm
Ultimatetensile
strengthNmm2
YieldstrengthMinimumNmm2
ElongationA5
Required CharpyV energy1) at
test temperature
Fracturemechanics
testing(CTOD)
Surfaceinspection
d lt 25 mdash mdash Visual
88d ge 25
800 - 1000 640 1442 J mdash
Visual andmagneticparticle(MPI) 4)
d lt 25 mdash mdash Visual
109d ge 25
1000- 1200
940 1242 J mdash
Visual andmagneticparticle(MPI) 4)
d lt 25 25 JTo be
documented3)
129
d ge 25
1200- 1400 1080 12 (10) 2)
25 J To betested 3)
Visual andmagneticparticle(MPI) 4)
1) Average value of three specimens One single value may be max 30 lower2) May be accepted on case-by-case basis3) Alternatively a Charpy-V notch energy of minimum 55 J at TD may be accepted4) For all bolts (100 ) connecting special or primary members and a random number of bolts connecting secondary
members magnetic particle testing shall be carried out at least 48 hours after completion of quenching andtempering for bolts with yield strength above 355 Nmm2 Inspection shall be in accordance with ASTM E 709Depth of longitudinal discontinuities shall not exceed 003 of the nominal diameter Transverse cracks will not beacceptable irrespective of crack depth and location Other surface irregularities will be considered in each case
345 Forged rings for slewing bearings
3451 Specifications of slewing rings essential for the structural and operational safety of the craneare subject to individual approval by the Society All relevant details shall be specified such as chemicalcomposition mechanical properties heat treatment depth and hardness of surface hardened layer andsurface finish of fillets Position of test specimens shall be indicated Method and extent of non-destructivetesting shall be specified and the testing procedures shall be stated Detailed information about method ofmanufacture shall be submitted
3452 For each new material of which the manufacturer has no previous experience and for any changein heat treatment of a material previously used a principal material examination shall be carried out Thismeans that the Society may impose additional requirements not specified in this standard The results shallbe submitted to the Society for consideration The programme for such examination shall be agreed with theSociety
3453 All test results shall comply with the approved specifications
3454 Steel for slewing rings shall satisfy the requirements given in Table 3-6
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 38Shipboard lifting appliances
DNV GL AS
Table 3-6 Slewing ring materials
Heat treatment According to approved Spec
Charpy V-notch test temperature TD
Average 42 JCharpy V-notch value
Single min value 27 J
Elongation A5 14
Fatigue properties Documentation may be required by type tests on specimen of ringsection
Fracture toughness Documentation may be required by type tests on specimen of ringsection in question
35 Steel castings
351 General
3511 Steel castings shall generally be manufactured in accordance with DNVGL-RU-SHIP Pt2 Ch2 Sec8Steel castings
3512 As an alternative to [3511] materials which comply with national or proprietary specifications maybe accepted provided such specifications give reasonable equivalence to the requirements given in [3511]or are approved for each specific application As a minimum the following particulars shall be specifiedmanufacturing process chemical composition heat treatment mechanical properties and non-destructivetesting See also DNVGL-RU-SHIP Pt2 Ch1 Sec1 [34] For machinery components see DNVGL-RU-SHIPPt4 Ch2 Sec1 [2]
352 Castings for general application
3521 Steel castings shall generally be manufactured in accordance with DNVGL-RU-SHIP Pt2 Ch2 Sec8Steel castings or other national or proprietary specification As a minimum the standard shall require impacttesting and mechanical properties according to Table 3-3 Other mechanical properties shall minimum beaccording DNVGL-RU-SHIP Pt2 Ch2 Sec8 Table 5 for welded castings and according to DNVGL-RU-SHIP Pt2Ch2 Sec8 Table 7 for unwelded castings
36 Iron castings
361 General
3611 Iron castings shall generally be manufactured in accordance with the DNVGL-RU-SHIP Pt2 Ch2Sec9 Iron castings
3612 As an alternative to [3611] materials that comply with national or proprietary specifications maybe accepted provided such specifications give reasonable equivalence to the requirements given in [3611]or are approved for each specific application See also DNVGL-RU-SHIP Pt2 Ch1 Sec1 [34]
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 39Shipboard lifting appliances
DNV GL AS
37 Steel tubes pipes and fittings
371 General
3711 See DNVGL-RU-SHIP Pt2 Ch2 Sec5 Steel pipes and fittings or other recognised standardcodeRecognition of other standards shall be evaluated by the Society
38 Aluminium alloy structures
381 General
3811 See DNVGL-RU-SHIP Pt2 Ch2 Sec10 Aluminium alloys
39 Composite materials
391 General3911 Requirements to be specially developed for the intended use applying the technology qualification processrequired by DNVGL-RP-A203 Technology qualification
310 Wires for ropes
3101 General
31011 Wires for ropes shall be made by LD (Linz-Donawitz) process (applies to steel wires) or by otherprocesses especially approved by the Society or an other classification society
3102 Materials
31021 The nominal tensile strength of steel wires shall be 1570 Nmm2 1770 Nmm2 or 1960 Nmm2Steel wires with higher nominal tensile strength (eg 2160 Nmm2) or austenitic and copper wires may beapproved on application provided they are suitable for the proposed lifting application
31022 The nominal tensile strength of steel wires shall not be exceeded by more than the values shown inTable 3-7
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 40Shipboard lifting appliances
DNV GL AS
Table 3-7 Positive tolerances for nominal tensile strengths
Nominal wire diameter d [mm] Limiting deviations [Nmm2]
020 up to lt 050
050 up to lt 100
100 up to lt 150
150 up to lt 200
200 up to le 600
+ 390
+ 350
+ 320
+ 290
+ 260
31023 Individual wires shall possess sufficient ductility measured by their ability to withstand a fixednumber of reverse bends andor twists without crack initiationThese requirements are regarded as fulfilled if the values specified in EN 10264 or in an equivalent standardrecognized by the Society are achieved
3103 Tolerances
31031 The tolerance on the wire diameter shall lie within the limits specified in EN 10264 or in anequivalent standard recognized by the Society
3104 Coating
Wires used for standing rigging shall be fully galvanizedWires used for running rigging shall be normally galvanizedThe zinc coating shall conform to the data shown in Table 3-8Wires made from austenitic steel need not to be coated
Table 3-8 Zinc coatings
Minimum mass per unit area of zinc coating [gm2] for typeNominal wire diameter d [mm]
Normally galvanized Fully galvanized
02 up to lt 025
025 up to lt 04
04 up to lt 05
15
20
30
--
--
75
05 up to lt 06
06 up to lt 07
07 up to lt 08
40
50
60
90
110
120
08 up to lt 10
10 up to lt 12
12 up to lt 15
70
80
90
130
150
165
15 up to lt 19
19 up to lt 25
25 up to lt 32
100
110
125
180
205
230
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 41Shipboard lifting appliances
DNV GL AS
Minimum mass per unit area of zinc coating [gm2] for typeNominal wire diameter d [mm]
Normally galvanized Fully galvanized
32 up to lt 37
37 up to lt 40
40 up to lt 45
135
135
150
250
260
270
45 up to lt 55
55 up to le 60
165
180
280
280
3105 Testing
31051 Individual wire tests shall be performed for every wire dimension represented in the strandsThe number of tests for each wire dimension shall be the same as the number of strands in the ropeThe tests may be performed before or after rope manufacture In the case of compacted ropes wire testsshall be carried out before rope manufacture
31052 At the option of the manufacturer the ductility test of wires shall be either tested by the reversebend test or by the twisting test specified in a recognized standard (eg ISO 7801 or ISO 7800)The test is considered successful if at least 95 of the wires withstand the bend or twisting test as specifiedin the applied standard without breaking
31053 The specified weight of zinc coating shall be determined and certified by the manufacturer bychemically stripping the coating and measuring the weight loss of the stripped wiresThe adhesion of zinc coating shall be verified by a winding test For the test the wires shall be wound on atest mandrel of the diameter specified in Table 3-9 as to form at least 10 adjacent turns The zinc coatingshall continue to adhere firmly to the substrate after winding At least five (5) wires of each size shall betested
Table 3-9 Winding test
Diameter of test mandrel expressed as a multiple of the wire diameter ofMethod of galvanizing
lt 15 mm ge 15 mm
fully galvanized 4 6
normally galvanized 2 3
31054 Where the tensile loading capacity of a wire rope testing machine is insufficient to test a wire ropein its entirety the breaking load of a wire rope can be determined from the results of tensile tests performedon individual wires (see [85112])
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 42Shipboard lifting appliances
DNV GL AS
SECTION 4 DESIGN AND CALCULATION PRINCIPLES
41 General
411 This section contains provisions of general validity governing the design and calculation of lifting applianceson seagoing shipsThe special provisions contained in the following sections of this standard shall be observed additionally orwith priority respectively
412 Calculations according to established calculation principles or standards eg according to EN 13001 or EN13852 may be accepted if the particular properties of seagoing ships as stated in these rules have beentaken into consideration
42 Design principles
421 General4211 Prerequisites for the design
42111 Determination and specification of the operating and seagoing conditions on which the designis based are in principle the responsibility of the customer and the manufacturer The shipyard shall beconsulted as well The specifications decided upon are of considerable importance for the reliable operationand expected service life
42112 The intended use of ships and lifting appliances the shipping routes and the operational area highship speeds and the shape of the ships hull shall be considered as required
4212 Design criteria for operating lifting appliancesEssential design criteria in addition to the statements in [422] to [425] are in particular
mdash the total service life ie the number of loading cycles within the expected service lifemdash the loading condition ie the relative or percentage frequency at which the various hoist loads are
reached or exceeded in the total service lifemdash the type of service eg handling containers general or palletized cargo grabs or provision under harbour
or sea conditions
4213 Design criteria for the status out of operation
42131 Essential criteria for the design are in relation to [4212] increased inclinations of the supportingstructure and increased wind loads as well as ship accelerations
42132 In particular cases loads caused by vibrations shall be considered which may be generated eg byship machinery or seagoing influences
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DNV GL AS
422 Environmental conditions
4221 Special attention shall be given to the operation site weather conditions humidity dust aggressivemedia oil and salt-bearing air exhaust gases and exhaust gas heat vibrations etc if known or specified bycontract
4222 Machinery and electrical installations shall be dimensioned with respect to temperature and humidityat least for the following limit values if no stricter limit values are specified
a) in enclosed spaces
mdash air temperature 0degC to +45degC
mdash relative air humidity 80
b) on the open deck
mdash air temperature
mdash lifting appliances in operation -10degC to +45degC
mdash lifting appliances out of operation -25degC to +45degC
mdash relative air humidity 80 and influence of salt spray
4223 Vibrations are in general not part of dimensioning of the shipboard lifting appliances Whereshipboard lifting appliances are prone to vibrations vibration analyses shall be performed
4224 Where necessary manufacturer ship yard or operator shall specify the environmental conditions inparticular
423 Design temperature4231 General
42311 Design temperature is a reference temperature used as a criterion for the selection of steel grades
42312 The design temperature TD is defined as the lowest service temperature for a lifting appliance (see[4232])
42313 For shipboard lifting appliances installed on ships with Crane notation the design temperatures ofthe lifting appliances shall be compatible with the design temperature specified for the ship
42314 The design temperature of shipboard lifting appliances shall generally not be higher than -10degCAs an exception from this requirement for shipboard lifting appliances operated in closed heatedcompartments with controlled temperature a design temperature of +10degC applies
42315 If not otherwise specified design temperatures according to Table 4-1 shall be applied
42316 Where the design temperature is specified below the values stated in Table 4-1 this shall beexplicitely stated by the shipyard or the manufacturer of the lifting appliance in the drawings or otherdocuments submitted to the Society for approval It shall be considered with respect to material selectionand processing (welding) as well as with respect to dimensioning of systems sensitive to low temperatures
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 44Shipboard lifting appliances
DNV GL AS
Table 4-1 Design temperature for shipboard lifting appliances
Type of lifting appliance Design temperature Lowest acceptable service temperature 1
Shipboard lifting appliances in general -10degC -30degC
Shipboard lifting appliances in closed heatedcompartments with controlled temperature +10degC 0degC
1) Conditions according to [42323] to be complied with
4232 Lowest service temperature
42321 Service temperature means the ambient air temperature during lifting operation
42322 Service temperature of a lifting appliance shall not fall below its design temperature Exceptionsfrom this requirement are specified in [42323]
42323 Exceptionally for shipboard lifting appliances service temperatures below design temperature maybe acceptable if following conditions are complied with
a) If the design temperature TD is -10degC or less then the lowest acceptable service temperature Tmin is20degC below design temperatureIf the design temperature TD is +10degC then the lowest acceptable service temperature Tmin is 0degC
b) The number nlow of lifting operations per year at service temperatures below the design temperature isto be limited as follows
nlow le N 1000
N = total number of all lifting operations in the expected life time for the lifting appliance (to betaken from load assumptions of the fatigue analysis)
If the fatigue analysis for a lifting appliance had been dispensed with then the number of liftingoperations at service temperatures below the design temperature shall be limited to nlow le 20 per year
c) The manufacturer of the lifting appliance shall agree on the low temperature Where necessary thesusceptibility of certain components to low temperatures shall be considered
424 Load assumptions4241 General
42411 Shipboard lifting appliances are subject to other and partly greater loads than lifting appliancesonshore This includes amongst others ship inclinations seagoing accelerations as well as increased windloads
42412 For the design in principle all loads shall be considered which act upon the lifting appliance in-operation and in the out-of-operation state
42413 The design as well as the calculation and dimensioning of all shipboard lifting appliances shall bebased on the following load assumptions if applicable
42414 The following sections of this standard may contain further load assumptions which are then to beobserved additionally or given preference where applicable for the lifting appliance under consideration
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 45Shipboard lifting appliances
DNV GL AS
42415 Where shipboard lifting appliances are exposed to special loads which are not stated in thisstandard then these shall be taken as a basis for design and dimensioningSpecial loads shall be indicated expressly by the shipyard or manufacturer of the lifting appliance in thedrawings or in other documents submitted to the Society for approval Regarding the proof according to437 the partial safety factor to be considered shall be agreed with the Society
4242 Dead loads
42421 Dead loads according to 11510 shall be calculated using recognized standards such as eg EN1991-1-1 or shall be determined by weighing
42422 Dead loads are calculated by multiplying the mass by the acceleration of gravity g = 981 mssup2
4243 Dynamic forces
42431 Dynamic forces due to drivesThe acceleration of lifting appliance components andor working loads due to drives generates positive ornegative dynamic forces depending on definition which shall be calculated as follows
force [N] = mass [kg] ∙ acceleration [ms2]Braking forces due to drives shall be assumed as negative dynamic forcesDynamic forces due to drives may normally be assumed as quasi-static loads They are specified in [5324]as design loads
42432 Seagoing dynamic forcesHorizontal dynamic forces due to motions of a floating body shall be considered for shipboard liftingappliances used in occasional sea operations in accordance with the method described in [5325]Vertical dynamic forces due to motions of a floating body shall be considered if the calculation is made inaccording with [53251] If AppA is applied they are included in the method used therein if Table 5-2 isapplied they may be ignoredSeagoing dynamic forces may be assumed as quasi-static loads
4244 Inclinations of the supporting structure
42441 Lifting appliances in operationLifting appliances shall be dimensioned for operation at the static minimum inclinations according to Table4-2Dynamic loads due to motions of the supporting structure shall be considered in according with [5325]
Static inclinations α (= heel) and β (= trim) shall be assumed to be acting simultaneouslySimplifying it may be assumed that heel and trim are superimposed as follows
The resulting angle ε shall be assumed to have the most unfavourable direction
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DNV GL AS
Table 4-2 Static minimum inclinations
Static minimum inclinationType of floating body
Heel angle α Trim angle β
Ships and vessels having ship-shape properties plusmn 5deg plusmn 2deg
Barges of length less than four (4) times breadthand catamarans plusmn 3deg plusmn 2deg
Floating docks plusmn 2deg plusmn 2deg
Semi-submersibles plusmn 3deg plusmn 3deg
The values of Table 4-2 assume sufficient stability of the floating body Where larger inclinations shall beexpected during operation of the lifting appliance then these shall be taken as the basisIn special cases to be proven by measurements or calculations the values may be lower than those in Table4-2For dimensioning the inclinations which are determined shall be increased by 1deg heel and 05deg trim
42442 Lifting appliances out of operationFor the calculation of dynamic forces in the out of operation state the dynamic inclinations as well as therespective accelerations of the floating body shall be observedFor this purpose the dynamic inclinations of the floating body according to Table A-1 shall be assumedSimplifying the calculation of dynamic forces may be performed according to AppA
4245 Wind loads
42451 GeneralShipboard lifting appliances shall in general only be operated up to a mean wind speed of approximately 80of the design wind speedAt higher wind speeds the lifting appliance shall be taken out of operation and be stowed in the stowingpositionSimplifying the statements in [42452] and [42453] are based on a constant mean wind speed acting inany assumed direction and heightStatic or dynamic calculations of wind loads in accordance with recognized rules or standards or calculationswith suitable wind load parameters may be accepted by the Society
42452 Calculation of wind loadThe wind load LW acting on a structure shall be assumed to have the most unfavourable direction and shallbe calculated using the following formula
[N]
q = v216 [Nm2] (dynamic pressure)v = wind speed according to [42453] [ms]cf = form coefficient according to [42454] [-]Aw = wind area [m2]
42453 Wind speedsThe determination of wind load shall be based on the wind speeds according to Table 4-3
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DNV GL AS
Table 4-3 Wind speeds
Wind speedMode of operation of the lifting appliance
in operation out of operation
Shipboard lifting appliances harbour operation 20 ms 50 ms 1
Shipboard lifting appliances sea operation 25 ms 50 ms 1
1) Not to apply for topped cranes
For topped shipboard lifting appliances out of operation the wind speed shall be calculated as a function ofheight according to the following formula
[ms]
hL = height of the centre of area of the boom above waterline [m]
The wind speed v is assumed to be constant along the height
Floating cranes shall be treated like shipboard lifting appliances
42454 Form coefficientsThe form coefficients may be determined according to AppC or simplified as follows
cf = 16 for rolled profiles and box girderscf = 13 for rectangular areas of closed super structures like eg engine housescf = 12 for cylindrical structural elements
42455 Wind areas located behind one anotherThe wind loads of areas located behind one another may be determined according to AppC or simplified asfollowsFor wind loads of areas located behind one another the wind load of the respective area lying behind may beassumed to be 75 of the area lying in front From the 9th area onwards the wind load remains constant at10
42456 Wind load on the working loadThe wind load acting on the working load shall be calculated according to [42452] based on the largestwind area of the working load and acting in the most unfavourable direction
Where a more precise information on the working load is not available the wind load may be calculated usingthe following values for cf ∙ Aw
WL le 50t [m2]
WL gt 50t [m2]
WL = working load [t]
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DNV GL AS
4246 Snow and ice loads
42461 The manufacturer has to specify by agreement with the client if and to what extent snow and iceloads shall be considered for individual operating conditions Generally lifting appliances with ice accretionshall not be operated
42462 Where ice accretion shall be considered and no empiric or specified values are available simplifieda general ice accretion of 3 cm thickness may be assumed for all parts of the construction which are exposedto the weather conditions
42463 The specific weight of the ice is assumed to be 700 kgm3 The specific weight of snow is assumedto be 200 kgm3
42464 In the case of ice load the wind load shall be related to the area increased by ice accretion
4247 Loads due to temperatureParts of the structure or other structural elements which cannot expand or contract freely shall be avoided ifpossible Otherwise the lower and upper temperature shall be agreed with the Society and the temperatureloads shall be considered in the calculated strength analyses
425 Special provisions4251 Conveyance of persons in the harbourThe following provisions imply safety devices which are required in principle in Sec9 Sec10 and Sec12such as eg
mdash emergency shut-down switches or buttonsmdash control elements return automatically to the neutral positionmdash load and load moment reducing motions when safety devices apply
42511 The safe working load for conveyance of persons (SWL(M)) of shipboard lifting appliances shall notexceed half of the safe working load (SWL) of the shipboard lifting appliance
Guidance noteIf a shipboard lifting appliance is designed for conveyance of persons exclusively its SWL(M) shall be half of the SWL the liftingappliance would have when handling cargoprovisions
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
42512 The maximum lowering and hoisting speed for the conveyance of persons shall not exceed 05 msThe control system shall be capable of observing this speed limitation
42513 At a lowering speed of more than 03 ms the control system shall be capable of setting-downgently the means of conveying persons
42514 The minimum lowering and hoisting speed for the conveyance of persons shall not be less than005 ms
42515 Means of conveying persons shall be attached to the lifting appliance by secured shackles or otherapproved fixed connections Cargo hooks with seawater-resistant safety latch are permitted if compatiblewith the master link of the meansAutomatically release hooks for life-saving appliances are not permissible
42516 Hoisting and luffing winches of shipboard lifting appliances for conveying persons shall be equippedwith a mechanical second brake The second brake shall be independent of the primary brake
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DNV GL AS
42517 If hydraulic cylinders are used for luffing knuckling or telescoping of a boom they shall beequipped with hydraulic restriction systems Alternatively two independent hydraulic cylinders can be usedof which each single one shall be capable to hold the safe working load resulting from the conveyance ofpersons (SWL (M)) if the other hydraulic cylinder failsSafety against failure shall then be verified for loading condition III5 as per [552]
42518 Special devices shall be provided to rescue passengers from a means of conveying persons in caseof the failure of the drive
4252 Conveyance of personnel at seaFor the conveyance of personnel at sea the provisions of [4251] apply with the exception of [42512]and [42513] In addition the following provisions shall be observed
42521 Aside from an emergency the following environmental conditions shall be adhered to unlessdeviating conditions are agreed upon
mdash average wind speed le 10 ms
mdash significant wave height le 2 m
mdash visibility conditions daylight or sufficient illumination
42522 Shipboard lifting appliances for occasional operations at sea shall be equipped with a manualoperational control which allows switching between normal operation and conveyance of personnel ifprovided for the conveyance of personnel
42523 Shipboard lifting appliances according to [42522] shall comply with the following conditions inthe conveyance of personnel mode if applicable
mdash There shall be an automatic de-activation of safety systems for release of the cargo runner (emergencysystem for hooking on of cargo hooks)
mdash There shall be an automatic de-activation of active or passive heave compensatorrsquos These are howeverpermissible for the handling of work boats if they are adjusted to these boats
mdash In addition to the main power supply an emergency power supply shall be available to ensure mainfunctions of the lifting appliance (lifting luffing slewing telescoping and knuckling) at a minimum speedof 10 of the nominal operational speed in the mode conveyance of personnel Exceptions (eg verylarge cranes) are individually to be agreed with the Society
4253 Sea lashing
42531 All mobile parts of shipboard lifting appliances such as derricks crane booms trolleys gantriesetc shall have a special park and stowage position where they can be lashed to be seaworthyExceptions like eg free hanging or topped booms require approval by the Society case by case
42532 Special stowage positions shall be provided for mobile lifting appliances They shall be selectedsuch that the prospective loads like eg ship accelerations wind and wash are minimized
42533 The lifting appliances as well as their support and lashing devices shall be sufficiently dimensionedfor the loads in the out of operation state
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DNV GL AS
43 Calculation principles
431 Basic requirements
4311 All strength analyses shall correspond to generally recognized rules of statics dynamics and strengthof materials
4312 Details on system measurements sections materials used etc in the drawings shall agree with thecorresponding calculations
4313 Mobile loads shall be assumed in the most unfavourable positions for the structural elementconsidered
4314 Where non-linear relations inherent to the system exist between loads and stresses stressdetermination shall be conducted according to 2nd order theory for γp-fold loads with consideration ofdeformations
4315 Calculations according to 2nd order theory shall be based on a reduced design value of the Youngsmodulus
Ed = Ek γm
Ed = design value of Youngs modulusEk = characteristic value of the Youngs modulusγm = partial safety factor for resistance values according to [43743]
Explanations on this can be found in [4371] and [4372]
432 Proofs required
4321 Normally the following proofs shall be submitted for all lifting appliances
mdash proof of structural safety according to [44]mdash proof of safety against overturning according to [45]mdash proof of fatigue strength according to [46]mdash proof of suitability for use according to [47]
4322 The following sections of this standard may contain more detailed andor additional information onproofs required for the lifting appliance considered there
433 Materials4331 General
43311 The materials intended for use shall be indicated in the calculation
43312 Regarding material selection the provisions in Sec3 apply
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DNV GL AS
4332 Calculated yield strength
43321 GeneralThe strength analyses according to this standard refer as a failure criterion to the yield strength of thematerialFor metallic materials without significant yield strength ReH the yield strength Rp02 is used insteadTo avoid brittle fracture the materials used shall be sufficiently ductileThis means that the failure of a structural element due to overload may possibly be indicated sooner by largeplastic deformationsFor less ductile materials with a small ratio of ultimate tensile strength Rm over yield strength ReH additionalsafety against reaching or exceeding the ultimate tensile strength is stipulatedThis is achieved in strength analyses by taking into consideration a reduced value for the yield strength ndash thecalculated yield strength fyr
43322 SteelsThe calculated yield strength fyr shall be determined as follows
fyr = 083 ∙ Rm le ReH (or le Rp 02)
Rm = ultimate tensile strength [Nmm2]ReH = yield strength [Nmm2]Rp02 = 02-yield strength [Nmm2]
Where austenitic steels are used with a ratio Rp02Rm le 05 subject to special approval by the Society fordimensioning the 1-yield strength Rp10 may be applied instead of Rp02
43323 Aluminium alloysIf aluminium alloys suitable for seawater according to DNVGL-RU-SHIP Pt2 Ch2 Sec10 are used the yieldstrength shall be determined as follows
fyr = 037 ∙ (Rp 02 + Rm) le Rp 02
Rm = ultimate tensile strength [Nmmsup2]Rp02 = 02-yield strength [Nmmsup2]
In the case of welded connections the respective mechanical properties in the welded condition shall beassumed If these values are not available the corresponding values in the soft condition shall be assumed
434 Section values4341 Hole weakening by bolts
43411 The sections to be considered are the net sections (including hole deduction) for all structuralelements stressed by tension
43412 A calculated deduction due to holes may be dispensed with for all sections stressed by compressionand shear if
mdash the maximum hole clearance is 1 mm andmdash the deformations of the structure shall not be limited
43413 Where the conditions according to [43412] are complied with the section values of sectionswhich are subject to bending may be determined simplified as follows
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 52Shipboard lifting appliances
DNV GL AS
For the tension side the net section and for the compression side the gross section shall be taken For thecentre of gravity the centre of gravity of the gross section shall be assumed
43414 Elastic deformations are normally to be determined using the gross sections
4342 Effective breadth of platingWhen determining section values the effective breadth of plating shall be taken into consideration ifnecessary The calculation of the effective breadth of plating may eg be conducted in according withEurocode 3 (EN 1993-1-5)
435 Particularities4351 Local stressesThe local stresses in the area of force transmissions and discontinuities such as eg diversions of forcesteps of a section cut-outs etc see Figure 4-1 shall be proven separately and superimposed on the globalstressesNotes regarding local stresses due to wheel loads may be taken from [495]
Figure 4-1 Examples for local force transmissions and discontinuities
4352 Tie rodsTie rods which may be subject to compressive stresses due to small deviations from the regular loadassumptions shall be proven in the same way as compression members
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DNV GL AS
436 Assessment procedures4361 General noteIn this standard the methods of partial safety factors and permissible stresses are allowed to be used fordesign assessment
4362 Partial safety factor methodThe partial safety factors method is generally applicable It enables weighting of different loads and is thestandard proof of this standard
4363 Method of permissible stressesThe method of permissible stresses is not generally applicable and therefore shall not be used if one or moreof the following structural characteristics exist
a) non-linearity between loads and stresses (compression-stressed structural elements with majordeformations requiring proof according to 2nd order theory)
b) dead loads with a favourable effect (counter- weightsoverhanging engine houses)c) pre-stresses due to
mdash weights (besides b) in particular mobile weights)mdash ropestension elementsmdash bolts (in general only relevant in special cases)
d) lifting appliance is not fixed and stability against turn-over has not been proven by tests
437 Proof by the method of partial safety factors4371 GeneralThe method of partial safety factors distinguishes between safety factors γm relating to resistance values andsafety factors γP relating to loads
4372 Definitions
43721 LoadsLoads is the term for all external influences which impact on a structureLoads can eg be dead loads hoisting loads dynamic loads temperature changes or enforced deformationsThe loads to be considered in each individual case are regulated in the following sections for the respectivelifting appliance
43722 StressesStresses is the term for the effects of loads on a structureStresses can eg be stresses and deformationsStresses are marked by the index Sldquo
43723 Load bearing capacitiesLoad bearing capacities is the term for the permissible limit values of a stressLoad bearing capacities are marked by the index Rldquo
43724 Resistance valuesResistance values are material properties like eg yield strength ultimate tensile strength and Youngsmodulus by which eg load bearing capacities and stiffness of cross-sections are calculated
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 54Shipboard lifting appliances
DNV GL AS
43725 Characteristic valuesCharacteristic values of loads or resistance values do not include safety factorsCharacteristic values are marked by the index k
43726 Design valuesDesign values of loads L are the characteristic values increased by the partial safety factor γP
Ld = γP ∙ Lk
Design values of resistance values WG are the characteristic values reduced by the partial safety factor γm
WGd = WGk γm
Design values are marked by the index dldquo
4373 General proof formatIn general the degree of utilization (stressutilization ratio) shall be calculated The proof is demonstrated ifthe degree of utilization is not larger than 100
As an alternative stress and utilization can be compared directly The proof is demonstrated if the stress isnot larger than the utilization
Sd Rd le 1 or Sd le Rd
Sd = design value of load determined from the impacts multiplied by varying partial safety factors γP
Rd = design value of load bearing capacity determined from the resistance values divided by the partialsafety factor γm
4374 Partial safety factors
43741 For the calculation the loads which lifting appliance is exposed to are increased by partial safetyfactors of varying magnitude
43742 The partial safety factors for loads are given in Sec5 together with the load combinations to beverified
43743 The partial safety factor for resistance values γm is always
γm = 110unless stated otherwise in individual cases
4375 Load combinations
43751 Loads according to [424] acting simultaneously shall be increased by the partial safety factorsaccording to [4374] and to be superimposed in load combinations
43752 Notes and explanations regarding load combinations are given in the following sections inconnection with the required proofs
438 Proof by the method of permissible stresses4381 General
43811 The method of permissible stresses is only applicable under certain prerequisites It is regarded tobe a special case within the method of partial safety factors see [4362] and [4363]
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 55Shipboard lifting appliances
DNV GL AS
43812 Depending on the type of design differing results are possible with the two methods of proofTherefore the Society reserves the right in individual cases to apply a proof using the method of partialsafety factors
4382 Proof formatsWithout partial safety factors the following proof formats exist
σ σzul le 1τ τzul le 1
σv σzul le 1or
σ le σzul
τ le τzul
σv le σzul
fyr = calculated yield strength according to [4332]γS = global safety factor depending on the load combinations according to Table 5-4 and Table 5-5
load combination I γS = 148
load combination II γS = 134
load combination III γS = 122
σzul = permissible stress for normal stresses and equivalent stresses (Mises)
τzul = permissible stress for shear stresses
44 Proof of structural safety
441 General
4411 The following statements shall be observed for proofs load bearing structural elements made of steeland aluminium as well as for proofs of special machinery elements according to the method of partial safetyfactors
4412 Calculation and dimensioning of machinery elements which are not dealt with may be performedusing recognized standards or generally recognized technology rules
442 Scope of proofs4421 General
44211 The proof of structural strength consists of two partial proofs
mdash the general stress analysis according to [4422] andmdash the proof of stability according to [4423]
44212 The internal forces and moments on which the proof of the structural element being consideredcross-section or a weldbolt are based shall include all impacting static and dynamic load components
44213 The proofs of structural safety shall be shown in each case for the most unfavourable loadcombination according to [4375]
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DNV GL AS
44214 If load combinations are not taken into consideration or proofs not carried out this shall besubstantiated in writing unless the reasons for doing so are obvious
4422 General stress analysisThe general stress analysis is the proof of safety against reaching the calculated yield strength according to[4332]
44221 GeneralThe designations of axes of structural elements used in this standard as well as forces and moments whichmay have an impact on a structural element are illustrated in Figure 4-2
Fxyz = Force in direction of the respective axis [N]Mxyz = Moment around the respective axis [Nmm]σxy = Normal stress in direction of the respective axis
[Nmm2]τ = Shear stress [Nmm2]
Figure 4-2 Axes of structural elements and possible loads
44222 Equivalent stressesWhere normal and shear stresses act simultaneously in a cross-section the equivalent stress σv shall becalculated from the respective allocated stresses Spatially oriented stresses shall be broken down to thecoordinate system according to Figure 4-2Generally the equivalent stress σv shall be calculated according to the distortion energy theory (von Mises)as follows
In the case of biaxial stresses the calculation of σv is simplified as follows
In the case of uniaxial stresses the calculation of σv is simplified as follows
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 57Shipboard lifting appliances
DNV GL AS
44223 Format of the strength analysisThe strength analysis shall be performed for both the individual stress components as well as the equivalentstresses analogous to [4373] as follows
σSd σRd le 1 σSd le σRd
τSd τRd le 1 τSd le τRd
σvSd σRd le 1
or
σvSd le σRd
σSd
τSd
σvSd
=design values of the stresses based on the loads multiplied by partial safetyfactors γP
= design values of the permissible stresses (load bearing capacity)
fyr = calculated yield strength according to [4332]
γm = partial safety factor according to [43743]
Where more accurate strength analyses according to recognized calculation methods eg according to themethod of finite elements are conducted or where test results exist the Society may depending on the factsagree to an increase of the locally permissible stresses
4423 Proof of stability
44231 Proof of calculated safety against lateral buckling lateral torsional buckling or buckling shall beconducted according to a recognized calculation principle or standard for all essential combinations of loads
44232 Proofs of stability for steel constructions may be conducted according to Eurocode 3 (EN 1993-1-1EN 1993-1-3 EN 1993-1-5 EN 1993-1-7)
44233 Proofs of stability for aluminium alloy constructions may be conducted according to Eurocode 9 (EN1999-1-1 EN 1999-1-4 EN 1999-1-5)
44234 Proofs of stability for constructions made of austenitic steel may be conducted according toEurocode 3 (EN 1993-1-4)
44235 When applying Eurocodes for stability proofs the following shall be taken into consideration
mdash Instead of safety factor γM1 according to Eurocode the value γm according to [43743] shall be usedmdash Instead of the yield strength the calculated yield strength fyr according to [4332] shall be used
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45 Proof of safety against overturning
451 General
4511 Lifting appliances and parts of lifting appliances not connected integrally to the residual structureshall be sufficiently safe against overturning at all timesFor mobile lifting appliances also whereat operating on a circular track safety against overturning shall beproven in all cases
4512 Safety against overturning of lifting appliances is a measure of its resistance to overturning anddrifting eg by wind andor inclinations of the supporting structureThe many factors which influence safety against overturning in the longitudinal and transverse directionsinclude dead load and dead load distribution track gauge wheel base safe working load and load radiusmotor and braking power and the deformations which occur under load
4513 Lifting appliances which travel on rails shall be equipped with devices to prevent overturning andshall generally be stable even without such devices
4514 Proof of safety against overturning ensures safe working if the equipment is normally and carefullyoperatedIt should be noted that the danger of overturning arising from inexpert or incorrect operation cannot beprecluded no matter how stringent the conditions for proof of safety against overturning
452 Proof of safety against overturningWith regard to safety against overturning a distinction is made between lifting appliance on rails and fork lifttrucksWhere the danger of overturning exists for parts of non-mobile lifting appliances the proof shall bedemonstrated analogously to [4521]
4521 Lifting appliances on rails
45211 Calculational proof is regarded as sufficient for the safety against overturning of lifting applianceson railsThis proof shall be conducted using the method of partial safety factors according to [437]Thereby the partial safety factors for loads according to [437] are generally to be considered
45212 Lifting appliances are deemed to be sufficiently safe against overturning if - relative to therespective most unfavourable tilting edge - in the most unfavourable proof and in consideration of the partialsafety factors the sum of restoring moments is larger than the sum of overturning moments
The following condition shall be observed
= sum of restoring moments
= sum of overturning moments
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45213 Where desirable or necessary eg in the case of existing lifting appliances proof of safety againstoverturning may also be provided by a special loading testThis test shall in each case be agreed with the Society who will also determine the magnitude of the testload and the nature of the test (static andor dynamic)
45214 Devices to prevent overturning shall be dimensioned for the overturning moment which wouldresult from twice the static hoist load or where lifting appliances without prevention devices are not safeagainst overturning in accordance with the forces occurring in operation
4522 Industrial cargo-handling vehiclesThe safety against overturning of industrial cargo-handling vehicles shall be determined on an inclinableplatform for each new typeOn the basis of results obtained from these measurements the manufacturer shall on demand revise andcertify the conditions ensuring stable operation on inclined planes (due to inclinations of the ship or thecamber and sheer of decks)
46 Proof of fatigue strength
461 General
4611 The proof of sufficient fatigue strength i e the strength against crack initiation under dynamic loadsduring operation is useful for judging and reducing the probability of crack initiation of structural membersduring the design stageDue to the randomness of the load process the spreading of material properties and fabrication factors andto the effects of ageing crack initiation cannot be completely excluded during later operation Thereforeamong other things periodical surveys are necessary
4612 The fatigue strength analysis shall be conducted according to requirements as given in this sectionor subject to agreement with the Society according to another recognized basic calculation principle
462 Application
4621 The fatigue strength analysis is in principle required for all structural elements connections andsupporting structures of lifting appliances which are exposed to dynamic loads for the states in operationand out of operation and may be demanded by the Society for any type of lifting appliance and operationalcondition
4622 The provisions stated here are applicable to constructions made of normal and high-strength hullstructural steels austenitic steels as well as aluminium alloys Other materials such as extra high-strengthstructural steel and cast steel can be treated upon agreement with the Society in an analogous manner byusing appropriate design S-N curves
4623 Low cycle fatigue problems are not subject to the following rules and shall be specially consideredwhere applicable
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463 Definitions
Figure 4-3 Dynamic load cycle
Δσ = applied stress range [Nmm2] (see also Figure4-3) defined asΔσ = σmax ndash σmin
σmax = maximum upper stress [Nmm2] of a stresscycle
σmin = minimum lower stress [Nmm2] of a stress cycleΔσmax= applied peak stress range [Nmm2] within a
stress range spectrumσm = mean stress [Nmm2] defined as
σm = (σmax + σmin) 2Δσp = permissible stress range [Nmm2]Δτ = corresponding range for shear stress [Nmm2]n = number of applied stress cyclesN = number of endurable stress cycles according to
S-N curve(= endurable stress cycles under constantamplitude loading)
ΔσR = fatigue strength reference value of S-N curve at2 middot 106 cycles of stress range [Nmm2](= FAT class according to Table B-1)
fn = factor considering stress spectrum and numberof cycles for calculation of permissible stressrange
ΔσRc = corrected fatigue strength reference value ofS-N curve at 2 middot 106 stress cycles [Nmm2]
D = cumulative damage ratio
464 Quality requirements (fabrication tolerances)
4641 The detail classification of the different welded joints as given in Table B-1 is based on theassumption that the fabrication of the structural detail or welded joint respectively corresponds in regard toexternal defects at least to quality group B according to DIN EN ISO 5817 and in regard to internal defects atleast to quality group C
4642 Relevant information shall be included in the manufacturing document for fabrication If it is notpossible to comply with the tolerances given in the standards this shall be accounted for when designingthe structural details or welded joints respectively In special cases an improved manufacture as stated in[4641] may be required eg stricter tolerances or improved weld shapes see also [46924]
4643 The following stress increase factors km for considering significant influence of axial and angularmisalignment are already included in the fatigue strength reference values ΔσR Table B-1
km = 115 butt welds (corresponding type A1 A2 A11)km = 130 butt welds (corresponding type A3 ndash A10)km = 145 cruciform joints (corresponding type D1 ndash D5)km = 125 T-joints (corresponding type D1 ndash D3)
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DNV GL AS
km = 125 fillet welds on one plate surface (corresponding type C7 C8)
Other additional stresses need to be considered separately
465 Stress range spectrum4651 Definitions
46511 The stress range spectrum of a design detail describes the frequency of the different stress rangesto be expected at that location during the lifetime of the lifting appliance
46512 The standard stress range spectrum of lifting appliances describes the frequency of the differentworking loads to be handled during the lifetime of the lifting appliance
46513 Regarding the fatigue strength analysis it shall be taken into consideration that the standard stressrange spectrum of lifting appliances and the stress range spectrum of a design detail may be different interms of form of spectrum and particularly in terms of number of load cycles or stress cycles respectively
4652 Stress range spectrum for the condition in-operation
46521 Regarding the fatigue strength analysis for the condition in-operation lifting appliances arenormally to be categorized in groups corresponding to the standard stress range spectra S0 to S7 accordingto Figure 4-4
46522 Where the operating conditions are precisely known individual clearly separated from each otherstructural groups or elements may or shall be categorized differently
46523 The number nmax of stress cycles during operation shall be provided by the manufacturer
46524 The stress spectra S0 to S6 are defined by the following equation (see Figure 4-4)
Δσ = stress rangeΔσmax = maximum stress range of the spectrum according to [464]n = number of stress cyclesnmax = total number of stress cycles
κ =
p = coefficient according to Table 4-4
For p = 0 κ = 15 shall be assumed
Table 4-4 Coefficients for the calculation of the κ-value
Spectrum S0 S1 S2 S3 S4 S5 S6
p 07 17 27 37 47 57 67
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46525 Applicable for the stress range spectrum S7
= 1 = constant
Figure 4-4 Standard stress range spectra
46526 Where the operating conditions of shipboard lifting appliances are exactly known individuallydetermined stress range spectra may be used for the fatigue strength analysis based on calculatedcumulative damage ratios The individual stress range spectra shall be proven by the manufacturer
4653 Stress range spectra for the condition out-of-operationThe fatigue strength analysis for the condition out of operation shall be conducted for the straight-linespectrum A according to Figure 4-4 and a total number of stress cycles nmax = 5 middot 107
466 Calculation of the maximum stress range
4661 The fatigue strength analysis is depending on the detail considered based on one of the followingtypes of stress
mdash For notches of free plate edges the notch stress σk determined for linear-elastic material behaviour isrelevant The fatigue strength is determined by the FAT class (ΔσR) according to Table B-1 type E2 andE3
mdash For welded joints the fatigue strength analysis is normally based on the nominal stress σn at the structuraldetail considered and on an appropriate detail classification as given in Table B-1 which defines the FATclass (ΔσR)
mdash For those welded joints for which the detail classification is not possible or additional stresses occurwhich are not or not adequately considered by the detail classification the fatigue strength analysis maybe performed on the basis of the structural stress σS in accordance with [468]
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4662 The maximum stress range for a construction detail shall be calculated from the maximum upperstress σmax and the minimum lower stress σmin in this detail
Δσmax = σmax- σmin
4663 The maximum upper stress σmax and the minimum lower stress σmin shall be determined each fromloads of the most unfavourable magnitude location and direction acting on the lifting appliance in the mostunfavourable position
Thereby all partial safety factors shall be set γp = 1
467 Fatigue strength analysis for free plate edges and for welded jointsusing detail classification4671 Definition of nominal stress and detail classification for welded joints
46711 Corresponding to their notch effect welded joints are normally classified into detail categoriesconsidering particulars in geometry and fabrication including subsequent quality control and definition ofnominal stress Table B-1 shows the detail classification based on recommendations of the InternationalInstitute of Welding (IIW) giving the FAT class (ΔσR) for structures made of steel or aluminium alloys (Al)It shall be noted that some influence parameters cannot be considered by the detail classification and that alarge scatter of fatigue strength has therefore to be expected
46712 Details which are not contained in Table B-1 may be classified either on the basis of local stressesin accordance with [468] or else by reference to published experimental work or by carrying out specialfatigue tests assuming a sufficiently high confidence level (see [4691]) and taking into account thecorrection factors as given in [46926]Details contained in Table B-1 produced by improved manufacturing technology may be classified bycarrying out special fatigue tests as described above Such classification of details shall be agreed upon withthe Society case by case
46713 Regarding the definition of nominal stress the arrows in Table B-1 indicate the location anddirection of the stress for which the stress range shall be calculated The potential crack location is alsoshown in Table B-1 Depending on this crack location the nominal stress range shall be determined by usingeither the cross sectional area of the parent metal or the weld throat thickness respectivelyBending stresses in plate and shell structures shall be incorporated into the nominal stress taking thenominal bending stress acting at the location of crack initiation
Guidance noteThe factor Ks for the stress increase at transverse butt welds between plates of different thickness (see type A5 in Table B-1) canbe estimated in a first approximation as follows
t1 = smaller plate thickness
t2 = larger plate thickness
Additional stress concentrations which are not characteristic of the FAT class itself eg due to cut-outs in the neighbourhood of thedetail shall also be incorporated into the nominal stress
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
46714 In the case of combined normal and shear stress the relevant stress range shall be taken as therange of the principal stress at the potential crack location which acts approximately perpendicular (withinplusmn45deg) to the crack front as shown in Table B-1 as long as it is larger than the individual stress components
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DNV GL AS
46715 Where solely shear stresses are acting the largest principal stress σ1 = τ may be used incombination with the relevant FAT class
468 Fatigue strength analysis for welded joints based on local stresses
4681 Alternatively to the procedure described in the preceding paragraphs the fatigue strength analysisfor welded joints may be performed on the basis of local stresses For common plate and shell structures inships the assessment based on the so-called structural (or hot-spot) stress σs is normally sufficientThe structural stress is defined as the stress being extrapolated to the weld toe excluding the local stressconcentration in the local vicinity of the weld see Figure 4-5
Figure 4-5 Structural stress
4682 The structural stress can be determined by measurements or numerically eg by the finite elementmethod using shell or volumetric models under the assumption of linear stress distribution over the platethickness Normally the stress is extrapolated linearly to the weld toe over two reference points which arelocated 05 and 15 times plate thickness away from the weld toe In some cases the structural stress can becalculated from the nominal stress σn and a structural stress concentration factor Ks which has been derivedfrom parametric investigations using the methods mentioned Parametric equations should be used with dueconsideration of their inherent limitations and accuracy
4683 For the fatigue strength analysis based on structural stress the S-N curves shown in Figure 4-6apply with the following reference values
ΔσR = 100 (resp 40 for Al) for the butt welds types A1 to A6 and for K-butt welds with fillet weldedends eg type D1 in Table B-1 and for fillet welds which carry no load oronly part of the load of the attached plate type C1 to C9 in Table B-1
ΔσR = 90 (resp 36 for Al) for fillet welds which carry the total load of the attached plate eg type D2in Table B-1
In special cases where eg the structural stresses are obtained by non-linear extrapolation to the weld toeand where they contain a high bending portion increased reference values of up to 15 can be allowed
4684 In addition to the assessment of the structural stress at the weld toe the fatigue strength withregard to root failure shall be considered by analogous application of the respective FAT class eg type D3 ofTable B-1In this case the relevant stress is the stress in the weld cross section caused by the axial stress in the plateperpendicular to the weld It shall be converted at a ratio of t(2 middot a)
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469 Design S-N curves4691 Description of the design S-N curves
46911 The design S-N curves for the calculation of the cumulative damage ratio according to [46101]are shown in Figure 4-6 for welded joints at steel and in Figure 4-7 for notches at plate edges of steel platesFor aluminium alloys (Al) corresponding S-N curves apply with reduced reference values of the S-N curves(FAT classes) according to Table B-1 The S-N curves represent the lower limit of the scatter band of 95 ofall test results available (corresponding to 975 survival probability) considering further detrimental effectsin large structuresTo account for different influence factors the design S-N curves shall be corrected according to [4692]
Figure 4-6 S-N curves for welded joints at steel
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DNV GL AS
Figure 4-7 S-N curves for notches at plate edges of steel plates
46912 The S-N curves represent section-wise linear relationships between log (Δσ) and log (N)
log(N) = 70 + m middot Q
Q = coefficient defined asQ = log(ΔσR Δσ) - 069897 m0
m = slope exponent of S-N curve see [46913] and [46914]m0 = inverse slope in the range N le 1 middot 107 defined as
m0 = 3 for welded jointsm0 = 35 divide 5 for free plate edges (see Figure 4-7)
The S-N curve for FAT class 160 forms the upper limit for the S-N curves of free edges of steel plates withdetail categories 100 ndash 150 in the range of low stress cycles see Figure 4-7 The same applies accordingly toFAT classes 32 ndash 40 of aluminium alloys with an upper limit of FAT 71 see type E1 in Table B-1
46913 For structures subjected to variable stress ranges the S-N curves shown by the solid lines in Figure4-6 and Figure 4-7 shall be applied (S-N curves of type M) ie
m = m0 for N le 107 (Q le 0)
m = 2 middot m0 ndash 1 for N gt 107 (Q gt 0)
46914 For stress ranges of constant magnitude (stress range spectrum S7) in non-corrosive environmentfrom N = 1 middot 107 the S-N curves of type O in Figure 4-6 and Figure 4-7 can be used thus
m = m0 for N le 107 (Q le 0)
m = 22 for N gt 107 (Q gt 0)
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DNV GL AS
4692 Correction of the reference value of the design S-N curve
46921 A correction of the reference value of the S-N curve (FAT class) is required to account for additionalinfluence factors on fatigue strength as follows
ΔσRc = fm fR fw fi ft fs ΔσR
ΔσR = FAT class according to Table B-1 or EN 1993-1-9fm = correction factor for material effect according to [46922]fR = correction factor for mean stress effect according to [46923]fw = correction factor for weld shape effect according to [46924]fi = correction factor for importance of structural element according to Table 4-5ft = correction factor for thickness effect according to [46925]fs = additional correction factor for structural stress analysis according to [46926]
For the description of the corrected design S-N curve the formulae given in [46912] may be used byreplacing ΔσR by ΔσRc
46922 Material effect (fm)For welded joints it is generally assumed that the fatigue strength is independent of steel strength ie
fm = 10For free edges at steel plates the effect of the materials yield strength is accounted for as follows
For aluminium alloys fm = 1 generally applies
46923 Effect of mean stress (fR)The correction factor fR shall be determined by the following formulae
fR = 10 for σm ge (∆σmax2) (range of tensile pulsating stresses)
fR = for ndash (∆σmax2) le σm le (∆σmax2) (range of alternating stresses)
fR = 1 + 2 c for σm le ndash (∆σmax2) (range of compressive pulsating stresses)
c = coefficient defined as
c = 0 for welded joints subjected to constant stress cycles(stress range spectrum S7)
c = 015 for welded joints subjected to variable stress cycles(corresponding to stress range spectrum A or S0divideS6)
c = 030 for unwelded base material
46924 Effect of weld shape (fw)In normal cases
fw = 10A factor fw gt 10 applies for welds treated eg by grinding Grinding removes surface defects such as slaginclusions porosity and crack-like undercuts to achieve a smooth transition from the weld to the base
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material Final grinding shall be performed transversely to the weld direction The depth should be about 05mm larger than the depth of visible undercutsFor ground weld toes of fillet and K-butt welds machined by
fw = 115 for disc grinderfw = 130 for burr grinder
Premise for this is that root and internal failures can be excluded Application of toe grinding to improvefatigue strength is limited to following details of Table B-1
mdash butt welds of type A2 A3 and A5 if they are ground from both sidesmdash non-load-carrying attachments of type C1 C2 C5 and C6 if they are completed with a full penetration
weldmdash transverse stiffeners of type C7mdash doubling plates of type C9 if the weld throat thickness according to [11326] was increased by 30mdash cruciform and T-joints of type D1 with full penetration welds
The corrected FAT class that can be reached by toe grinding is limited for all types of welded connections ofsteel to fw ΔσR = 100 Nmm2 and of aluminium to fw ΔσR = 40 Nmm2For butt welds ground flush the corresponding reference value of the S-N curve (FAT class) shall be choseneg type A1 A10 or A12 in Table B-1For endings of stiffeners or brackets eg type C2 in Table B-1 which have a full penetration weld and arecompletely ground flush to achieve a notch-free transition the following factor applies
fw = 14The assessment of a local post-weld treatment of the weld surface and the weld toe by other methods egultrasonic impact treatment shall be agreed on in each case
46925 Plate thickness effect (ft)In order to account for the plate thickness effect application of the reduction factor ft is required for buttwelds oriented transversely to the direction of applied stress for plate thicknesses t gt 25 mm
n = exponent for additional notch effect at weld toe defined asn = 020 as weldedn = 010 toe-ground
k = exponent for misalignment (see [4643]) defined ask = 010 for butt welds with km = 130k = 005 for butt welds with km = 115
km = factor according to [4643]
For all other weld connections consideration of the thickness effect may be required subject to agreementwith the Society
46926 Correction factor for structural stress analysis (fs)If the fatigue strength analysis for welded joints is based on local stresses according to [468] then thereference value ΔσRc of the corrected S-N curve shall be determined according to [4643] taking intoaccount the following additional correction factor which describes influencing parameters not included in thecalculation model such as eg misalignment
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DNV GL AS
Δσsmax = applied peak stress range within a stress range spectrumΔσsb = bending portion of Δσsmax
krsquom = effective stress increase factor due to misalignments under axial loading defined askrsquom = km ndash 005
km = stress increase factor due to misalignments under axial loading at least km according to[4643]
If the fatigue strength analysis for free plate edges and for welded joints is based on detail classificationaccording to [467] then fs = 10
Table 4-5 Influence of the importance fi of a structural element on the fatigue strength analysis
Not safe to operate structural elementAccessibility Safe to operate
structural element No hazard to persons Hazard to persons
Accessible structuralelements 10 09 083
Badly accessible structuralelements 095 087 08
Safe to operate structural elements are parts with restricted consequences of a failure ie where the local breakage ofa structural element does not result in the failure of the structure or fall-down of the load
Not safe to operate structural elements are parts where the local breakage of a structural element results in immediatefailure of the structure of fall-down of the load
4610 Proof46101 Calculation of the cumulative damage ratio
461011 Where the fatigue strength analysis is based on the calculated cumulative damage ratio thepartial damages Di caused by the operating conditions in operation and out of operation shall bedetermined as follows
K = total number of blocks of the stress range spectrum for summation (in general K ge 20)nk = number of stress cycles in block kNk = number of endurable stress cycles determined from the corrected S-N curve (see [469]) taking
Δσ = Δσk
Δσk = stress range of block k
For this purpose in the condition in operation standard stress range spectra according to [46524] or[46525] or individually determined stress range spectra according to [46526] may be applied For thecondition out of operation the straight-line stress range spectrum according to [4653] shall be applied
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461012 The proof of fatigue strength is demonstrated if for the total cumulative damage ratio D thefollowing condition is met
46102 Permissible stress range
461021 The fatigue strength analysis may be performed based on the permissible maximum stressranges For this purpose in the condition in operation standard stress range spectra according to[46524] or [46525] shall be applied for the condition out of operation the straight-line stress rangespectrum according to [4653]The requirements given in the following are applicable for fatigue strength analyses conducted separately forthe conditions in operation and out of operationA superposition of the damages caused by the conditions in operation and out of operation is notrequired provided that the maximum stress range caused by the condition out of operation does notexceed 10 of the maximum stress range caused by the condition in operation Otherwise the fatiguestrength analysis shall be conducted on the basis of the calculated cumulative damage ratios according to[46101] or upon agreement with the Society
461022 The maximum stress range of the spectrum shall not exceed the permissible value Δσp
Δσmax le Δσp
Δσmax = maximum stress range according to [466]Δσp = permissible stress range according to [461023]
461023 The permissible stress ranges shall be calculated by the following formula
Δσp = fn middot ΔσRc
ΔσRc = corrected FAT class according to [46921]fn = factor for the shape and extent of the spectrum according to Table 46 to Table 4-10
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Table 4-6 Factor fn for the determination of the permissible stress range for welded joints (m0=3)
Number of stress cycles nmaxStressspectrum 2∙104 5∙104 105 3∙105 6∙105 106 3∙106 6∙106 107 5∙107 108
S0 1654 1294 1068 784 644 558 409 336 291 195 167
S1 1263 970 787 568 461 397 284 232 201 137 119
S2 1025 775 623 443 357 304 215 174 151 105 092
S3 836 623 500 352 282 240 168 134 116 082 072
S4 693 516 412 288 230 195 136 108 093 066 058
S5 592 438 348 244 194 164 114 091 077 056 048
S6 513 378 302 209 166 140 098 078 066 047 041
S7 470 345 275 191 151 127 089 070 059 043 037
Table 4-7 Factor fn for the determination of the permissible stress range for free edges of plateswith (m0 = 35)
Number of stress cycles nmaxStressspectrum 2∙104 5∙104 105 3∙105 6∙105 106 3∙106 6∙106 107 5∙107 108
S0934
1251 1818
1019 1739
873 1620
677 1548
574 1496 391 333 296 209 184
S1775
983 1668
787 1595
665 1485 420 372 282 238 211 151 134
S2665
809 1568
638 1497
534 1394 333 290 217 182 161 117 105
S3562
665 1475
520 1414 320 266 230 171 141 125 093 083
S4475
555 1400
430 1350 262 217 188 138 114 100 076 068
S5407
473 1340
366 1300 222 183 159 116 095 084 063 056
S6354
412 1296
317 1260 191 157 136 100 082 071 054 048
S7325
377 1270
290 1235 174 143 123 090 074 064 049 043
1) For ΔσR lt 125 [Nmm2](ΔσR = FAT class according to Table B-1 or EN 1993-1-9)
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Table 4-8 Factor fn for the determination of the permissible stress range for free edges of plateswith (m0 = 4)
Number of stress cycles nmaxStressspectrum 2∙104 5∙104 105 3∙105 6∙105 106 3∙106 6∙106 107 5∙107 108
S0778
883 1
1007 2
685732 1
848 2
620662 1
745 2
528560 1
598 2
473500 1
436458 1
365 322 293 219 195
S1647
693 1
809 2
562600 1
668 2
502536 1
580 2
418443 1
372388 1
339 275 240 217 161 145
S2554
594 1
674 2
475507 1
552 2
421449 1
473 2
356363 1
304 275 217 186 168 127 115
S3467
500 1
560 2
397424 1
453 2
349372 1
285 248 224 172 146 132 101 092
S4395
424 1
470 2
333356 1
377 2
291311 1
237 205 183 140 118 106 083 075
S5339
363 1
401 2
284304 1
320 2
248266 1
201 174 154 117 099 088 069 063
S6296
317 1
349 2
247265 1
278 2
215230 1
173 150 133 101 085 075 06 054
S7270
290 1
319 2
225241 1
254 2
196211 1
158 137 120 092 077 068 054 049
1) For ΔσR lt 150 [Nmm2]2) For ΔσR lt 140 [Nmm2]
(ΔσR = FAT class according to Table B-1 or EN 1993-1-9)
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Table 4-9 Factor fn for the determination of the permissible stress range for free edges of plateswith (m0 = 5)
Number of stress cycles nmaxStressspectrum 2∙104 5∙104 105 3∙105 6∙105 106 3∙106 6∙106 107 5∙107 108
S0 729 642 583 496 447 414 349 314 291 230 209
S1 607 526 471 394 352 323 269 240 221 175 160
S2 519 446 395 327 288 263 217 192 177 142 130
S3 438 371 327 267 235 214 174 153 141 114 106
S4 371 311 273 221 194 176 142 124 114 094 087
S5 317 266 233 188 164 149 120 105 095 079 073
S6 277 231 201 163 142 128 103 090 081 068 063
S7 253 211 184 148 129 116 093 081 073 061 057
Table 4-10 Factor fn for the straight-line stress spectrum with nmax = 5 middot 107
Welded joints Free edges of plates
m0 = 3 m0 = 5 m0 = 4 m0 = 35
353 363 366 365
47 Proof of suitability for use
471 General
4711 Shipboard lifting appliances as well as its structural elements and equipment shall be such designedand dimensioned that its safety and proper functioning is not adversely affected or endangered by one ormore of the influences stated hereafter
mdash deformations(eg formation of large amplitudes of vibration bending loads on hydraulic cylinders of telescopic beams)
mdash vibrations(eg generated by simultaneous operation of several lifting appliance drives by ship machinery orinfluences of sea state)
mdash heat(eg expansion overheating of drives or brakes)
mdash highest position of boom(see [12211])
4712 Suitability for use shall be demonstrated in the course of the initial testing on board
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472 Permissible deformations4721 Compression members
47211 The uniform deflection of compression members under permissible load shall not be larger than therod length divided by 250
47212 The uniform deflection of unloaded compression members or compression members loaded by deadload only which are special or primary structural elements (see [3121]) shall not be larger than the rodlength divided by 500
47213 The uniform deflection of unloaded compression members or compression members loaded by deadload only which are secondary structural elements (see [3121]) eg wind or framework bracings shallnot be larger than the rod length divided by 350
4722 Tension membersThe uniform deflection of unloaded tension members shall not be larger than the rod length divided by 50
48 Joints
481 Proof of weld joints4811 PrerequisitesThe strength of welding consumables shall be equal to or higher than that of the structural elements to beconnectedFor further general prerequisites see Sec11
4812 General strength analysis
48121 GeneralWeld thicknessrsquos which are the basis of the strength analysis are given in [114] for various shapes ofwelds
48122 Welds located in the plate planeThe permissible stress of welds located in the plate plane is the design value of the permissible stress of theadjoining plate according to [44223]
48123 Fillet weldsFor fillet welds the strength analysis may be conducted according to DNVGL-RU-SHIP Pt6 Ch13 oraccording to a recognized basic principle of calculation or standard
48124 Plates loaded by tension transversely to the direction of rollingSteels having through thickness ductility (Z-steel) may be required for plates and wide flat bars see also[3214]
4813 Proof of fatigue strengthRegarding the proof of fatigue strength the statements in [46] apply
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DNV GL AS
482 Proofs for bolted connections4821 General
48211 Bolted connections shall be dimensioned according to recognized guidelines basic principles ofcalculation or standards which possibly also allow for a fatigue strength analysis for the bolts
48212 The approaches according to [4822] and [4823] in principle imply that
mdash connected areas are secured against distortion eg by use of at least two (2) boltsmdash contacting areas are smooth and free from greasemdash the use of bolts of strength class 129 is agreed with the Society
4822 Gusset connections with fitting-bolts (fitting-bolt shear connections)
48221 DefinitionIn the case of fitting-bolt shear connections the loads to be carried are transferred by form-fitting Theseforces generate shear stresses in the bolts and bearing stresses at the gussets
48222 ConstructionFigure 4-8 shows a typical gusset connection If it is intended to be constructed as a fitting-bolt shearconnection the following notes shall be observed
mdash The clearance between bolt and drilling hole shall correspond to the tolerance classes h13 and H11 (orless) according to ISO 286-2
mdash Bolt shafts shall be as long as the thickness of the parts to be connected Where due to the cylindric shaftlength it is not possible to tighten the bolts washers shall be used
mdash Controlled pre-stressing of bolts is not required however a suitable securing device against looseningmdash A special surface treatment of the contact areas is not requiredmdash Forces to be transferred may at the maximum be distributed over five (5) (strength classes 46 and 56)
or three (3) (strength classes 88 109 and possibly 129) bolts per row to be arranged one after anotherin the direction of force
Figure 4-8 Example of a gusset connection
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DNV GL AS
Regarding the edge and hole distances according to Figure 4-8 the limit values according to Table 4-11apply
Table 4-11 Limit values for edge and hole distances
Min Max 1
Edge distances e1 and e2 15 middot dℓ 4 middot t + 40 mm
Hole distances p1 and p2 30 middot dℓ The lesser value of 14 middot t or 200 mm
1) t ndash thickness of the thinnest external plate
48223 Permissible stresses for bearing stress and shearing-offFor the bearing stress of structural elements made of steel as well as for the shearing-off of bolts thefollowing permissible stresses apply
(bearing stress)
(shearing-off)
ReH = yield strength of structural elements andor gussets according to material standard (nominal value)ReHs = yield strength of bolts according to Table 4-12
Correction coefficients ασ ατ
a) Multishear bolt connections
Rms = ultimate tensile strength of bolts according to Table 4-12 [Nmm2]Rm = ultimate tensile strength of structural elements according to material standard (nominal value)
[Nmm2]
b) Single-shear bolt connectionsασe = 078 middot ασm
ατe = 077
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DNV GL AS
Table 4-12 Strength values of bolts
Strength class 46 56 88 109 129
ReHs [Nmm2] 240 300 640 900 1080
Rms [Nmm2] 400 500 800 1000 1200
48224 Proofs for transmissible bolt forcesTo determine the largest bolt forces for the example in Figure 4-8 the following forces shall be addedgeometrically
For the most unfavourably stressed fitting-bolts on a connection or joint the following proofs for shearing-offof bolts and bearing stresses of the connected parts shall be provided
mdash bearing stresses Frd le ds middot tmin middot σzul
mdash shearing-off Frd le As middot nf middot τzul
Frd = largest resulting bolt force (rectangular to the bolt axis)ds = shaft diameter of the fitting-bolt (nominal diameter + 10 mm)tmin = smallest effective plate thicknessAs = cross-section area of shaft of fitting-boltnf = number of effective shear areas (single-shear or multishear)σzul τzul = permissible stresses according to [48223] [Nmm2]
In the case of a dynamic shear load the fatigue strength analysis shall be conducted for the mostunfavourably loaded fitting-bolt as follows
Stress spectra shall be determined according to [46]
The maximum stress range of the shear stress Δτmax shall be determined according to [46] for the shaftcross-section of the fitting-bolt
The design S-N curve for shear stress of fitting-bolts is shown in Figure 4-9
The fatigue strength analysis may be conducted on the basis of calculated damage ratios according to [46]
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DNV GL AS
As an alternative the fatigue strength analysis may be conducted on the basis of permissible stress rangesfor the standard spectra S0 to S7 according to [46] as follows
Δτmax le fnmiddot fi middot ΔτR
Δτmax = maximum stress range of the shear stress for the shaft cross-section of the fitting-boltΔτR = reference value for the stress range of the shear stress at 2middot106 stress cycles
ΔτR = 100 Nmm2
fn = factor for the shape and extent of the spectrum according to Table 4-13fi = influence of the importance of the structural element according to Table 4-5
Figure 4-9 Design S-N curve for shear load of fitting-bolts
48225 Proofs for structural elements and gussetsThe strength analyses for the structural elements and gussets connected with each other shall be based onthe cross-sections designed for tension compression shear and bending according to [434]For the permissible stresses see [4422]
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DNV GL AS
4823 Gasset connections with prestressed bolts (friction-grip connections)
48231 DefinitionWith friction-grip connections the forces to be sustained are submitted by friction between the contact areas(frictional locking)Fitting-bolts with the normal clearance do not effect any increase in the transmissible forces
Table 4-13 Factor fn for standard stress range spectra S0 to S7 according to [465] and design S-Ncurve according to Figure 4-9
Number of stress cycles nmaxStressspectrum 2middot104 5middot104 105 3middot105 6middot105 106 3middot106 6middot106 107 5middot107 108
S0 729 642 583 496 447 414 349 313 288 224 201
S1 607 526 471 394 351 323 269 238 218 167 151
S2 519 446 395 327 288 263 216 191 173 132 119
S3 438 371 327 267 235 214 174 153 138 103 094
S4 371 311 273 221 194 176 142 124 113 082 076
S5 317 266 233 188 164 149 120 105 095 069 062
S6 277 231 201 163 142 128 103 090 081 059 053
S7 253 211 183 147 128 116 093 081 073 053 046
48232 ConstructionFigure 4-8 shows a typical gusset connection For construction purposes the following notes shall beobserved
mdash Bolt holes shall not exceed the shaft diameter by more than 10 mmmdash The bolts shall be pre-stressed by controlled procedures and under consideration of the dispersion of the
installation force to the maximum installation force FMmax = αs middot ReHs middot Aσ where Aσ is the stress cross-section of the bolt Preferably the pre-stress coefficient is αs = 07 Well-founded deviations in the rangeof 06 le αs le 08 may be permitted
mdash Up to a thread diameter of 30 mm the pre-stress may be effected by the application of a torque Withlarger diameters hydraulic lengthening shall be applied
mdash For the contact areas a special surface treatment is required according to [48233]mdash Casting compound for compensation of unevennesses in the contact areas is not permissiblemdash Only bolts of strength class 88 109 and possibly 129 may be usedmdash The forces to be submitted may be distributed over 3 rows of bolts at a maximummdash The hole distances shall comply with the requirements according to [48222]mdash Only one plate of a gusset connection may have a plate thickness which is equal to or higher than the
bolt diametermdash Bolts of strength class 129 require a highly accurate layout in the supporting areas under the head and
nut
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DNV GL AS
48233 Friction coefficient microThe friction coefficient depends on the surface treatment and shall be selected as follows
micro = 050 for surfaces
mdash of shining metal layers steel shot or sand blasted without unevennessmdash steel shot or sandblasted and covered with aluminiummdash steel shot or sandblasted and metal covered by a metal cover made of a zinc material which
effects a friction coefficient of at least 05
micro = 040 for surfaces steel shot or sand blasted and coated with a 50 microm to 80 microm thick alkali-zinc-silicate layer
micro = 030 for surfaces shiny metallic cleaned with a steel brush or by flame deseaming
micro = 020 for surfaces free of rust oil and dirt
48234 Proof of transmissible forcesA sufficient slide resistance shall be proven for the most unfavourable bolt in a connection or joint seeexample in [48224] using the following condition
Frd le Fμd middot nr
Fμd = force transmissible by friction in 1 friction areanr = number of effective friction areaAσ = stress section-area of the bolt according to Table 4-14Fa = external tension force in the direction of the bolt axismicro = friction coefficient according to [48233]ΔFSetz = loss of pre-stress force by setting according to [49142]αA = tightening factor of the tightening procedure used
αA = FMmaxFMmin
FMmax = maximum installation force in consideration of the dispersion of installation force for thetightening procedure used
FMmin = minimum installation force in consideration of the dispersion of installation force for thetightening procedure used
Additionally sufficient resistance against shearing-off and bearing pressure according to [4822] shall beproven including the calculation of the shear capability of the stress cross-section Aσ
48235 Proof of surface pressure under head and nut of the boltFor material S 235 and where applicable also for S 355 proof of the permissible surface pressure under thehead or nut of the bolt respectively shall be to carried out in the following way
If proof cannot be provided tempered washers shall be used
σp zul = permissible surface pressure in according with Table 4-15 [Nmm2]Aa = smallest contact surface of the bolt head or nut considering bore diameter and chamfers [mm2]
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DNV GL AS
Fad = design value of the external tensile force in the direction of the bolt axisΦ = tensioning factor according to [49132]
48236 Proofs for structural elements and gussetsFor the strength analyses the statements according to [48225] apply It may be assumed that 13 of theforce Fμd transmissible by friction has already been transmitted before the bolt hole see [48234]
Table 4-14 Stress and core sections of bolts
Diameter [mm] Stress section Aσ [mm2] Core section AK [mm2]
Metric ISO thread according to DIN 13
12 843 7625
14 115 1047
16 157 1441
18 193 1751
20 245 2252
22 303 2815
24 353 3243
27 459 4271
30 561 5190
Metric thread with large clearance according to DIN 2510 Sheet 2
33 668 617
36 786 723
39 943 873
42 1083 999
45 1265 1174
48 1426 1320
52 1707 1590
56 1971 1833
64 2599 2426
72 3372 3174
80 4245 4023
90 5479 5226
100 6858 6575
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DNV GL AS
Table 4-15 Permissible surface pressure under heads and nuts of bolts
Material σp zul [Nmm2]
S235 260
S355 C45N 46G2N 46Cr4N 420
C45V 46Cr4V 42CrMo4V 700
GG25 800
483 Proofs for rivet connectionsFor proof of rivetshear connections the statements in [4822] apply analogously Instead of shaftdiameter the hole diameter shall be usedOnly hydraulic riveting is permissible The clamping length of the rivet shall be restricted to the value 65 middotdrivet where drivet is the nominal diameter of the rivet
49 Special structural elements
491 Flange connections with pre-stressed bolts4911 General
49111 In the case of flange connections with pre-stressed bolts the forces to be sustained are transmittedby tensional load of the bolts and possibly by friction fitting
49112 The provisions under [4913] and [4914] do not apply to flanges for the connection of largeslewing bearings In this respect [5741] shall be observed
4912 ConstructionFigure 4-10 shows a typical flange connection For construction purposes the following notes shall beobserved
mdash Bolt holes may be larger than the shaft diameter ds by the value ΔdΔd le 01 middot ds le 30 mm
mdash In general the bolt distance s (see Figure 5-4) shall not be larger than 6 middot dsmdash In general the span length of bolts shall be at least 3 middot dsmdash At least 3 threads shall remain freemdash The bolts shall be pretensioned by controlled procedures The degree of utilization ν of the yield strength
ReHs of the bolt in the mounted condition is preferably in the range 07 le ν le 09 Well-foundeddeviations may be permitted
mdash Up to a thread diameter of 30 mm pretension may be conducted by application of a torque in the case oflarger diameters hydraulic lengthening is required
mdash The contact surfaces require a special surface treatment according to [48233]mdash Casting compound for compensation of unevennesses of the contact areas is not permissible un-less
otherwise stated by slewing bearing makersmdash Only bolts of strength class 88 109 and possibly 129 may be usedmdash Bolts of strength class 129 require a highly accurate layout in the supporting areas under the head and
nut
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DNV GL AS
4913 Forces acting on a flange connection
49131 Figure 4-10 shows a typical flange connection with its essential dimensions and the proportionalexternal axial force Fa per bolt sectorThe external axial force Fa acting on the individual bolt location of the flange connection may normally bedetermined by means of elastomechanics from the operational loads of the gusset connectionIn the case of an excentric load the compensating line of action of the external axial force has the distanceaers from the bolt axis The distance aers shall be determined from the location of the zero point of thebending moment curve of the system which is the nearest to the bolt
49132 The external force Fa in the connecting parts (tension force) acts as an additional load on theprestressed bolt and reduces the surface pressure in the parting line The force ratio Φ governs the portion ofthe external axial force which acts on the bolt additionally to the prestressing force as well as the remainingportion which discharges the tensioned structural elements
The force ratio Φ depends on the resiliences of the bolt and the tensioned structural elements theexcentricity of the tensioning andor the external operational force as well as the leading-in of the force Thereliable determination of Φ is therefore complex and shall in principle be conducted by way of measurementtechniques or based on recognized calculation procedures
Provided that the bending of the bolt due to the excentricity of the tensioning and the bending of the bolt dueto the excentricity of the external axial force Fa do not superimpose each other in the same direction Φ maybe approximately calculated as follows
Φ = α for proofs in [49141] [49143] [49151] and [48235]
Φ = 0 for proofs in [49142] and [4915]
δs = axial resilience of the bolt [mmN]δp = axial resilience of the tensioned structural elements [mmN]lk = clamping length [mm]ds = shaft diameter of the bolt [mm]Es = Youngs modulus of the bolt [Nmm2]Ep = Youngs modulus of the tensioned structural elements [Nmm2]dw = head bearing diameter [mm]g = flange dimension according to Figure 4-10 [mm]f = bolt distance [mm]
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DNV GL AS
Figure 4-10 Flange connection
4914 Proofs for the external tension force Fa of the boltThe proofs described in the following apply to bolt connections with an external axial force Fa according to[49131] provided that
mdash Tensioned structural elements form simple prismatic bodiesmdash The load on the bolt is proportional to the external axial forcemdash Where external loads are absent the surface pres-sure in the parting line of the prestressed bolt
connection shall to a large extent evenly distributed
A surface pressure in the parting line of the prestressed bolt connection to a large extent evenly distributedmay normally be assumed if the dimensions of the parting line are as follows
g lt dw+tf
tf = thickness of the thinner flange plate
Bolt connections which are in addition to an external axial force or solely loaded by an external bendingmoment shall be proven separately
49141 Proof of yield strength of the boltIn the mounted condition the following condition shall be observed
FMmax le FMzul
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DNV GL AS
Where torsion-free tightening procedures are applied the permissible installation force FMzul is as follows
FMmax = maximum installation forceFMzul = permissible installation forceReHs = yielding strength of the boltν = predefined degree of utility of the yield strength in the mounted conditionAσ = stress cross-section of the bolt according to Table 4-14dσ = stress diameter of the boltd2 = effective diameter of the boltP = pitch of threadμG = friction coefficient in the thread
If there is no information about the friction coefficient μG in the thread the friction coefficient shall beestimated conservatively eg according to VDI 2230 Part 2 with consideration of surface properties andlubricants used
In service the equivalent stress of the bolt shall not exceed the permissible value
In the case of torsion-free tightening procedures or in the case of complete reduction of torsion stresses inthe thread in service proof of operational stress of the bolt may be conducted as follows
σvd = design value of the maximum equivalent stress of the bolt in operationσzd = design value of the maximum tensile stress of the bolt in operationτredd = design value of the reduced maximum torsion stress of the bolt in operationFSd = design value of the maximum bolt force in operation
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DNV GL AS
49142 Proof against open gapThe following condition shall be met for the proof against open gap (see Figure 4-10)
FVmin = lowest pre-stressing force of the boltFMmin = smallest installation forceαA = tightening factor of the tightening procedure used (see [48234])ΔFSetz = loss of pre-stressing force due to setting [N]
(a 2-fold pre-stressing with time-lag reduces the setting to a residual value which may possiblybe disregarded)
δs δp = resilience of the bolt and the tensioned structural elements according to [49132] [mmN]aers = distance between the compensating line of action from Fa and the bolt axis according to
[49131]feff = the smaller value of f or (dw + tf)geff = the smaller value of g or (dw + tf)z = for g le dw + tf the smaller value of 0 or ((geff 2) - e)
for g gt dw + tf the smaller value of 0 or (g - (geff 2) - e)
In the case of through-bolt connections for tf the thickness of the thinner gusset plate shall be assumed inthe case of screw-in connections the thickness of the gusset plate with the through-bore
Minor one-sided gapping of the parting line is accepted in the above condition Large-area gapping of theparting line may be accepted if the bolt connection by means of measurement techniques or based onrecognized calculation procedures while considering the progressive increase of the bolt stress due toremoval of tensioned structural elements is proven separately
49143 Proofs of fatigue strengthIn the case of dynamic loads proof of fatigue strength of the bolts shall be conducted as stated in thefollowing
Stress range spectra shall be determined according to [46]
The maximum stress range of the normal stress Δσmax shall be determined according to [46] for the stresscross-section of the thread of the bolt
For a proof of fatigue strength of gaping bolt connections eg by numeric calculation methods Δσmax shallbe determined for the lowest prestress force of the bolt FVmin
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DNV GL AS
When the stress range of the normal stress Δσmax is calculated tensile and bending stresses in the stresscross-section of the thread of the bolt shall be taken into consideration For the bending stress in the cross-section of the threads stress cross-section the following applies
σb = bending stress in the stress cross-section of the thread of the boltds = shaft diameter of the bolt
The design S-N curves for proofs of fatigue strength of prestressed bolts are shown in Figure 4-11
The proof of fatigue strength may be conducted on the basis of calculated cumulative damage ratiosaccording to [46]
Alternatively the proof of fatigue strength may be conducted based on permissible stress ranges for thestandard spectra S0 to S7 according to [46] as follows
Δσmax le fnmiddot ksmiddot fimiddotΔσR
ks = 1 for d le 30 mm(30d)025 for d gt 30 mm
Δσmax = maximum stress range of the normal stress in the stress cross-section of the boltΔσR = reference value of the stress range of the normal stress at 2 middot 106 stress cyclesΔσR = 71 Nmm2 for bolts either tempered or rolled as final treatmentΔσR = 50 Nmm2 for all other boltsfn = factor for shape and extent of the spectrum according to Table 4-16fi = influence of importance of structural element according to Table 4-5ks = influence factor for sized = nominal thread diameter
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DNV GL AS
Figure 4-11 Design S-N curves for prestressed bolts
Table 4-16 Factor fn for standard stress range S0 to S7 according to [465] and design S-N curveaccording to Figure 4-11
Number of stress cycles nmaxStressspectrum 2middot104 5middot104 105 3middot105 6middot105 106 3middot106 6middot106 107 5middot107 108
S0 1654 1294 1068 784 644 555 406 333 287 182 151
S1 1263 970 787 568 461 397 284 229 195 123 103
S2 1025 775 623 443 357 304 215 172 146 089 076
S3 836 623 500 352 282 240 168 134 114 068 058
S4 693 516 412 288 230 195 136 108 092 054 046
S5 592 438 348 244 194 164 114 091 077 045 037
S6 513 378 302 209 166 140 098 078 066 039 031
S7 467 345 273 189 151 127 088 070 059 035 028
4915 Proof of transmissible forces in the clamping gapThe statements in [48234] apply where nr = 1Normally this proof shall not be conducted for the connection of large diameter slewing rings
49151 Proof of surface pressure below head and nut of boltThe statements in [48235] apply
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DNV GL AS
49152 Construction and calculation of flangesConstruction
The dimensions a b and c in Figure 4-10 shall comply with the following requirements
1) a mdash not larger than necessary for clamping tools2) b mdash sufficiently large for generating the supporting force3) c mdash sufficiently large for the weld including the excess length required for the welding process4) b a ge 075
The workmanship of the weld next to the connecting bolts requires special diligence
Calculation of flange thickness
The gusset thickness tf may simplified be calculated as follows
αe = coefficient for the construction of the wall50 for cylindric walls60 for flat walls
tw = wall thickness according to Figure 4-10σwd = design value of the stress in the wall (including partial safety factors γpi)σRd = design value of the permissible stress in the flange according to [4422]
492 Hydraulic cylinders4921 GeneralHydraulic cylinders shall be designed and manufactured in accordance with DNVGL-CG-0194 design loadsshall be determined on basis of the operating conditions lifting appliance in operation and lifting applianceout of operationFollowing deviations from DNVGL-CG-0194 shall be observed
mdash proof of stability according to [4423] and [4923]mdash proof of wall thickness according to [4922]mdash proof of eye strengthgeometry according to [7343]mdash proof of fatigue strength according to [46]
4922 Simplified dimensioning of cylinder pipes
49221 For thin-walled cylinder pipes the required wall thickness twerf may be calculated as follows if therequirement according to [49222] is complied with
Da = outer diameter [mm]pc = setting pressure of the relief valves according to [9622] [bar]fyr = calculated yield strength according to [4332] [Nmm2]
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DNV GL AS
49222 The formula in [49221] for the required wall thickness is based on the shear stress hypothesisTherefore the following condition shall be complied with if the cylinder pipe is dimensioned using thisformula
σℓ = longitudinal stress in the cylinder pipe (characteristic value without partial safety factors γpi)
49223 The wall thickness tw of the cylinder pipe shall comply with the following requirement
tw = wall thickness of the cylinder pipetwerf = required wall thickness according to [49221]c = corrosion allowance minimum 03 mm
49224 Cylinder pipes not complying with the condition according to [49222] shall be proven accordingto [44]In this case the partial safety factor for the internal pressure (= setting pressure pc of the safety valves) is
γp = 134
49225 A calculated strength analysis shall be conducted for the connecting welds of the pipes
49226 In order to avoid local bending stresses the head and bottom plate of the cylinder pipes shall notfall below the following minimum thickness
tp = thickness of head or bottom plate respectivelytw = wall thickness of the cylinder pipe
4923 Proof of stability
49231 The proof of stability is according to [4423] to be conducted for the most unfavourablecombination of buckling length ℓki and respective pressure (depending on the kinematics of the liftingappliance)
49232 The design force shall include the partial safety factors γp as well as any dynamic coefficients (ψ)and shall be calculated for the most unfavourable load combination
49233 As an imperfection for the proof of stability a distortion of the hydraulic cylinder of ℓki300 shall betaken into consideration
49234 At the ends of the cylinder the following moment shall be assumed due to friction of the carrierbolts
Nd = design force (pressure) in the hydraulic cylinder including the partial safety factors γp
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DNV GL AS
micro = 008 (= friction coefficient)dB = bolt diameter
49235 If a buckling proof of a hydraulic cylinder will be conducted according to Eurocode 3 EquivalentMember Method the rod geometry shall be laid down for the entire buckling length
4924 Tensile stressesIn the case of tensile-stressed hydraulic cylinders particular attention shall be paid to the thread of thepiston rod during strength analysis
493 Large cylindric pipes4931 Dimensions and loadsFigure 4-12 shows the dimensions and loads of circular cylinder shells
rm = radius related to the middle of wall thickness [mm]tw = Wall thickness [mm]
r = pipe length [mm]Da = outer diameter (nominal diameter) [mm]σx = longitudinal stress [Nmm2]τ = shear stress [Nmm2]σφ = circumferential stress [Nmm2]
Figure 4-12 Dimensions and loads of circular cylinders
49311 The longitudinal and shear stresses are calculated as follows
σx = longitudinal stress [Nmm2]τ = shear stress [Nmm2]Fx = force in x-direction [N]Fz = force in z-direction [N]Mz = bending moment [Nmm]Mx = torsional moment [Nmm]
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DNV GL AS
4932 Proofs of stability
49321 Proofs against buckling shall be performed according to [4423] Proofs against shell buckling maybe conducted according to EN 1993-1-6
49322 Regarding the application of the proofs of stability according to EN 1993-1-6 the following shall beobserved
mdash Instead of safety factor γM1 according to the Euro-code the value γm according to [43743] shall beused
mdash Instead of the yield strength the calculated yield strength fyr according to [4332] shall be used
49323 Proofs against shell buckling need not be conducted if the following requirements are compliedwith
a) pipes loaded by stress in circumferential direction
E = Youngs modulus [Nmm2]206 middot 105 Nmm2 for steel
ReH = yield strength according to material standards [Nmm2]
b) pipes loaded by compression in longitudinal direction
c) pipes loaded by shear
d) very long pipes loaded by compression
ℓki = buckling length of the pipe [mm]
Guidance noteThese proofs apply provided that the edges are radially undisplacable
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
49324 The requirements according to a) to d) apply provided that the imperfections according to[4933] are not exceeded during manufacture
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DNV GL AS
4933 Imperfections due to manufacture
49331 CurvaturesIn the case of outward or inward curvatures caused by manufacture the depth gauge f according to Figure4-13 shall not exceed 1 of the smallest gauge length The following gauge lengths apply
mdash gauge length in longitudinal direction of the pipe [mm]ℓmx = (in the unwelded area)
= (in the area of welds)
mdash gauge length in circumferential direction [mm]ℓmφ =
(in the unwelded area)
= (in the area of welds)
tmin = thickness of the thinner plate adjacent to the weld
Figure 4-13 Curvature including designations
49332 Out-of-roundnessThe out-of-roundness is defined as follows
[]
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DNV GL AS
Figure 4-14 Measurement of the diameters for determination of out-of-roundness
The permissible out-of-roundness Uadm may be calculated as follows
for mm
[] for mm
for mm
Proof format U le Uadm
49333 Excentricities in x-directionPlanned eccentricities or eccentricities due to manufacture located at the centerline of joints of plates withequal or differing wall thickness tw shall not exceed the following values ex
ex le 02 middot tmin le 3 mm
tmin = the smaller of the two plate thicknesses
494 Shear connection of circular structural elementsRegarding the connection of circular masts posts and crane columns with eg deck plates the requiredplate thickness of the deck plating tp and the required weld thickness a may be determined according to thefollowing formula
or [mm]
tp = required minimum thickness of deck platesa = required minimum thickness of weldD = connection diameter [mm] (Da or possibly Di)fyr = calculated yield strength according to [4332] [Nmm2]γm = partial safety factor for resistance values according to [43743] [-]Fz = maximum horizontal force to be transmitted [N]Mx = torsional moment of the connection [Nmm]
The internal forces Fz and Mx are design values and include the partial safety factors γp for loads according to[4374]
Regarding the designation of axes see Figure 4-12
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DNV GL AS
495 Local loads due to wheel loads4951 General
49511 Local loads due to wheel loads occur mainly with rails girders of crane rails and girders of trolleysStructural elements which are eg loaded by wheels of fork lift trucks shall be treated analogously
49512 Local loads shall be taken into consideration when the proof of structural safety according to [44]as well as the proof of fatigue strength according to [46] are conducted
4952 Girders of crane rails
49521 For the calculation of the local compression stresses the relationships as shown in Figure 4-15apply
ℓd = length of pressure distribution [mm]ℓd = 2 middot hs + ℓf
hs = distance between contact area of the wheel andintersection line considered [mm]
f = length of contact area of the wheel [mm]f = 02 middot rℓ le 50 mm
rℓ = running radius [mm]FR = wheel load [N]
Figure 4-15 Pressure distribution of wheel loads
49522 Regarding the connecting welds of crane rails made of square steel bars and welds joining web andflange it shall be assumed that the transmitted pressure takes place solely through the welds
4953 Girders of trolleys
49531 In Figure 4-16 typical local deformations are shown highly magnified
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DNV GL AS
FR = wheel loadσxσy
= local and global stresses
Figure 4-16 Local deformation of girders of trolleys (highly magnified)
49532 Calculation of local stresses in the lower flanges of girders for trolleys may be conducted inaccordance with a recognized calculation method or standard eg Federation Europeenne de la Manutention(FEM) Section IX book 9341
49533 For general strength analysis local and global stresses shall be superimposed with the localstresses reduced to 75
49534 In the case of lower flanges welded to the web for the connecting weld a proof of fatigue strengthmay possibly be required
496 Bolt connections
4961 Bolts shall be secured against falling out Outer bearing plates and gussets shall be secured againstgapping
4962 Bolt connections shall be proven according to [482]
497 Eye plates and eye rods
4971 Proof of eye plates may be conducted according to [7343]
4972 Eye rods according to Figure 4-17 may be dimensioned as follows
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DNV GL AS
F = design value of the tensile force (including partial security factor γp according to [4374])fyr = calculated yield strength according to [4332]γm = partial safety factor for resistance values according to [43743]
Figure 4-17 Example of an eye rod
498 Joints of hollow profile girdersDimensioning of hollow profile girder joints may be performed according to EN 1993-1-8Alternatively a shape strength analysis for the joints of hollow profiles to other hollow profiles or openprofiles may be conducted based on another recognized calculation method
499 Stairs ladders platforms and railings4991 Load assumptions
49911 Accesses platforms etc shall be dimensioned for a distributed load of at least 3000 Nm2 or for amovable single load of 1500 N
49912 Guard-rails and toe boards shall be dimensioned for a lateral load in the form of a movable singleload of 300 N
49913 The loads according to [49911] and [49912] need not be considered for the global calculationof lifting appliances
4992 Proof of structural safety
49921 Proof of structural safety shall be conducted according to [44]
49922 The partial safety factor for the loads is γp = 134
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DNV GL AS
SECTION 5 CRANES AND SUPPORTING STRUCTURES
51 General
511 Description of contents
5111 This section contains requirements for design and dimensioning of cranes and their supportingstructures onboard ships which are also correspondingly applicable to other lifting appliances and theirsupporting structures according to [1131]
5112 The type of design is not subject to restrictions However the requirements given in [57] shall betaken into account
5113 The dimensioning is based on Sec4 and distinguishes between the conditions in service and out ofservice for all proofs
512 Influences caused by the ship and the shiprsquos operation
5121 Apart from special tasks such as eg handling of hatch covers or offshore activities the shiprsquosinfluence shall also be considered for the design and dimensioning of cranes on board ships predeterminedeg by the form of the hull its bending and torsional stiffness or the shiprsquos operationPossible influences to be considered may be
mdash arrangement of the cranes on the shipmdash stability of the shipmdash area of operation of the shipmdash high ship speedmdash sea lashing of the cranesmdash special operating conditions
5122 The increase of load radius of cranes due to the existing heel of the ship andor the heel generatedby the lifting of load may be taken advantage of upon approval by the Society The values of Table 4-2 shallbe complied with
513 Dimensioning of cranesThe cranes listed in the following shall be dimensioned according to different criteria
5131 Shipboard cranes
51311 Cranes for harbour operation
51312 Cranes for sea operation
5132 Floating cranesDepending on their use floating cranes shall be dealt with like shipboard cranes for harbour or sea operationrespectively
5133 Lifting appliances not handling cargoShipboard lifting appliances not handling cargo shall be dealt with like shipboard cranes for harbouroperation taking into consideration their service or environmental conditions
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DNV GL AS
514 Dimensioning of supporting structures
5141 The principal supporting structures are
mdash crane columnsmdash crane foundationsmdash runways for mobile cranesmdash crane boom supportsmdash structural transits into the shiprsquos hull
5142 Crane columns and crane foundations shall be dimensioned similarly like the allocated cranes whereapplicable also according to [5412]
5143 When dimensioning runways the requirements given in [495] as well as according to [5744]shall be observed
5144 Crane boom supports shall be dimensioned according to [566]
52 Crane groups
521 General
5211 The allocation to crane groups may be of influence on the determination of hoist load coefficientsthe main aspect however is the fatigue strength
5212 Non-distinct allocations shall be agreed with the Society This applies in particular to side andauxiliary hoists
5213 The following allocations to crane groups in each case refer to the main hoist of a crane
522 Crane group A
5221 Crane group A includes mainly cranes which do not handle cargo and which with the exception ofhatch cover cranes and hose cranes are not always exposed to the full safe working load Such cranes arecharacterized by irregular use and longer rest periods
5222 Cranes of group A1 which also launch and recover life-saving appliances shall be dimensioned inaddition according to the LSA-Code
5223 Crane group A is further subdivided as follows
52231 Crane group A1 includes cranes for the operation of the ship in the harbour such as eg
mdash provision cranesmdash engine room cranesworkshop cranesmdash hatch cover cranesmdash hose cranes
52232 Crane group A2 includes cranes for the operation of the ship at sea such as eg
mdash service cranesmdash engine room cranes (used at sea state)
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DNV GL AS
52233 Crane group A3 includes floating cranes not used for cargo-handling like eg
mdash mounting cranes
523 Crane group B
5231 Crane group B primarily includes cranes used for cargo-handling and which are not always exposedto the full safe working load These cranes are characterized by regular use and longer rest periods
5232 Crane group B is further subdivided as follows
52321 Crane group B1 includes shipboard cranes for cargo-handling in the harbour using spreaders orhooks such as eg
mdash container cranesmdash general cargo cranes
52322 Crane group B2 includes cranes for cargo-handling at sea using hooks such as eg
mdash general cargo cranes
52323 Crane group B3 includes floating cranes for cargo-handling using hooks such as eg
mdash floating cargo cranes
524 Crane group C
5241 Crane group C primarily includes cranes for cargo-handling and which are regularly exposed to thefull or nearly full safe working load
5242 Crane group C is further subdivided as follows
52421 Crane group C1 includes shipboard cranes for cargo-handling in the harbour using grabs hooks orspecial load-handling devices such as eg
mdash grab cranesmdash pallet cranes
52422 Crane group C2 includes ship cranes for cargo-handling at sea using grabs such as eg
mdash grab cranesmdash lighter cranes
52423 Crane group C3 includes floating cranes for cargo-handling using grabs such as eg
mdash grab floating cranesmdash lighter floating cranes
525 Change of crane group
5251 In the cases of a change of crane group change to the safe working load or change to the loadradius in addition to an assessment of drawings the manufacturer shall calculate the estimated residuallifetime where applicable
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DNV GL AS
53 Design loads
531 General
5311 The loads acting on the structural components of cranes and their supporting structures aresubdivided as follows
mdash regular loadsmdash irregular loadsmdash special loads
5312 Cranes for the conveyance of persons shall comply with the requirements given in [4251] and[4252]
5313 If necessary loads not addressed in the following shall be properly taken into account The rating ofsuch loads and considering them in the corresponding load combinations shall be agreed with the Society
532 Regular loads5321 Dead loads (LE)Dead loads shall be determined in accordance with [4242] A distinction should be made between loadingand unloading dead loads acting on each structural element
5322 Hoist load (LH)The definition of hoist load is given in [11522] Regarding the crane dimensioning the safe working load(SWL) shall be regarded as part of the hoist loadDepending on the type of operation and considering a dead weight portion (LEA) according to Figure 1-1hoist load shall be determined as follows
mdash harbour operation LH = LEA + SWLmdash sea operation LHsee = LEA + SWLsee
SWLsee shall be calculated according to [54321]
5323 Loads from driving over an uneven runwayWhere the design conditions according to [5744] are met the application of vertical dynamic forces causedby driving over an uneven runway may be omitted Or else the application of the load shall be agreed withthe Society
5324 Dynamic forces due to drive systems
53241 GeneralThe dynamic forces to hoist loads and to components of lifting appliances caused by drive systems may bedetermined in a simplified manner using the method described in the followingThe designations vertical and horizontal refer to the coordinate system of the cranes
53242 Vertical dynamic forces due to lifting of a loadThe acceleration forces generated by the lifting of a resting load during harbour operation shall be consideredby application of the hoist load coefficient ψ according to [5431]The acceleration forces generated by the lifting of a resting or moving load during sea operation shall beconsidered by application of the hoist load coefficient ψsee according to [5432]
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DNV GL AS
53243 Vertical dynamic loads due to suspended loadGenerally for a suspended load no lifting or braking forces need to be considered This also applies forbraking a crane boom with suspended load
53244 Horizontal dynamic forces due to lifting of a loadIn the case of lifting a resting load during harbour operation the horizontal components of the load LH middot ψresulting from the shiprsquos heeling angle according to Table 4-2 shall be assumed as horizontal dynamic forcessee also [53262]In the case of lifting a resting or moving load during sea operation the horizontal component of the loadLHsee middot ψsee resulting from the shiprsquos inclinations according to Table 4-2 and the cargo runner deflection angleaccording to [53263] shall be assumed as horizontal dynamic forces
53245 Horizontal dynamic forces due to suspended loadThe accelerations at the crane boom peak due to rotating slewing pivoting and telescoping motions shall beindicated by the manufacturer
If no other proof is given the radial acceleration br for rotating and slewing cranes may be calculated asfollows
ω = (π middot n) 30 = angular speed [1s]r = rotatingslewing radius [m]v = ω middot r = circumferential speed [ms]n = rpm [1min]
In the case of rotating cranes for hoists on the ship or on the installation half of the circumferential speedmay be assumed
In the case of rotating or slewing cranes the tangential acceleration bt may be assumed to be equal to theradial acceleration br if no other proof is given
The horizontal forces of the working load and the dead load of the crane boom due to the ships inclination εand the rotating or slewing acceleration may be added vectorially For ε see [42441]
53246 Horizontal dynamic forces with mobile cranesHorizontal dynamic forces caused by starting and braking in the direction of travelling shall be indicated bythe manufacturer If such manufacturerrsquos information is not available at least 16 of the loads of powered orbraked wheels shall be assumedThe wheel loads are calculated from the dead loads of the crane and the hoist load Oscillatingly suspendedhoist loads may be disregardedIn the case of an off-center location of the center of gravity the horizontal side forces which occursimultaneously shall be considered as well
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DNV GL AS
5325 Dynamic forces generated by ship motions
53251 General noteThe following requirements apply exclusively for the dead loads LE of cranes For a more accuratedetermination of the dynamic forces the requirements given in [547] apply
53252 Cranes in serviceVertical dynamic forces
Generally vertical dynamic forces during operation of cranes at sea need not be allocated any loadcombination according to [552] and they also need not be explicitly proven
Horizontal dynamic forces due to the inclination of the crane base
For the sea operation of cranes the horizontal forces resulting from the ship inclinations according to Table4-2 may be assumed unless not deviant indicated by the operator
The inclination of the crane base may be considered to be an obliquely positioned system or by distribution ofthe forces into components
Horizontal dynamic forces due to the acceleration of the crane basis
For the sea operation of cranes in addition to the horizontal forces the following horizontal accelerations bhshall be assumed if cranes are operated at significant wave heights of H13 gt 2 m
mdash barges and catamarans bh = 075 middot (H13 ndash 2) ge 0 [ms2]
mdash ships bh = 05 middot (H13 ndash 2) ge 0 [ms2]
mdash semi-submersibles bh = 025 middot (H13 ndash 2) ge 0 [ms2]
H13 = significant wave height [m]
53253 Cranes out of serviceIn the condition out of service at sea the vertical and horizontal dynamic forces may be calculatedaccording to AppA
5326 Diagonal pull forces due to cargo runner deflection angles
53261 GeneralDiagonal pull forces may be generated when a load is hoisted due to a relative shift between load and craneboom peak They shall be superimposed to the ship inclinations of Table 4-2Cargo runner deflection angles in the longitudinal and transverse direction of a crane boom shall beconsidered as occurring simultaneously in the dimensioning process
53262 Harbour operationIn general diagonal pull forces due to cargo runner deflection angles need not be taken into considerationduring harbour operation
53263 Sea operationShipboard cranes
When not determined more precisely the cargo runner deflection angle shall be assumed as
φl = φq = H13 [deg]
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DNV GL AS
φl = deflection angle in longitudinal direction of the crane boomφq = deflection angle in transverse direction of the crane boomH13 = significant wave height [m]
For cranes with a slewing mechanism the deflection angle in transverse direction may be halved if therequirement given in [57321] is met
Floating cranes
For floating cranes with a safe working load SWL le 60 t the requirements given in this subsection apply Inthe case of higher safe working loads the requirements given in [57322] shall be met additionally
5327 Partial dropping of the working load during normal operation
53271 When a part of the working load WL is dropped during normal operation as eg by cranes withgrabs or load magnets this may be accounted for by application of a dropping factor fa
53272 The load FSa which shall be used for dimensioning see Figure 5-1 shall be calculated as follows
φ = 05 for grabs or slow load dropping= 10 for load magnets or fast load dropping
Figure 5-1 Dropping of a part of the working load (examples)
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DNV GL AS
53273 When the dropping factor is fa lt 0 the load FSa may become negative as well This corresponds toa load directed upwards
5328 Tie-down force of the cargo hooksWhen cargo hooks are tied-down for the load condition crane out of service this load shall be considered asthe tie-down force This load shall be indicated by the manufacturer If no information is available this loadmay be assumed to be 10 of the safe working load (SWL)
533 Irregular loads5331 Wind loadsWind loads shall be assumed according to [4245]The total wind load acting on a crane structure is the sum of the single wind loads acting on its variousstructural components
5332 Snow and ice loadsFor snow and ice loads the requirements given in [4246] apply
5333 Temperature loadsFor temperature loads the requirements given in [4247] apply
5334 Side forces when driving (diagonal drive)
53341 The side forces occurring when the crane or trolley is being driven shall be taken into consideration
53342 When two (2) wheels or wings are mounted for one (1) rail the two forces generated by one-sided guidance may be calculated by multiplying the wheel or wing load with the side force coefficient γSk
according to Figure 5-2 The side force coefficient γSk depends on the ratio between span bs and wheelspacing ℓr
53343 Two-sided guidances or more than two (2) wheels or wings on one (1) rail shall be consideredseparately
Figure 5-2 Side force coefficient γSk
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DNV GL AS
534 Special loads5341 Dynamic test loadsThe dynamic test loads LPdyn for cranes shall be taken from Table 13-2 The hoist load coefficient ψ may bereduced using the following formula
ψP = (1 + ψ) 2
5342 Buffering forces
53421 At the ends of carriage ways of cranes and trolleys arrestors shall be mounted with buffersattached either to them or to the cranesBuffers shall be dimensioned such that they are capable to absorb 70 of the kinetic energy of the liftingappliance driving at maximum speed The mass of oscillatingly suspended hoist loads are not considered
53422 The impact force on the buffer shall be determined from the buffer characteristic and - in order totake into consideration the dynamic effect of the buffering force - to be multiplied with the following factor fp
fp = 125 for buffer with linear characteristic= 160 for buffer with rectangular characteristic
53423 Lower speeds than according to [53421] may be assumed if reliable (redundant) appliancesreduce the speed in way of the runway ends
5343 Loads on stairs ladders platforms and railingsFor access loads see the requirements given in [499]
5344 Loads due to safety systemsThe loads LS due to safety systems such as eg
mdash AOPS (Automatic overload protection system)mdash MOPS (Manual overload protection system)mdash ELRS (Emergency load release system)
shall be indicated by the crane manufacturer
5345 Tear-off of the hoist loadIn the catastrophic case of the hoist load torn off this results in fa = - 1 according to [53272] and Figure5-3 fa and with this the calculated load directed upwards becomes minus LH
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DNV GL AS
Figure 5-3 Hoist load torn off (see [5345])
54 Hoist load coefficients
541 General
5411 The hoist load or the loads resulting from it shall be multiplied with an allocated hoist load coefficientfor the lifting of the resting load If the crane has several hoisting appliances or differing hoisting speedsindividual hoist load coefficients shall be allocated to each of them
5412 For the strength analysis of load-bearing structural elements as far as its fastening to the ship hullreduced hoist load coefficients may be applied if the corresponding dampening in the load-bearing system isproven by calculation or measurement
542 Hoist load coefficient ψ as a function of crane group and hoistingspeed
5421 For harbour operations the hoist load coefficient may be simplified taken from Table 5-1
5422 An individual calculation of the hoist load coefficient according to [543] may be necessary oradvisable
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DNV GL AS
Table 5-1 Hoist load coefficient for different crane groups
Crane-group Hoist load coefficient ψ ψmin
A1 117
B1
C1 135
For descriptions of crane groups see [522] to [524]vh according to Table 5-2
Table 5-2 Hoisting speed in the course of lifting the load
Hoisting gear type and hoisting speed vhLoad combination
HD 1 HD 2 HD 3 HD 4
LK I + LK II vhmax vhF vhF 05vhmax
LK III 1 minus vhmax minus vhmax
1) For hoisting gear types HD 2 and HD 4 the hoist load coefficient ψ calculated from vhmax shall be proven as loadcombination III1
HD 1 = creep hoist not possibleHD 2 = creep hoist selectable by the crane driverHD 3 = creep hoist switched on automatically until the load is lifted from the groundHD 4 = hoisting speed is infinitely variable by the crane drivervhmax = maximum constant hoisting speed of the allocated load [ms]vhF = constant creep hoisting speed [ms]
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DNV GL AS
543 Calculation of the hoist load coefficient ψ as a function of the cranestiffness5431 Harbour operation
54311 Calculation of the hoist load coefficient ψThe hoist load coefficient shall be calculated as follows
ψmin = minimum value according to Table 5-1vh = hoisting speed in the course of lifting of the safe working load according to Table 5-2 [ms]cs = crane stiffness according to [5433] [kNm]SWL = safe working load [t]
54312 Simplified calculation for jib cranes with hoisting and luffing ropesIn the case of jib cranes with hoisting and luffing ropes only the hoisting and luffing ropes as well as thecrane boom need to be included in the simplified calculation The hoist load coefficient ψ is then calculated asfollows
5432 Sea operation
54321 Calculation of the hoist load coefficient ψsee
vr = relative speed between load and hook in the course of lifting the load [ms] according to[54322]
cs = crane stiffness [kNm] according to [5433]SWLsee = safe working load at sea [t]ψ = hoist load coefficient for harbour operation
With the exception of cranes dimensioned only for sea operation the following condition shall be observed
54322 Relative speed between load and hookvr = 05 middot vh + vsee [ms] for LC I [55211]
vr = vh + vsee [ms] for LC III [55231]
vh = hoisting speed in the course of lifting the respective safe working load (SWLsee) according to Table5-2 [ms](The minimum hoisting speed according to [57311] shall be taken if larger than vh)
vsee = speed induced by seastate according to Table 5-3
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DNV GL AS
Table 5-3 Speed induced by seastate vsee
From thelocationof thecrane(va)
to the cargo deck or to the sea surface (vd)
Fixedinstallation
Semi-submersible FSO FPSO Large barge Small barge Supply ship Sea surface
Fixedinstallation 0 025middot(H13)
075 032middot(H13)075 038middot(H13)
075 050middot(H13)075 070middot(H13)
075 085middot(H13)067
Semi-sub-
mersible025middotH13 035middot(H13)
090 040middot(H13)088 047middot(H13)
087 060middot(H13)083 073middot(H13)
080 090middot(H13)070
FSOFPSO 040middotH13 045middotH13 053middot(H13)
088 062middot(H13)090 070middot(H13)
090 080middot(H13)087 (H13)
078
Largebarge 060middotH13 065 middot H13 070middot(H13)
094 075middot(H13)094 085middot(H13)
094 090middot(H13)094 120middot(H13)
080
Smallbarge 110middotH13 111 middot H13 116middot(H13)
094 118middot(H13) 097 120middot(H13)
097 130middot(H13) 094 140middot(H13)
091
va = vertical speed of the crane boom peak [ms]
vd = vertical speed of the cargo deck or sea surface [ms]
H13 = significant wave height [m]
5433 Calculation of the crane stiffness cs
54331 Principals of calculationThe stiffness of a crane depends on the load radius and the height of the load hookFor calculation of the crane stiffness besides the ropes all load-bearing structures as far as the fastening ofthe crane column or the crane base shall be taken into consideration with the exception of [54312]Regarding the approach of the rope stiffness the Youngacutes modulus indicated by the rope manufacturer shallbe taken
54332 Permissible simplification for the calculationFor round strand ropes without a more precise proof a Youngrsquos modulus of 10 middot 105 Nmm2 based on thegross cross-section may be taken Curve-shaped load radius diagram
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DNV GL AS
If the load radius diagram is curve-shaped the crane stiffness shall be calculated at least for the end pointsand the one-third points of the regarded range of load radius Based on these values a continuous curvemay be determinedStep-shaped load radius diagramIf the load radius diagram is step-shaped the stiffness shall be calculated for each load level As analternative the stiffness may be calculated for the minimum load radius of each load level These valuesapply then for the whole range of one levelHeight of the cargo hookFor operations in harbour conditions it may be assumed that the cargo hook is at the altitude of the craneboom pivot point For operations in seastate conditions it may be assumed that the cargo hook is 6 m abovethe water surface except for underwater operations
544 Calculation of the hoist load coefficient for hoists onboard the shipFor hoists onboard the ship the simplified hoist load coefficient for sea operations may be assumed to be
ψsee = 115 + 051 middot vh ge ψ
vh = hoisting speed in the course of lifting the safe working load according to Table 5-2 [ms]ψ = hoist load coefficient for harbour operation
545 Calculation of the hoist load coefficient for auxiliary hoistsThe hoist load coefficient for auxiliary hoists is calculated (simplified) to be
ψ = 120 + 068 middot vh ge ψmin = 145
546 Calculation of the hoist load coefficient by means of hydrodynamicanalysis
5461 Using model tests or stochastic and hydrodynamic calculation methods the hoist load coefficient canbe determined more accurate These methods generally apply for all service conditions of the crane
5462 The calculation shall be performed under consideration of the motion behavior of the floating bodiesinvolved and the stiffness of the crane Influences of special appliances such as rope-spindling devices orheave compensators may be taken into account in the process
5463 The calculation shall include at least the following influences if applicable
mdash vertical and horizontal motions of the cargo deckmdash motion behavior of the floating body on which the crane is mountedmdash load-bearing structure of the cranemdash hydrodynamic properties of a floating or submerged loadmdash influence of anchoring systemsmdash environmental conditions agreed
5464 The calculation shall be submitted to the Society for the design assessment of the crane as adocument for information In particular the influences listed in [5463] shall be represented clearly in thedocument
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DNV GL AS
55 Load combinations and partial safety factors
551 General
5511 The load combinations regarded as essential for cranes and their supporting structures are listed inthe Table 5-4 (cranes in service) and Table 5-5 (cranes out of service)Further load combinations may be relevant if necessary
5512 Only those load combinations from Table 5-4 Table 5-5 and further load combinations if necessarywhich are essential or necessary for the actual structural element under consideration shall be verified
5513 Regarding load combinations for operation at sea instead of ψ the hoist load coefficient ψsee forunderwater operations the hoist load coefficient ψu shall be taken
5514 The load combinations for the proof of safety against overturning are listed in Table 5-6
5515 The partial safety factors γpi shall be taken from Table 5-4 to Table 5-6
552 Explanations regarding load combinations for cranes in serviceaccording to Table 5-45521 Load combinations IThe load combinations I include regular loads in normal service
55211 I1 ndash Lifting and setting-down of the safe working loadAll regular loads which occur during lifting and setting-down of a load shall be superposed as required forthe load combination I1For vertical and horizontal dynamic forces the requirements given in [5324] and [5325] apply
55212 I2 ndash Suspended loadAll regular loads which are generated by acceleration and deceleration forces of hoisting gear luffing gearand travelling gear when a load is positioned shall be superposed as required for the load combination I2taking into consideration static ship inclinations and possible diagonal pull
5522 Load combinations IIThe load combinations II include regular loads during normal service combined with non-regular loads
55221 II1 ndash Load combination I1 with wind loadsLoad combination II1 results from load combination I1 plus appropriate wind loads Snow ice oretemperature loads are only to be assumed upon agreement
55222 II2 ndash Load combination I2 with wind loadsLoad combination II2 results from load combination I2 plus appropriate wind loads Snow ice oretemperature loads are only to be assumed upon agreement
55223 II3 ndash Constant drive including diagonal pullFor load combination II3 all loads shall be superimposed as required which occur at constant drive includingdiagonal pull Snow ice or temperature loads are only to be assumed upon agreement
Standard mdash
DN
VG
L-ST-0377 Edition O
ctober 2018Page 113
Shipboard lifting appliances
DN
V G
L AS
Table 5-4 Load combinations and partial safety factors for cranes in service
Load combinations
I II IIILoadcate-gories
Loads i Reference
γpi I1 I2 γpi II1 II2 II3 γpi III1 III2 III3 III4 III5
Dead loads LE(including inclination of crane base) 1 [5321] 122 1 10 10 116 1 10 10 10 1101 102 10 10 10 10
Hoist load LH 6
(including inclination of crane base) 2 [5322] 134 ψ 10 122 ψ 10 10 110 mdash mdash 10 mdash 10
Dynamic forces due to drives3 3 [5324] 134 mdash 10 122 mdash 10 mdash mdash mdash mdash mdash mdash mdash
Regularloads
Diagonal pull 4 [5326] 134 ψ 10 122 ψ 10 mdash mdash mdash mdash mdash mdash mdash
Wind loads in operation 5 [5331] 122 10 10 10 110 mdash 02 mdash mdash 10
Snow and ice loads 6 [5332] 122 10 10 10 mdash mdash mdash mdash mdash mdash
Temperature loads 7 [5333] 116 10 10 10 mdash mdash mdash mdash mdash mdash
Non-regularloads
Side forces during drive 8 [5334] 116 mdash mdash 10 mdash mdash mdash mdash mdash mdash
Hoisting of hoist load at vhmax 9 Table 5-2 110 ψmax mdash mdash mdash mdash
Dynamic test load Lpdyn(including inclination of crane base) 10 [5341] 110 mdash ψp mdash mdash mdash
Buffing forces 11 [5342] 110 mdash mdash 10 mdash mdash
Specialloads
Loads caused by safety systems 4 5 12 [5344] 110 mdash mdash 10 mdash
Partial safety factor γm for resistance values 110 110 110
Global safety factor γs 148 134 122
1) When load components have a favourable effect γpi = 095 If masses and centres of gravity are determined by weighing 095 middot γpi may be assumed2) Components caused by inclination of crane base may be neglected3) Applicable for load components from dead load and hoist load4) Emergency stop shall be verified by a practical test with a test load of LPdyn see [132422]5) Loads which may be generated by activated safety systems shall be indicated by the manufacturer6) For load combination III5 LH = SWL (M)
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DNV GL AS
5523 Load combinations IIILoad combinations III include special load combinations
55231 III1 ndash Hoisting of the safe working load at maximum hoisting speedComplementing load combination I1 load combination III1 includes operating errors during hoisting of theload The hoist load coefficient shall be determined for the maximum possible hoisting speedrelative speedbetween load and hook and the respective load level
55232 III2 ndash Test loadsLoad combination III2 includes hoisting of the dynamic test load at 20 wind load
55233 III3 ndash Buffer forcesLoad combination III3 comprises the impact of a crane with hoist load against the end buffers
55234 III4 ndash Safety systemsLoad combination III4 comprises loads which may result from activated safety systems
55235 III5ndash Failure of hydraulic cylinderLoad combination III5 contains special load combinations covering a cylinder failure of a lifting applianceconveying persons
Table 5-5 Load combinations and partial safety factors for cranes out of service
Load combinations
IA IIIALoad
categories Loads i Reference
γpi IA1 γpi IIIA1
Dead loads LE 1 [5321] 122 1 10 110 1 10
Dynamic forces due to ship motions 2 [53253] 134 10 110 10Regular loads
Tie-down force of the cargo hook 3 [5328] 122 10 110 10
Snow and ice loads 4 [5332] 110 10Non-regularloads Temperature loads 5 [5333] 105 10
Special loads Wind loads out of operation 6 [5331] 110 10
Partial safety factor γm for resistance values 110 110
Global safety factor γs 148 122
1) Where load components have a favorable effect γpi = 095
553 Explanations regarding load combinations for cranes out of serviceaccording to Table 5-55531 Load combination IALoad combination IA includes regular loads for cranes out of service
55311 IA1 ndash Combination of regular loadsFor load combination IA1 all regular loads shall be superimposed as required
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DNV GL AS
5532 Load combination IIIALoad combination IIIA includes special load combinations for cranes out of service
55321 IIIA1 ndash Special load combinationFor load combination IIIA1 the wind loads out of operation shall be superimposed with the regular loads asrequired Snow ice or temperature loads are only to be assumed as non-regular loads upon agreement
Table 5-6 Load combinations and partial safety factors for proof of safety against overturning
Load combinations
I II IIILoadcategories Loads i Reference
γpi I1 γpi II1 γpi III1 III2
Dead loads LE (including inclinationof the crane base) 1 [5321] 110 1 10 110 1 10 110 1 10 10
Hoist load LH (including inclinationof the crane base) 2 [5322] 134 10 122 10 110 minus 10
Dynamic forces due to drives 2 3 [5324] 134 10 122 10 110 minus 10
Regular loads
Diagonal pull 4 [5326] 134 10 122 10 minus minus minus
Non-regular loads Wind loads in operation 5 [5331] 122 10 110 02 10
Dynamic test load Lpdyn (includinginclination of the crane base) 6 [5341] 116 10 minus
Special loads
Buffer forces 7 [5342] 110 minus 10
1) Where load components have a favourable effect γpi = 0952) Applicable for load components from dead load and hoist load
554 Explanations regarding load combinations for the proof of safetyagainst overturning according to Table 5-65541 Load combination ILoad combination I includes regular loads under normal operation
55411 I1 - Combination of regular loadsFor load combination I1 all regular loads shall be superimposed as necessary
5542 Load combination IILoad combination II includes regular loads in normal operation together with non-regular load
55421 II1 - Load combination I1 with wind loadsLoad combination II1 results from load combination I1 plus allocated wind loads
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DNV GL AS
5543 Load combination IIILoad combinations III comprise special load combinations
55431 III1 - Test loadsLoad combination III1 considers the hoisting of the dynamic test load at a 20 wind load
55432 III2 - Buffer forcesLoad combination III2 comprises the impact of a crane with hoist load against the end buffers
56 Proofs
561 General
5611 The following proofs shall be conducted for all structural elements connections and supportingstructures of cranes for the conditions in service and out of service
mdash strength analysis according to [44] and [48]mdash proof of stability according to [44]mdash fatigue strength analysis according to [46]
5612 The following proofs shall be conducted for a complete crane as required
mdash proof of safety against overturning according to [45]mdash proof of suitability for use according to [47]
5613 For the proof of crane boom supports and rectan-gular crane columns the requirements given in[566] and [567] apply
562 Strength analyses and proofs of stability
5621 Strength analyses and proofs of stability shall be conducted using the partial safety factors of Table5-4 or Table 5-5 respectively for the load combinations of [55]
563 Fatigue strength analyses
5631 In general fatigue strength analyses shall be conducted for the load combination I of Table 5-4 andTable 5-5 with the partial safety factors γpi = 10As a basis for dimensioning regarding fatigue strength analyses the crane manufacturer shall provide loadcycles and the respective load spectrum (see also Table 5-7)
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DNV GL AS
Table 5-7 Load spectra and load cycles (examples application not mandatory) for shipboard andfloating cranes in harbour operation
Crane groupaccording to [52] Crane type
Loadspectrumaccordingto [465]
No ofload cycles
Hatch cover crane
Engine roomworkshop crane
Provision crane
S6
S2
S2
20000
10000
20000A1
Shipboard cranes
Hose crane S6 50000
A3Floating cranes
Mounting crane
SWL le 60 t
60 t lt SWL le 500 t
SWL gt 500 t
S2
S3
S4
80000
50000
20000
Container crane SWL le 60 t S3 350000
B1Shipboard cranes General cargo crane
SWL le 60 t
60 t lt SWL le 250 t
250 t lt SWL le 500 t
SWL gt 500 t
S2
S3
S4
S4
250000
100000
70000
50000
B3Floating cranes
Cargo-handling crane
SWL le 60 t
60 t lt SWL le 250 t
250 t lt SWL le 500 t
SWL gt 500 t
S2
S3
S4
S4
300000
125000
80000
60000
Grab craneSWL le 60 t
SWL gt 60 t
S5
S5
600000
450000C1Shipboard cranes
Pallet crane S6 600000
Grab craneSWL le 60 t
SWL gt 60 t
S5
S5
700000
500000C3Floating cranes
Lighter crane S5 2000000
5632 For cranes with load cycle numbers le 20000 a fatigue strength analysis may be dispensed with
5633 The fatigue strength analysis for the condition out of service shall be conducted for a load cyclenumber of 5 middot 107 This assumes a straight-line spectrum A according to Figure 4-4
5634 Superposition of in service and out of serviceA superposition of the fatigue damage due to the conditions in service and out of service is not necessaryas long as the maximum stress in the condition out of service does not exceed 10 of the maximum stressin the condition in service Or else the load spectrum applicable for the analysis and the allocated load cyclenumbers shall be agreed with the Society
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DNV GL AS
564 Proof of safey against overturning
5641 The proof of safety against overturning shall be conducted with the partial safety factors and loadcombinations according to Table 5-6 unless not shown in practice see [45213]
565 Proof of suitability for use5651 Proof procedures
56511 Proofs of suitability for use may be performed in the course of the initial testing on boardmathematically or as a combination of both procedures
56512 In general the mathematical proof of suitability for use shall be conducted for the load combinationI according to Table 5-4 and Table 5-5 using partial safety factors γpi = 10
5652 Proof of permissible deflection of crane boomsThe maximum deflection of pressure-loaded crane booms shall correspond to the crane boom length dividedby 350 if the dead weight alone is considered and to the crane boom length divided by 250 if dead weightplus hoist load are consideredThe peak of crane booms under bending stress which are held by luffing cylinders shall in general not exceeda vertical lowering of the maximum crane boom length divided by 100For special crane types (eg telescopic cranes knuckle boom cranes) and cranes made from extra highstrength steels higher boom peak lowering may be accepted by the Society based on single case approvals
5653 Proof against remaining in the highest crane boom position
56531 Where no restoring or warning devices according to [122112] are provided a proof of suitabilityfor use shall be shown for crane booms handled by luffing ropes under the following boundary conditions
mdash dead load coefficient φe = 095 for all load components of the crane boom unless they are confirmed byweighing Else φe = 10
mdash static ship inclinations according to Table 4-2mdash hoist load coefficient ψ = 10mdash wind load acting unfavourably calculated from 80 of the mean design wind speed in service according
to [4245]mdash consideration of all friction and guide losses
56532 For crane booms handled by cylinders the requirements given in [122113] apply
566 Proof of crane boom supportsCrane boom supports shall be proven for the load combinations in Table 5-5 and the allocated partial safetyfactors In addition the following shall be observed
mdash The dead load also includes the dead load component of the crane boommdash Where a relative movement is possible between the crane boom and the crane boom support additionally
an alternating friction force shall be considered with a friction coefficient of at least μ = 015mdash tie-down force of a cargo hook (see [575])
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DNV GL AS
567 Proof for rectangular crane columnsA general strength analysis shall be conducted regarding the maximum corner stress This is done byallocating the maximum crane moment MKmax to the main axes of the crane column in the most unfavourabledistribution
57 Requirements for design and equipment
571 GeneralThe following statements complement the requirements given in this and other sections of this standardStructural elements details of equipment and design which are not covered shall be dealt with according tothe Generally recognized rules of good practice
572 Supporting structures5721 Design requirements for crane columns
57211 Access to cranesRegarding the accesses to cranes inside or outside of crane columns the statements in [10622] and[12214] apply
57212 Design and calculationIn the case of tapered transition components which transit from a cylindrical crane connection to arectangular column special attention shall be paid to the knuckle line between the cambered parts and theplane gussets If necessary thicker plates shall be providedIn way of connections of tapered or trapezoid transitions of crane columns knuckle lines especially of evenplates shall be stiffened if necessary by bulkheads in order to absorb the deviation forcesThe transition parts and their connection areas described above require special care regarding fabricationand suitable mathematical proofsThe connection of container supports to crane columns requires special care regarding design and calculation
57213 Execution of cylindrical crane columns weldsIn the case of cylindrical crane columns all transverse and longitudinal welds shall be the full penetrationtype
57214 Execution of rectangular crane columns weldsAll transverse welds of rectangular crane columns shall be the full penetration type Regarding longitudinalwelds the following applies
a) Longitudinal welds in the plates shall be the full penetration typeb) The connecting welds at the corners may be dimensioned for the maximum shear force and may be
executed as fillet welds
57215 Connection to the ship hullWherever possible crane columns should be linked to the hull over a full deck height if necessary eg in thecase of crane columns located at the shiprsquos side even to a greater depth into the structure of the shipSupporting structures interrupted by decks shall have well aligned connections If necessary control boresshall be provided which shall be welded up after the controlFor the shear connection of inserted cylindrical crane columns the required plate thickness of the connectingdeck or of the connecting weld may be calculated according to [494]
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DNV GL AS
Crane columns which due to their location act as stiffness-discontinuities in the longitudinal and transversestructures of ships such as eg laterally arranged crane columns with outer longitudinal walls which areattached to the shell plating of the ship shall have suitable taper brackets as requiredCrane columns shall not be connected to hatch coamings if possible Where the connection to hatchcoamings cannot be avoided suitable measures are required like eg tapered brackets and strengthanalyses for the additional loads
5722 Requirements for the design of the stowage trough of crane boom supports
57221 If possible the stowage trough shall embrace the stowage spur or a stowage holm without majorclearance (10 to 20 mm at maximum) and be lined with wood or other suitable material
57222 The gripping effect in the stowage trough caused by torsion of the shiprsquos hull in particular withcrane booms which are not stowed lengthwise shall be counteracted by a suitable design
57223 Where a luffing rope operated crane boom is not fixed downwards by tying-down of the cargo hooklocking devices shall be provided in way of the stowing trough in order to prevent of the crane boom comingoffThese devices shall not restrain the relative motions between stowing trough and crane boom
57224 Each stowing trough shall be accessible by means of ladders or climbing irons and locally provide asuitable area for operating control andor maintenance purposes
573 Hook speeds when operating under sea state5731 Minimum hoisting speed
57311 Cranes with a safe working load le 60 tWhen operating under sea state conditions the hoisting speed shall be high enough to avoid repeatedcontact between load and cargo deck after hoisting
It is recommended that the uniform minimum hoisting speed vhmin does not fall below the following value
mdash multiple- reeved cargo runner vhmin ge 03 middot vsee [ms]
mdash single-reeved cargo runner vhmin ge 05 middot vsee [ms]
vsee = sea state-induced speed according to Table 5-3 [ms]
57312 Cranes with a safe working load gt 60 tWhen operating under sea state conditions the hook speed resulting from superimposing the hoisting andthe luffing speed as well as the ballast speed of the floating body shall be high enough to avoid damage tothe crane or the load from repeated contact between load and cargo deck
5732 Horizontal hook speed
57321 Revolving cranes with a safe working load le 60 tDuring loading and unloading of floating bodies it is important that the crane hook is capable of following thehorizontal movement of the cargo deck
It is recommended that the uniform slewing speed vω at the crane boom peak at about frac34 of the maximumload radius does not fall below the following value
vω ge 060 middot vsee [ms]
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DNV GL AS
vsee = sea state-induced speed according to Table 5-3 [ms]
57322 Revolving cranes with a safe working load gt 60 tThe luffing speed and luffing acceleration shall be sufficient to ensure control of transverse load oscillationLoad arresting ropes which limit the swinging of the load may be taken into consideration according to theireffectiveness
5733 Luffing speedIt is recommended that the uniform vertical luffing speed vW at the crane boom peak at about frac34 of themaximum load radius does not fall below the following value
vW ge 010 middot vsee [ms]
574 Design details5741 Connection of slewing bearings
57411 Proof of boltsThe bolt connection shall be dimensioned according to recognized guidelines calculation principles orstandards according to which if need be also a fatigue strength proof for the bolts can be conducted egVDI 2230The global safety factors according to [4382] shall be provenSpecial care shall be taken over the determination of the maximum bolt force as eg an opening of the gapincreases the bolt force non-linearThe stiffness of the slewing bearing can have a significant influence on the stress distribution in theconnecting structure The sector force Fa for the maximum loaded bolt according to Figure 5-4 shall bedetermined according to a recognized calculation procedure (eg FEM calculation under consideration of theconnecting structures stiffness) or by measurementA simplified bolt proof according to [57412] can be conducted on condition the restrictions for applicationaccording to [74121] are complied with
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DNV GL AS
Figure 5-4 Bolt sector and sector force
57412 Simplified bolt proofRestrictions for application
The simplified bolt proof can be applied if
mdash the outer bolt circle diameter does not exceed 35 mmdash stiffness of connecting structures (eg crane house crane pedestal) is approximately equal over the
circumferencemdash foot bearings of jibs and if applicable bearings of hydraulic cylinders on the crane house sufficiently
distant from the base plate of the crane housemdash the bolts of the standing and of the rotating ring are even distributed over the circumference and their
quantity per ring is not less than 12mdash the following relations are kept
a le 2 middot dℓ
b ge 15 middot dℓ
ba ge 075
a b dℓ according to Figure 5-6
d = thread diameter of bolt
Format of proof
The following relations shall be kept
Zmax Zlimit le 1 or Zmax le Zlimit
Zmax = maximum tensile force in bolt [kN]Zlimit = limit value of tensile force in bolt [kN]
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DNV GL AS
Maximum tensile force in bolt
The maximum tensile force in the bolt is calculated as follows
Zmax = f middot Znom [kN]
Znom = nominal tensile force of the highest loaded bolt of a multiple bolt connection [kN]f = form factor according to Table 5-8 [-]
Table 5-8 Form factors
Tensile class of boltKind of flange connection
88 109 129
Tensioning procedure with torsion 13876 13592Ball bearing
Tensioning procedure without torsion 11563 1132713451
Tensioning procedure with torsion 12923 12659Roller bearing
Tensioning procedure without torsion 10769 1055012528
Figure 5-5 Forces on a large slewing bearing
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DNV GL AS
Forces on a large slewing bearing
For the terms and forces in Figure 5-5 the following abbreviations are valid which apply to the outer ringanalogously
Dr = roller circle diameter [mm]Dt = pitch circle diameter [mm]Dm = middle diameter of pedestal [mm]a = distance between pitch circle and middle of pedestal wall [mm]br = vertical force lever [mm]e = distance between bolt centre and start of chamfer (constraint lever) [mm]hr = horizontal force lever [mm]tf = flange thickness [mm]tw = wall thickness of pedestal [mm]
Load from the crane
The following loads shall be determined including the global safety factor γs according to [4382] for themost unfavourable load combination according to Table 5-4 and Table 5-5
MSd = tilting moment [Nmm]VSd = vertical force [N]HSd = horizontal force [N]
Forces acting on the ring per bolt sector
According to Figure 5-5 the following forces are valid in case VSd is pointing in that direction shown in Figure5-5 (compressive force)
[N]
[N]
[N]
D = lowest value of Dm Dt and Dr
ns = number of boltsFhd = Fvd middot γh [N]Fhz = Fvz middot γh [N]
Fhd Fhz forces between the rings with influence to the bolt forces
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DNV GL AS
γh = horizontal force coefficient= 0 for multi row bearing= 0577 for single row ball bearing= 1 for single row cross roller bearing
Calculation of maximum nominal tensile force
Based on the dimensions according to Figure 5-5 and on the forces acting on the bearing ring the maxi-mumnominal tensile force is calculated as follows
Znom =
Limit value of tensile force of bolt
The limit value of tensile force of the bolt shall be calculated as follows
Zlimit = σlimit middot Ak 1000 [kN]
σlimit = limit stress according to Table 5-9 [Nmm2]Ak = core section of bolt according to Table 4-14 [mm2]
Table 5-9 Limit stresses of bolts
Tensile class 88 109 129
Limit stress σlimit [Nmm2] 560 768 912
57413 Requirements for the flangeFlange connection
In general the upper part of crane columns which are provided with a flange for connection to a slewingbearing shall be designed according to Figure 5-6 In the case of an inner bore circle the same conditionsapply
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DNV GL AS
Figure 5-6 Upper part of crane column
Dimensioning of the flange
Dt = partial circle diameterDa = outer cylinder diametertf = flange thicknessdℓ = bore diameterr = corner radius
a = external partial circle
a = internal partial circle
h = height of connection areatw1 = cylinder wall thickness in the connection areatw2 = cylinder wall thickness below the connection area
The flanges shall be designed and dimensioned according to [49152] As far as no proof by FE-computation has been conducted in addition the following conditions shall be met
tf ge 3 middot tw1
tw1 ge 15 middot tw2
Facing
The flange thickness shall still be warranted after the facing
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DNV GL AS
Flange evenness
The evenness of the connecting areas on a slewing bearing shall meet the requirements given by themanufacturer of this bearing
Use of compounds
The use of compounds in order to achieve the evenness required by the manufacturer of the slewing bearingis only accepted in exceptional cases for repair purposes upon agreement by the Society and slewing bearingmanufacturer
57414 Requirements for the cylinder wall in the connection areaDimensioningThe wall thickness t1 and the connection weld shall be dimensioned with regard to fatigue strengthHeight of connectionAs far as no proof by FE-computation has been conducted the height of the uppermost cylinder sectionaccording to Figure 5-6 shall at least be 02 middot Da where the upper limiting point is formed either by the loweredge of the flange or by the lower edge of brackets
57415 Revolving circle diameter of the slewing bearingsThe diameter of the revolving circle shall correspond to the mean diameter of the upper and lower connectioncylinder if possible in order to avoid additional measures such as eg welding of bracketsWhere brackets shall be attached they shall not be spaced further than two bore distances
57416 Requirements for bolts and boresIn general the span length of bolts shall be at least 5 middot dsAt least 6 thread turns shall remain freeThe connecting bolts of slewing bearings of cranes of the groups B2 B3 and C shall have rolled threadsThe size of bolt bores shall be indicated by the bearing manufacturer (in general according to [4912])
5742 Doubling platesDoubling plates for the transmission of tension forces and bending moments are not permissible
5743 Cruciform jointsRegarding cruciform joints for the transmission of forces perpendicular to the roll direction the requirementsgiven in [48124] apply
5744 Joints of runwaysRunways shall be welded continuously and the welds shall be executed such that no vertical dynamic forcescan be induced when travelling
575 Securing of the hook in the condition crane-out-of-serviceThe swinging of cargo hooks in the condition crane-out-of-service shall be prevented by design unless theyare tied-down The tie-down force may exceed 10 of the safe working load SWL only in cases where thiswas a basis for the dimensioning
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DNV GL AS
SECTION 6 SPECIAL LIFTING APPLIANCES AND MEANS OFTRANSPORT
61 General
611 This section deals with the requirements for the design and dimensioning as well as for the manufacture andoperation of special lifting appliances and means of transport
612 With respect to requirements for the materials to be used as well as for manufacture and welding theprovisions in Sec3 and Sec11 apply
613 Calculation and dimensioning shall be based on Sec4 and Sec8 as well as further sections as requiredDeviating requirements given in this section shall be observed
614 For machinery components and the electrical fittings on special lifting appliances and means of transport therequirements given in Sec9 and Sec10 shall be complied with if applicable
615 Interchangeable components shall be selected using recognized standards The dimensioning of non-standardinterchangeable components can be carried out in accordance with Sec7
62 Rope and chain hoists
621 General
6211 The requirements that follow apply to rope and chain hoists regardless of drive mode which are notused for handling cargo They only apply to manually operated devices however where relevant
6212 Handling of goods for ship operation is not regarded as cargo handling
622 Manufacture6221 MaterialsIn addition to the steels and materials generally used for machinery components special steels aluminiumplastics and other materials can be used if they are appropriate for the intended use
6222 DimensioningThe requirements given in [613] also apply to foundations or runway girders of rope and chain hoistsproduced in series
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DNV GL AS
623 Equipment and safety regulationsFor all types of drive the requirements given in Sec12 shall also be observed if applicable In addition thefollowing applies
6231 Overload protection
62311 Series productionFor hydraulic pneumatic and electrical hoist drives effective overload protection devices shall be providedIn the case of hydraulic hoist drives pressure relief valves are permissible up to a safe working load of 1000kgAs regards response limits and response tolerances of overload protection devices the settings orparameters given by the manufacturer apply
62312 Individual productionFor rope and chain hoists manufactured by individual or special production the requirements given in[12411] apply
6232 Hook travel limits
62321 General requirementsRope and chain hoists shall have limit switches for the upper and lower hook positionIn the case of power-operated rope and chain hoists the limit switches shall act mechanically andorelectrically on the hoist drives
62322 Series productionFor hydraulic pneumatic and electrical hoist drives effective limit switches for the hook travel shall beprovided
62323 Individual productionFor rope and chain hoists manufactured by individual or special production limit switches for the upper andlower hook position shall be provided which function electrically
6233 Runway limitAs regards runway limit the requirements given in [5342] and [1242] apply if applicable
6234 Slack rope limitIn special cases slack rope monitoring and limitation may be required eg at high hoist speeds withmultiple coils or if required by the mode of operation
6235 Eye plates for load testsIt is recommended suitable eye plates be fitted to the shiprsquos hull for load tests on hoisting ropes and hoistingchains located below deck For this kind of load test the application of the test load shall be conducted with aseparate manual hoist only but not with the power drive of the rope or chain hoist itself
624 Means of suspension6241 Hoisting ropes
62411 GeneralHoisting ropes and their end attachments are covered by the requirements given in Sec8Wire ropes made of stainless materials as well as synthetic fibre ropes may be allowed for special purposesif suitable and if the design of the hoist rope is verified accordingly
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DNV GL AS
62412 Safety against fractureSafety against fracture is defined by the coefficient of utilization γD1 or γF according to Table 8-2 and Table8-4 and this shall be applied to the maximum static hoisting rope force
When using rope hoists below deck γD1 may be le 40For the use of rope hoists above deck the following applies
a) In the case of rope hoists manufactured by series production γD1 may be le 40 unless nationalregulations dictate otherwise
b) For rope hoists manufactured by individual or special production the values in Table 8-2 and Table 8-4shall be used without limitation of γD1 or γF
6242 Hoisting chains
62421 GeneralHoisting chains shall comply with recognized standardsChain wheels of hoisting chains as well as their end links or fasteners for leading-in the tow chain shallconform to standards
62422 Safety against fractureThe breaking load of hoisting chains shall be at least the γK-fold of the chains maximum static towing forceThe following coefficients of utilization γK shall be applied
γK ge 50 (power-driven)
γK ge 40 (operated manually)
6243 Interchangeable components
62431 Interchangeable components such as eg cargo hooks shackles and rope sockets shall complywith recognized standards and shall be dimensioned for test loads according to Table 7-4
62432 The dimensions of the eye plates on normal strength and high strength shackles shall comply withthe Tables in Sec7
62433 Regarding the use of detachable rope end attachments (rope sockets or rope clamps) therequirements given in [8423] apply
625 Assessment of drawings and manufacturing survey6251 Series production
62511 Manufacturers of rope and chain hoists made by series production are permitted to produce undertheir own responsibility and to certify their products themselves if the manufacturing processes and productsare certified in a legally-binding and recognized manner eg by type approvalFor those in addition to drawings of foundations or runway girders including fastenings the followinginformation at a minimum shall be submitted if applicable
mdash designation of manufacturer and typemdash safe working load(s) and dead weight(s)mdash hoist speed and operating speed if applicablemdash type of drivemdash type(s) of electrical protection see [10617]mdash further information as required
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DNV GL AS
62512 For the Societys type approval DNVGL-CP-0338 applies
6252 Individual production
62521 Rope and chain hoists manufactured by individual or special production are subject to assessmentof drawings and manufacturing survey by the Society
62522 For the assessment of drawings the list of documents to be submitted in [21] shall be applied asand where relevant In addition the following drawings and information shall be submitted if applicable
mdash housingmdash rollers including fastening to housingmdash form-locking drive devices such as eg rack bars and pinionsmdash runway limitsmdash details of hoisting ropes and hoisting chains including end attachmentsmdash rope-sheaveschain wheelsmdash foundations or runway girders including fasteningsmdash stowage position including fastening devicesmdash further documents as required
62523 For manufacturing survey the requirements given in [132] apply
626 Tests and examinations on board
6261 For the initial test and examination the requirements given in [133] apply
6262 For the periodic testing and examinations the requirements given in [134] apply
627 Documentation6271 IdentificationFor the identification of rope and chain hoists the requirements given in [132421] [1325] and [1326]and [1335] apply
6272 Certificates
62721 Certificates for productionSeries productionRope and chain hoists manufactured by series production shall be delivered with a test report as well as withtest reports for all means of suspension such as ropes chains and interchangeable componentsIndividual productionFor rope and chain hoists manufactured by individual or special production the Societys product certificatebased on an examination before delivery is requiredThe Societys product certificates shall be submitted for all means of suspension such as ropes chains andinterchangeable components
62722 Certificate for load testsCertificates to be issued after every load test due to national regulations are described in [137]For rope and chain hoists which shall not be subjected to ongoing control by the Society the Society mayrecognize deviating forms or certificates not issued by the Societys surveyor
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DNV GL AS
6273 Register book
62731 All certificates for means of suspension and load tests investigation reports as well as informationfor operation (manuals maintenance protocols etc) where applicable shall be compiled in a register bookand stored For details see [137]
63 Ramps and car decks
631 General
6311 Testing investigation and certification of ramps and car decks fixed to the ship is part of theclassification of the ship
6312 As regards naval-architectural concerns such as ships strength water-tightness impact stress bythe sea etc the requirements given in DNVGL-RU-SHIP Pt3 apply
6313 The following requirements relate to mobile shipboard ramps and car decks operated under load
632 Production6321 MaterialsIn addition to ship structural steels other steels and aluminium may also be used for load-bearingconstructions if they are suitable for the intended purposeFor machinery components materials shall be selected in accordance with the DNV GL rules
6322 Dimensioning
63221 The dimensioning of steel or aluminium ramp or car deck construction shall comply with therequirements given in [6312]
63222 For the dimensioning of structural or machinery components of rope or chain drives a hoist loadcoefficient of ψ = 115 shall be applied to moved masses consisting of safe working load (SWL) and deadweight
Guidance noteConcerning safe working load for conveyance of persons see [42511]
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
633 Equipment and safety regulations6331 Scratch boards railings and barriers
63311 Ramps and car decks shall be fitted with scratch boards railings and barriers as necessary For thedimensioning of railings [4992] appliesScratch boards for motor vehicles shall be designed to meet the line loads according to Table 6-1
Table 6-1 Loading scratch boards
Vehicle type Line load Height of load application
Passenger vehicles 2 kNm 03 m
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DNV GL AS
Vehicle type Line load Height of load application
Trucks 5 kNm 05 m
63312 The construction of scratch boards railings and barriers including their associated safety devicessuch as eg colour markings photoelectric barriers and warning signals are subject to drawing assessmentby the Society
6332 Anti-slip safeguardsRamps shall be fitted with welded-on or bolted-on anti-slip safeguardsIn special cases anti-slip paint may be permitted in lieu
6333 Ramp inclinationRamp inclination shall not in general exceed the ratio 110
6334 Permissible deflection
63341 The permissible deflection of ramps and car decks under safe working load in the stowed positionshall not exceed
f =
where
f = deflection (depth gauge)bs = spacing of supports (span)
63342 In the stowed position the deflection may not endanger either the water-tightness of the ship orany cargo (eg vehicles) underneath
6335 Stowage positions
63351 In the stowage positions provided ramps and car decks shall not be hung on ropes or chains butshall have mechanical supports and locks
63352 Supports and locks shall be dimensioned according to the requirements given in [6312] andsafeguard the water-tightness of the ship where ramps are part of the shell
634 Means of suspension6341 Hoisting rope and suspension rope
63411 GeneralFor hoisting ropes and suspension ropes and their end attachments the requirements given in Sec8 applyWire ropes of stainless materials as well as synthetic fibre ropes may be permitted for special purposes inindividual cases if they are suitable and if the design of the rope drive is adjusted accordinglySynthetic fibre ropes for the transport of persons are only permitted under special conditions
63412 Safety against fractureSafety against fracture is defined by the coefficient of utilization γD1 or γD2 according to Table 8-2 and shallbe applied to the maximum static towing rope force
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DNV GL AS
For hoisting ropes the following safety factors shall be applied depending on the mode of operation inaccordance with Table 8-2
mdash operation without working load = γD1 ge 36mdash operation with working load = γD1mdash operation involving persons = γD1 middot 20
Ramps which are not supported at their free end when used by vehicles may apart from chains also befixed by hoisting ropes or special suspension wires In this case the following safety factors shall be used
mdash hoisting ropes or guided suspension ropes = γD1 middot 20mdash suspension ropes not guided = γD2 middot 20
6342 Hoisting chains and suspension chains
63421 GeneralHoisting chains and suspension chains shall comply with recognized standardsChain wheels as well as their end links or fasteners for leading in the tow chain shall be selected inconformance with standards
63422 Safety against fractureThe breaking load of hoisting chains and suspension chains shall be at least the γK-fold of the chainsmaximum static towing force Depending on the mode of operation the following coefficients of utilization γKshall be applied
mdash operation without working load = γK ge 28mdash operation with working load = γKge 40mdash operation involving persons = γK ge 80
6343 Interchangeable components
63431 The requirements given in [62431] and [62432] shall be observed
63432 Detachable rope end attachments (rope sockets or rope clamps) are not permitted for rope drivesof ramps and car decks
6344 Hydraulic cylindersHydraulic cylinders shall be dimensioned in accordance with [492]
635 Assessment of drawings and manufacturing surveyRamps and car decks are subject to design assessment of drawings and manufacturing survey
6351 Assessment of drawingsFor the assessment of drawings the list of documents to be submitted in [21] shall be applied as and whererelevant In addition the following drawings and information shall be submitted if applicable
mdash overview drawing with layout and numbering of ramps and car decks where applicablemdash complete rope drives and chain drivesmdash guide blocks including fasteningsmdash scratch boards barriers and railingsmdash rigging plansmdash additional documents as required
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DNV GL AS
6352 Manufacturing surveyFor the manufacturing survey the requirements given in [132] apply
636 Tests and investigations on board6361 Initial test and investigation
63611 For the initial test and investigation the requirements given in [133] apply
63612 The load tests with test loads according to Table 13-2 shall be performed statically in the stowagepositions and dynamically for the movable installations
6362 Periodic testing and investigations
63621 As part of the shiprsquos classification ramps and car decks are subject to annual class surveys and 5-year class renewal surveys Instead provision is made for annual performance tests but not for 5-year loadtests
63622 Where required by national regulations ramps and car decks shall be treated like cargo gear Therequirements given in [134] apply in this case During the 5-years load tests [63612] shall be observed
637 Documentation6371 IdentificationFor the identification of ramps and car decks the requirements given in [1325] [1326] and [1335]apply
6372 Certificates
63721 Manufacturing certificatesThe manufacturer of ramps and car decks shall supply the Societys product certificates for all meansof suspension such as ropes chains interchangeable components and hydraulic cylinders as well as forwinchesAs confirmation of investigation before delivery the Societys manufacturing survey report is required forevery ramp and every car deck or for every series of such ship components
63722 Certificates for load testsAs a confirmation of the load tests the Societys product certificate is required for every ramp and every cardeck or for every series of such ship componentsWhere due to national regulations ramps and car decks shall be treated like cargo gear the requirementsgiven in [1336] and [1346] apply
6373 Register book
63731 All certificates for means of suspension and load tests investigation reports as well as informationabout operation (manuals maintenance protocols etc) where applicable shall be compiled in a registerbook and stored For details see [137]
63732 Confirmation of the class surveys according to [63621] is effected within the scope of shipclassification Relevant excerpts of the survey report for the ship may be added to the documentation file
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DNV GL AS
64 Lifting appliances for research work
641 General
6411 Lifting appliances for research work are employed for the extraction of seabed samples and watersamples for towing and for general handling of research equipment In the process ropes cables or acombination of both are utilized
6412 Exceptional loads may result from large rope or cable lengths from ship movements or fromextraction devices getting caught as well as being pulled out of the sediment
6413 Lifting appliances for research work are eg
mdash stern gantry cranemdash slewing gallowsmdash lateral outriggermdash hatch beammdash lifting appliances with special functionsmdash A-frames
642 Treatment of lifting appliances for research workLifting appliances for research work is treated like lifting appliances not intended for the handling of cargoThe following specific features however shall be considered
643 Special features6431 Dimensioning
64311 Lifting appliances for research work shall be dimensioned for the breaking loads of ropes or cablesFor the dimensioning the following load combination shall be assumed following Table 5-4 load combinationIII
mdash dead loads γpi = 110mdash ropecable breaking load γpi = 110mdash diagonal pull γpi = 110mdash partial safety factor for resistance values γm = 110
In general for this purpose the diagonal pull shall be assumed for the most unfavourable direction as follows
mdash lifting 15degmdash towing longitudinally to the ship 30degmdash towing transversely to the ship 45deg
64312 Where lifting appliances for research work are also intended for handling goods for ship operationit shall also be dimensioned accordingly
64313 Interchangeable components shall be selected in such a way that the breaking load of ropes orcables corresponds to the test loads of the interchangeable components stated in Table 7-4
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DNV GL AS
6432 Marking
64321 When marking lifting appliances for research work the requirements given in [1325] applyInstead of SWL and a quantity in kg or t the minimum breaking load of the rope as MBLRope and a quantity[kN] shall be used
64322 Where several ropes or cables are attached to one lifting appliance marking is required on everysingle rope or cable
64323 Where lifting appliances for research work are also intended for handling goods for ship operationit shall also be marked with SWLWhen determining the quantity to be indicated the breaking load of the rope shall be divided by thecoefficient of utilization γD1 in accordance with Table 8-2 and then to be converted into kg or t
6433 Operating manual
64331 An individual operating instruction shall be prepared for every lifting appliance for research work inwhich the special features of operation and control are described
64332 Operating manuals are subject to design assessment and shall remain permanently on board aspart of the lifting appliance documentation
65 Industrial cargo-handling vehicles
651 General
6511 The following requirements apply to industrial cargo-handling vehicles (eg fork lift trucks or wheelloader) in series production which are certified in a legally-binding or recognized manner unless otherwiseprovided by national regulations
6512 Prerequisites for use on board are proofs of safety against overturning see [4522] and at aminimum the existence of test reports
6513 The requirements given in [653] and [654] apply only to industrial cargo-handling vehicles whichremain in permanent employment on board
652 Safety regulations
6521 The employment of industrial cargo-handling vehicles on board presupposes that decks and hatchcovers are adequately dimensioned to be run over
6522 Where industrial cargo-handling vehicles remain permanently on board fastening arrangements(eg eye plates) for securing for use at sea shall be fitted both to the vehicle and to the hull
6523 The use of industrial cargo-handling vehicles powered by IC engines or by non-explosion-proofelectric motors is not permitted in hazardous locations and areas
6524 Industrial cargo-handling vehicles run on fuel may only be used in cargo spaces if there is adequateventilation Otherwise only battery-powered vehicles shall be employed
6525 The use of fuels with a flash point below 60degC is not permitted
6526 In general fork-lift trucks to be used on board shall have a tiltable lifting frame
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DNV GL AS
653 Control measures6531 Initial controlBefore start of operation the following measures are required at a minimum
mdash check the information documents included with deliverymdash function check with safe working loadmdash test run over the operational areas with safe working load as proof the deck or hatch covers are
sufficiently strong
6532 Regular controlsIndustrial cargo-handling vehicles are subject to inspection and regular control by the ships management atintervals not exceeding six (6) monthsThese controls shall be confirmed in a suitable manner and added to the documentation
654 Documentation6541 CertificationFor the control as per [6531] the Societys surveyor issues a Societys product certificate
6542 IdentificationFor stamping correlating to the product certificate the requirements given in [1335] apply
6543 Register book
65431 All certificates for load tests investigation reports as well as information about operation (manualsmaintenance protocols etc) where applicable shall be compiled in a register book and stored For detailssee [137]
65432 In addition to the certificate as per [6541] the manufacturerrsquos documentation shall be includedin the register book This also applies to all confirmations of control measures by the ships management see[6532]
66 Means of conveying persons or personnel
661 Shipborne working baskets
6611 Newly-manufactured working baskets shall meet the requirements given in EN 14502-1
6612 Shipborne working baskets shall be treated in all respects similarly to lifting appliances not handlingcargo Their dimensioning and testing shall however be subject to the static test loads according to Table 7-2
662 Requirements for lifting appliances for conveying persons orpersonnelLifting appliances for conveying persons or personnel shall comply with the requirements given in [4251]and 4252 with respect to dimensioning operation and control
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DNV GL AS
663 Landing booms6631 General
66311 The provision and the arrangement of landing booms (swinging booms for conveying persons) arerequired by the St Lawrence seaway authority
66312 Landing booms shall only be used for conveying one single person at a time
66313 Landing booms shall be treated as lifting appliances not handling cargo except where otherwisedetermined in what follows
6632 Dimensioning
66321 Landing booms together with the associated posts shall be designed for a static test load LPstat of300 kg (Table 7-1 load condition III2 without wind and hoist load coefficient)
66322 Ropes and interchangeable components shall be designed in addition to the dead loads for a staticboom load of 150 kg at a minimum
66323 The slenderness ratio of a landing boom may not exceed a value of 200
The following equations apply
IL = moment of inertia of boomAL = cross-section area of boom
6633 Construction and layout
66331 The load radius of landing booms shall be about 9 m
66332 If landing booms are equipped with several span ropes (eg a second span rope about halfwayalong the boom) the length of these intermediate span ropes shall be adjustableThe length adjustment of the intermediate span rope shall be effected in such a way that no unfavourablestress may arise under load (cantilever effect)
66333 Landing booms shall be operated exclusively by hand The lowering system shall allow gentle set-down
66334 Landing booms shall be located in the forward portion of the ship roughly at the point where thebow has widened to the full beam and shall swing forward from aft
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DNV GL AS
6634 Assessment of drawings and manufacturing survey
66341 Landing booms together with the associated posts shall be constructed according to the drawingsapproved by the Society
66342 Because all components are normally easily accessible for subsequent controls manufacturingsurvey is not required in general Test reports shall be included in the delivery
6635 Tests and investigations on board
66351 For the tests and investigations on board the requirements given in [133] and [134] apply withthe following deviations
66352 Landing booms shall be tested before start of operation and periodically every 5 years eitherstatically by swinging a test load of 300 kg or by swinging lowering and braking a test load of 200 kg
6636 DocumentationWith respect to identification certification and documentation the requirements for lifting appliances nothandling cargo apply see Sec13
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DNV GL AS
SECTION 7 LOAD-HANDLING DEVICES AND INTERCHANGEABLECOMPONENTS
71 General
711 This section covers the requirements for design and calculation as well as production and employment ofload-handling devices and interchangeable components
712 With respect to requirements for the materials to be used as well as for production and welding theprovisions in Sec3 and Sec11 apply
713 For machinery components and electrical equipment of load-handling devices the requirements given inSec9 and Sec10 shall be complied with where relevant
72 Load-handling devices
721 GeneralThe following requirements apply to load-handling devices according to [11532] as well as to suspensionswhich are integral part of a load-handling device see [11559]
Guidance noteSuspensions which are not integral part of a load-handling device are not subject to this standard
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
722 Design principles7221 GeneralRelevant requirements given in Sec4 shall be complied with
72211 Suspension ropes rope slings and their rope attachments shall comply with the requirements givenin Sec8If a product certificate (CG4LA4) for the rope is submitted and proof is provided that the rope connectionshave been produced by manufacturers with the Societys approval then further requirements forinterchangeable components may be dispensed withRegarding the rope deflection the reduction of the minimum breaking load which depends on the ratio Ddshall be taken into account
72212 Suspension chains and their end attachments shall comply with recognized standards
72213 Regarding the suspension height of loose gear it shall be pointed out that the opening angle ofsuspension ropes or chains shall not exceed 120deg and of ramshorn hooks shall not exceed 90deg
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DNV GL AS
72214 In order to warrant balance (safety against turn-over) of the total system or parts of it consistingof loose gear andor load it is assumed in the requirements given in this section that both the loose gear andthe loads have a positive stability height see illustration in Figure 7-1
Figure 7-1 Balance conditions
72215 Arrangement of suspension gearA predefined arrangement of suspension gear may be considered as load-handling device Examples areshown in Figure 7-2Regarding 4-leg arrangements of suspension gear without load equalisation it shall be taken intoconsideration that these systems are statically indeterminate The individual legs of the arrangement arestressed depending on the rigidity of the load or the load-handling device to be handled Where the load orthe load-handling device has high rigidity the load distribution on each leg of the arrangement of suspensiongear shall be verified by static calculation Without verification of the actual load distribution in the completesystem (arrangement of suspension gear and load or load-handling device) only 2 legs shall be assumed asload-bearing
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DNV GL AS
G1 = 3-leg arrangement of suspension gear(statically determinate load connectingpoints are not in one vertical plane)
G2 = 4-leg arrangement of suspension gearsymmetrical (statically indeterminate withrigid load) The total load is carried eitherby leg S1 and S3 or by S2 and S4 Thecentre of gravity of the load (SP) is locatedin both of the planes spanned by S1S3and S2S4
G3 = 4-leg arrangement of suspension gearasymmetrical (statically indeterminate withrigid load) see also notes under G2
G4 = 4-leg arrangement of suspension gear withload compensation on one side (staticallydeterminate with sufficient geometry ofload compensation)
G5 = 4-leg arrangement of suspension gear withframe spreader (statically indeterminatesee also notes under G2)
G6 = 4-leg arrangement of suspension gear withtwo spreaders (statically determinate)
Figure 7-2 Suspending systems for typical arrangements of suspension gear
7222 Traverses
72221 Traverses may only be loaded symmetrically to the centre of gravity of the load unless they aredimensioned for asymmetric loading and marked accordinglyIf there are more than two (2) attachment points between the traverse and the load the strength analysisshall be conducted with consideration of rigidity of the load (statically indeterminate system)Alternatively devices may be fitted which indicate the load
72222 Where longitudinal lifting beams have under-slung transverse lifting beams using tension elementsthis system shall be designed for safe operation in accordance with the static degrees of freedom Sufficientstrength shall be proven by a strength analysis
72223 Telescopic traverse parts shall be lockable in their working positions
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DNV GL AS
7223 Frame traversesspreader
72231 In the case of adjustable container spreaders the movable beams shall either lock into the desiredworking positions or constructional measures shall be taken to ensure that the beams are accurately placedand held in these positions
72232 Container spreaders shall be equipped with indicators showing in a suitable manner whether thetwist locks are locked or unlocked
72233 Locking pins which automatically unlock when unloaded are not acceptable
7224 Grabs and lifting magnets
72241 The structural design and operating mode of grabs and lifting magnets shall be suited to theintended type of cargo
72242 The mechanical strength and electrical equipment of grabs and lifting magnets shall company withthe requirements given in this standard
72243 Closing ropes of grabs shall be protected in a suitable way against excessive wear
72244 Lifting magnets shall comply with the requirements given in EN 13155
723 Calculation principles7231 General
72311 Calculations and dimensioning of load-handling devices are subject to the requirements given inSec4 and Sec5
72312 Regarding the loads to be considered and the proofs to be provided the following requirementsshall be observed
7232 Design loads
72321 GeneralThe loads acting on load-handling devices are subdivided as follows
mdash regular loadsmdash irregular loadsmdash special loads
If necessary loads not addressed in the following shall be considered additionally in a suitable way Thegrading of such loads and the consideration of them in the corresponding load combinations shall be agreedwith the Society
72322 Regular loadsDead load LE
Dead loads shall be determined in accordance with [4242]Working load (WL)The working load is defined in [11566] When dimensioning the load-handling device this is assumed to bethe safe working load (SWL)
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DNV GL AS
Dynamic forces caused by drivesRegarding the dynamic forces caused by drives the provisions of [5324] apply including the followingadditions
mdash For dimensioning in general only those vertical dynamic forces shall be considered which are covered bythe hoist load coefficient ψ Therefore the working loads shall be multiplied by the maximum hoist loadcoefficient ψ for this application of the allocated lifting appliances
mdash SWL shall be always relevant for dimensioning This shall be ensured by the conditions in [5432]mdash If load-handling devices or interchangeable components cannot be allocated to lifting appliances the
following hoist load coefficient shall be used
SWL le 10 t le 160 t le 500 t le 1000 t gt 1000 t
ψ 16 14 13 12 115
This is only permissible if the lifting appliance is used in harbour operations When used under seawayconditions the increased requirements given in the lifting appliance used thereby shall be considered
72323 Irregular loadsWind loadsWind loads shall be assumed according to [4245]Snow and ice loadsIf snow loads shall be considered these shall be provided by the manufacturerIf ice loads shall be considered these shall be determined according to [4246]
72324 Special loadsTest loadsLoad-handling devices shall be dimensioned for a static test load LPstat according to Table 7-2 or if moreunfavourable for the dynamic test load of the lifting appliance according to [5341] including the reducedhoist load coefficient ψP
max (LPstat LPdynmiddotψP)Lateral impactFor frame-type traversesspreader a lateral impact of 110 of the maximum vertical load in the frame levelshall be assumed
7233 Load combinations and partial safety factors
72331 GeneralThe load combinations deemed to be essential for load-handling devices in operation are compiled in Table7-1For the condition cranes out of operation the load combinations and partial safety factors according to Table5-5 shall be assumed regarding strength analysisAccording to circumstances further load combinations may ariseFrom the load combinations in Table 7-1 and where required further load combinations only thosecombinations which are prevailing or necessary for the structural element being considered shall be proved
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DNV GL AS
Table 7-1 Load combinations for load-handling devices under operating conditions
Load combinations
I II IIILoadcate-gories
Loads i Reference
γpi I1 γpi II1 γpi III1 III2 III3
Dead loads LE 1 [723221] 122 1 10 116 1 10 110 1 10 10 10Regularloads Working load WL 2 [723222] 134 Ψ 122 Ψ 110 - - Ψ
Wind loads underoperating conditions 3 [723231] 122 10 110 - 02 -Irregular
loadsSnow and ice loads 4 [723232] 122 10 - - - -
Hoisting the hoistload at vhmax
5 Table 5-2 110 ψmax - -
Test load 6 [723241] 110 - ψp -Specialloads
Lateral impact 7 [723242] 110 - - 10
Partial safety factor γm for resistance values 110 110 110
Global safety factor γs 148 134 122
1) Where load combinations have a favourable effect γpi = 095 may be assumed If the components masses andcentre of gravity is determined by weighing 095 middot γpi may be assumed
72332 Comments on the load combinations for load-handling devices under operating conditions Table7-1The load combinations I1 II1 III1 and III2 correspond to those given in [552]Consideration of the deviation of the loads centre of gravityDue to an unexpected and not precisely determinable deviation in the centre of gravity stresses on the load-handling devices shall be considered assuming an inclined position deviating 6deg from the ideal location inrelation to both main axes This load condition shall be examined additionallyIII3 - Lateral impactThe load combination comprises the loads due to hoisting of the hoist load including a lateral impact
7234 Proofs
72341 GeneralThe load-handling devices shall be dimensioned taking into consideration the following pointsThe centre of gravity is located in the axis of symmetry of the suspensionRegarding frame-type traverses or spreaders the bending rigidity of the load shall also be evaluated withrespect to load transfer and possibly to be included in the static strength analysis Without proof of the staticstrength of the frame-type traverse or spreader as an overall system complete with the load only two loadattachment points may be assumed to be load-bearing
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DNV GL AS
72342 Strength analysesRegarding the strength analyses in general the statements in [44] and [48] apply The load combinationsshall be formed using the values for the partial safety factors according to Table 7-1Telescopic parts of traverses or spreadersIn the case of the telescopic parts of traverses or spreaders careful attention shall be paid to the transverseforce in the overlapping area and to the force transferred at the outlet as well as at the inner end of themovable part
72343 Proof of stability (buckling lateral torsional buckling warping)For proof of stability the statements in [44] apply in general The load combinations shall be formed usingthe partial safety factors according to Table 7-1Special boundary conditions for traversesRegarding the proof of stability of traverses special boundary conditions shall be assumed for thedetermination of the critical buckling load It shall be considered that there is no fork bearing ie the proofsof stability used in the general steel engineering to determine the critical buckling load are not applicableFor the determination of the minimum potential energy due to outer and inner forces only the restoringmoments between the traverses suspension and the loads suspension can be applied which are activatedby the eigenmode of the traverse In determining the ideal lateral torsional buckling moment (Mki) theseboundary conditions shall be appliedSystem assumptions for the determination of MKi for traverses (ideal lateral torsional buckling moment)See Figure 7-3 to Figure 7-5Boundary conditions for the proof of traverses
mdash determination of the section forces and deformations in accordance with 2nd order theorymdash application of the geometrical replacement imperfections using ΔS = L150 (maximum ΔS of the
eigenmode) see Figure 7-3mdash limitation of the torsional angle Φ le 03 rad see Figure 7-4 and Figure 7-5
72344 Fatigue strength analyses for load-handling devicesFor fatigue strength analyses in general the statements in [56] apply Generally they shall be conducted forthe load combination I of Table 7-1 using a partial safety factor of γpi = 10For load-handling devices with stress cycles le 20000 a fatigue strength analysis may be dispensed with
72345 Proofs of suitability for useFor proofs of suitability for use in general the statements in [47] apply Generally they shall be conductedfor the load combination I of Table 7-1 using a partial safety factor of γpi = 10TraverseThe maximum deformation shall be limited to le L500 related to the traversesrsquo lengthFrame-type traversespreaderThe maximum bending deformation due to the dead weight shall be limited to le L1000 related to thespreadersrsquo length the maximum bending deformation shall be limited to le L500 related to the spreaderslengthContainer spreaderThe maximum bending deformation (bending stiffness) of the spreader shall be limited such that the liftlocks cannot unlock under operational conditions
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DNV GL AS
Figure 7-3 Eigenmode of the traverse
724 Assessment of drawings and manufacturing survey7241 Assessment of drawings
72411 The general requirements given in Sec13 shall be observed
72412 Regarding the documents to be submitted for design assessment [21] shall be applied as andwhere relevant In addition the following documents shall be submitted
mdash overview drawings showing all variations of functions loads and load fasteningsmdash workshop drawings of all steel componentsmdash strength analyses for all load-bearing components (static dynamic fatigue strength as required)mdash stowage and fastening devices for shipborne load-handling devicesmdash additional documents as required
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DNV GL AS
Figure 7-4 Eigenmode of the traverse
Figure 7-5 Eigenmode of the traverse
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DNV GL AS
7242 Manufacturing survey
72421 The general requirements given in Sec1 shall be observed
72422 The manufacturing survey and acceptance testing before delivery is required in principle
72423 For load-handling devices which are still accessible for comprehensive examination aftercompletion manufacturing survey may be dispensed with subject to the consent of the Societys surveyorAcceptance testing is required in every case where appropriate together with the first load test
72424 The requirements to be met by the manufacturer are set out in [112]
725 Tests and examinations7251 Tests
72511 Before being put into use and after every major modification or repair to load-bearing parts load-handling devices shall be subjected to a functional and load test in the presence of the Societys surveyor
72512 Regularly repeated load testing of load-handling devices is not prescribed internationally by ILO Itshall be noted however that various flag administrations do have regulations on this
72513 The static test loads given in Table 7-2 are applicable to load-handling devices according to thedefinition in [11532]
Table 7-2 Static test loads for load-handling devices
Safe working loads (SWL) of load-handling devices Static test loads 1 LPstat
up to 10 tabove 10 t up to 160 t
above 160 t
2 times SWL(104 times SWL) + 96 t
11 times SWL1if applicable to be multiplied with fd according to [7333]
7252 Examinations
72521 Before being put into use after each load test and after each modification or repair to load-bearingparts all load-handling devices shall be subjected to a thorough examination by the Societys surveyor andwhere necessary a functional test in his presence
72522 In addition to the regulations according to [72521] all load-handling devices shall besubjected to a visual examination by the Societys surveyor at least every 12 months as well as a thoroughexamination every five (5) years and where necessary a functional testFor due dates of examinations the provisions in [1342] are applicable
726 DocumentationFor marking see [74]
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DNV GL AS
7261 Certification
72611 After each load test using the prescribed test load according to Table 7-2 the Societys surveyorissues one of the two following certificates Functional tests are not specially certified
72612 For a ships load-handling device a product certificate Form CG3 will be issued For use on boardmore than one ship additional copies may be issued
72613 For load-handling devices which cannot be allocated to a particular ship a Societys productcertificate will be issuedFor use on board the Societys product certificate requires to be transcribed by the Societys surveyorinto Form CG3 in order to warrant international acceptance In addition the load-handling device shall bestamped with the new certificate number
7262 Register book
72621 As described in [137] the product certificates Form CG3 are added to the register book of liftingappliances carried on boardUpon request by the operator an individual register book for load-handling device can be issued for use onboard more than one ship
72622 For all examinations according to [7252] the Societys survey report will be compiled Inaddition the examinations are confirmed in the register book of lifting appliances
72623 The Societys product certificates will be handed out to the operator without a register book Theoperator shall add these certificates and survey reports according to [72624] to his own documentation
72624 The confirmation of examinations of load-handling devices for which a Societys product certificatehas been issued is effected by the survey report
73 Interchangeable components
731 General
7311 Although not stated in [11528] eye plates and bolt connections shall be treated asinterchangeable components
732 Design and construction
7321 Block frames shall be designed in such a way that ropes cannot get caught between the sheave andthe block cheeks
7322 Cargo hooks shackles swivels and rings shall be forged Exceptions to this rule require the consentof the Society
7323 Grades of cast steel shall be selected according to recognised standards The consent of the Societyis required in every instance for other grades of cast steel
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DNV GL AS
7324 Galvanization is permitted only with forged components of fully killed steels Galvanization of forgedinterchangeable components may take place only after the load testing of the componentsWhere delivery is carried out by a recognised manufacturer it shall be documented that a stress test hasbeen conducted at the manufacturer under application of the minimum test loads in accordance with DNV GLrules including crack test
7325 The galvanizing of cold-formed components is permitted only if the suitability of the material for thispurpose has been proved
733 Interchangeable components conforming to recognized standards7331 Determination of the safe working loadThe safe working load shall be determined without partial safety factors and hoist load coefficientsdepending on the location of use
mdash in the lifting appliance according to Sec5 load combination Imdash in the loose gear according to [7233] load combination I
Where applicable the safe working load determined as above shall be increased by additional multiplicationwith dynamic factor fd according to [7333]
7332 For interchangeable components conforming to standards a choice shall be made according to theindicated nominal sizes The nominal sizes correspond to the safe working load according to [7331]
7333 In all cases where the hoist load coefficient ψ is greater than the value of ψzul the permissible loadon which the choice of the nominal size is based shall be increased by the following dynamic factor fd
ψ = hoist load coefficient according to [52]ψzul = permissible hoist load coefficient according to Table 7-3
Table 7-3 Permissible hoist load coefficient ψzul
SWL ψzul
up to 60 t 16
above 60 t to 160 t
above 160 t 11
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DNV GL AS
734 Basic principles for proofs for interchangeable components notcorresponding to a recognized standard7341 General
73411 For the calculation and the dimensioning of interchangeable components the requirements given inSec4 and Sec5 apply
73412 The load for dimensioning is determined depending on the location of service taking intoconsideration partial safety factors and hoist load coefficients
mdash using load combinations for the lifting appliance according to [55]mdash using load combinations for the load-handling devices according to [7233]
Additionally the static test load LPstat according to Table 7-4 with a partial safety factor of γpi = 110 shall beobserved for the determination of the load for dimensioning
7342 Proofs
73421 GeneralBasis for the dimensioning is the applicable design load for dimensioning which shall be determined accordingto [73412]The calculation of non-standardized interchange-able components may be carried out using suitablecalculation methods according to the provisions in Sec4A method to determine the strength of non-standardized eye plates is given in [7343]Proof of bolt connections may be provided according to [482]
73422 Strength analyses and proofs of stabilityFor strength analyses generally the statements in [44] and [48] apply They shall be conducted using thedesign load for dimensioning
73423 Proofs of fatigue strengthFor the proofs of fatigue strength the statements in [46] apply In general they shall be conducted using theload combination I of Table 5-4 or Table 5-1 with the partial safety factor γpi = 10For interchangeable components with load cycles le 20000 the proof of fatigue strength may be dispensedwith
7343 Non-standardized eye plates
73431 The determination of the design stress for eye plates which correspond to Figure 7-6 and to theboundary conditions according to [73432] may be performed using the following method unless a moreprecise proof is provided
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Figure 7-6 Eye plate
R = outer radius of head [mm]r = bore radius [mm]c = cheek width [mm]e = change of head height [mm]t = plate thickness [mm]β = inclination angle of flanks [deg]ϑ = angle of force attack [deg]rB = bolt radius [mm]T = clearance between bolt and bore [mm]a = head height [mm]S(γpi middot Li) = design load for dimensioning [kN]
73432 Boundary conditionsFor the dimensioning the following boundary conditions shall be adhered to
i) Radii ratio ρ of the eye
ii) Clearance T boltbore
T = 2 (r ndash rB) le 02 middot r le 3 mmFor bolt diameters of 50 to 300 mm a clearance between bolt and bore of 3 to 6 mm can be permittedHowever in this case the design load shall be increased by 5
iii) For moving bolt connections a wear of ΔT = 2 mm shall be taken into consideration in the strengthanalysis
iv) Inclination angle of flanks 0deg le β le 45degv) Angle of load application 0deg le ϑ le β
73433 Determination of the stress for dimensioning and stress proofThe stress for dimensioning is calculated as follows
σd max = α middot σN
α = form factor as per [73435]σN = nominal stress as per [73434]
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It shall be proven that
σd max le Rd
with
73434 Nominal stress due to design loadThe nominal stress due to design load without friction component is calculated as follows
with
(see also Table 7-1)
SWL = safe working load on eye plate
c = R + e sin β - r
The nominal stress component due to friction (friction coefficient micro) between bolt and bore is calculated asfollows
Consequently the nominal stress due to the design load including friction component is calculated as follows
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73435 Determination of form factorIn general the form factor is calculated as follows
with
(base value)
(components due to inclination of flanks)
(components due to change of heat height)
(components due to angle of load application)
and (radii ratio)
(change of head height ratio)
73436 Connection to supporting structureThe connection to the supporting structure (see Figure 7-6 cross section ko-ck) shall be proven separately inaccordance with Sec4
735 Assessment of drawings and manufacturing survey7351 Assessment of drawings
73511 Assessment of drawings is not required for interchangeable components and eye plates whichconform to recognized standards
73512 Details or drawings shall be submitted for interchangeable components or eye plates which aremade of materials andor to designs which do not conform to a recognized standard
7352 Manufacturing surveyThe manufacturing survey is not required for interchangeable components and eye plates
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736 Tests and examinations7361 Tests
73611 Interchangeable componentsProduct certification of interchangeable components requires the following tests
a) Each interchangeable component in the unpainted and as far as possible ungalvanized condition shallbe subjected to a static load test performed on a calibrated and approved testing machine using the testloads given in Table 7-4
b) Destructive testing of product samples may be required as deemed necessary by the Societys surveyorGuidance noteFor example destructive testing of product samples may be required if interchangeable components are subject to heattreatmentThe requirement for destructive testing may be independent from the interchangeable component conforming to a recognizedstandard or not
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
After modifications or repairs to interchangeable components a static load test according to a) shall berepeated for the single interchangeable component disconnected from its designated shipboard liftingappliance A repeated dynamic load test according to [1333] is not requiredRegularly repeated load testing of individual parts of interchangeable components is not prescribedinternationally by ILO They are load tested together with the lifting appliance or load-handling device towhich they are fastened
73612 Eye platesEye plates which are integral parts of lifting appliances and load-handling devices are included in the loadtests of themEye plates for assembly and maintenance work as well as for transportation purposes require a strengthanalysis with respect to their welding joints and the supporting structures These analyses will be checkedwithin the scope of assessment of drawingsLoad tests with agreed static test loads may be conducted on request of the ships owner
Table 7-4 Static test loads for interchangeable components
Line Interchangeable components Permissible loads SWL 1 Static test loads LPstat 2
1 chains rings hooksshackles swivels etc
up to 250 t
over 250 t
2 times SWL
(122 times SWL) + 20 t
2 single-sheaved blockswith and without becket all 2 times SWL
3 multi-sheaved blocks
up to 250 t
over 250 t up to 1600 t
over 1600 t
2 times SWL
(0933 times SWL) + 27 t
11 times SWL
1) The permissible load SWL of single and multi-sheaved blocks is equal to the permissible load on the suspension2) If need be to be multiplied with fd according to [7333]
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7362 Examinations
73621 Interchangeable componentsThe manufacturer and dealer shall present all interchangeable components to the Societys surveyor in anunpainted and if possible ungalvanized condition for examination of the dimensions and workmanshiptogether with the certificates covering the materials usedAfter the static load test each component is thoroughly examined by the Societys surveyor and shall if thesurveyor considers it necessary be taken apart for closer scrutinyAfter start of operation every interchangeable component shall be subjected to an examination by theSocietys surveyor at least every 12 months as well as to a thorough examination every five (5) years Forhighly stressed components non-destructive tests may be carried outComponents shall if the surveyor considers it necessary be taken apart for closer scrutiny
73622 Eye platesEye plates which are integral parts of lifting appliances and load-handling devices are examined togetherwith themEye plates according to [73612] including their joints are examined before their first employment afterevery load test and at agreed intervalsExaminations of eye plates may be complemented by crack and ultrasonic tests upon agreement Theseexaminations are mandatory if the visual inspection during the examination gives reason to do so
737 Documentation7371 Interchangeable componentsFor marking see [74]
73711 CertificatesThe Societys surveyor issues a certificate for each interchangeable component which has successfullyundergone a load test and a thorough examinationThis certificate gives details of the manufacturer or supplier the date of the test special materials (extra highstrengthlow temperature) the size of the test load and the permissible loadThe Societys Form CG3 is used for shipboard lifting appliances gear or interchangeable components and theSocietys product certificate for all othersFor the transcription of the Societys product certificate into Form CG3 for use on board the requirementsgiven in [72613] apply as and where relevantFor closer definition of tested and examined components the following details are entered on the certificates
mdash shackles bolt diameter where the inside width is non-standard the following dimensions shall beindicated in the order shown diameter of the shackle in the middle of the bow bolt diameter and insidewidth
mdash cargo hooks and swivels nominal sizemdash blocks groove diameter of the sheave and the sheave pin diameter together with the type of head fitting
and an indication of whether or not a becket is fittedmdash double yoke pieces bolt diameter and length of the double yoke piece between the bolt centresmdash rope sockets nominal size and details of the material testmdash cable joints nominal sizemdash rigging screws nominal size or thread diameter and the type of bolt head (oval eye round eye or fork
eye)mdash chains diameter of the round steel bar external width of the chain link and length of the chain
Where interchangeable components are manufactured according to approved drawings the certificates alsoindicate the relevant drawing together with the date and the Societys reference number of the approval
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73712 Register bookIn accordance with the requirements given in [137] the product certificates Form CG3 are added to theregister book of lifting appliances on boardInterchangeable components which are integral parts of lifting appliances or load-handling devices areexamined together with themFor the devices survey reports are compiled and the examinations are confirmed in the register book of liftingappliancesFor interchangeable components which are certified by the Societys product certificate the requirementsgiven in [72623] and [72624] apply as and where relevant
7372 Eye plates
73721 Eye plates in accordance with [73612] are included in the documentation of the devices statedthere
73722 The tests and examinations of eye plates in accordance with [73612] are confirmed by surveyreports
74 Marking of load-handling devices and interchangeablecomponents
741 Manufacturers plateLoad-handling devices according to [11532] shall be fitted with a manufacturers plate which shall includeat least the following information if applicable
mdash manufacturers namemdash type of load-handling devicemdash serial numbermdash year of constructionmdash characteristics where applicable such as eg nominal pressure nominal voltage filling volume etcmdash safe working load(s)mdash dead loadmdash with lifting beams traverses and spreaders a symbol for the inclination angle of the allocated suspension
ropes or chains
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742 Stamping7421 General
74211 Stamping is regarded to be the proof of a test andor examination Load-handling devices andinterchangeable components shall therefore undergo (renewed) load testing if a certificate is required in thisregard
74212 The stamp height shall be at least 6 mm
7422 Load-handling devices
74221 Scope of stampingAll load-handling devices which has successfully undergone testing and thorough examination is stamped asfollows
mdash certificate number together with the code letters of the examining inspection officemdash stamp with the month and year of testingmdash safe working load in tonnes or kg preceded by the letters SWLmdash dead load in t or kg preceded by the letters WT
74222 Stamp locationThe stamp shall be applied on one side in a prominent position if possible in the centre but not concealedby the marking
74223 Multiple stampingLoad-handling devices subjected to manufacturing survey are double-stamped (see Table 7-5)After periodic load tests and re-issuing of product certificates stamping is not repeated
7423 Interchangeable components
74231 Scope of stampingEach interchangeable component which has successfully undergone testing and thorough examination isstamped as follows
mdash certificate number together with the code letters of the examining inspection officemdash stamp with the month and year of testingmdash permissible load in tonnes or kg preceded by the letters SWLmdash permissible rope hoist in tonnes or kg with blocks eg
mdash single-sheaved block without becket
SWLrope
6 t3 t
mdash single-sheaved block with becket
SWLrope
15 t5 t
mdash multiple-sheaved blocks with 4 sheaves
SWLrope
64 t8 t
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Table 7-5 Examples of stamping and marking
Documentation Load-handling devices Interchangeablecomponents
Certificate FormThe Societys
product certificateAcceptance testing
L 8924 H03 15
StampingCertificate Form
CG3 or the Societysproduct certificate
Load test
L 2429 H04 15
SWL 30 t
WT 5 t
L 6743 H02 15
SWL 15 t
rope 5 t
(single-sheavedblock with becket)
Marking Rigging plansSWL 30 tWT 5 t
---
AbbreviationsSafe working load SWL
Weight WTPermissible load SWL
With interchangeable components made of special materials the stamp is extended with the followingletters if applicable
mdash H for extra high strength materialmdash T for low-temperature materials
Where interchangeable components are composed of several single parts which may be disassembled suchas eg shackle hook and shackle round nut each part will get this special stamp
74232 Stamp locationThe stamp shall be applied to the following locations for the parts given below
mdash shacklesto one of the limbs close to the eye
mdash cargo hooksto the side of the hook close to the suspension
mdash swivelsto the traverse the oval eye only gets the anchor stamp
mdash blocksto the side bar if any otherwise to the side plate close to the point of suspension of the block
mdash double yoke piecesto the middle of one side
mdash rope socketsto the conical section opposite the existing stamp for material testing
mdash cable jointsto the middle of one side
mdash rigging screwson the body to every eye head fitting or double lug head fitting plus the Societys stamp
mdash suspension ropes and slingsto a permanently fastened small metal plate
mdash chainsto the last link at each end
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74233 Special featuresWith a permissible load up to 15 t the figure on the stamp shall be rounded to one decimal place Withvalues of 15 t and over the figure shall be rounded to a whole numberFor the galvanization of forged interchangeable components the requirements given in [7324] apply Thestamp shall still be recognizable after galvanization or where required it shall be re-stampedThe stamp height shall be at least 6 mm or 4 mm for small partsOn small parts to which it is difficult or impossible to apply the whole stamp the month and year of testingmay be omitted followed if necessary by the certificate number and the permissible load where requiredThe following is applicable for stamping of small parts
mdash components with a SWL of 16 t and overThese are stamped in full as described in [74231]
mdash components with a SWL between 025 t and 10 tThese only receive the Societys stamp and where required also the permissible load
mdash components with a SWL of less than 025 tThese only receive the Societys stamp and where required the stamp shall be waived
743 Marking of load-handling devices
7431 Load-handling devices shall be permanently marked in a prominent position on both sides in themanner described in [7432] and [7433]The inscription shall comprise characters at least 80 mm in height the permanence of which shall be assuredby punching by applying weld seams or small metal plates adequately fastened The fatigue strength of themarked components shall not be unduly impaired by these measuresGlued-on lettering foils are not permitted
7432 Lifting beams traverses and spreaders shall be marked as follows
mdash safe working load SWL in t or kgmdash dead load WT in t or kg (mandatory if over 100 kg)mdash special types of fastening or loading
7433 Grabs and lifting magnets shall be marked as follows
mdash safe working load SWL in t or kgmdash dead load WT in t or kgmdash capacity in m3 for grabs
75 Wear damage repair
751 Load-handling devices
7511 With respect to tolerable reduction in the plate thickness due to rusting or wear the requirementsgiven in [1362] apply
7512 With respect to a reduction in the safe working load of load-handling devices covered by [11532]as an alternative to removal from service in the event of damage inadmissible wear or other causes therequirements given in [1369] apply
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752 Interchangeable components
7521 Interchangeable components such as bolts chains rings etc as well as eye plates shall bereplaced if the parts are visibly deformed if the diameter is reduced by 10 at some points or if the area ofthe load-bearing cross-section is reduced by 20
7522 The use of welding to repair cracks in or worn portions of interchangeable components is generallynot permitted The same applies to bolts and other removable elements of load-handling devicesThe Society reserves the right to approve such repairs in special cases Then the following shall be observed
75221 After repair of forged interchangeable components evidence shall be provided that heat treatmenthas been carried out
75222 After repair of interchangeable components a load test in accordance with [73611] is required
75223 Renewal of axles bolts and rope-sheaves in general does not require rerunning of the load tests
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SECTION 8 ROPES AND ROPE ACCESSORIES
81 General
811 Scope
8111 The following requirements apply to wire ropes and synthetic fibre ropes used as running andstanding rigging for shipboard lifting appliances and load-handling devices
812 Certification requirements
8121 CG4 certificates will be issued by a DNV GL surveyor based on individual tests and examinations aslaid down in [851]
8122 LA4 certificates will be issued by wire rope manufacturerfitter based on DNVGL manufacture surveyarrangement (MSA)
82 Wire ropes
821 General requirements
8211 Wire ropes shall conform to recognized standards such as eg EN 12385
8212 For employment on deck wire ropes for running rigging shall be drawn galvanized and wire ropesfor standing rigging shall be fully galvanizedAfter being galvanized the ropes shall be impregnated and conserved with non-thermosetting and acid-freegrease in order to avoid penetration of water and subsequent corrosion
8213 Galvanized wire ropes with diameters of less than 8 mm are not permitted for shipboard liftingappliances and loose gear exposed to the weather
8214 Free rope ends shall be seized tapered or socketed to prevent fraying of the rope ends or to preventchanges in the lay lengths of the rope and strands
8215 Special rope designs Lang lay ropes ropes with a nominal tensile strength of more than 1960 Nmm2 and ropes of austenitic or stainless materials may on application be approved provided that they aresuitable for the proposed use
8216 Wire ropes of stainless materials shall be suitable for use in marine atmospheresTo avoid crevice corrosion the materials used for the wires shall have a sufficiently high chromium andmolybdenum contentSteels are regarded as resistant to crevice corrosion in a marine atmosphere if the sum W is 29 or overwhere
W = Cr [] + 33 middot Mo [] ge 29
8217 Ropes with a nominal diameter exceeding 5 mm shall at least consist of 100 single wires runningrigging shall at least have six (6) strands
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822 Definitions
8221 Running rigging refers to all ropes passing over rope sheaves or guide rolls or wound on winchesirrespective of whether or not the ropes are moved under load
8222 Standing rigging refers to all wire ropes which are not turned round or wound on to winches suchas shrouds stays pendants etc Standing rigging shall be fitted with thimbles or rope sockets
8223 Rope slings refer to ropes forming an integral part of lifting appliances or load-handling deviceswhich are used to attach loads
8224 The calculated breaking load Fr of a rope is the product of the theoretical metal cross-section and thenominal tensile strength of the wires
8225 The minimum breaking load Fmin of a rope is the product of the calculated breaking load Fr and theSpinning Factor ks
8226 The actual breaking load Fwi of a rope is the load determined by a tensile test to destruction of thecomplete rope
8227 The proven breaking load Fn of a rope is the product of the measured aggregate breaking load Feand the spinning factor ks
8228 The measured aggregate breaking load Fe of a rope is the sum of the individually determinedbreaking loads of all the wires in the rope ascertained by tensile tests
8229 The spinning factor ks is an empirical factor which takes account of the strength reduction due tostrandingThe spinning factors of established types of wire rope are given in relevant standards or manufacturersinformation
823 Dimensioning
8231 The breaking load FBr of wire ropes for lifting appliances and loose gear shall not be less than theproduct of the Rope Tension FS and one of the safety factors γDi shown in Table 8-2
FBr ge FS middot γDi
FBr = actual breaking load Fwi or proven breaking load Fn
8232 The Rope Tension FS is the maximum force calculated for load condition I1 disregarding the hoistload coefficient ψ but taking into consideration the losses due to friction and bending in the rope sheaves Inaddition the following shall be observed
82321 For the partial safety factors γpi = 10 may be applied
82322 The determination of rope tensions taking into consideration the sheave friction and bendingresistance of the ropes is based on a frictional coefficient of 5 per turn for friction bearings and 2 perturn for anti-friction bearingsWhere calculations shall be performed with smaller frictional coefficients special proof of these shall beprovided
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82323 Rope deflection angles due to static ship inclinations do not increase the hoisting rope forceEnforced rope deflection angles due to acceleration forces or eg the drift of a vessel result in an increase inthe hoisting rope force They can however within the scope of this standard be ignored when dimensioninghoisting ropes or rope slings
82324 When dimensioning luffing ropes and standing rigging the deflecting angles of hoisting ropes shallbe considered in principle if they effect an increase in rope forces
82325 For shipboard lifting appliances and load-handling devices where an increased hoist load coefficient(gt ψzulS) shall be applied the rope tension FS shall be multiplied by the dynamic factor fds For ψzulS andfdS see [82326] and Table 8-1 This applies in particular to lifting appliances which will be dimensionedonly for sea operation (see [5432]) or for lifting appliances in grab operation
82326 The factor for consideration of an increased dynamic to be used for calculation of the rope tensionshall be determined as follows
ψ = hoist load coefficient according to [54]ψzulS = permissible hoist load coefficient according to Table 8-1
Table 8-1 Permissible hoist load coefficient ψzulS
SWL ψzulS
up to 10 t 16
over 10 t up to 160 t
over 160 t 15
82327 Where the efficiency of rope end joints is below 80 the loss of breaking force shall becompensated up to 80
82328 Wire ropes for multi-rope grabs shall be dimensioned in addition to the dead weight of the grabfor the following loads
mdash closing rope double lever control SWLmdash closing rope single lever control 23 SWLmdash holding cable 23 SWL
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Table 8-2 Safety factors for wire ropes
Safety factors γD1 1
Safe working load (SWL) of lifting appliances and loose gear 2 Running rigging
up to 10 t 5
over 10 t up to 160 t
over 160 t 3
Safety factors γD2 1
Safe working load (SWL) of lifting appliances and loose gear 2 Standing rigging
up to 10 t 4
over 10 t up to 160 t
over 160 t 3
Safety factors γD3 1
Weight of load Rope slings 3
up to 10 t 6
over 10 t up to 160 t
over 160 t 36
1) If applicable to be multiplied with fdS (see [82325])2) For lifting platforms ramps and car decks the following loads shall be applied
mdash operation without working load moved dead loadsmdash operation with working load moved dead loads + safe working load (SWL)
3) Rope slings which are not turned round may be treated as wire ropes for standing rigging provided that both endsare fitted with thimbles or rope sockets
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8233 Reduction in breaking load of the ropeWhere wire ropes are wound around design elements with a small diameter (eg shackle bolts crane hooksload connecting elements etc) the permissible breaking load shall be reduced
D = diameter of the slung partd r = rope diameter
The breaking load of the wire rope shall be reduced for the following range of diameters
1 le Ddr le 9
(Ddr lt 1 is not permissible)
The reduced breaking load shall be determined according to the following formula
FBrredu = reduced breaking loadFBr = breaking load of the non-deformed rope (no rope bending)
Within spliced sections the rope shall not be slung with small radii
Alternative provisions for the dimensioning of wire ropes for ramps and car decks can be found in [6341]
824 Requirements for rope drives8241 Interaction between ropes and rope drums
82411 In determining the necessary length of wire ropes and the length of drum it shall be borne inmind that at least three (3) safety turns shall remain on the drum at all timesThe requirement for three (3) safety turns also applies to luffing ropes with respect to the stowing position ofthe crane boom
82412 It shall be ensured that ropes are wound up properly on the rope drums The length of rope drumsshall in general be designed such that no more than three (3) layers of rope may be wound on top of eachotherWhere the number of layers exceeds three (3) a special coiling device or other system or equipment shallbe provided
82413 Uncut rope drums may only be used with the consent of the Society
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82414 Grab cranes shall have a rope-spindling guide in principle if the hoist rope drum cannot be clearlyviewed by the operator at all times Rope-spindling guides are grooved drums and rope-spindling devices andsimilar devices
82415 Design requirements for rope drums are described in [952]
82416 Wire ropes which are wound on to drums in several layers shall have a steel core For heavy loadsropes with compressed strands are recommended
82417 The first rope layer shall be tension loaded
82418 The direction of rope runout shall be coordinated with the direction of rotation of the drums toavoid twisting of the ropesThe winding direction of ropes on rope drums shall be clearly recognizable at the drums and where requiredthe winding direction shall be indicated
8242 Rope-sheaves
82421 Design features shall prevent ropes from being jammed between rope-sheaves and side plates orleaving the rope grooveThe distance between the upper edge of rope-sheaves and eg side plates shall not exceed 13 with plasticrope-sheaves 14 of the rope diameter or 8 mm at most
82422 If rope sheaves made of metallic material are not manufactured according to a recognizedinternational standard (eg DIN 15063) case by case design approvals or type approvals are required andmaterial requirements according to Sec3 apply
82423 Where plastic rope-sheaves are used they shall be type-tested In the case of single layer spoolingon the rope drum at least the sheave which generates most of the alternating bends in the rope shall beproduced from steel Alternatively defined criteria for scrapping or usage periods may be approved
82424 The following requirements apply to the design of rope grooves
mdash depth of groove ge radic2 times nominal rope diametermdash diameter of groove 106 to 108 times nominal rope diametermdash opening angle 45deg to 60deg
8243 Pitch diameter of sheaves and rope drumsThe required rope sheave and rope drum pitch diameters relative to rope diameter dr shall be as shown inTable 8-3For all other types of wire ropes the ratio shall be agreed with the Society in each individual case
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Table 8-3 Minimum pitch diameter 1 of rope sheaves and rope drums for standardized wire ropes
Minimum pitch diameter for rope drums 3Applicationcrane group 2
Minimum pitchdiameter for
rope sheaves 3 Ungrooved drums Grooved drums
Nominal tensilestrength of wire ropes 4
Wire ropes notoperated under load 10 dr 11 dr 10 dr 1770 Nmm2
A 19 dr 21 dr 17 dr 1960 Nmm2
B 21 dr not permitted 19 dr 1960 Nmm2
C1 23 dr not permitted 21 dr 1960 Nmm2
C2 + C3 26 dr not permitted 23 dr 1960 Nmm2
1) The pitch diameter is the sum of the nominal diameter of a sheave or drum and the nominal wire rope diameter Incase of rope sheaves and machined drums the nominal diameter is measured in the bottom of the groove
2) For crane group definition see [52]3) Where non-rotating or poorly-rotating ropes are used it is recommended that the diameters indicated be increased
by 104) Where ropes with a higher nominal tensile strength are used the prescribed diameters shall be increased
proportionally
8244 Lateral deflection angle of the rope
82441 The lateral deflection of wire ropes relative to the plane of the groove in the rope-sheave or ropedrum shall not be greater than 114 (4deg)
82442 In the case of poorly-rotating ropes the lateral deflection angle shall not be greater than 128 (2deg)
82443 Exceptions to the above requirements are made for unwinding hoist ropes Special wear-reducingdesign measures shall be taken for lifting appliances at sea frequently
8245 Employment of swivelsNon-rotation-resistant ropes shall not be used with a swivelFor rotation-resistant ropes the use of a swivel is recommended
83 Synthetic fibre ropes
831 General requirements
8311 Synthetic fibre ropes shall comply with recognized standards (eg DNVGL-OS-E303)
8312 Synthetic fibre ropes except carbon fibre ropes may be used for standing rigging and for runningrigging of special lifting appliances which is stressed moderately subject to agreement with the SocietySynthetic fibre ropes may also be used for the cargo tackles of landing booms according to [663] with theexception of carbon fibre ropes The agreement of the Society is required for other applications
8313 Synthetic fibre ropes shall be stabilized with respect to light and heat
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8314 Free rope ends shall be yarn-wound to prevent disintegration of the rope structure Synthetic fibreropes may be partially melted
832 Definitions
8321 The terms running rigging standing rigging and rope sling as well as the term actual breakingload Fwi are defined in [822]
8322 The proven breaking load Fn of a synthetic fibre rope is the load calculated from the breakingload of the yarns contained in the rope multiplied by a reduction factor or that load determined by testing inaccordance with the requirements of DNVGL-OS-E303
8323 The reduction factor is an empirical value which takes account of the loss of strength due tostrandingThe reduction factors shall be taken from recognized standards
833 DimensioningIn the case of synthetic fibre ropes used for lifting appliances or load-handling devices the breaking load FBrshall not be less than the product of the static rope tension FS and one of the safety factors γF given inTable 8-4
FBr ge FS middot γF
FBr = required breaking load of the rope analogous to [8231]FS = rope tension according to [8232]
Table 8-4 Safety factors for standardized synthetic fibre ropes
Nominal diameter of rope [mm] Coefficient of utilization γF
10 ndash 13
14 ndash 17
18 ndash 23
24 ndash 39
40 and over
12
10
8
7
6
For non-standardized synthetic fibre ropes γF shall be agreed with the Society
Synthetic fibre ropes shall be dimensioned with respect to their 3-T endurance and shall comply with DNVGL-OS-E303
Synthetic fibre ropes shall be operated according to their designated service The designated servicefor synthetic fibre ropes shall assure that adequate margins are maintained towards exceeding the 3-Tendurance and other relevant failure modes DNVGL-ST-E407 can be taken as guidance
The 3-T endurance and other aspect of dimensioning of synthetic fibre ropes are outlined in DNVGL-RP-E305
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834 Requirements for rope drives
8341 Synthetic fibre ropes shall not be used on capstan heads or other devices where a major slippagemay occur
8342 Synthetic fibre ropes shall only be wound up in one layer Winding shall be performed under tension
8343 The required rope sheave diameters relative to the nominal rope diameter dr shall be as shown inTable 8-5For non-standardized synthetic fibre ropes the rope sheave pitch diameter shall be agreed with the Society
Table 8-5 Minimum pitch diameter 1 of rope sheaves for standardized synthetic fibre ropes
Rope material Minimum pitch diameter for rope sheaves
polypropylene
polyamide
polyester
4 dr
6 dr
6 dr
1) The pitch diameter is the sum of the nominal diameter of the sheave and the nominal rope diameter The nominaldiameter of a sheave is measured in the bottom of the groove
8344 The required diameters of rope drums shall be agreed with the Society in each case
8345 The lateral deflection of synthetic fibre ropes relative to the plane of the groove of rope sheaves orrope drums shall not be greater than 114 (4deg)
8346 The number of safety turns remaining on rope drums shall be as specified by the manufacturer ofthe winch but not less than
mdash five (5) safety turns in generalmdash three (3) safety turns if the rope is connected positive locking with the rope drum
84 Rope-end attachmentsRope-end attachments shall be designed in accordance with recognized standards eg the following
841 Splices for wire ropes and synthetic fibre ropes
8411 Wire ropes and synthetic fibre ropes shall not be made up of parts spliced together
8412 Loop splices (eye splices) and thimble splices shall conform to standard EN 13411-2 or be ofequivalent designThe dimensions of thimbles shall comply with standard EN 13411-1 (Shaped steel thimbles for wire ropes)or standard DIN 6899 (Steel thimbles for fibre ropes) as appropriate
8413 Provided that [82411] and [8346] are met rope ends connected to winches may be splicedwithout thimbles see [9526]
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DNV GL AS
8414 Splices of any kind are not permitted for cranes of types B and C because of their inadequatefatigue strength
8415 Splices shall not be sheathed
842 End attachments for wire ropes8421 Rope sockets
84211 Rope sockets (open and closed sockets) into which wire rope ends shall be socketed shall conformto standard EN 13411 On application other designs may be approved
84212 The socketing process using metal or plastic resin shall be performed as prescribed in standardEN 13411-4 and may only be carried out by companies which have been approved by national accreditedcertification bodiesOnly approved cast materials may be used Rope sockets shall be marked with the code letter of themanufacturing company
8422 Wrought ferrules
84221 Wrought aluminium alloy ferrules shall conform to EN 13411-3Flemish eyes as per DIN 3095 shall be used wherever possible for the end attachments of the hoisting andluffing ropes of lifting appliances if the lifting appliances are working with grabs
84222 On application swaged or rolled end fittings (terminals) may be approved
84223 Application of ferrules in accordance with [84221] and [84222] may only be carried out byapproved companies Ferrules shall be marked with the code letter of the manufacturing company
8423 Detachable end joints
84231 Cable joints (wedge clamps) may only be used if the ropes are permanently under tension Theyshall be clearly visible and readily accessible to facilitate inspectionThe free end of the rope shall be secured from being pulled through eg by rope sockets The safeguardconnection of the rope end to the load-bearing part of the rope shall not be force-transmitting However itshall be capable of bearing 10 of the rope tension FSCable joints shall correspond to EN 13411-6 Up to a rope diameter of 8 mm EN 13411-7 may also beapplied
84232 Rope sockets as per EN 13411-5 are not permitted This does not apply to the securing of free ropeends to cable joints
84233 With regard to the attachment of rope ends to winch drums the requirements given in [9526]and [9527] apply
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DNV GL AS
85 Tests and examinations
851 Manufacturing survey8511 Wire rope and synthetic fibre ropes
85111 GeneralWith regard to testing and examination of ropes the requirements given in the DNV GL rules as stated in[8121] applyInstructions for the testing and use of ropes and an excerpt from the Societys rules for wire ropes andsynthetic fibre ropes shall be found on the reverse sides of the Societys certificates CG4 and LA4
85112 Tensile testsAfter manufacturing ropes shall be subjected to a tensile test which is mandatory for the issue of theSocietys certificate The following appliesRopes shall be loaded to destruction in their entirety Where the tensile force of the testing machine is notsufficient to perform a tensile test for the whole rope individual wires or yarns shall be loaded to destructionin a prescribed procedure and the breaking load of the rope determined by calculationFrom every manufactured length of a wire rope up to 10 000 m a test sample shall be tensile tested in itsentirety to destruction The test length shall be equal to 30 times the diameter of the rope subject to aminimum of 600 mm The minimum breaking load shall achieve the value specified for the rope in questionin the standard In the case of manufactured lengths of more than 10 000 m a second test sample shall betaken and testedWhere the tensile loading capacity of the testing machine is insufficient to test the wire rope in its entiretythe breaking load of the rope shall be determined from the results of tests performed on the individualwires For this purpose a strand shall be taken from every manufactured length of rope of 5000 m or lessand its constituent wires shall be individually subjected to a tensile test eg to EN 12385 The wire testspecimens shall have an initial measured length of 100 mm or 200 mm The nominal tensile strength shall bedetermined on the basis of the nominal wire diameterThe test shall be deemed successful if
mdash the calculated breaking load achieves the values specified in the relevant standard andmdash at least 95 of the rope wires meet the requirements stated in [31022]
For this purpose the individual test values shall be applied to the total number of wires in the rope andmultiplied by the realization factor shown in Table 8-6
Table 8-6 Realization factors
Rope construction Ropes with fibre core Ropes with steel core
6 x 7
6 x 19
6 x 24
6 x 36
6 x 37
09000
08600
08700
08400
08250
08379
08007
--
07821
07681
The results of the tensile tests of the ropes shall achieve the values prescribed in the relevant ropestandards
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DNV GL AS
Tensile tests of ropes shall be performed in the presence of the Societys surveyor if
mdash the manufacturer is not approved by the Society to test and issue certificates on his own authoritymdash special rope designs are not covered by the Societys approvalmdash the customer requests it
Before each tensile test the protocols on the checks performed by the manufacturer shall be presented tothe Societys surveyorFollowing every tensile test checking the diameter tolerances method of manufacture and manufacturersprotocols the Societys surveyor will issue a certificate of test and thorough examination of wire rope orsynthetic fibre rope using one of the forms stated in [8621]
85113 Dimensional check of wire ropesThe diameter of each wire rope shall be measured at two points located at least 1 m apart in two directionsapproximately perpendicular to each other The difference between the smallest and the largest result maynot be more than 4The average value of the four measurements shall be considered to be the actual rope diameter and shall liewithin the permitted tolerances The number and diameter of the individual wires shall also be verified
Marking85114 Ropes shall be marked by woven-in identification bands and coloured identification threads Thefollowing shall be taken into accountThe identification band shall carry the name or mark of the manufacturer and in the case of the Societysapproval in addition the manufacturerrsquos identification number assigned by the SocietyThe colour of the identification thread gives information about the nominal tensile strength of wires or thetype of yarn used (identification colour)For steel wire ropes the colour of the identification threads shall be as follows
mdash nominal tensile strength 1570 Nmm2 - whitemdash nominal tensile strength 1770 Nmm2 - greenmdash nominal tensile strength 1960 Nmm2 - yellow
The coloured identification thread may be dispensed with if the identification band itself carries theidentification colour
8512 End attachments
85121 End attachments which are not standardized or do not correspond to standards are subject to anassessment of drawings
85122 With regard to tests and examinations of rope sockets cable joints and terminals the requirementsgiven in [735] apply For terminals it may be required to produce specimens connected to a small length ofrope
85123 In the case of short ready-made units the rope sockets and terminals can be load-tested togetherwith the rope
852 Initial testingRopes and their end attachments are subject to a visual inspection and a check of the relevant certificateswithin the scope of the initial testing of lifting appliances
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DNV GL AS
853 Periodic testing8531 Wire ropes and synthetic fibre ropes
85311 In the scope of the periodic testing of lifting appliances and load-handling devices the ropes shallbe examined by the Societys surveyor with regard to condition and fitness for use
85312 When ropes are examined attention shall be paid to deformation crushing corrosionrottennessand broken wires If necessary the ropes shall be twisted open for an internal examination
85313 Special attention shall be paid to the end attachments There broken wires or yarns shall beexpected with wire ropes also corrosion especially with downward hanging end attachments Sheathingsshall be removed for examination
85314 Sheaves used for length compensation within tackle where a rope only seems to be resting areparticularly prone to wire ruptures caused by regular compensation motions
85315 Where splices have become loose the ropes shall be shortened and spliced again or whererequired replaced
8532 End attachmentsWith regard to end attachments the requirements given in [85311] apply Attention shall be paid to wearcracks and corrosion
8533 Discard criteria for wire ropes
85331 Generally discard criteria according to ISO 4309 shall apply
85332 Wire ropes which are regularly employed under water shall be shortened in the vicinity of the fixedload-lifting attachment (eg the hook) at least once per year in order to enable the cut-off end which shouldhave a minimum length of 1 m to be thoroughly examined and subjected to a tensile testIf the remaining breaking load is below 80 of the (initial) actual breaking load the rope shall be discardedIf the remaining breaking load is 80 or above the (initial) actual breaking load an estimate shall be madebased on the condition and the period of employment whether the rope may be employed for another year
85333 Wire ropes employed above deck shall be discarded at the latest after the following periods ofemployment even when no external damage is visible
mdash running rigging 10 yearsmdash standing rigging 15 years
Wire ropes may be employed for a longer period of time if a certificate of fitness has been issued by arecognized rope company or by the rope manufacturer after a thorough examination
86 Documentation
861 Marking8611 Wire ropes and synthetic fibre ropes
86111 Ropes are marked by the method described in [85113]
86112 With regard to ropes the rope tension Fs calculated according to [8232] shall not be less thanthe permissible load SWL stamped on the end attachments
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DNV GL AS
86113 With regard to ropes with splices a small metal plate stamped in accordance with [7423] shallbe fastened near an end attachment
8612 End attachmentsEnd attachments for wire ropes are stamped like interchangeable components see [7423] Whereapplicable this is also possible on ferrules or terminals taking account of [84233]
862 Certificates8621 Wire ropesAfter the tension test in cases described in [85112] the Societys surveyor will issue the followingSocietys product certificate
mdash Form CG4
Wire rope manufacturers approved by the Society will issue the following product certificate
mdash Form LA4
8622 End attachmentsWith regard to certification of end attachments the requirements given in [73611] apply
863 Storage of rope certificatesAs described in [137] product certificates for ropes and product certificates for end attachments will beadded initially and after each re-issue to an allocated register book on board
864 Confirmation of examinations
8641 Ropes and end attachments which are integral parts of lifting appliances or load-handling deviceswill be included in the annual thorough examination of them
8642 The confirmation of examinations of ropes and end attachments which cannot be allocated toparticular lifting appliances or load-handling devices will be effected by a survey report Form 409a for theseparts
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DNV GL AS
SECTION 9 MECHANICAL PARTS
91 General
911 General
9111 This section contains requirements for the mechanical parts of shipboard lifting appliances andwhere required also load-handling devices
9112 Complementary or more comprehensive requirements in particular for mechanical parts not coveredhereafter shall be taken from the following rules
mdash DNV GL rulesmdash recognized standards and requirements where applicable to lifting appliances unless contrary to the
provisions in this section
9113 The requirements given in Sec1 shall be observed if applicable
9114 The provisions in Sec3 Sec11 and Sec12 apply to the materials the manufacture and the safetyrequirements of mechanical parts
912 Scope of application
9121 Table 2-1 to Table 2-3 indicate the essential mechanical parts which are subject to assessmentof drawings as deemed necessary by the Society and which shall be delivered in the designated mannertogether with test reports or inspection certificates
9122 The requirement for an assessment of drawings and the type of certificate depends on the safetyrelevance of the components with respect to their strength and reliability and on the operational mode andthe type of certification of the lifting appliances
9123 Table 2-1 to Table 2-3 reflect the general requirements given by the Society The Society reservesthe right to impose additional requirements or to permit deviations
9124 The Society reserves the right to impose additional requirements for all kinds of mechanical partsshould this be necessary on account of new findings or operational experience
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DNV GL AS
92 Design criteria and operational requirements
921 General
9211 Mechanical parts of shipboard lifting appliances and load-handling devices shall be designed for theenvironmental conditions agreed on or prescribed and be capable of being operated without problem underthese conditions
9212 The effects of deformation of the supporting structure on machinery and equipment shall beobserved
9213 Mechanical parts shall be designed in such a way that repairs and regular maintenance are easy toperform using on-board tools
922 Dimensioning
9221 Mechanical parts shall be dimensioned in such a way as to provide adequate strength in respect ofdynamic stress peaks plus adequate fatigue strength in relation to the load and service lifeWith respect to dimensioning attention shall be paid particularly to the stress peaks arising duringacceleration and retardation and if applicable the dynamic influences resulting from lifting and lowering ofloadsProof of fatigue strength may be provided in accordance with the section I of FEM
9222 All mechanical parts shall measure up to the special circumstances of operation on board ships suchas ship movements and acceleration increased corrosion temperature changes etc
9223 With regard to structural design and fastening in general acceleration of 07 g in the frequencyrange from 13 to 100 Hz shall additionally be considered see also [9231]
923 Effects of vibration
9231 Machinery and equipment shall not cause any vibrations and shocks which may unduly stress othercomponents or the structure of the lifting appliance and load-handling device The permissible amplitudesand accelerations are stated in the DNVGL-RU-SHIP Pt4 Ch2
9232 If compliance with the permissible values of amplitude and acceleration cannot be ensured bystructural measures damping measures are required
9233 Within the frequency ranges which occur there shall be no resonance phenomena in componentssupport- and suspension arrangements - nor within equipment
924 Lubrication
9241 Lubrication of the moving parts of lifting appliances and load-handling devices shall be guaranteedunder all operating conditions
9242 Each grease-lubricated bearing shall be provided with its own proven type of grease nipple
9243 Accessibility to manual greasing points shall be ensured
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DNV GL AS
925 Corrosion protectionComponents at risk of corrosion shall be given suitable corrosion protection
93 Power drivesThe requirements given in [92] shall be observed In addition the following applies
931 Drives in general
9311 Power drives shall be adequately dimensioned for the working conditions laid down to allow trouble-free and low-vibration operation
9312 For electrical drives and electrical controls in general the requirements given in Sec10 areapplicable
932 Main drives
9321 Main drives of shipboard lifting appliances shall be dimensioned in such a way that the installedpower meets the requirements given in [9311] for all combinations of motion and speedWhere the installed power is not sufficient to execute all motions simultaneously at nominal load and at fullspeed the speed shall be reduced automatically
9322 Diesel engines shall not be capable of running at excessive speeds or being stalled
94 Slewing gears and slew rings
941 Slewing gears
9411 Slewing gears shall be designed for maximum operating torque and where the gears are of a self-locking type they shall be equipped with a slewing gear brake
9412 Slewing gears on board ships shall be designed in such a way that in the event of the vesselspermissible inclination being exceeded by 5deg none of the materials employed shall be stressed beyond 90of its yield point
9413 In the case of slewing gears on board ships it shall be taken into account that it might be necessaryin the out of operation condition to reduce the load on the slewing gear brakes by means of locking devices
9414 Slewing gears of shipboard cranes working at sea state shall be dimensioned for at least 13 timesthe design torque based on wind transverse tension and inclination of the cranersquos base and shall have atleast two (2) independent drives
942 Slew rings9421 Large roller bearings
94211 The design of large roller bearings shall together with the connecting structures and the bolting besuitable for the intended operation and the intended environmental conditions
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DNV GL AS
94212 The connecting flanges on the lifting appliance and foundations shall be adequately distortion-resistant their surfaces machinedAccuracy of plane and distortion shall be within the tolerances stated by the manufacturerThe mating surfaces shall be steel to steel Casting of synthetic material is permitted only in exceptionalcases and requires the Societys approval in each individual case see [57412]
94213 Large roller bearings shall be designed in such a way that a failure of important runway elementsdoes not result in a total loss of the lifting appliance
94214 If large roller bearings have to be dismantled during employment for an internal examinationspecial dismantling equipment shall be available which can hold the lifting appliance and raise it after theconnecting bolts have been unscrewedAs an alternative the lifting appliance shall have special eyebolts for lifting by another appliance and a safeplace for setting-down
94215 Where an interchange of seals is intended large roller bearings shall be designed such that this isenabled without dismantling of the bearings or loosening of the connecting bolts
94216 With respect to the materials to be used as well as their heat treatment and proof of mechanicalproperties the requirements given in [134] apply
9422 Bolting of large roller bearingsIn addition to [5741] the following applies
94221 The fixed ring at the foundation or at the crane column shall be bolted at even intervals around itscircumference
94222 For bolting of the rotating ring to the lifting appliance uneven bolt intervals may be applied if thesafety of such bolting is verified by calculation or measurement
94223 The distance between the bolts shall in general not exceed six (6) times the bolt diameter
94224 The requirements for the bolts are as followsUp to a diameter of le 30 mm bolts may be preloaded according to the instructions of the slew ringsmanufacturer by applying a torqueFor larger diameters preloading shall be by hydraulic elongation This calls for increased thread tolerancesWith respect to the materials to be used for the bolts as well as the proof of their mechanical properties
9423 King pins and support rolls
94231 If not safe by design lifting appliances shall be secured against overturning by king pins andsupport rolls also with rolls which engage from below where required
94232 The rotating system shall meet the following requirements
mdash support rolls shall be installed in a stationary positionmdash support rolls and king pins shall be easily accessible for maintenance and inspection support rolls also for
exchange purposesmdash after failure of one support roll even under load the lifting appliance shall still be capable of being turned
into a secure position
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DNV GL AS
95 Winches
951 Design
9511 Winches shall be of a reversible type ie the lowering process shall also be motor-controlled
9512 Design features incorporated in each winch shall ensure that the load cannot run back inadvertently(eg by a ratchet wheel self-locking gears non-return valves automatic brakes etc)
9513 The use of belts or friction discs to transmit power between the winch drum and the reverse travelprevention device referred to in [9512] is not allowed
952 Rope drums
9521 The drum diameter shall be determined in accordance with the intended purpose of the winch inaccordance with [8243] or a recognized standard
9522 The calculated hoop stress of winch drums σh shall not exceed 85 of the material yield stress
9523 Rope drums shall be provided with flanges whose outer edges extend above the top layer of rope byat least 25 times the rope diameter unless the rope is prevented from overriding the flange by a spoolingdevice or other meansIt shall be ensured that ropes can wind onto drums properly and without excessive deviation
9524 The number of safety-turns left on the rope drum shall not be less than three (3)
9525 Rope grooves shall comply with the following requirements
mdash groove diameter ge 105 middot rope diameter dsmdash groove depth ge 033 middot rope diameter ds
9526 In the case of multiple winding wedges at the flanges shall facilitate the ropes onto the second layerunless special measures are provided such as
mdash small lateral deflection le 15degmdash cable guidesmdash lebus grooving
9527 Rope-end attachments at the winch drum shall be designed in such a way that
mdash the ropes are not pulled over edgesmdash the end fastening cannot be released unintentionallymdash the end fastening is easy to inspect
If the end attachment of wire ropes is based on clamping at least three (3) clamping plates shall be usedThe construction of end attachments for synthetic fibre ropes shall be agreed with the SocietyFor nominal loads up to 12 t and lifting appliances which are only occasionally loaded spliced rope loops canalso be used
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DNV GL AS
9528 The following conditions shall be met for the minimum required rope tension force Fa at the drum
95281 Shipboard lifting appliances
FS = rope tension as per [8232]γD1 = safety factor for wire ropes as per Table 8-2 (where applicable [8233] shall be observed)μ = coefficient of friction between rope and drum Applicable values are
mdash smooth drum μ le 008mdash grooved drum μ le 010
α = wrap angle For 3 turns isα = 6 middot π
95282 Shipboard lifting appliances working at sea state
FBr = rope breaking load according to [8231]
The Societys may also demand this rope tension for other lifting appliances if this is employed under similaroperational conditions eg for floating cranes operating at sea
953 Brakes
9531 Each winch shall be fitted with a braking device capable of braking and holding the maximumpermitted load safely under all operating conditions and this action shall not generate inadmissible dynamicinfluencesThe minimum friction coefficient of the brake shall not exceed 03 in the design calculationThe winch and its substructure shall be able to safely withstand the forces set up during braking
9532 Having regard to the dynamics of the braking action the braking torque shall exceed the maximumload torque by an adequate safety margin As a guide the maximum braking torque may be set at about80 above the maximum load torqueIf need be fdS according to [82326] shall be considered
9533 The required braking device may take the form of
mdash self-locking gearmdash mechanical brake with brake pads or brake discsmdash a hydraulic or pneumatic device which prevents lowering of the load ormdash electromotive brake
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DNV GL AS
and shall be actuated when
mdash the control returns to the neutral positionmdash a safety device comes into actionmdash the power supply fails ormdash on hydraulic installations a non-scheduled pressure loss occurs
9534 Hydraulic retention brakes shall comply with the following requirements
mdash The shut-off valve of hydraulic motors shall activate at the low-pressure connection in the case ofpressure loss
mdash Hydraulic motors shall have a shut-off valve hydraulic cylinders a valve according to [9624] which shallbe fitted directly at the high-pressure connection
mdash A hydraulic motor and cylinder shall always be fed with a sufficient quantity of working fluid also the fluidsupply in the event of power failure eg by gravity
mdash Shut-off valves and valves according to [9624] shall be capable of absorbing the pressure impactscaused by braking
9535 Electromotive brakes additionally require a mechanical holding brake (drum brake or spring-loadedmotor brake)
9536 Braking devices shall be designed in such a way that on the one hand they may be adjustable onthe other the designed braking effect cannot easily be interfered with Due to humidity oils or impuritiesbraking power shall not decrease below the design valueWhere a gear box is arranged between brake and drum the load-bearing components shall be dimensionedlike the corresponding components of a brakeSpring-loaded braking pads or discs shall be loaded by pressure springsChecking wear to braking pads or discs shall be possible without dismantling the braking unitSelf-blocking brakes are only admissible for stowage or idle positions
9537 The following requirements apply to shipboard cranes and floating cranes which transport persons
95371 In addition to the normal working brake hoisting and luffing winches shall be fitted with asecondary brake which is independent in terms of mechanical and operational layout
95372 Secondary brakes shall have their own independent control circuit and at least be dimensioned towithstand loads as per [4251] and [4252]
954 Winch drives9541 Power drivesFor power drives the requirements given in [93] and [9614] apply
9542 Manual drives
95421 Manual drives shall incorporate the following features
mdash The crank handle turns in the same direction for all gear ratiosmdash Crank handles have a crank radius of approximately 350 mm and a rotatable grip sleevemdash Detachable crank handles are safeguarded against being detached unintentionallymdash The load is hauled in manually with a force of max 160 Nmdash A speed of about 30 revmin-1 is not exceeded
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DNV GL AS
95422 Where winches are constructed for both powered and manual operation the power- and manualsystems shall be mutually interlocked
955 Couplings
9551 Clutch couplings between the drive and the rope drum are only permitted where one of the means toprevent runback stipulated in [9512] has been provided
9552 Where winches have more than one disengageable drum only one drum shall be in operation at anytime
9553 Control levers shall be safeguarded against unintentional operation
956 Gearing
9561 The design of gearing shall conform to established engineering practice location positioning andmode of operation shall be taken into account
9562 Gearing shall amongst others include the following characteristics
mdash easy access for maintenancemdash facilities for checking the oil levelmdash ventilation- and oil filler pipes appropriate to the locationmdash inspection openings
957 Controls and monitoring instruments
9571 The controls and monitoring instruments shall be clearly arranged on the control platform
9572 Controls and monitoring instruments shall be permanently clearly and intelligibly marked with thedirection or the function of the movements they control see [1242]
9573 The arrangement and direction of movement of controls and monitoring instruments shall match thedirection of the movement which they control
9574 The operating movement range of control levers shall be less than 300 mm and when released theyshall return automatically to the neutral position
9575 In the case of push-button controls there shall be a separate button for each direction of movement
96 Hydraulic systems
961 General requirements
9611 The dimensioning and design of hydraulic systems shall conform to the established rules ofengineering practice Safe operation under all envisaged service conditions shall be ensured by suitableequipment (eg filters coolers control devices and primary pressure control) and by selecting anappropriate hydraulic fluid
9612 Hydraulic systems shall be protected against overpressure and against overspeed of the load by acorresponding limitation of flow rate and pressure
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DNV GL AS
9613 Instead of pipes high pressure hoses may be used These shall comply with the requirements givenin EN 13135-2 or an equivalent standardThe hoses shall be suitable for the proposed operating fluids pressures temperatures operating andenvironmental conditions and be appropriately laid and of an approved design
9614 For hydraulically-powered winches a standstill brake to prevent slip is required if necessitated by theconstruction of the winchAny slip occurring shall generally not exceed the equivalent of one revolution of the drum or 1 m hooklowering per minute whichever is the lesser
962 Hydraulic cylinders
9621 Hydraulic cylinders shall be dimensioned for 11 times relief pressure pc and dynamic forces which mayoccur in and out of service
9622 The relief pressure pc of the safety relief valves shall be set at a sufficiently high level that dynamicforces which may occur can be absorbed and hoist load coefficients are considered
9623 Piston rods shall be sufficiently rigidly connected to the piston or telescopic rod in order to meet therequirements for calculation given in [4923]The stroke of the piston rods shall be limited by end stops which shall be capable of preventing the pushing-out of the piston rods even at the utmost pressure and dynamic load If necessary devices for terminaldamping or end limitation shall be provided
9624 With telescopic cylinders extending and run-in of the telescopic rods shall be conducted in aspecified order
9625 Load-bearing hydraulic cylinders eg for lifting luffing folding and telescoping of crane booms aswell as for slewing of lifting appliances shall be provided with a device which maintains the position of theload the crane boom or the lifting appliance in the event of pressure loss and failure of a pipe or hose lineSuch a device may be an automatic shut-off brake valve a pilot-operated check valve or a load holdingvalve and shall be installed inside or outside directly at the cylinder
9626 The type of fastening and the design of the bearings shall safeguard that no unacceptable externalbending moments can be transmitted to the hydraulic cylinders
963 Hydraulic tanks
9631 Regarding dimensioning of hydraulic tanks tasks like eg cooling (radiation of heat) eliminating airand depositing contaminants shall be taken into consideration At the same time the container shall be ableto accommodate the total amount of oil in the system
9632 Hydraulic tanks shall be fitted with
mdash fluid level indicator (including minimum and maximum values)mdash access openingmdash outlet valvemdash ventilation
Design operational and environmental conditions may in addition require cooling andor heating of thetanks
9633 Pressure tanks shall be capable of withstanding a 2-fold maximum working pressure and shall have asafety valve against overpressure
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DNV GL AS
97 Protective measures and safety devices
971 Protective measures
9711 Moving parts flywheels rope and chain drives rods and other components which might come toconstitute an accident hazard for the handling staff shall be provided with protection against accidentalcontact The same applies to hot mechanical parts pipes and walls not provided with insulation
9712 Measures shall be taken to provide power supply lines with effective protection against mechanicaldamage
9713 Cranks for starting internal combustion engines shall disengage automatically once the engine startsrunning
9714 Machinery employed in potentially explosive areas shall comply with the requirements given in EN13463-1
972 Safety devices
9721 Winches and drive systems shall be equipped with adjustable protection devices (eg pressure reliefvalves winding and slip clutch thermal overload relays) Following a power failure drives shall not restartautomatically
9722 Devices provided to unlock slewing or hoisting gear are only permissible for special operationalpurposes or as emergency measures eg on offshore cranes
9723 Safety devices shall not be rendered unserviceable by environmental conditions at the point ofinstallation because of dirt or springs breaking There shall be a means of checking the devices
98 Assessment of drawings and manufacturing survey
981 Assessment of drawings
9811 The general requirements given in Sec2 shall be observed
9812 In addition the mechanical parts indicated in Table 2-1 to Table 2-3 are subject to assessment ofdrawings within the scope indicated there
982 Manufacturing survey9821 General
98211 Mechanical parts shall be manufactured by staff qualified in handling the installations and devicesnecessary During manufacture and before delivery the parts shall undergo the quality tests required inaccordance with state-of-the-art technology and experience
98212 All materials shall be suited to the intended purpose Proof of the mechanical properties of thematerials used shall be furnished Identification of the materials shall be possible on the basis of testcertificates or reports
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DNV GL AS
98213 Mechanical parts which require a Societys product certificate according to Table 2-2 and Table 2-3are subject to manufacturing survey by the SocietyThe Society inspection in charge decides in coordination with the manufacturer on type and scope ofmanufacturing survey and certification taking the in-house quality control andor approval for productioninto considerationWith respect to assistance by the manufacturer during manufacturing survey by the Society therequirements given in [1322] shall be observed
9822 Tests and examinationsThe following requirements contain general test requirements and in addition provisions for themanufacturing survey by the Society
98221 GeneralFor the acceptance tests before delivery and if applicable also for the manufacturing survey the Societyssurveyor shall be given material test and internal control certificates test reports and manufacturingdocuments in particular approved drawings including the relevant design approval letter as a prerequisitefor the tests and examinations described belowTest reports shall include the following information if applicable
mdash designation of type and nominal dimensionsmdash purchase and order numbermdash drawing numbermdash results of internal controlsmdash certificate numbers of material tests and non-destructive testsmdash additional details as necessary
For series-production components other test procedures may be agreed with the Society instead of theprescribed ones if they are accepted to be equivalentThe Society reserves the right to extend the scope of testing if necessary and also to subject suchcomponents to a test for which testing is not expressly required in this standardWhere mechanical parts shall be used for the intended purpose for the first time the Society may ask for atype approval
98222 WinchesAfter completion winches shall be subjected to an examination and functional test at nominal rope tensionby repeated hoisting and lowering of the nominal load During the functional test in particular the brake andsafety devices shall be tested and adjustedWhere winches are designed for a holding force greater than the nominal rope tension the nominal ropetension shall be tested dynamically and the holding force staticallyWhere winches are designed with a constant tension device the maintenance of constant tension shall beproven for all levels of tension set by the designThe above tests including the setting of the overload protection can also be performed on board togetherwith the functional testing of the lifting appliance In this case a functional test at available load shall beperformed at the manufacturersTesting of winches at test load will be performed within the scope of initial tests of the lifting appliance see[1333]
98223 Load-bearing hydraulic cylindersHydraulic cylinders for hoisting luffing telescoping and slewing are load-bearing componentsLoad-bearing hydraulic cylinders shall undergo a functional test at relief pressure and a pressure test at testpressure The test pressure shall be 15 times relief pressure pc however with relief pressures over 200 barit need not be higher than pc + 100 bar
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DNV GL AS
See [9625] in the case of series-production of lifting appliances of the same type and with multiplecylinders eg with slewing cranes with luffing folding andor telescopic crane booms a regular check on thecylinders at a minimum of 125 times the relief pressure may be acceptedThe Societys surveyor is entitled to ask for cylinders to be tested which are selected at random
98224 Large roller bearingsThe material properties of forged rings shall be tested according to [345] by tensile tests and by notched-bar impact tests and shall comply with the requirements given in the agreed specificationThe manufacturer shall in addition ultrasonically test the rings for internal defects and certify that thematerials are free from defects which may impair the performance characteristicsRings shall be heat-treated as appropriate to the material and the running surfaces shall be hardenedadditionally After hardening the runway surfaces of the rings shall be crack-tested along their entire lengthCracks may be removed by grinding if by this measure the functional capability of the slewing ring is notimpaired Residual cracks are not permitted The Societys surveyor may demand the crack test be performedin his presenceThe hardened runways shall undergo a hardness test at least eight (8) points equally distributed along thecircumference The hardness values shall be within the specified rangeWhere there are reasonable doubts about the hardened depth proof shall be furnished using specimenswhich have been hardened under the same conditions as the ring under considerationFor the acceptance test before delivery the large roller bearing shall be assembled and presented to theSocietys surveyor The functional capability (slewing without load) the bearing clearance and the accuracy inplane and round travelling are thereby to be tested In addition the dimensions shall be checked randomlyas deemed necessary by the surveyor
98225 Bolts and nuts for large roller bearingsWith respect to tests and examinations of bolts and nuts the DNV GL rules for metallic materials DNVGL-RU-SHIP Pt2 applies
98226 Mechanical and hydromechanical partsWith respect to tests and examinations of mechanical and hydromechanical parts DNVGL-RU-SHIP Pt4 applywhere relevantParts not covered by DNV GL rules shall be tested and examined using appropriate procedures agreed withthe Societys surveyorInstead of testing at the manufacturers tests can also be performed on board within the scope of initial testsof the lifting appliance if practicable
99 Documentation
991 Marking
9911 Each mechanical part shall be marked by the manufacturer in a suitable way The marking shall atleast include the following if applicable
mdash manufacturers namemdash year of constructionmdash designation of typemdash purchase order number or serial numbermdash characteristics such as nominal load nominal pressure nominal voltage etcmdash additional details as necessary
9912 If after the acceptance test before delivery the requirements for issuing a Societys productcertificate are complied with the tested mechanical part will be stamped in a prominent position
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DNV GL AS
The stamp shall include the following information
mdash certificate number together with the code letters of the examining inspecting officemdash stamp with the month and year of testing
For hydraulic cylinders additionally
mdash working pressuremdash testing pressure
For winches additionally
mdash rope tension [kN]mdash holding force [kN]
For slewing gear rings additionally
mdash abbreviation for the material typemdash melting charge numbermdash specimen number
9913 The winding direction of ropes on rope drums shall be clearly recognizable on the drumsWhere required the winding direction shall be indicated appropriately on the drum or winch
992 Certificates
9921 Table 2-2 and Table 2-3 show the required types of certificates for essential mechanical partsThe lifting appliance manufacturer shall order the stated parts together with the required certificates theparts manufacturer shall include them in the delivery
9922 The certificates listed in Table 2-2 and Table 2-3 are not part of the lifting appliance documentationon board
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DNV GL AS
SECTION 10 ELECTRICAL EQUIPMENT
101 General
1011 General
10111 This section contains the requirements for electrical equipment of shipboard lifting appliances andwhere applicable also of load-handling devices
10112 Additional or more comprehensive requirements eg for switch cabinets and for electricalequipment not covered hereafter can be taken from the following
mdash DNVGL-RU-SHIP Pt4 Ch8mdash DNVGL-RU-SHIP Pt4 Ch9mdash recognized standards and regulations where applicable to shipboard lifting appliances unless contrary to
the requirements given in this section
10113 The requirements given in Sec1 shall be observed where relevant
1012 Scope of application
10121 Table 2-1 is a list of the essential electrical equipment which is subject to assessment of drawingsas deemed necessary by the Society and which shall be delivered together with test reports or inspectioncertificates
10122 The requirement for an assessment of drawings and the type of certificate depend on the safetyrelevance of the equipment with respect to its suitability and reliability and on the operational mode andorthe type of certification of the shipboard lifting appliances
10123 In case of founded exceptions also the approval and certification of electrical equipment not listedin Table 2-1 to Table 2-4 can be required if they are exceedingly relevant for the safety andor reliablefunction of the lifting appliance
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DNV GL AS
102 Design criteria and operational requirements
1021 The electrical control and switch gear as well as the motors shall be designed or arranged in such a waythat necessary maintenance of contacts contactors collectors slip rings brakes etc can be carried out withmeans available on board
1022 Switch and control cabinets as well as motors arranged on deck shall be provided with adequate heating forthe standstill condition if sufficient internal space is available
1023 When choosing electrical equipment the expected environmental conditions such as humidity heat cold andvibrations shall receive special consideration In addition the following applies
10231 In general acceleration of 07 g in the frequency range from 13 to 100 Hz shall also be taken intoaccount as regards design and mounting
10232 Plug-in cards with electronic controls may have to have extra fastenings
1024 Where special circuits for lighting standstill heating etc are fed through separate power supply switches sothat they can also be operated when the main supply to the lifting appliance is switched off special measuresshall be taken in the switchgear to prevent direct contact with live parts A double feed shall be indicated bylabels
1025 For supply lines fixed laid to shipboard lifting appliances including the external fixed cabling marine cableshall be used as per DNVGL-RU-SHIP Pt4 Ch8
1026 An adequate power supply shall be provided on board or if applicable onshore Onshore power supply shallbe adapted to the supply system onboard
103 Drives and brakes
1031 Driving power
10311 All motors shall be dimensioned in accordance with their envisaged purpose and expected use
10312 In the case of shipboard lifting appliances the working speeds laid down for the safe working loadshall be maintained also at the vessels prescribed minimum inclinations
10313 The required power for winches is calculated from the rated pull and the rated rope speed of thefirst layer of rope on the drum taking gearing efficiency into account
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DNV GL AS
1032 Winch drivesFor winch drives the following operating modes Si are defined
10321 For drives up to about 5 t SWL started very frequently (about 160-400 starts per hour) with shortload travel and lifting periods duty type S5 ie intermittent periodic duty with electric braking with thestarting process and electrical braking influencing the heating-up of the motor
10322 For drives with long load travel and lifting periods and less frequent starts (up to about 160 startsper hour) duty type S3 ie intermittent periodic duty without the starting and braking processes having anynoticeable effect on the heating-up of the motor
10323 For heavy loads with prolonged load handling and lengthy intervals duty type S2 ie short-timeduty with an ensuing interval long enough for the driving motor to cool down approximately to the ambienttemperature Preferred duration of duty is 30 min
10324 In the case of hydraulic drives the electric motors driving the pumps shall be matched to the givenconditions Possible operating modes are S1 (continuous running) or S6 (continuous operation periodic duty)In the case of mode S6 particular regard shall be paid to the mode of operation of the hydraulic unit egthe power required during idling
10325 The driving motors shall be capable of running-up at least 13 times against the rated torqueWhen designing the motors the moment of inertia of the gearing shall be taken into account The moment ofinertia of the driven masses shall be based on an inertia factor FJ of at least 12
10326 The duty types S1 to S3 S5 and S6 are defined in IEC 60034-1 In addition the following applies
103261 When operating in type S5 at least 160 starts per hour shall be possible This is based on theassumption that 50 of the starts will be without load
103262 Where the requirements are more stringent than [103261] the drives shall be designed for240 320 or 400 starts per hour
10327 For operating modes S5 and S3 differing duty times shall be assumed depending on the serviceconditions For the operating steps a total operating period of 25 of the overall total shall be considered Inaddition the following applies
103271 In the case of more stringent requirements than given in [10327] (shorter intervals betweenthe separate hoisting operations) duty times of 40 60 or 75 shall be chosen
103272 In the case of pole changing motors where all the speed steps are designed for the rated loadand where generally the top speed step is reached by switching through the individual lower steps theoverall operating period shall be shared out between the individual switching steps
103273 If one of the speed steps is intended for light-hook operation only the overall operating periodapplies only to the operating steps However the light hook step shall be designed for at least 15 of theoverall operating period
1033 Brakes
10331 The frequency of operation of the brakes shall correspond to that of the associated motor It isassumed that when operating braking will only ever be effected from a low-speed stepThe braking equipment shall function automatically and arrest the load with the minimum possible impact
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DNV GL AS
10332 Winches shall as a matter of principle be equipped with safety brakes which brake the load safelyat any speed if the power supply fails
104 Cables and lines
1041 Supply line
10411 As a matter of principle power shall be supplied via suitable cables possibly using cable trolleys orcable drums with integral slip ringsAll cables and lines shall be flame-resistant and self-extinguishing Furthermore all cables shall be approvedby the Society possibly UV-radiation resistant and where hydraulic systems are concerned oil resistant
10412 Devices eg cable drums introduced to prevent the lines dragging on the floor during operationshall be designed in such a way that the inner bend radius of the cables does not remain under the followingvalues unless otherwise stated by the cable maker
mdash in the case of cables with an external diameter up to 215 mm five (5) times the cable diametermdash in the case of cables with an external diameter exceeding 215 mm 625 times the cable diameter
1042 Wire cross-sections
10421 Dimensioning shall take the load into account possibly giving consideration to an utilisation factorand the expected ambient temperature
10422 For lifting appliances with only one driving motor particularly with electro-hydraulic drive systemsthe power supply shall be dimensioned as appropriate to the rated current at the maximum operating stagefor continuous operation
10423 For lifting appliances with several motors for calculation of the amperage 100 of the powerof the hoisting unit motor plus 50 of the power of all remaining drives may be used as a basis Theamperage resulting shall be applied as the continuous operation valueThese values also apply to the dimensioning of slip ring bodies and brushes
1043 Laying of cables10431 General
104311 Fastening for cables shall measure up to the vibrations expected during lifting appliance operation
104312 Cables suspended from cable trays or running vertically shall if secured by means of plasticstraps as a matter of principle also be fastened in this area with corrosion-resistant metal clips or metalstraps at intervals of at least 1 m where they pass from one tray to another
104313 Openings for passing through cables shall be deburred and lined so that the cable sheathingcannot be damaged by sharp edges
104314 Leakage of hydraulic oil into control cabinets switchgear and cable boxes shall be avoidedtherefore wherever practicable cables shall be introduced into the boxes or cabinets from below Wherethey are introduced from above they may have to be additionally sealed in areas exposed to the risk of oilleakage in an appropriate way
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DNV GL AS
10432 Cable trays
104321 Cables shall be laid on adequately strong corrosion-resistant cable trays Exceptions to this arepossible when laying single cables eg to light fittings
104322 Cable trays shall be arranged so that hydraulic oil from hydraulic systems cannot drip onto thecables Where this is not possible oil guards shall be provided
10433 Cable bundles
104331 In revolving cranes or in swing cranes with a limited slewing range all circuitssupply lines maybe led in via flexible cable bundles suitably arranged in the rotational centre of the crane column
104332 Suspended cable bundles shall be appropriately led at both ends over curved cable trays with aradius of curvature not less than 10 times that of the thickest cable and fastened there in such a way thatthe weight of the bundle is distributed as evenly as possible over all the cables depending on their size
104333 Cable bundles shall not strike or rub against anything during slewing and in the event ofmovement of the lifting appliance lifting appliance parts or the ship
1044 Cable drums and cable trolley trays
10441 Drum-wound cables shall be dimensioned in such a way that even with the cable fully wound onand under normal operating power load the cable does not heat up beyond its permitted limit
10442 For cable trolleys minimum bend radii are as follows
mdash cable up to 8 mm outside diametermdash three (3) times the conductor diametermdash cable up to 125 mm outside diametermdash four (4) times the conductor diametermdash cable over 125 mm outside radiimdash five (5) times the conductor diameter
10443 In the case of flat cables the thickness of the cable corresponds to the outside diameter of roundcables
105 Switches
1051 Crane main switchescrane circuit breakers
10511 Shipboard lifting appliances shall be fitted with a manually operated circuit breaking device withwhich all movement can be stopped It shall be possible to isolate all the electric equipment from the mainsusing the circuit breaking device The circuit breaking capacity shall be sufficient to switch off simultaneouslyboth the power of the largest motor when stalled and the total power of all other consumers in normaloperationThe off-position shall be capable of being locked The off position shall only be indicated after havingreached the prescribed air and creepage distances The circuit breaking device shall only have one on andoff position with dedicated arresters
10512 A circuit breaking device may also be used as a load switch if it permits the maximum short-circuit power to be switched off safely Dimensioning shall be carried out in accordance with IEC Publication60947-4-1 Type 2
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DNV GL AS
10513 In the case of electro-hydraulic lifting appliances the load switch shall also switch off power to thehydraulic pump motor(s)
1052 Limit switches
10521 The control circuits of the safety limit switches shall be designed on the closed-circuit currentprinciple or shall be self-regulating
10522 In the case of automated or programme-controlled motion processes (including use ofmicroprocessor systems) the continued safe functioning of movement limitation systems shall be ensuredeven in the event of a fault or malfunction in the computerThis may be achieved by using separate control elements or additional main frame independent electronicunits insofar as these have been approved by the Society and the switching has been qualified as safe bythe Society as regards its safety aspect (fault elimination assessment)
10523 In programme-controlled movement processes limit switches may not be used for operationalspeed or movement measurement
10524 Where the hazard analysis has shown that a second movement limiter shall be provided failure ofthe first limiter shall be indicated to the crane driver
106 Protective measures and safety devices
1061 Protective measures
10611 In general the operating voltage for motor drives should not exceed 690 volts and for controlsheating and lighting systems 250 volts Insulation shall be all-pole
10612 All equipment with a working voltage exceeding 50 volts connected via movable cable shall beearthed via a protective conductor inside the cable The following shall be observed
106121 For cable cross-sections up to 16 mm2 its cross-section shall match that of the main conductorsfor those exceeding 16 mm2 it shall be at least half that of the main conductors
106122 If power is supplied via slip rings the protective conductor shall be provided with a separate slipring
10613 Any non-earthed conductor shall be provided with overload and short-circuit protection inaccordance with DNVGL-RU-SHIP Pt4 Ch8
10614 For motors monitoring of the winding temperatures is recommended as protection againstinadmissible heating If the admissible temperature or load is exceeded power shall be switched off Switch-off due to thermal overload should be indicated Lowering of the load shall be still possible after the electricdrive has been switched off due to overheating
10615 Switches switchgear and control cabinets shall be located in such a way that work on them andoperational tests can be performed safely For arrangements inside the crane column gratings or platformsshall be provided
10616 The service passage in front of switchgear and control cabinets shall not be less than 05 m widewith 180 m headroom If this headroom cannot be maintained it may be reduced to 140 m if the passageis at least 07 m wide
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DNV GL AS
10617 As a minimum the following protective systems (contact- foreign body- and water protection)shall be provided
106171 For electrical installations below deck or in the enclosed spaces of shipboard lifting appliances theprotective system shall be at least IP 44 in dry spaces at least IP 20
106172 For electrical installations on deck the protective system shall be at least IP 56 under certaincircumstances eg where there is a heightened risk of dust even IP 66
10618 Where required electrostatic discharges shall be prevented by earthing andor connection ofmetallic components
10619 Control stands crane drivers cabins and hand-operated equipment shall be fitted withmechanically locked emergency shut-down switches or push-buttons See also the requirements given in[1243]
106110 Motors in particular for lifting and luffing gear shall be selected and protected in such a way thatin the event of power failure they do not overspeed in the time before the brakes respondEven after the response of the overspeed protection device the speed limits shall not be exceeded
106111 Electrical appliances which are employed in areas with a potentially explosive atmosphere shallcomply with the requirements given in respective international or national regulations regarding explosionprotection eg the directive 949EG and IEC 60079
1062 Safety devices10621 Controls
106211 Control handles shall be constructed in such a way that at the least the stop position engageswithout fail In systems with pole-changing motors a separate notch shall be allocated to each speed stepWhen the control handles are released they shall automatically move to the stop position
106212 Following failure of the electric power supply and when this is restored or following operationof the emergency switch-off button or push-button restarting the drives shall only be possible via the stopposition
106213 Where winch motors are provided with a speed step designed for light-hook operation only thecontrol mechanism shall automatically prevent this step operating when there is a load on the hook This alsoapplies to other part-load operating steps
106214 Radio controls programmed control mechanisms or microprocessor systems shall have been typetested by the Society Alternatively their operational safety may be proved in a different way recognized bythe Society
10622 Lighting
106221 In addition to an adequate main lighting system for the lifting appliance working area anemergency lighting system shall be provided for the cabin and the area of descent where crane columns arehigher than 10 m in the cabin at the crane column and at the switch gear and machinery
106222 Emergency lighting systems should be guaranteed to last about 30 min and shall preferably beconnected to the emergency power supply As an alternative the Society may approve a battery-operatedemergency power supply
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DNV GL AS
106223 Where emergency lighting is powered by batteries the emergency power supply chargers forthese lamps shall be connected to a separate circuit not switched off by the load-circuit switch
107 Assessment of drawings and manufacturing survey
1071 Assessment of drawings
10711 The general requirements given in Sec13 shall be observed
10712 In addition to the requirements given in Sec13 the electrical equipment listed in Table 2-1 aresubject to assessment of drawings in the scope indicated there
1072 Manufacturing survey10721 General
107211 Electrical equipment shall be manufactured by qualified staff handling the necessary installationsand devices During manufacture and before delivery the parts shall undergo the quality tests required inaccordance with state-of-the-art technology and experience
107212 Electrical equipment which requires a Societys product certificate according to Table 2-2 to Table2-4 is subject to manufacturing survey by the Society where requiredThe Society inspection in charge decides in conjunction with the manufacturer on type and scope ofmanufacturing survey and certification taking into consideration the in-house quality control andor approvalfor productionWith respect to assistance by the manufacturer during manufacturing survey by the Society therequirements given in [1322] shall be observed
10722 Tests and examinationsThe following requirements contain general test requirements and in addition provisions for themanufacturing survey by the Society
107221 GeneralFor the acceptance tests before delivery and if applicable also for the manufacturing survey the Societyssurveyor shall receive certificates for material tests and internal controls test reports and manufacturingdocuments in particular approved drawings including the allocated design approval letter if requiredaccording to Table 2-2 to Table 2-4 as a prerequisite for the tests and examinations described belowTest reports shall include the following information if applicable
mdash designation of type and nominal dimensionsmdash purchase and order numbermdash drawing numbermdash results of internal controlsmdash certificate numbers of material tests and non-destructive testsmdash additional details as necessary
For series-production electrical equipment other test procedures may be agreed with the Society instead ofthe prescribed ones if they are accepted as equivalentWhere electrical equipment shall be used for the intended purpose for the first time the Society may ask fora type approval
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DNV GL AS
107222 Electrical equipmentElectrical equipment shall be tested according to DNVGL-RU-SHIP Pt4 Ch8 and to undergo a functional testif possible
108 Documentation
1081 Marking
10811 Any electrical equipment shall be marked by the manufacturer in a suitable way The marking shallat least include the following information if applicable
mdash manufacturers namemdash year of constructionmdash designation of typemdash purchase order number or serial numbermdash characteristics such as nominal speed nominal voltage etcmdash additional details as necessary
10812 If after the acceptance test and before delivery the requirements for issuing a Societys productcertificate are complied with the electrical equipment will be stamped in a prominent positionThe stamp shall include the following information
mdash certificate number together with the code letters of the examining inspecting officemdash stamp with the month and year of testing
1082 Certificates
10821 Table 2-2 to Table 2-4 show the required types of certificate for essential electrical equipmentThe lifting appliance manufacturer shall order the stated equipment together with the required certificatesand the equipment manufacturer shall include them in the delivery
10822 The certificates listed in Table 2-2 to Table 2-4 are not part of the ILO lifting appliancedocumentation on board and shall not be filed in the CG1
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DNV GL AS
SECTION 11 CONSTRUCTION OF STEEL COMPONENTS
111 General
1111 This section contains requirements for the construction of steel components for shipload lifting appliancesand load-handling devices with a special focus on welding
1112 Complementary or more comprehensive requirements and special details shall be taken from the following
mdash DNVGL-RU-SHIP Pt3mdash DNVGL-RU-SHIP Pt2mdash recognized standards or regulations
1113 The requirements given in Sec1 shall be observed where relevant
1114 With respect to materials to be used the requirements given in Sec3 apply
112 Requirements for manufacturers
1121 General requirements
11211 Manufacturers shall be equipped with installations and devices suitable for professional and properhandling of the individual materials manufacturing methods components etcThe Society reserves the right to check the production shop in this respect and to impose requirementsconcerning this matter or to reduce the scale of operations according to the capabilities of the productionshop
11212 The manufacturer shall have a sufficiently qualified staff of experts The supervising and controllingpersonnel shall be indicated to the Society including their areas of responsibility The Society reserves theright to ask for certified proof of qualifications
1122 Quality control
11221 By means of an effective internal quality control the manufacturing works shall ensure thatconstruction and assembly comply with this standard the approved documents (drawings specificationsetc) or with the conditions stated in the approvals
11222 It is the responsibility of the manufacturing works to observe this standard and to meet the specialrequirements associated with the assessment of documents or the conditions imposed with the approvalExaminations carried out by the Society do not release the manufacturing works from this responsibility
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DNV GL AS
11223 It is the responsibility of the manufacturing works to make sure that production conditions andquality correspond to those of the approval test The Society cannot take any responsibility that productscomply with this standard which have been tested in an approval test or at random during production in allparts or during the entire production process
11224 The Society may reject further use of products processes etc which have proved unsatisfactoryduring application in spite of an earlier satisfactory approval test and may demand they be improvedincluding proper verification
1123 Workmanship11231 Details in the production documents
112311 The production documents (workshop drawings etc) shall include all those details which areessential for quality and functional capability of the component under consideration This includes ndash besidesdimensions ndash eg details on tolerances surface finish quality (reworking) special production processes aswell as tests and requirements as appropriate
112312 All the important details of the welding eg the types of base material configuration anddimensions of the welds welding method welding consumables heat treatment tests to be performed andany special requirements imposed shall be indicated in the production documents (drawings parts listsetc) In special cases the Society may require submission of a welding schedule
112313 Where quality or functional capability of a component is not assured or dubious the Society mayask for suitable improvements This also applies as and where relevant to complementary or additional (egstrengthening) components even if these were not required for the assessment of drawings or were notrequired due to poorly detailed presentation
11232 Cut-outs edges of plates
112321 Openings boreholes and other cut-outs shall be rounded with a sufficiently large radius
112322 The face areas (cut areas) of cut-outs shall be finished cleanly and without notches Notchesand the like due to flame-cutting shall not in general be repaired by welding but shall be ground into a flattrough Edges shall be broken or in cases of very high loads rounded
112323 Exposed edges of plates or flanges cut by flame-cutting or a shearing machine shall not besharp-edged and shall be reworked where required as stated in [112322] just as notches and the likedue to flame-cutting This applies as and where relevant to welded joints transitional sections or similardiscontinuities
11233 Cold forming
112331 Where plates are formed at low temperatures (bending flanging beading) the inner bendingradius ri should not fall below 3∙t (t = plate thickness) it shall however be at least 2∙t These values referonly to ship hull structural steels and comparable structural steels without welding in the cold formed areas
112332 Before cold forming flame- or shear-cut burrs shall be removed in order to avoid cracksFollowing cold forming the components in particular the lateral ends of bent plates (plate edges) shall bechecked for cracks Affected components shall be disqualified (minor cracks excepted) Repair by welding isnot permitted
112333 Forming of plates structural shapes tubes etc shall be carried out according to a specificationoutlining the successive and controlled steps Forming of steel above 650degC shall be subject to agreement(adverse effects on material properties)
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DNV GL AS
11234 Assembly straightening work
112341 During assembly of single components excessive force shall be avoided If possible majordeformations of single components shall be straightened prior to further assembly
112342 Girders stiffeners and the like which are interrupted by transverse components shall beassembled in a well aligned manner If necessary on essential components control bores shall be made forthis purpose which shall be welded closed again afterwards
112343 Straightening works ndash after completion of welding works ndash shall be conducted in such a way thatno noticeable deterioration of material properties takes place In case of doubt the Society may require atype approval or production test samples
11235 Corrosion protection
112351 All steel components shall be provided with suitable corrosion protection For shop primer see[11514] and [11515]
112352 Hollow spaces eg box girders tubular pillars and the like which are demonstrably or by generalexperience permanently air-tight need not be preserved internally During assembly the hollow spaces shallbe clean and dry
112353 The wall thickness of load-bearing parts shall be at least 4 mm Lower wall thicknessrsquos are subjectto the consent of the Society in each individual case
112354 Welded-on reinforcing rings shall be protected against rusting underneath
112355 Bolts nuts and associated elements shall be protected by hot-dip galvanizing according torelevant standards ie BS 729 or ASTM A 153-82 Alternatively they may be fully encapsulated and theopen space be filled with inhibited oil grease etc Other protection methods may be accepted upon specialconsideration by the SocietySpring washers of corrodible materials shall not be used if exposed to the marine atmosphere
1124 Conditions for welding11241 Approval to weld
112411 All works including subcontracting firms wishing to carry out welding operations on parts ofshipboard lifting appliances and load-handling devices shall have at their disposal the necessary equipmentand qualified personnel and be approved by the Society for this work see DNVGL-RU-SHIP Pt2
112412 Approval for fabrication shall be applied for from the Society with the appropriate documentationExisting approval by other independent testing institutions may be taken into account if the relevantdocuments are submitted
112413 The works shall have at their disposal the necessary workshops equipment machinery anddevices to carry out the welding work properly This includes also eg stores and drying equipment for thewelding consumables and auxiliary material equipment for preheating and for heat treatment test meansand equipment as well as weather-protected areas for the outdoor execution of welding works
112414 The works shall have at their disposal qualified welders or staff sufficiently trained for handlingfully mechanical or automatic welding installations In addition they shall have at their disposal qualifiedwelding supervisorsinspectors responsible for the professional execution of the welding tasks
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DNV GL AS
112415 The suitability of the welding method used in conjunction with the materials in question shall beproved to the Society in an appropriate way The Society may to this end require method checks (test weldsnon-destructive and mechanical-technological tests) in presence of the Societys surveyor
112416 The (non-destructive) testing of weld connections shall be conducted by appropriately qualifiedtesters following a suitable test procedure The Society may demand a test of ultrasonic testers in presenceof the Societys surveyor The scope of tests shall be indicated in the test documentation The test reportsshall be submitted to the Society
11242 Welders
112421 Welders for manual or semiautomatic welding shall be examined according to recognizedstandards (eg EN 287 or ISO 9606 or ASME Section IX) Regarding the welding method base materialwelding consumable and welding position and the test shall cover the conditions of the type of productionenvisaged
112422 A welders qualification test remains valid for two years with effect from the test date providedthat during this period welding work is constantly performed in the range of approval of the test and the workof the welder is monitored by the welding supervisorsinspectors at all times
112423 The required number of qualified welders depends on the size of the works and the scope ofwelding tasks in presence of the Societys surveyor At least two qualified welders are required per weldingmethod
11243 Supervision of welding
112431 Every work carrying out welding shall employ its own welding supervisorinspector Thissupervisorinspector shall have a suitable deputy in the welding shop The welding supervisorinspector shallbe responsible for supervising the preparation and execution of the welds and if applicable their testing
112432 Welding supervisorsinspectors shall have training and the experience appropriate to theproduction requirements and furnish the necessary proofs to the SocietyAccording to the nature and scope of the welding work performed the supervisory function may be exercisedby a welding engineer (welding engineering specialist or comparably trained engineer) a welding expert orsome other person with adequate specialist qualifications
112433 The names of the responsible welding supervisorsinspectors and their deputies shall be madeknown to the Society
112434 Changes in the personnel responsible for supervising welding shall automatically be reported tothe Society
11244 Welding consumables auxiliary materials
112441 Welding consumables type approved by the Society or accepted based on welding procedure testsshall be used
Guidance noteWelding consumables type approved by the Society are recommended The type approved welding consumables are listed oninternet httpsapprovalfinderdnvglcom
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112442 For highly stressed components and parts stressed at low temperatures for high- and extra highstrength steels steel castings and forgings and for low-temperature welding work hydrogen-controlledwelding consumables and auxiliary materials are preferable
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DNV GL AS
112443 Welding consumables and auxiliary materials for special materials may also be tested andapproved together with the welding method Such approvals are however restricted to the userrsquos works andremain valid for at most one year unless repeat tests are performedWelding consumables and auxiliary materials jointly tested in this way may be replaced by other equivalentmaterials approved for the application in question
11245 Welding methods procedure tests
112451 Only those welding methods may be employed whose suitability for the application in question haseither been established by general practice or proved by a procedure test
112452 Procedure tests for the purpose of proving the satisfactory application of the procedure in thewelding shop and adequate quality of the results obtained shall be performed under production conditionson the premises of the company using the method in all cases where materials other than normal-strengthshipbuilding steels A to D or comparable structural steels forging steels and types of casting steel shallbe welded or welding methods other than manual arc welding (E) or partly-mechanised inert gas shieldedwelding (MAG) shall be employedProcedure tests shall also be performed where these processes are applied in a special manner eg in single-side welding using a (ceramic) weld pool support see DNVGL-RU-SHIP Pt2 Ch4 Sec5 [22]
112453 The scope of the test the samples the test specimens and the requirements shall be determinedfrom case to case depending on the proposed application in general accordance with DNVGL-RU-SHIP Pt2Ch4 Sec5 Account may be taken of procedure tests carried out elsewhere (on submission of the reports)
Guidance noteAs alternatives to the requirements given in [112453] the following standards will be accepted
mdash ASW D11
mdash EN ISO 15614-1 (for steel)
mdash EN ISO 15614-2 (for aluminium)
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112454 Welders employed for procedure tests are on successful completion of the test deemed qualifiedfor the procedure employed or the materials concerned
113 Design details
1131 General
11311 The materials selected for the design shall in every respect be appropriate to the designrequirements the production and the intended useIf necessary special measures shall be adopted
11312 The design of the structure shall achieve a power flow as undisturbed as possible without localdiscontinuities and steps in rigidity and to be suitable for construction and meet the requirements for long-lasting and reliable operation
11313 The following requirements refer only to welded joints For the design of screw joints therequirements given in [482] apply
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DNV GL AS
1132 Configuration of welded joints11321 Welded joints in general
113211 Welded joints shall be planned in such a way as to ensure that they are readily accessible duringfabrication and can be executed in the optimum welding position and welding sequence
113212 Welded joints and welding sequences shall be designed to minimize residual weld stresses andavoid excessive deformation Welded joints shall therefore not be over-dimensioned
113213 All welded connections shall be configured to achieve a power flow as undisturbed as possiblewithout major internal or external notches or rapid changes of rigidity and without impeding expansion
113214 The requirements given in [113213] apply as and where relevant to the welding of secondarycomponents on primary structures too the highly stressed areas of which and the exposed plate or flangeedges of which shall be kept free from notches caused by welded joints if possible
113215 Welded joints shall be designed to ensure that the proposed weld type and quality (eg completeroot fusion in the case of single- and double-bevel butt welds) can be satisfactorily achieved under the givenfabricating conditions Failing this provision shall be made for welds which are easy to execute and their(possibly inferior) load-bearing capacity shall be allowed for when dimensioning the welds
113216 Welded joints in girders and profiles (especially field joints) shall not if possible be located in anarea of high stresses Welded joints on flanges with cold formed bending positions shall be avoided
113217 Highly stressed welded joints which are therefore normally subject to compulsory inspectionshall be designed to facilitate application of the most appropriate inspection technique (radiographyultrasonic or surface crack inspection possibly in combination) so that tests offering reliable results can becarried out
11322 Welded nodes in tubular structures
113221 Depending on tube wall thickness and angle of intersection nodes linking relatively small tubeseg in tubular-frame crane jibs may be designed either in the form of fillet welds or of single-bevel welds asin [11424]
113222 The nodes of relatively large tubes where the wall thickness of the branches exceeds about 8mm shall be designed in the form of full-penetration single bevel welds as shown in Figure 11-1 Where thestress is lower single-bevel welds with a backing strip as in [11424] may also be used
113223 The weld configuration chosen and the effective weld thickness shall be taken into account in thedimensioning (especially in the proof of fatigue strength) and shown in detail on the drawings Where proofof fatigue strength is required the quality of surface finish required shall also be specified on the drawings
11323 Transitions between differing dimensions
113231 Differing dimensions shall be made to match gradually by means of gentle transitions Wheregirders or sections have web plates of different heights the chords or bulbs shall be brought to the sameheight by tapering or by slitting and splaying or reducing the height of the web plate The transition lengthshall be three times the difference in height
113232 Where the joint is between plates of differing thicknesses thickness differences of more than 3mm (see Figure 11-2) shall be evened out by bevelling the extending edge with a 13 slope or in accordancewith the notch Thickness differences of less than 3 mm may be evened out within the weld
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DNV GL AS
113233 For connection to plates or other relatively thin-walled elements steel castings and forgingsas shown in Figure 11-3 shall be provided with matching tapered elements or cast or forged-on weldingflanges respectively
11324 Localised closely grouped welds minimum spacing
113241 Local close grouping of welds and short distances between welds shall be avoided Adjacent buttwelds shall be separated by at least
50 mm + 4 times plate thicknessFillet welds shall be separated from each other and from butt welds by at least
30 mm + 2 times plate thickness
113242 The width of plate areas (strips) subject to replacement shall however be at least 300 mm or 10 timesplate thickness whichever is the greater
113243 Reinforcing plates welding flanges hubs or similar components welded into plating shall have thefollowing minimum dimensions
Dmin = 170 + 3 (t ndash 10) ge 170 mm
Dmin = minimum diameter of round or length of side of polygonal weld-on parts [mm]t = plate thickness [mm]
The corner radii of polygonal weld-on parts shall be at least 50 mm
Figure 11-1 Single-sided weld connections (tube connections not accessible from inside)
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DNV GL AS
Figure 11-2 Accommodation of different thickness
Figure 11-3 Welding flange on steel castings or forgings
11325 Welding cut-outs
113251 Welding holes for (subsequent) butt or fillet welding following the fitting of transverse parts shallbe rounded (minimum radius 25 mm or twice the plate thickness whichever is the greater) and (especiallywhere the loading is mainly dynamic) shall be provided with ldquogentlerdquo run-outs and appropriately notch-freecircumferential welds see Figure 11-4
113252 Where joints are fully welded prior to the fitting of transverse parts no welding holes are neededprovided any weld reinforcement is machined away before fitting
Figure 11-4 Welding cut-outs
11326 Local reinforcements doubling-plates
113261 Where plating is subject to locally increased loading (eg girder or pipe walls) thicker plates shallwherever possible be used rather than doubling-plates As a matter of principle bearing bushes hubs etcshall take the form of thicker welded-in plating regarding this see also [11243]
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DNV GL AS
113262 Where doubling-plates cannot be avoided they shall not be thicker than twice the plate thicknessDoubling-plates wider than about 30 times the doubling-thickness shall be welded to the underlying platingby welding with cut-outs at intervals not exceeding 30 times the thickness of the doubling-plateWhen welding with cut-outs these shall preferably be designed in form of elongated holes lying in thedirection of the principal stress
113263 Doubling-plates shall be welded along their (longitudinal) edges by continuous fillet welds with athickness
a = 03 times thickness t of the doubling-plateAt the ends of doubling plates as shown in Figure 11-5 thickness a along the terminal edges shall be
a = 05 times thickness t of the doubling platethough it shall not exceed the plate thicknessThe weld transition angles between the terminal edge and the plating shall be 45deg or less
Figure 11-5 Weldings at the ends of doubling plates
Where proof of fatigue strength is required the configuration of the end of the doubling plate shallcorrespond with the detail category selected
11327 Welding in cold-formed areas
113271 Welding is permitted at and close to cold-formed structural areas provided that the followingmaximum degrees of cold deformation are not exceededThe degree of cold deformation of special and primary structural elements shall be less than 5 (ri ge 10 xplate thickness) for carbon-manganese steel and less than 20 (ri ge 2 x plate thickness) for austenitic andferritic-austenitic steelFor carbon-manganese steels the allowable inside bending radius may be reduced below the above valuesFor additional requirements see DNVGL-RU-SHIP Pt3 Ch3 Sec1 [273]
Guidance noteWelding of cold formed hollow sections made of normal and high strength steel with increased degree of cold deformation might bepermitted providing acceptance of the respective profile standard Special consideration shall be taken for the risk of cold crackingin the welded zone eg reduce level of diffusible hydrogen in the weld material preheating In general hot formed hollow sectionsare recommended
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
113272 For extra high strength steels the necessary minimum bending radius shall in case of doubt bedetermined by qualification tests or be given by the steel manufacturer
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DNV GL AS
11328 Bend reinforcements
113281 Bent structural elements eg the chords of girders where the change of direction means thatforces are generated or shall be transmitted perpendicular to the bend shall be adequately supported at thebending location The conditions set out in [113271] shall be complied with
113282 Where welded joints at bending locations cannot be avoided three-plate welds generally as in[11426] may be used Such connections shall be depicted in detail on the drawings
114 Types of weldsThe chosen type of weld shall be suitable and sufficiently dimensioned or favourably designed to transfer thetype (static dynamic) and magnitude of forces
1141 Butt joints
11411 Depending on plate thickness welding procedure and -position butt welds shall take the form ofsquare single- or double-V welds (X welds) in conformity with the standards (eg EN 12345 EN 22553ISO2553 EN ISO 9692-1 -2 -3 or -4)
11412 Where other forms of weld are envisaged these shall be depicted specially in the drawings Weldgeometries for special welding processes (eg submerged-arc single-side and electro-gas or electro-slagwelding) shall have been tested and approved as part of a procedure test
11413 Butt welds shall as a matter of principle be grooved out on the root side and given at least onecapping pass Exceptions to this rule eg in the case of submerged-arc welding or the aforementionedprocesses also require to be tested and approved as part of a procedure testThe theoretical throat shall be the thickness of the plate or where the plates are of differing thicknessthe lesser thickness Where proof of fatigue strength is required the detail category depends on theconfiguration (quality) of the weld
11414 If the above conditions cannot be fulfilled eg where welds are accessible from one side only opensquare-edge joints with back-up bars or permanent machined or integrally cast backing as in Figure 11-6shall be usedThe calculated weld thickness may be taken as 90 of the (lesser) plate thickness t maximum (t-1) mmWhere proof of fatigue strength is required these welds shall be placed in the corresponding detail category
Figure 11-6 Single-side welds with permanent weld pool supports (backings)
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DNV GL AS
1142 Corner- T- and double-T- (cross) welds
11421 Full-penetration corner- T- and double-T- (cross) welds for the full connection to the abuttingplates shall take the form of single- or double-bevel joints with the minimum possible shoulder and anadequate gap as shown in Figure 11-7 The root shall be grooved out and welded from the reverse side
Figure 11-7 Single- and double-bevel welds with full root penetration
The theoretical weld thickness shall be the thickness of the abutting plate Where proof of fatigue strength isrequired the detail category depends on the configuration (quality) of the weld
11422 Corner- T- and double-T- (cross) welds with a defined root defect f as shown in Figure 11-8 shalltake the form of single- or double-bevel welds as described in [11421] with reverse-side welding butwithout grooving-out of the root
Figure 11-8 Single- and double-bevel welds with defined incomplete root penetration
The theoretical weld thickness may be taken as the thickness t of the abutting plate minus f being equal to02 t up to a maximum of 3 mm Where proof of fatigue strength is required these welds shall be placed inthe corresponding detail category
11423 Corner- T- and double-T- (cross) welds with an unwelded root face c and a defined incomplete rootpenetration f to be taken into consideration shall take the general form shown in Figure 11-9
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DNV GL AS
Figure 11-9 Single- and double bevel welds with an unwelded root face and a defined incompleteroot penetration
The theoretical weld thickness shall be the thickness t of the abutting plate minus (c + f) f being equal to02 t up to a maximum of 3 mm Where proof of fatigue strength is required these welds shall be placed inthe corresponding detail category
11424 Corner- T- and double-T- (cross) welds accessible from one side only may as shown in Figure11-10 be made either as butt joints with a weld pool support analogous to those described in [11414] oras one-sided single-bevel welds analogous to those in [11422]
Figure 11-10 Single-side welded T-joints
The theoretical weld thickness shall similarly be determined in accordance with [11414] or [11422]Where proof of fatigue strength is required use of these welds shall be avoided if possible
11425 In the case of flush corner joints ie where neither of the plates projects joint configurations asshown in Figure 11-11 shall be used with bevelling of the plates shown as upright to avoid the danger oflamellar rupture (stepwise cracking)
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DNV GL AS
Figure 11-11 Flush fitted corner joints
11426 Where in T-joints the main stress acts in the plane of the plates shown in the horizontal position inFigure 11-12 (eg in plating) and the connection of the vertical (edge-on) plates is of secondary importancethen (except in the case of mainly dynamic stresses) three-plate welds as shown in Figure 11-12 may beusedThe theoretical weld thickness of the joint connecting the horizontal plates shall be determined in accordancewith [11413] The required a dimension is determined by the joint connecting the vertical (edge-on)plate and shall where necessary be ascertained by calculation as for fillet welds
Figure 11-12 Three-plate welds
1143 Fillet welds
11431 Fillet welds shall as a matter of principle be made on both sides Exceptions to this rule (eg inthe case of closed box girders and in the case of primary shear stress parallel to the weld) require approvalin every instance The thickness a (the height of the inscribed equilateral triangle) shall be determined bycalculationThe leg length z of a fillet weld see Figure 11-13 shall not be less than 14 times the fillet weld thicknessa
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DNV GL AS
11432 The thickness of fillet welds shall not exceed 07 times the lesser thickness of the parts to bewelded (generally the web thickness) The minimum thickness is defined by
amin = [mm] (but not less than 3 mm)
t1 = the lesser plate thickness [mm] (eg the web thickness)t2 = the greater plate thickness [mm] (eg the chord thickness)
11433 The aim with fillet welds shall be to have a flat symmetrical cross-section with good transitionto the base metal Where proof of fatigue strength is required it may be necessary to carry out machining(grinding-out the notch) depending on the detail category The weld shall extend at least to the immediateproximity of the theoretical root point
11434 Where mechanical welding processes are used which produce a deeper penetration going wellbeyond the theoretical root point and capable of being reliably and uniformly maintained under productionconditions it is permissible to take account of the deeper penetration when determining the fillet weld throatThe mathematical dimension
shall be determined by reference to the configuration shown in Figure 11-13 and shall take into accountthe value of min e which shall be established for each welding procedure by a procedure test The weldthickness shall in relation to the theoretical root point not be less than the minimum thickness for filletwelds specified in [11432]
Figure 11-13 Fillet welds with increased penetration
11435 Depending on the welding technique used an increase of the a dimension of up to 1 mm maybe stipulated when laying down welds over production coatings particularly liable to cause porosity Thisparticularly applies when using fillet welds of minimum thickness sizeThe extent of the increase shall be determined on a case to case basis according to the nature andmagnitude of the stress based on the results of the production-coating tests according to DNVGL-RU-SHIPPt2 The same applies in turn to welding processes too in which there is a likelihood of insufficient rootpenetration
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DNV GL AS
115 Workmanship and testing of weld jointsWelding workmanship shall comply with DNVGL-RU-SHIP Pt2
1151 Weld preparation and assembly
11511 When preparing and assembling structural parts care shall be taken to ensure compliance with theprescribed joint geometry and root face (air) gaps Where the permissible root face gap is slightly exceededit may be reduced by build-up welding at the weld edges Inserts or wires are not allowed to be welded intothe gap
11512 Plates and profiles shall be aligned accurately especially where joints are interrupted by transverseparts The magnitude of the permissible misalignment of plate edges depends on the particular structuralpart the plate thickness and the stress see DNVGL-RU-SHIP Pt2
11513 In the welding zone structural parts shall be clean and dry Scale rust slag grease paint (exceptfor production coatings) and dirt shall be removed carefully prior to welding
11514 If plates profiles or structural parts are given a corrosion-inhibiting coating (shop primer) beforewelding this shall not impair the quality of the welds
11515 Only those weldable production coatings shall be applied for which the Societys report of noobjection exists based on a pore formation tendency test
1152 Protection against the weather preheating
11521 The working area of the welder shall be protected in particular for outside work against winddampness and cold In the case of submerged-arc welding special care shall be taken to protect againstdraughts When working outdoors it is recommended in any case to dry heat the weld edges in unfavourableweather conditions
11522 In low temperatures (component temperatures below 5degC) suitable measures shall be taken (egcovering large-area heating preheating in particular when welding at relatively low heat input eg with thinfillet welds or with thick-walled components) to ensure that the welding work can proceed satisfactorily Ifthe temperature drops below -10degC no further welding should be performed if possible
1153 Welding positions and sequence
11531 Welding work shall be performed in the most favourable welding position Welding in restrictedpositions eg positions PE or PD (overhead) shall be restricted to unavoidable cases
11532 Vertical downward welding of fillet welds shall not be applied to lifting appliance componentsand lifting appliances including supporting structure (eg crane columns) even after a successful weldingprocedure test
11533 Obstruction of weld shrinkage shall be minimized by the choice of a suitable construction andwelding sequence
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DNV GL AS
1154 Workmanship
11541 The welds shall have sufficient penetration and clean regular weld surfaces with soft transitionsto the base material Excessive overthickness and grooves as well as notches at the edges of plates or cut-outs shall be avoided
11542 Cracked tacks may not be welded over but shall be removed by machining In multi-pass weldingthe slag from preceding passes shall be removed completely Pores visible slag inclusions and cracks maynot be welded over but shall be removed by machining and repaired
1155 Repair of defectsRepair of major defects of workmanship may only be undertaken after agreement with the Society Thisapplies similarly to the repair by welding of worn broken or otherwise damaged parts Prior to repair work onload-bearing structural parts a sketch of the repair shall be submitted
1156 PreheatingRegarding the requirement for and amount of preheating several decisive criteria exist eg chemicalcomposition plate thickness two- or three- dimensional heat dissipation environmental or componenttemperature heat input due to welding (energy per unit length) see DNVGL-RU-SHIP Pt2
1157 Heat treatment
11571 The nature and scope of any heat treatment which may have to be applied to welded structuralparts depends on their residual stress state (weld geometry and thickness rigidity of part) and thecharacteristics of the material concerned ie its behaviour or any change in characteristics to be expectedwhen subjected to heat treatment Generally it is a matter of stress-relieving or annealing treatment Thesteelmakers directions and recommendations shall be followed
11572 Depending on the type of material concerned flash butt welds shall be subjected to normalising orquenching and tempering treatment
11573 The way in which the mechanical properties of the weld are affected by subsequent heat treatmentis one of the factors to be investigated in the weld-procedure test In addition to this the Society may call forproduction tests
11574 Any non-destructive tests required shall be carried out after heat treatment
1158 Non-destructive tests
11581 The nature and scope of non-destructive tests depends on the importance and loading of the partconcerned (its component class) and on the possible weld defects or effects on the base metal which mayarise from the welding technique position etc
11582 By way of example in Table 11-1 the tests required for the important parts of shipboard liftingappliances and load-handling devices have been compiled Additionally as a guide requirements imposed onwelded connections in the form of assessment categories according to EN ISO 5817 have been addedWelds in aluminium shall comply with ISO 10042 level B (applies for category special) or level C (applies forcategory primarysecondary)
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DNV GL AS
Where proof of fatigue strength is required the test requirements given in the detail category table usedapply The manufacturing documents (drawings welding diagram test schedule) shall contain for eachstructural component comprehensive information concerning the nature and scope of the tests required
Table 11-1 Test specifications for welded connections
Test method RequirementsCategory
of member Type of connectionVisual Magnetic
particle 3) Radiography 1) Ultrasonic 4) ISO 5817
Butt weld 100 100 100 - B
Cross- and T-jointsfull penetration welds 100 100 - 100 B
SpecialCross- and T-jointspartly penetration
and fillet welds100 100 - - B
Butt weld 100 20 20 - C
Cross- and T-jointsfull penetration welds 100 20 - 20 C
PrimaryCross- and T-jointspartly penetration
and fillet welds100 20 - - C
Butt weld 100 Spot 2) Spot 2) - C
Cross- and T-jointsfull penetration welds 100 Spot 2) - Spot 2) C
SecondaryCross- and T-jointspartly penetration
and fillet welds100 Spot 2) - - C
1) May be partly or wholly replaced by ultrasonic testing upon agreement2) Approximately 2-53) Liquid-penetrant testing to be adopted for non-ferromagnetic materials4) Ultrasonic testing shall not be used for thicknesses less than 10 mm
Remarks
mdash With the Societys consent dye penetrant testing may be used instead of magnetic particle testingmdash Deviations from the recommended assessment categories - even in respect of individual criteria - may be agreedmdash The Societys surveyor retains the right to determine or alter the position of random tests and to increase the scope
of tests particularly if there is an accumulation of defects
11583 Non-destructive tests shall be carried out by suitably qualified personnel
11584 The tests shall be carried out in accordance with accepted practice The results shall be presentedto the Societys surveyor at the latest at the acceptance testing of the components
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DNV GL AS
11585 NDT acceptance criteria for components machined after forgedcastUnless otherwise specified in this standard or approved manufacturers specification acceptance criteria fromfollowing documents can be used for NDT of machined components
mdash IACS Recommendations No68Guidelines for non-destructive examination of hull and machinery steel forgings(acceptance criteria for inspection zone I to be applied)
mdash IACS Recommendation No69Guidelines for non-destructive examination of marine steel castings(acceptance criteria for quality level 1 to be applied)
NDT testing shall be focused on critical areas Extend shall br specified by manufacturer and shall beaccording to recognized standards
Guidance noteThe objective and scope of quality control for materials material testing and documentation thereof is to verify that the relevantproperties as specified by designer and accepted by the Society are obtained
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
1159 Production tests
11591 If the manufacturing process or any subsequent (heat) treatment which may be required leadsto the expectation of a substantial change in or indeed deterioration of the properties of the material or thewelded connection the Society may stipulate production tests to prove that the mechanical qualities remainadequate
11592 Production tests during the course of manufacture shall as a matter of principle be performedwhen welding is carried out on cold-formed portions made from materials with a minimum nominalupper yield point of more than 355 Nmm2 with a wall thickness of 30 mm or more and with degrees ofdeformation of 3 permanent elongation ε and over
Elongation in the external tensile zone
r = internal bending radiust = plate thickness
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DNV GL AS
116 Assessment of drawings and manufacturing survey
1161 Assessment of drawingsFor the assessment of drawings of steel components the requirements given in Sec13 shall be observed Inaddition to the welding diagrams and test plans stated there the following applies
11611 Details on welded joints in the documents to be verified
116111 In the documents to be verified and to be submitted for approval production details shall beincluded which are relevant to the quality of the welded joint and the verification by the Society Besides thematerials and the weld geometry this requires the following information
mdash weld preparation procedure (mechanical thermal etc)mdash welding method welding positionsmdash welding consumables and auxiliary materialmdash preheating and heat conduction during welding where requiredmdash weld composition and number of layersmdash welding sequence (in special cases)mdash root side grooving (method)mdash possibly finishing (heat) treatmentmdash number and location of production specimens to be welded simultaneously if required
116112 As long as weld preparation and workmanship of the welds (in combination with approved weldingmethods welding consumables and auxiliary materials) comply with the accepted practice of weldingtechnology this standard and other recognized standards the Society may waive a special description ordetails in the test documentation
11612 Description of welded joints
116121 The description of welded joints including the gap and weld geometry shall eg comply with thestandards EN 12345 EN 22553ISO 2553 EN ISO 9692-1 -2 -3 or -4 The designations in the documentsto be verified (drawings etc) shall be well-defined eg by standard symbols
116122 Deviating weld geometries or symbols in the documents to be verified (drawings weldingdiagrams or specifications) shall be presented or commented on in detail and require approval by the Society(eg in connection with the assessment of drawings or with a procedure test)
1162 Manufacturing surveyRegarding manufacturing survey by the Society the requirements given in [133] and the followingrequirements apply
11621 Surveillance of production
116211 Steel components shall be surveyed during production with respect to workmanship andcompliance with the approved drawings The start of production shall be indicated in good time to the Societyinspection in charge in order to enable the Societys surveyor to survey the complete production process
116212 Professional proper and complete execution of the joining processes shall be ensured by means ofthorough controls by the factory
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DNV GL AS
116213 If the manufacturing process or any subsequent (heat) treatment which may be required maylead to a substantial change in or deterioration of the properties of the material or the welded connectionthe Society may stipulate in-production tests to prove that the mechanical qualities remain adequate
1163 Acceptance test
11631 Before delivery of steel components a suitable date for the acceptance test shall be agreed withthe Society inspection in charge
11632 For the acceptance test before delivery the manufacturer shall have ready the followingdocuments
mdash purchase and order documentsmdash workshop drawingsmdash drawings approved by the Society including design approval lettermdash results of internal checksmdash material test certificatesmdash certificates or protocols of welding testsmdash further documents as required
117 Documentation
1171 Marking
11711 Where the Society acceptance test before delivery has not given reason for complaint the steelcomponent shall be stamped as follows
mdash stamp with the month and year of testingmdash the Societys certificate number as per [11721] together with the code letter(s) of the examining
inspection office
11712 Where the steel components are produced in the lifting appliance manufacturers works a specialstamp and certification of these parts after manufacturing will be dispensed with This will be included in theacceptance test before delivery of the assembled lifting appliance
1172 Certification
11721 The Societys surveyor will issue a Societys product certificate for each finished and tested steelcomponent This certificate includes the following information
mdash manufacturers namemdash date and reference number of the approved drawingmdash replica of stamp
11722 The certificate issued according to [11721] is not part of the lifting appliance documentation onboard
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DNV GL AS
SECTION 12 TECHNICAL AND OPERATIONAL SAFETYREQUIREMENTS
121 General
1211 This section contains selected provisions in addition to the previous sections as regards safety of shipboardlifting appliances and the protection of persons based on the following requirements for design fitting andoperation of these devicesFurther requirements or measures shall be taken from the relevant standards and regulations if applicable
1212 A general precondition for the safe operation of shipboard lifting appliances is first of all its dimensioning andits design and equipment in accordance with Sec6 to Sec13 of this standardComplementary details regarding rope drives mechanical parts and electrical equipment are given in Sec8to Sec10
1213 For load-handling devices the requirements given in this section apply similarly where relevant
122 Design requirements
1221 Shipboard lifting appliances in general12211 Highest boom position
122111 GeneralEach boom shall be capable of being lowered in the highest position with or without working loadCombinations of different influences shall be taken into account
122112 Rope-operated boomsWith rope-operated booms the boom weight and the influence of all systems which prevent it remaining inthe highest position shall be sufficient to overcome all losses due to friction and turningTo prevent remaining in the highest boom position a restoring device may be provided which shall becontrolled from the crane drivers cabinAlternatively a warning device for the crane driver may be installed which warns of further luffing in duetime This device is only permissible if it is reasonable from a technical and operational point of view
122113 Cylinder-operated boomsWith cylinder-operated booms the cylinder force shall be great enough to comply with the requirementsgiven in [122112]
12212 Secondary componentsSecondary components and auxiliary structures such as inter alia ladders consoles cable trays shall not ifpossible be welded to highly stressed components Where appropriate a proof of fatigue strength shall befurnished
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DNV GL AS
12213 Access to crane driversacute cabins
122131 Crane drivers cabins shall be designed and arranged in such a way and be of such a size thatthey are easily accessible no matter what the position of the crane An accident-proof standing position for asecond person shall be provided within the area of the crane driverrsquos cabin
122132 If there is a danger that the regular access to the driverrsquos cab can be obstructed (eg in case ofan accident fire etc) an independent emergency exit shall be providedAs an alternative to an emergency exit a personnel descent device type approved by a recognizedorganization may be used Suspension points of personnel descent devices shall be designed and tested inaccordance with EN 795
122133 If normal access is impossible when the cabin is occupied a second entrance of sufficient sizewhich may also be the emergency exit shall be provided
122134 Where the floor of the crane cabin is not more than 5 m above the deck it is sufficient if the cabincan be reached without particular danger when the crane is in one position but can be left via an emergencyexit no matter what the position of the crane
12214 Accesses in general
122141 Unobstructed access to all essential components of the lifting appliance shall be ensured formaintenance and repair purposes by means of suitable accesses platforms ladders and standing spaces
122142 The headroom of entrances shall be at least 2 m the clear width at least 06 m The clear heightof the opening may be reduced by a sill up to 06 m high
122143 Ladder rungs and climbing irons shall be of 2020 square steel bar set edgewise with a footstepwidth of at least approx 30 cm From a climbing height of 25 m and above a safety cage or track for safetyharness shall be provided
122144 LaddersThe inclination of ladders measured from the horizontal shall be at least 65degLadder rungs and climbing irons shall be of 2020 (L = 300) or 2222 (300 lt L le 350) square steel bar setedgewise with a footstep width of at least 30 cm The horizontal distance from fixed structures shall be atleast 15 cmThe distance of the lowest ladder rung from the deck or platform shall be between 100 mm and 400 mmClimbing irons shall have a uniform distance of 300 mm from each otherThe minimum distances and spaces to be kept clear for movement within the reach of a ladder (see alsoFigure 12-1 and Figure 12-2) are
mdash 750 times 750 mm in front of the climbing irons excluding obstacles extending into this space(in exceptional cases a limit down to 550 times 550 is permissible however in this case obstacles such asbrackets shall be covered in order to prevent injuries)
mdash 150 mm behind the ladder measured from the axis of the climbing ironmdash 75 mm as an access clearance for the hands on each side of the ladder and around vertical hand grips
A fall arresting device (safety cage or guide rail for a safety harness) shall be provided if
a) the mounting height exceeds 25 m orb) a falling height of more than 30 m is possible
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DNV GL AS
Figure 12-1 Minimum clearances and movement space
For ladders with a height of more than 3 m or of any length (if a falling height of more than 3 m is possible)the following requirements also apply
mdash The lowest safety cage retainer shall not be positioned lower than 22 m above the deck or platformmdash The retainers shall have uniform spacing of not more than 900 mmmdash The safety cage shall at a minimum consist of five (5) longitudinal strutsmdash The clearance between climbing iron and rear cage shall be between 550 mm and 750 mm
The maximum vertical length of a ladder between two platforms is 6 mThe ladder shall stop at intermediate platforms The ladder which arrives ends at the platform and thefollow-on ladder is offset (not above the opening in the platform)The rails of the ladder shall extend past the upper platform by at least 1 m or hand grips shall be fixed up tothis height
122145 LandingsplatformsOuter edges of platforms or floors shall be provided with a coaming unless people andor items slipping isprevented by other meansFloors and their coverings respectively shall be skid-proofPlatform openings require a cover if a ladder located above the platform may be adjusted on the opening(eg if the upper ladder is fastened to rotating crane parts)The cover shall be capable of being held in the open position
122146 Guard railsThe height of guard rails of accesses platforms etc shall be at least 090 m and be provided with an upperhandrail and a rail at mid-height A foot-bar with a minimum height of 010 m shall be providedWhere guard-rails are used to separate working areas from traffic areas their clearance from moveable partsshall be at least 010 m
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DNV GL AS
Figure 12-2 Safety cage
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DNV GL AS
1222 Mobile shipboard lifting appliances12221 General requirements
122211 Rail-mounted cranes and trolleys shall be protected from derailment overturning and dislodgingand against unintentional movement in a seaway and in operation Rail stops as well as warning devices andrail clearers for lifting appliances on deck shall be provided
122212 Cranes and trolleys which can be moved athwartships shall be fitted with a form-locking drive(rack and pinion drive or equivalent) The drive shall be self-locking or fitted with brakes
122213 For cranes and trolleys in engine and pump rooms up to a safe working load of 10 t which can bemoved athwartships the requirement given in [122212] is considered to be complied with if the load canbe safely held also in a seaway by suitable fastening devices (tackles pulleys and the like)
122214 Cranes and trolleys which can be moved fore and aft shall be fitted with a self-locking driveor with brakes For such cranes calculations shall be submitted proving that the cranes are able to moveagainst a 2deg inclination and against a wind load 50 higher than specified in [5331] for operation at seaand with or without load by friction contact
122215 Cranes and trolleys with a safe working load over 10 t which can be moved fore and aft shall befitted with a direct drive as given in [122212] if they shall be employed for working at sea state Thispredominantly includes cranes and trolleys above the main engine
122216 Each crane rail shall be arranged parallel to the design waterline of the ship
122217 Where the operator has to move with the crane or trolley control unit the speed of travel may notexceed 05 ms
12222 Industrial cargo-handling vehiclesFor industrial cargo-handling vehicles the requirements given in [65] apply
123 Equipment
1231 Highest boom position
12311 Shipboard lifting appliances whose booms are held by luffing ropes shall be equipped with buffersfor the uppermost position
12312 The requirements given in [12472] shall be observed when designing buffers
1232 Control stands and controls
12321 Control stands and controls shall be designed and located in such a way that the crane driver hasan unobstructed view of the area of operation or at least of the person guiding him
12322 The control stands of cranes for cargo handling shall be closed driver cabins constructed of fire-resistant material with adequate lighting heating and ventilation They shall be fitted with accident-proofwindow panes sun shields window wipers protective grids and with one suitable fire extinguisher
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DNV GL AS
12323 The controls shall be marked to indicate their function Movement of the controls shall beappropriately related to the corresponding crane movements eg
mdash When a vertical lever is pulled towards the operator a horizontal lever is raised or a swivel lever or hand-wheel turned clockwise the load shall rise or the crane move backwards
mdash When a vertical lever is pushed away from the operator a horizontal lever is pushed down or a swivellever or hand-wheel turned anticlockwise the load shall descend or the crane move forwards
mdash As regards the slewing or rotation of cranes the direction of slewing or rotation of the crane shall agreewith the direction or layout of the controls
12324 Additional requirements for the controls and the control mechanism are given in [10621]
1233 Load radius diagramCranes with load radius-dependent safe working loads shall have a load radius diagram in the drivers cabinThe actual load radius shall be continually visible to the driver
1234 Working hours counterCranes belonging to crane group Band C (see [57]) shall be provided with working hours countingmechanisms
1235 LightingFor the main and emergency power lighting of shipboard lifting appliances the requirements given in[10622] apply
1236 Fresh air supplyFor closed control stands sufficient supply of fresh air shall be provided Air inlets shall be arranged in theopen-air and such that no contamination with exhaust gas dust or fueloil mist may occur
1237 Protection and precautions against fire and explosionNecessary protection and precautions against fires and explosions shall be considered The number capacityand location of fire extinguishers shall be adequate for the type of crane and its intended service
124 Safety devices
1241 Overload protection12411 Load limit
124111 Lifting appliances shall have overload protection devices These shall be activated if the responseof the load being raised or lowered exceeds a pre-determined amount which shall not be greater than theeffect of a static load equal to the SWL times the hoist load coefficient for which the lifting appliance hasbeen designed
124112 Where lifting appliances have variable safe working loads the overload protection device shalladjust automatically to the actual load radius
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DNV GL AS
124113 For rope and chain hoists manufactured by series production the manufacturers settings andtolerances apply see [62311]
12412 Load moment limitation
124121 Where lifting appliances have variable safe working loads a load moment limitation device is alsorequired in addition to the overload protection device
124122 Devices for limitation of the load moments shall act directly on the luffing andor telescope drivesOn hydraulic systems suitable pressure limitation devices are permissible
12413 Load reduction after an overloadAfter the overload protection devices are activated the load or load moment reducing motions of the liftingappliance and its mobile components shall still be possible
1242 Motion limiter12421 General requirements
124211 The end positions of all motions which can be performed by lifting appliances or their mobilecomponents shall be limited in an appropriate and safe way For rotary motions this is only applicable if theyare restricted by local circumstances
124212 For conventional derrick boom systems exceptions from the requirements given in [124211]can be permitted
124213 It shall not be possible for end positions to be overridden Exceptions eg for maintenance andboom stowage require written approval by the Society
124214 If required motion limiters shall also have an influence on other motions in order to avoiddamage This may eg be required for the highest hook position of booms with luffing ropes see also[12472]
12422 Motion limitation by limit switches
124221 Limit switches shall be designed and positioned in such a way that their efficiency is not affectedby the weather or by dirt accumulation Movement in the opposite direction shall be possible after they areactivated Proximity switches shall preferably be used
124222 Limit switches shall be located and adjusted in such a way that no damage can occur even if theyare approached at maximum speed and with full safe working load If necessary pre-limit switches shall beused
124223 Regarding additional requirements for limit switches see [1052]
12423 Motion limitation by design measures
124231 Limit switchesFor hydraulically operated lifting appliances with low operating speeds and safe working loads up to 1000 kglimit stops with damping if required may be permitted as a motion limitationFor rope and chain hoists from series-production the requirements given in [62322] apply
12424 Runway limitFor limit stops of movable cranes the provisions in [5342] are applicable
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DNV GL AS
1243 Emergency switcheskeys
12431 On control stands inside cabins or at manual controls an emergency switch or emergency cut-outwith mechanical locking device shall be provided
12432 The emergency shut-down shall cut off the power supply and all motions In the case of hydraulicdrives the emergency shut-down shall also act on the drive of the hydraulic pumpReturn to service shall be solely from the zero position of the respective controls or operating instruments
12433 Emergency switcheskeys shall meet the requirements given in EN 418 and continue to function inthe event of any failure of the control system
1244 Slack rope limiter
12441 In particular cases a slack rope limiter may be required eg with fast hoisting speeds withoutautomatic creep hoist multiple coils or if required for a special mode of operation
12442 For shipboard lifting appliances and floating cranes operating at sea slack rope limiters in the liftingand luffing system as well as a slack rope indication for the crane driver are requiredThe slack rope limitation system of shipboard cargo cranes operating at sea shall stop the winch(es)automatically
1245 Secondary brake for lifting appliancesLifting appliances used for the conveyance of persons or personnel shall be equipped with a secondary brakeat the hoist and luffing winch The requirements given in [4251] [4252] and [9537] apply
1246 Alarm devices
12461 Outside the driverrsquos cabin on cranes used for the handling of cargo a signal horn shall be providedby which the crane driver can raise an acoustic signal which can definitely be heard in the working area ofthe crane
12462 Mobile deck cranes shall give an optical and acoustic alarm while moving
1247 Strain of shipboard lifting appliances due to safety devices
12471 The movements and dynamic loads occurring following the response of safety devices shall be keptto a minimum if possible
12472 Motion limiters for the highest boom position shall be designed in such a way that after depositingthe load no damage may occur from the unloaded luffing ropes
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DNV GL AS
125 Passive protective measures
1251 Safety distances
12511 In accessible areas the distance between fixed parts of the ship and moving parts of the liftingappliance shall be at least 050 m in all directions and where passageways adjoin at least 060 mIf at certain points a distance of 050 m cannot be provided the area concerned shall be identified withprominent black and yellow paintwork Warning notices shall be fitted
12512 A distance of at least 050 m shall be provided between the lower edge of the boom in its lowestworking position and fixed parts of the ship
1252 Safety of access and transport
12521 Working passages operating platforms stairs and other areas accessible during operation shall besecured by railings
12522 All lifting appliances shall be fitted with a signboard forbidding access or ascent by unauthorizedpersons
12523 In utility spaces (on board ships and in cranes) adequately-dimensioned securing facilities for pull-lift hoists or holding devices shall be fitted at suitable points
12524 To permit load tests on shipboard lifting appliances inside utility spaces eye plates shall beprovided at suitable points see [6235]
1253 Corrosion protection
12531 For general requirements regarding corrosion protection the provisions of [11235] apply for steelcomponents and [8212] for wire ropes
12532 Components which are employed for hoisting services under water eg load-handling devices shallbe designed in such a way that as far as possible no seawater can ingress
126 Stowage and lashing devices
1261 General requirements
12611 It shall be possible for all wheeled shipboard lifting appliances and mobile components of shipboardlifting appliances to be positioned or where required supported for sea use as well as to be fastenedsecurely by suitable devices or guys see [4253]
12612 Supporting or fastening devices shall be designed in such a way that inadmissible forces or loadsmay not be transmitted to the lifting appliance or the components thereof caused by deformations of theshiprsquos hull in a seaway
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DNV GL AS
1262 Wheeled lifting appliances
12621 Wheeled lifting appliances shall be located in stowage positions which as far as possible areexpected to suffer the least loads in a seaway
12622 For free-travelling lifting appliances such as eg industrial cargo-handling vehicles suitablestowage spaces and lashing eyes or other suitable devices shall be provided
1263 Revolving cranes
12631 Revolving cranes with booms or projecting machinery rooms require supporting structures for thesecomponents and a special blocking device to relieve the slewing gear
12632 Where booms or projecting machinery rooms with an out of operation status shall not be stowedor supported written approval by the Society is required
12633 Booms with luffing ropes shall be guyed downwards either hanging free or supported Where thebrakes of the lifting appliance are designed for it this requirement can be complied with by proper fasteningof the cargo hook and prestressing of the hoisting ropes Prestressing shall be specified by the manufacturerSupported booms may also be fastened properly to the boom support see [5722]For booms with luffing cylinders the guy or fastening may be dispensed with provided that a correspondingapproval is at hand
12634 Where not serving to guy the boom cargo hooks shall be stowed in special devices at the boom oron deck Grabs or other large andor heavy loose gear shall be stowed on deck
1264 Design and dimensioning
12641 Boom supports supporting stowage and lashing devices shall be designed and dimensioned withthe same diligence and to the same criteria which apply to lifting appliances
12642 Stowage and lashing devices shall be dimensioned like lifting appliances out of operation accordingto [56]
127 Operational requirements
1271 Shipboard lifting appliances in general12711 Marking of hoisting capacity
127111 All lifting appliances shall be marked permanently and prominently with the safe working loadSWL and the corresponding load radiusIn the case of load-radius dependent safe working loads lifting appliances shall be marked in several placesDetailed information regarding marking of shipboard lifting appliances is given in [1325]
127112 All loose gear shall be marked permanently and prominently with the safe working load SWL andthe dead load WT the latter if WT ge 100 kgDetailed information regarding marking of loose gear is given in [743]
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DNV GL AS
12712 Ship stability
127121 In the absence of any special measures the shiprsquos stability alone shall suffice to ensuresimultaneous operation of all shipboard lifting appliances for transhipment handling or transport of cargounder all operational conditions of the shipIn doing so the inclinations andor motions of the ship which are the basis for dimensioning the liftingappliance shall not be exceeded
127122 Special measures as per [127121] can be eg
mdash operational restrictionsmdash ballasting by water or weightsmdash supporting the ship ashoremdash utilization of stabilizing pontoons
Special measures always require instructions recorded in writing and supervisory personnel and whererequired also additional monitoring devices These requirements also apply to fully automated operation
127123 The influence of lifting appliances on the shiprsquos stability shall be verified by calculation Thesecalculations shall be included in the stability documentation of the ship
12713 Failure of the drive power
127131 A design shall be employed auxiliary means shall be available and measures shall be taken to setdown suspended loads as safely as possible in the event of a failure of the drive powerMobile lifting appliances andor mobile lifting appliance components may for this purpose possibly betransferred into a more favourable load position
127132 If no other lifting appliances are available the following auxiliary meansmeasures may eg beemployed
mdash plug-on auxiliary drivesmanual pumpsmdash eye plates attached to the lifting appliance for use by pull-lift hoists for small loadsmdash mechanical ventilation of brakes or opening of valves
Mechanical ventilation of brakes or opening of valves is only permissible if the design conditions regardingintake of the released energy allow for it Required waiting periods for cooling-down shall be observed
127133 Shipboard lifting appliances used for the conveyance of persons shall be equipped with suitablerescue equipment Descender devices may be employed for the descent from work-baskets
12714 Conveyance of persons or personnelShipboard lifting appliances used for the conveyance of persons or personnel shall comply with therequirements given in [4251] and [4252] with regard to dimensioning control and operationPersons or personnel may only be transported at daylight or sufficient illumination and under environmentalconditions (windseaway) which are considered to be acceptable by the supervisor in charge
12715 Communication
127151 Crane drivers shall have an unobstructed view of the load and the working area under all workingconditions or else personnel guiding them see also [12321]
127152 If necessary equipment shall be provided or measures taken which allow safe transmittance ofinstructions from the guiding person(s) to the crane driver or the person handling the crane
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DNV GL AS
1272 Wheeled lifting appliancesFor wheeled lifting appliances the operational requirements given in [1222] [12462] and [1251] apply
1273 Floating cranes
12731 Where pontoons carrying floating cranes under load are operated in calm water a safety distance ofat least 050 m shall be maintained between the deck edge at the lowest corner and the surface of the waterWhen working in unprotected waters a safety distance of at least 100 m shall be maintained
12732 The transport of loads suspended from the crane hook across unprotected waters is subject in eachcase to approval by the Society who may for this purpose issue a Conveyance certificate if necessary
12733 In the event of the floating structure being grounded the cranes located on it may only beoperated if the structure is designed for that situation
1274 Responsibility of the ships management
12741 Special working conditions operational restrictions release and safety measures shall be recordedin writing and included with the corresponding lifting appliance documentation
12742 Maintenance and control measures performed by the ships management andor external personnelshall be confirmed properly in the lifting appliance documentation or added to itIn the Societys register book for lifting appliances Form CG1 Part 4 is provided for entries of this kind see[137]
12743 If the limit values for wind ship inclination ship motion or temperature specified in [424] arereached lifting appliances shall be put out of operation and where required be stowed in a special way andor be lashed for sea see [126]Deviating limit values may be specified for shipboard lifting appliances operating in a seaway or at lowtemperatures
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DNV GL AS
SECTION 13 TESTING AND EXAMINATION OF SHIPBOARD LIFTINGAPPLIANCES
131 General
1311 Description of content
13111 Subsections [132] to [135] contain requirements for testing examination marking andcertification of shipboard lifting appliances used for cargo handlingThese provisions apply analogously to shipboard lifting appliances not handling cargo which are onlyexpressly mentioned if required
13112 The requirements given in [136] apply for the evaluation and treatment of worn-out or damagedlifting appliance components
13113 The lifting appliance documentation described in [137] includes the following items
mdash types and systems of certificationmdash compilation of product certificates in register books (certification of lifting appliances)mdash confirmation of investigations inspections by the ships management replacement of components as well
as repair and maintenance activitiesmdash rigging plansmdash operating and maintenance instructions
1312 Supplementary requirementsSupplementarydeviating requirements apply to the following lifting appliances equipment and means oftransport
13121 Lifting appliances
mdash rope and chain hoists ([62])mdash ramps and car decks ([63])mdash lifting appliances for research work ([64])mdash industrial cargo-handling vehicles ([65])
13122 Equipment
mdash interchangeable components (Sec7)mdash wire ropes and synthetic fibre ropes (Sec8)mdash mechanical parts (Sec9)mdash electrical equipment (Sec10)
13123 Means of transport
mdash load-handling devices (Sec7)mdash shipborne working baskets ([661])mdash landing booms ([653])
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DNV GL AS
1313 DefinitionsIn addition to [115] the following definitions apply
13131 Tests
131311 Function testThe designation function test is applied to testing of all possible movements or functions as well as tocontrol limiting and safety equipmentThis test shall generally be carried out with available weightsTo test and if applicable to adjust load monitoring equipment calibrated weights or if permitted calibratedforce measuring devices shall be made available
131312 Load testThe designation load test is given to the test with the prescribed test load LPdyn or LPstatThe purpose of the load test is to prove adequate strength safety against hidden defects and - if applicable -adequate safety against overturning
13132 Examination
131321 Thorough examinationA thorough examination means a detailed visual inspection supplemented if necessary by other suitablemeans or measures in order to arrive at a reliable conclusion as to safetyIf deemed necessary by the Societys surveyor parts of the interchangeable components of the load-handling device or of the lifting appliance shall be dismounted and where required dismantled
131322 InspectionThe term inspection means a visual inspection whereby - as far as is possible by this means - it shall bedetermined whether continued use can safely be permitted
132 Manufacturing survey
1321 General
13211 In addition to the following provisions the general requirements given in Sec1 and for steelconstruction the requirements given in [1162] shall be observed
13212 Manufacturing survey is required in principle The Society may however dispense with it for liftingappliances manufactured in series which is not used for cargo handling and which fulfils the requirementsfor omitting assessment of drawings see [132] In this case manufacturerrsquos test reports may be accepteddeviating from the certificates stated in [13271]
13213 Commencement of construction of a lifting appliance shall be advised to the Society in sufficienttime for the Societys surveyor to attend the construction process from the very beginning
13214 The basis for the manufacturing survey at the manufacturer of the lifting appliance is the approveddocumentation according to Sec2 plus if applicable further documentation certificates reports andinformation from the manufacturer which the Societys surveyor needs for assessment of the parts to beexamined
13215 Regarding manufacturing survey and lifting appliance documentation subcontracting firms shallprovide certificates and test reports in the scope specified in Sec6 to Sec10
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DNV GL AS
1322 Participation by manufacturers
13221 As far as necessary and advisable the works shall check all components during and aftermanufacture for completeness dimensional accuracy and proper workmanship
13222 Following checking and if required repair by the works the components shall be presented to theSocietys surveyor for inspection during appropriate phases of construction normally in easily accessible andunpainted conditionCertificates for components and equipment delivered by subcontractors shall be submitted
13223 The Societys surveyor may reject components not adequately pre-checked and stipulate that theybe presented again following checking by the works and if required repair
13224 Components to be tested shall be indicated for the Societys inspection in good time forexamination
13225 In order to enable the Societys surveyor to perform his duties he shall be given access to theworkshops in which components for testing are manufactured and assembled Manufacturers shall makeavailable to the surveyor the personnel and material support required to carry out the prescribed tests
1323 Manufacturing survey
13231 The Societys surveyor examines the components constructed at the manufacturers or suppliedwith regard to condition marking and certification He surveys the assembly of the lifting appliance andexamines workmanship and agreement with approved documents and witnesses the test runs and functionaltests as appropriate or agreed
13232 Testing of materials for the manufacture shall be proven to the Societys surveyor in accordancewith the Societys rules for materialsThe certificatesreports for the materials used as well as proofs on welding and non-destructive materialtests shall be presented to the Societys surveyor
13233 Components which are not type-tested but subject to tests and examination shall as far aspossible be tested at the manufacturers test plant in the presence of the Societys surveyor in an agreedscope or as prescribed by this standardRegarding series production instead of the prescribed tests other testing methods can be agreed with theSociety provided that they are accepted to be equivalent
13234 Where machines devices or electrical equipment are provided for the intended purpose for the firsttime the Society may demand a type-test
1324 Factory acceptance test (FAT)13241 General
132411 Shipboard lifting appliances assembled ready for operation or completely equipped assemblygroups shall be presented to the Societys surveyor before they leave the manufacturers works
132412 After completion of agreed test runs or tests lifting appliances or lifting appliance assemblygroups shall be subjected to a thorough examination The testing methods applied are at the discretion of theSocietys surveyor Following tests on the test plant lubricating and hydraulic oil filters shall be checked forimpurity
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13242 Tests and examinations to be carried out
132421 General
mdash checking of documentationmdash examination in respect of workmanship compliance with the approved documents and for completenessmdash checking of safety clearances and passive protection measuresmdash examination of accesses ladders rails and platformsmdash examination of the cabin or the control stand and the control equipmentmdash examination of the manufacturers plate on which at a minimum shall be permanently indicated
mdash manufacturers namemdash year of constructionmdash serial numbermdash where applicable type designationmdash safe working load(s) and load radius (radii)
mdash examination of marking see [1325]
mdash additional tests andor examinations as required
132422 Test runNewly designed lifting appliances shall be test-run in the presence of the Societys surveyor according to aprogramme approved by the Society If possible this shall take place at the manufacturers but with theSocietys consent it may also take place elsewhere or at the place of operation
Guidance noteNewly designed lifting appliances can typically be characterized by
mdash significant change or new design of mechanism (eg wire rope reeving) andor
mdash significant increase of safe working load (enlargement of an old design) andor
mdash significant change or new design of load-bearing structure andor
mdash significant change or new design of machinery andor
mdash significant change of safety devicessystems andor
mdash additional application of new safety devicessystems (eg AOPS MOPS ELRS)
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
Shipboard lifting appliances subject to special operating conditions shall undergo test runs under theseconditions At least one of every different type of lifting appliance shall be tested in this wayThis for instance means that the test run shall be performed with the ship also at the stipulated inclinationA test run may cover the following insofar as applicable
mdash checking the interaction of all movable parts and functionsmdash function test under available loadmdash brake test with dynamic test load according to Table 13-2 by releasing the operators controlmdash emergency brake test with dynamic test load according to Table 13-2 (see also [133324])mdash checking the emergency load release devicemdash endurance tests on all power units under safe working load with heating measurementmdash noise measurement (also in the cabin)mdash measurement of power consumption and contractually agreed speeds under safe working loadmdash additional measurements including electrical ones if necessarymdash checking and adjustment of all valves and control equipmentmdash pressure testsmdash testing and adjustment of all safety devices and limit stopsmdash testing of lighting ventilation intercom etcmdash testing of fire protection system
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mdash further tests as required
Guidance noteBrake tests with test load shall be restricted to the required number Emergency tests shall as far as possible be performed onlyonce
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
Easing of testing requirements shall be agreed with the Society
132423 Proof of safety against overturningFor the proof of safety against overturning for wheeled lifting appliances the requirements given in [4522]and [6512] apply
1325 Marking of the lifting appliance13251 Lifting appliance number
132511 The sequential numbering of shipboard lifting appliances shall agree with the details in thecertificates and rigging plans
132512 The following rule for numbering shall be applied
mdash first all lifting appliances for cargo handling starting from the fore and arranged in pairs progressing fromport to starboard starting on deck then below deck
mdash next all lifting appliances needed for operating the ship but none of the gear exclusively for launching life-saving equipment Here also starting on deck then below deck
132513 The number of the lifting appliance shall be preceded by Nr or also No
13252 Safe working load(s)
132521 The safe working load(s) of lifting appliances for cargo handling shall be indicated in metrictonnes t on other lifting appliances especially with lower safe working loads the indication may also be inkilograms kgThe safe working load(s) of lifting appliances shall be preceded by the letters SWL where applicable withthe following additions
mdash SWL (P) for pairs of lifting appliancesmdash SWL (G) for lifting appliances with grabsmdash SWL (M) for conveyance of persons
13253 Load radius (radii)
132531 The load radius (radii) of lifting appliances shall be indicated in metres ldquomldquo When variable theminimum and the maximum value each
132532 Gantry and bridge cranes with trolleys are not given a load radius indication
13254 Details of execution
132541 The marking giving details of the safe working load shall be in writing at least 80 mm high andthat regarding lifting appliance number or boom inclination at least 50 mm high
132542 This marking shall be permanently applied eg by means of metal plates or by tracing thecontour with a centre-punch or by means of welding spotsGlued-on foils are permitted only for lifting appliances under deck
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132543 The marking for the safe working load and if applicable the load radius shall be located clearlyapart from the lifting appliance number
Table 13-1 Examples of markings
Item No onboard the ship Safe working load Load radius Lifting appliance type Meaning of the marking
Lifting appliance with boom
No 3 SWL 40 t 24 ndash 32 m In the indicated area of load radiusloads up to 40 t may be transported
No 2SWL 250 tSWL 120 t
SWL 60 t
35 ndash 12 m35 ndash 255 m
35 ndash 34 m
Crane with 3 load steps The loadradius limits of the allocated safeworking loads shall not be exceeded1)
No 4SWL (G) 264 t
SWL 30 t28 ndash 28 m28 ndash 28 m
In the indicated area of loadradius loads up to 264 t can betransported during grab operationup to 30 t in general cargooperation 2)
Nos 2 + 3 SWL (P) 60 t 26 ndash 31 m
revolving cranes
In the indicated area of load radiusloads up to 60 t may be transportedby 2 cranes slewing jointly
No 1 SWL 50 t minusgantry cranewith foldabletrolley girders
In the whole operating range of thegantry crane and the trolley loadsup to 50 t may be transported
SWL 50 tSWL 186 t
36 ndash 14 m36 ndash 40 m
Crane with variable load range 3)
No 2
SWL 5 t 44 ndash 42 m
revolving crane
Marking for the auxiliary hoist
Lifting appliance without boom
No 10 SWL 16 t minus bridge cranelifting platform
Safe working load of the liftingappliance
No 18 SWL 3 ndash 6 t minus rope hoist
Where the hoisting rope has a singlereeve loads up to 3 t may be liftedup to 6 t in the case of double reeve4)
1) In the crane drivers cabin a load radius diagram shall be visibly displayed2) The difference between SWL (G) and SWL results from the different hoist load coefficients see Table 5-2
The safe working load SWL (G) includes the dead load of the grab As an example a grab may be marked as follows
SWL 24 t underneath WT 24 t3) Information about the curve-type variation of the safe working loads can be taken from the load radius diagram
displayed in the crane driveracutes cabin4) The types of reeve shall be marked properly on the lifting appliance In the case of more than double reeve an
operating instruction is required
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DNV GL AS
13255 Location
132551 The marking shall be applied at a clearly visible location with jib cranes at both sides with gantrycranes at the fore and aft side of the gantry relative to the longitudinal direction of the ship
132552 In the case of lifting appliances which can be combined in pairs additional marking shall beapplied at a suitable location for the combined loadOn slewing cranes with crane booms arranged on a common crane column this marking shall be applied atthe fore and aft parts of the column relative to the longitudinal direction of the ship
13256 Examples of marking
132561 Marking is part of the safety measures for the operation of lifting appliances and therefore subjectto examinationWhere variable equipment and reeve options exist operating instructions are required
132562 In Table 13-1 some typical marking examples are listed including explanationsSpecial marking requires agreement with the Society
1326 Stamping of lifting appliances
13261 Prior to the Societys issuance of the product certificate or manufacturing survey report as per[13271] the lifting appliance shall be stamped as follows
mdash the certificatereport number with the distinguishing letters of the Societymdash the stamp with month and year of test
13262 An additional stamp covering the safe working load is not applied until after the load test has beencarried out
13263 Cranes shall be stamped at the bottom end of the left-hand jib spar next to the point where it joinsthe crane houseLifting appliance assembly groups and lifting appliances other than cranes shall be stamped in a prominentposition
1327 Certification and reporting of manufacturing surveys and tests
13271 For all shipboard lifting appliances cargo winches luffing and slewing cylinders completed andtested (FAT) in accordance with [1324] a Societys product certificate is issued by the Societys surveyorWhere lifting appliances or their assembly groups are manufactured and surveyed without FAT they receive amanufacturing survey report eachWhere interchangeable components and loose gear are already a part of the lifting appliance during themanufacturing survey product certificates of form CG3 shall be providedFor wire ropes which are already part of the lifting appliance at the manufacturing survey product certificatesof form CG4LA4 shall be providedThis paragraph does not apply to chain and rope hoists manufactured in series production
13272 Apart from explanatory notes concerning the acceptance procedures the Societys productcertificates and survey reports as per [13271] may contain notes regarding other certificates (eg CG3CG4LA4) protocols etc such as eg the following details
mdash manufacturers namemdash type designation and production number
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DNV GL AS
mdash safe working load(s) and if applicable load radius (radii)mdash date and the Societys reference number of the design approvalmdash associated ship (yard no or DNV GL Ship ID No)mdash stamp
133 Initial test and examination
1331 General
13311 Prior to commissioning an initial test and examination within the scope described in [1332] to[1334] at the place of operation is requiredThe sequence of steps for the test and examination is as deemed necessary by the Societys surveyor whoalso decides the scope of his examination
13312 During practical testing of lifting appliances dependent on an external power supply care shall betaken to ensure that the test is carried out using the type of power supply envisaged from the ships mainWhere ships are fitted for shoreside power supply shore and ship power shall be compatible
13313 The certificates and rigging plans stated in [133412] shall be presented as proof ofmanufacturing survey and as an integral part of the lifting appliance documentation
1332 Function test
13321 This test serves to provide proof of the good working order of all components installed systemsand safety devices The test procedure is at the Societys surveyors discretion
13322 In the case of permanently installed lifting appliances the function test amongst other thingsserves to verify whether parts of the ships structure or the ships equipment restrict the working range orimpede the working process
13323 The function test to be carried out for the Societys surveyor does not normally serve to checkwhether all possible operations wanted by the operator can be effected Proving this is the responsibility ofthe manufacturer or supplier
13324 With the exception of the test on the overload protection devices the function test may be carriedout with any given load see also [131311]
13325 A function test using a test load requires the manufacturerrsquos consent
1333 Load test13331 General requirements
133311 All shipboard lifting appliances shall undergo a load test with weights prior to being put intoservice The test shall be carried out at the place of operation in order that their respective foundations ordriveways be included in the test
133312 In the case of lifting appliances below deck which are difficult to access load tests mayalternatively be conducted using a calibrated load measuring instrument whose indication of measuredvalues shall remain constant for five minutesThe instrument shall have an accuracy of plusmn 25 or better
Standard mdash DNVGL-ST-0377 Edition October 2018 Page 240Shipboard lifting appliances
DNV GL AS
If the safe working load SWL of any lifting appliance exceeds 15 t use of load measuring instruments shallbe avoided
133313 Lifting appliances shall be subjected to a dynamic load testThe size of the test load shall be taken from Table 13-2
Table 13-2 Dynamic test loads for shipboard lifting appliances
Application range Test loads (LPdyn) 1)
Shipboard liftingappliances in general
20 t lt
50 t lt
SWL
SWL
SWL
le 20 t
le 50 t
125 ∙ SWL
SWL + 5 t
110 ∙ SWL
Ramps car decks andlifting platforms 2)
20 t lt
50 t lt
(SWL + WT)
(SWL + WT)
(SWL + WT)
le 20 t
le 50 t
125 ∙ SWL + 025 ∙ WT
SWL + 5 t
110 ∙ SWL + 010 ∙ WT
SWL = safe working load according to [11554]
WT = dead weight of moved masses of ramps car decks or lifting platforms
1) If applicable to be multiplied with fd according to [7333]2) If ramps car decks or lifting platforms are designed for conveyance of persons exclusively the dynamic test load
may be calculated with SWL(M) instead of SWL In this case an additional static load test with test load based onSWL is required
13332 Load test performanceFor the dynamic load test to be performed for the Societys surveyor the test load shall be lifted slowly andif possible also slewed and luffed In detail the following applies
133321 For lifting appliances generally the test load shall be lowered rapidly and braked in variouspositions andor settings Braking shall be effected by releasing the control levers
133322 Cranes under test load shall run the full travelling distance or at maximum load radius slowlycover the full swinging or slewing range Additionally the minimum load radius shall be tested and in thecase of cranes with radius dependent safe working loads also an intermediate value
133323 Regarding crane columns and their integration into the ships hull as well as lifting appliancefoundations in general tests according to [133321] are required in longitudinal and transverse directionsof the ship ie to fore and aft and to port and starboard each
133324 For lifting appliances used for cargo handling one emergency brake test with the test load byoperating the emergency switch or button shall be carried out either at the manufacturers or at the place ofoperation
133325 When carrying out the load test care shall be taken to ensure that all movable parts are able tooperate freely in all the lifting appliance andor derrick booms positions all ropes are unobstructed by anyother parts and the ropes can wind satisfactorily onto the winch drums
133326 In the case of ramps the test load arrangement shall conform to the intended operating mode
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DNV GL AS
13333 Requirements for hoisting winches
133331 If the pull of the hoisting-winch is insufficient to lift the test load a second winch or other liftingappliance may be brought in to assist with the hoist Braking and holding the test load however shall beaccomplished using solely the winch belonging to the lifting appliance
133332 Where hoisting-winches have not lifted the test load by themselves proof shall be obtained bytesting that with the maximum number of layers of rope on the winch drum the safe working load is hoistedsatisfactorily by the winches
133333 The ability of the winch to hold the test load with the drive to the winch switched off shall beproved In doing so no slip shall occur with the exception of hydraulic winches without standstill brakes see[136824]
133334 Hydraulic cranesIf hydraulic cranes are unable to lift a test load 25 greater than the safe working load because of thepressure limit lifting the maximum possible load is sufficient This shall however exceed the safe workingload by at least 10
1334 Examination13341 Documentation check
133411 Priority shall be given to checking if the assessment of drawings for lifting appliances cranecolumns boom supports and lashing equipment foundations runways and all supporting structures has beenconcluded successfully and if all structural modifications or changes possibly resulting therefrom have beencarried out
133412 Manufacturing survey shall be documented by product certificates andor manufacturing surveyreports The lifting appliance documentation remaining onboard shall include
mdash rigging plansmdash product certificates for interchangeable components and load-handling devicesmdash product certificates for ropes
133413 Regarding the certificates stated in [133412] their correct correlation to the certified structuralparts or components shall be checked by comparing the stamping andor properties of these partsThe certificates shall be checked with respect to correctness in form and content
13342 General visual inspectionThe general visual inspection may eg refer to the following checks
mdash general condition completeness and correct riggingmdash assembly interfaces between components constructed on site and components suppliedmdash undisturbed power transmission through transversely arranged plates such as deck plates (Where
required this shall be checked by means of drilling holes which shall be welded up after the check)mdash inscription of number SWL and where required load radiusmdash warning and indication signboards as well as warning paintwork where requiredmdash accesses to lifting appliances and to control standsmdash accesses to driver cabins and working and control platforms inside and outside the lifting appliance and to
boom supportsmdash emergency descentsmdash condition and equipping of control stands and driver cabinsmdash working area of the lifting appliance
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DNV GL AS
mdash range(s) of sight for the operator from inside the driver cabin
13343 Examination after the load testAfter the load test the load-bearing components of lifting appliance shall undergo a visual inspectionThis examination shall if possible exclude the formation of possibly permanent deformations or cracks atforce application points or at special design details
1335 Stamping
13351 If the initial tests and examinations have not given rise to any objections the lifting appliance shallbe stamped before the relevant certificates are issued
13352 Cranes with boom shall be stamped at the bottom end of the right-hand jib member and next tothe point where that member is connected to the crane house and in a prominent position on all other liftingappliances
13353 The stamp shall contain the following information
mdash shipboard number of the lifting appliancemdash stamp with the month and year of testmdash safe working load of the lifting appliance in [t] or where required in [kg] and the permissible minimum
and maximum crane load radius in [m] Where the safe working load varies with the load radius the safeworking load and the corresponding load radius shall be stated for the maximum and minimum values
mdash certificate number and distinguishing letters of the Society
1336 Certification of the initial tests and examinations
13361 Following performance of the tests and examinations and stamping the Societys surveyor issuesthe certificate Form CG2 for load-tested lifting appliances handling cargo and OLA201 for load tested liftingappliances not handling cargoCG2 or OLA201 for shipboard lifting appliances covered by Crane notation shall be endorsed with additionalremark COVERED BY CRANE NOTATION
13362 The tests and examinations of the lifting appliance are confirmed by the Societys surveyor in aregister book of Form CG1 to which the certificate and the survey report are added
13363 The certification and documentation system for shipboard lifting appliances is described in [137]
134 Periodic tests and examinations
1341 General
13411 Shipboard lifting appliances subject to periodic tests and examinations by the Society shall beexamined at regular intervals by the Societys surveyor and subjected to load tests in his presence
13412 The intervals between examinations and between the load tests described below are customaryinternationally Deviating national requirements shall be taken into account if applicable
13413 In cases where a lifting appliance dependent on an external power supply is tested therequirements given in [13312] apply
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DNV GL AS
1342 Due dates13421 Examinations
134211 Lifting appliances and load-handling devices shall be examined annually by the Societys surveyorunless other intervals are required by national regulationsThe operator is as a matter of principle obliged to give the Society due notice of the examination
134212 The following examinations vary depending on type and scope
mdash annual examinations see [1343]mdash five-yearly examinations see [1344]
13422 Load tests
134221 No later than five years after the load test a further load test is required for shipboard liftingappliances to be performed in the presence of the Societys surveyorThe operator is as a matter of principle obliged to give the Society due notice of the load testA regular recurrent load test of loose gear is not required internationally by ILO
134222 For practical reasons load tests shall coincide if possible with the five-yearly examination
13423 Exceeding the due date
134231 In the case of shipboard lifting appliances subject to the regulations of ILO the intervals of oneand five years regarding examinations and load tests shall not be exceededThis applies on the analogy to recurrent thorough examinations of load-handling devices
134232 In the case of lifting appliances not subject to the ILO regulations the interval stated in[134231] may be exceeded by up to three months when admitted by the Flag State Administration Thisapplies also to related load-handling devicesThis does not however postpone the due date of the next examination The same applies inversely to testsperformed before the due date
134233 Where the intervals stated in [134231] and [134232] are exceeded the validity of entrieson examinations performed and the validity of product certificates expires in the register bookIn the case of classified shipboard lifting appliances the respective class notation is suspended once the fiveyear interval has been exceeded by more than three months
1343 Annual examinationsThe purpose of annual examinations shall confirm technical safety of operation within the periods of five-yearly examinations
13431 Scope of examinations
134311 The scope of examinations depends on age condition and frequency of use of lifting appliancesNormally lifting appliances need not be unrigged and dis-mantled for the performance of yearlyexaminations
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DNV GL AS
134312 Essentially the scope of examination comprises
mdash checking documentation and certificates for completeness and validity and with reference to maintenanceand inspection measures arranged or performed by the shiprsquos management
mdash checking of the records done by responsible person in the form CG1 in the Part III and Part VImdash checking for completeness and correct rigging or reeving respectively using the rigging plansmdash checking for damage wear deformation corrosion soiling oil leakage etcmdash checking for proper markingmdash function test using available loadmdash random examination of the interchangeable components and correlation to the relevant certificates based
on the stamps appliedmdash verification of newly-fitted partsmdash recording the examination carried out in the register book or where required in a corresponding
certificatemdash preparation of a survey report
134313 The list in [134312] is by way of an example The actual scope of tests and examinations isat the discretion of the Societys surveyor whereby negative findings may require further examinations ormeasures see [13442]
13432 Dealing with components
134321 Use of steels liable to age is not permitted as a matter of principle so that heat treatment ofcomponents at regular intervals is not required
134322 Components which do not comply with these rules or which are worn to the permitted limits shallbe replaced by new ones with the prescribed dimensions
134323 Any parts renewed since the last examination shall be submitted to the Societys surveyortogether with the certificates required
1344 Five-yearly examinations13441 General
134411 The purpose of five-yearly tests and examinations shall confirm or generate a solid technical basisfor the upcoming annual examinations
134412 Five-yearly examinations and load tests shall be performed if possible at the time of ClassRenewal ie during the period in shipyard refit to have available sufficient technical equipment test weightsand interchangeable components if necessary
13442 Scope of examinationsIn accordance with these rules five-yearly examinations shall extend and complement the examinationsdescribed in [13431] and where required the measures described thereafter which may if necessary beextended
134421 Examination of structural and interchangeable componentsIf deemed necessary by the Societys surveyor individual parts shall be dismantled and if necessaryunrigged for the examination All parts found to be unsafe to operate shall be repaired or replacedThe Societys surveyor is entitled to demand a load test or a load test repeat for lifting appliancesinterchangeable components or load-handling devices if deemed necessary
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DNV GL AS
134422 Examination of slew ringsSlew rings shall be examined with respect to bearing clearance noise lubrication and corrosionThe tight fit of the pins shall be checked by at least one random hammer testWhere increased internal wear is suspected extruded grease shall be checked by an appropriate method forabraded particlesSlew rings of shipboard cargo cranes operating at sea which are not equipped with special control andmeasuring devices shall be checked regularly by special control measures agreed with the manufacturerWhere increased internal wear becomes apparent it may be required to remove the slew ring and todismantle it for examinationThe associated drives and brakes shall be checked with respect to wear function and general condition
134423 Examination of hydraulic cylindersApart from a thorough visual inspection with respect to straightness oil leakage bearing clearance andabsence of cracks in the connecting structures a function test of pipe burst safety valves or similar safetycomponents with available load is required
134424 Examination of winchesWinches shall be examined with respect to
mdash condition fastening and functionmdash wear to brakes rope grooves and flanged discsmdash sufficient lubricationmdash function of safety equipmentmdash correct rope windingmdash observance of the required safety turnsmdash tight fit and absence of corrosion of the rope-end attachment(s)
Guidance noteFor wire ropes the number of required safety turns is specified in [82411] for synthetic fibre ropes the number of requiredsafety turns is specified in [8346]
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
134425 Crack testsWhere a visual inspection gives reason for this the Societys surveyor may request crack tests using theprocedure appropriate to each caseThe following areas of design need particular attention
mdash flange connection of the slew ring at the crane column or the foundationmdash connections between longitudinal and transverse structural members of crane boomsmdash bend areas of all kinds especially on crane columnsmdash connections between crane columns and hatch coamingsmdash corner connections of crane gantriesmdash power transmission in the direction of thickness of platesmdash special (noticeable) details of construction
134426 Examination for corrosionThe following areas of design need particular attention
mdash supporting areas of crane booms at stowage devicesmdash loose ropes with downward hanging end attachments see [85313]mdash contact areas without watertight sealing eg in case of welded eye platesmdash special areas of design where water may accumulate
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DNV GL AS
1345 Load tests
13451 For the performance of load tests the requirements given in [1333] apply however no emergencyshut-down test is required nor tests with several different safe working loads load radii and ship directions
13452 At the five-yearly load tests of shipboard lifting appliances solely testing with test load based onthe maximum safe working load at the associated maximum load radius will suffice
13453 At the five-yearly load tests the tests are if possible to be performed using weights The weightsshall be calibrated and certified or verifiable
13454 The magnitude of test load shall correspond to Table 13-2 In exceptional cases a lower testload may be used with hydraulically driven lifting appliances where the working pressure cannot becorrespondingly increased see [133334]
13455 Five-yearly load tests of lifting appliances under deck may alternatively be conducted using acalibrated load measuring instrument whose indication of measured values shall remain constant for fiveminutesThe instrument shall have an accuracy of plusmn 25 or betterIf the safe working load SWL of any lifting appliance exceeds 15 t use of a load measuring instrument as faras possible shall be avoided
1346 Confirmation of periodic tests and examinations
13461 Following performance of the tests and examinations the Societys surveyor will issue thecertificate Form CG2 for load-tested lifting appliances handling cargo and OLA201 for load tested liftingappliances not handling cargo
13462 The tests and examinations of the lifting appliances used for cargo handling and associated load-handling devices will be certified by the Societys surveyor in the register book Form CG1 Part I II and thecertificate CG2 will be added to the register book
13463 The tests and examinations of the lifting appliances not used for cargo handling and associatedloosed gear will be certified by the Societys surveyor in the register book Form CG1 Part IV V
13464 The stamping required according to [1335] in advance of the issuing of certificates is in generalnot required for periodic load tests
13465 The system of certification and documentation for lifting appliances is described in [137]
135 Extraordinary tests and examinationsModifications damage renewals and special occasions may require extraordinary load tests andorexaminations as described in the following
1351 General
13511 The operator shall inform the Society if essential modifications are intended to be made to liftingappliances or load-handling devices when damage affecting safety has occurred or renewal of load-bearingstructural elements shall be carried out
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DNV GL AS
13512 In the cases described above the Society decides on the respective measures examinations andload tests
13513 Any essential modification and any repair or renewal of load-bearing components with theexception of ropes and interchangeable components shall be subject to manufacturing surveys according to[132] Where this is not possible in individual cases because of the circumstances a re-examination shall becarried out on a suitable date
13514 Extraordinary load tests and examinations may be credited towards the periodic tests andexaminations if they comply with the prescribed conditions with respect to type and scope
13515 All load tests shall be performed using weights in the manner described in [1345]Regarding certification of tests and examinations the requirements given in [1346] apply
1352 Essential modifications
13521 Essential modifications are subject to the same tests and examinations as the initial manufacture
13522 Essential modifications include besides renewal of load-bearing components modifications of
mdash safe working loadmdash load radiusmdash hoisting andor luffing systemsmdash cable tackle system unless different types of reeve are provided in the designmdash load-bearing components
13523 Non-essential modifications include modifications which will in no way affect safety andor functionof lifting appliances or load-handling devices Such modifications shall be presented to the Society surveyoron his first visit to the ship after the modification has been carried out
1353 Damage
13531 The requirements given in [136] shall be observed when an evaluation is made whether damageunduly affects the safety of lifting appliances or load-handling devices
13532 Damage affecting safety requires an examination of the damage and a repair plan with specificdetails which is subject to approval by the SocietyFollowing repair an examination within the necessary scope and a load test are required
13533 Depending on the evaluation of the damage lifting appliances or load-handling devices shall be putout of operation or where required be operated at reduced safe working load andor load radiusRegarding repairs and operation at reduced safe working load the requirements given in [1369] apply
13534 Damage which does not affect safety shall be presented to the Societys surveyor at the first visitto the ship after the occurrence of the damage
1354 Renewals
13541 Following each renewal of load-bearing components of lifting appliances or load-handling devices aload test and an associated examination of this gear is required
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DNV GL AS
13542 The requirements given in [13541] do not apply to ropes and interchangeable componentsbecause these are tested examined and certified independentlyRenewal of axles pins rope-sheaves etc do not in general require a new load testThe renewal of all parts mentioned shall be pointed out to the Societys surveyor on the occasion of thefollowing examination
13543 Following replacement or repair of winches a load test is required unless the winch has been load-tested on a test plant and certified accordingly
13544 Special occasionsThe Society reserves the right to ask for extraordinary load tests andor examinations in specially justifiedcases
136 Wear damage repair
1361 General
13611 The details which follow regarding deformation wear tolerances etc shall be considered asreference values to assess the remaining margin of safety of damaged corroded or worn componentsIn the case of major damage of shipboard lifting appliances or in cases of doubt the Society shall beconsulted
13612 Any damaged worn or corroded part which is not replaced shall once the tolerances have beenexceeded be restored to the original dimensions using equivalent materialsRegarding an alternative reduction of the safe working load see [13691]
13613 For worn or corroded parts which are close to reaching the tolerance limits the Societys surveyormay determine a time period for repair or replacement
13614 Regarding load-handling devices interchangeable components and ropes see also [75] and[8533]
1362 Acceptable reduction of plate thickness
13621 For plates profiles and pipes the acceptable reduction of plate thickness is 10
13622 In cases of limited local corrosion or wear a reduction of plate thickness of up to 20 is acceptableprovided this does not result in a reduction of the load-bearing capacity of the cross-section
13623 In cases of isolated pitting a reduction of plate thickness of up to 30 is acceptable
13624 Due to the above reductions of plate thickness the characteristic values of a cross-section underconsideration may be weakened at the most by 5
1363 Acceptable cracks
13631 In special or primary components (see [312]) no cracks can be tolerated
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DNV GL AS
13632 In lateral wind bracing latticework crosspieces and similar stiffeners or knee plates whose purposeis to reduce the slenderness ratio or stiffen load-bearing structures cracks up to the following lengths areacceptable if there is evidence that they do not extend into the load-bearing structure
mdash 10 of the connection lengthmdash 3 times plate thickness
the lower of the two values applyingIn the case of pipes the connection length is the circumferenceIn the case of box girders or beams each chord web and flange width shall be considered separately as aconnection length
1364 Acceptable deformations13641 Deflections
136411 Compression barsUnder the maximum permissible loading compression bars may not display uniform deflection greater thanthe equivalent of the bar length divided by 250Unstressed compression bars or those stressed only by their own weight which are category 1 componentsmay not display uniform deflection greater than the equivalent of the bar length divided by 500Unstressed compression bars or those stressed only by their own weight which are category 2 componentssuch as lateral wind bracing or latticework crosspieces may not display uniform deflection greater than theequivalent of the bar length divided by 350
136412 Tension barsTension bars shall not when unstressed display uniform deflection greater than the equivalent of the barlength divided by 50
136413 BoomsjibsFor booms subject to compressive stress under permissible load the requirements given in [136411]apply The uniform deflection due to the dead weight alone shall not be greater than the equivalent of thecrane boom length divided by 350The lowering of the top of the boom under load andor dead weight is not limited when the permissible loadis observed
13642 Deformation of chords and flanges
136421 I-BeamsEach half-flange may individually or together be deformed by up to 15 of its breadth measured from webto outer edge
136422 Angle profilesFlanges of angle profiles may individually or together be deformed by up to 15 of their breadth measuredfrom flange to outer edge
1365 Acceptable indentationsThe following requirements presuppose smooth transition pieces and apply provided that no bends foldscracks or thinning have developed
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DNV GL AS
13651 Compression bars
136511 Cylindrical pipesPipes forming category 1 components
The following conditions shall be observed
ℓ le d
b le 025 d
f le 05 t
where
ℓ = length of indentation measured in the longitudinal direction of the pipeb = breadth of indentationf = depth of indentation (depth gauge)d = outer diametert = wall thickness
Pipes forming category 2 components
The following conditions shall be observed
a) central range (13 ℓ) b) outer range
ℓ le d ℓ le 15 middot d
b le 05 middot d b le 07 middot d
f le t f le 2 middot t
136512 Rectangular tubes and box girdersIn the case of rectangular tubes and box girders indentations at the corners may have a depthcorresponding to 8 of the smallest side dimensionFor acceptable indentations of plates the requirements for cylindrical pipes similarly apply Instead of thediameter the side dimension of the plate under consideration shall be taken
136513 I-BeamsThe webs of I-beams may not have any indentations
136514 Angle profilesAngle profiles may not have any indentations at the corners
13652 Tension barsIn the case of tension bars the indentation depth may be up to one third of the indentation length The outerdimensions of hollow profiles however shall not be reduced by more than 25 in the indentation areaIf necessary the requirements given in [4352] shall be observed
13653 Girders subject to bending
136531 Indentations at bearing or load introduction points are not acceptable