SUNDYNE LMC 341F COMPRESSOR

Instruction and Operation Manual

August 2007

Effective: August 2007 Visit our website at www.sundyne.com

COPYRIGHT All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted in any form or by any means, electronic, mechanical, photocopying, recording or otherwise without the prior permission of Sundyne Corporation. © 2007 Sundyne Corporation

WARRANTY Sundyne Corporation warrants to Buyer for a period of twelve (12) months from the date of being placed in service (but not to exceed eighteen (18) months after the date of shipment) that the equipment at the time of shipment will be free from defects of design, material and workmanship. If any defects or malperformance occur during the warranty period, Sundyne’s sole obligation shall be limited to alteration, repair or replacement at Sundyne’s expense, F.O.B. Factory, of parts or equipment, which upon return to Sundyne and upon Sundyne’s examination prove to be defective. Equipment and accessories not manufactured by Sundyne are warranted only to the extent of and by the original manufacturers’ warranty. Sundyne shall not be liable for damage or wear to equipment caused by abnormal conditions, vibration, failure to properly prime or to operate equipment without flow or caused by corrosives, abrasives or foreign objects. THE FOREGOING WARRANTY IS EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES, WHETHER EXPRESSED OR IMPLIED INCLUDING ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR ANY PARTICULAR PURPOSE. In no event shall Sundyne be liable for consequential or incidental damages.

INTRODUCTION AND SAFETY..................................................................................... 1

Text Symbols .............................................................................................................................................................1

Equipment and Safety Precautions .....................................................................................................................1

EXPLOSION/FIRE HAZARD .......................................................................................... 2

USING THIS MANUAL: .................................................................................................. 3

1. INSTALLATION.......................................................................................................... 4

INTRODUCTION TO THE SUNDYNE COMPRESSOR ................................................. 5

Inspection ...................................................................................................................................................................5

Short-term Storage...................................................................................................................................................5

Long-term Storage ...................................................................................................................................................5

Installing the Suction and Discharge Piping - Guidelines .............................................................................6

Seal Environment Control System .......................................................................................................................7

Baseplate Grouting ..................................................................................................................................................9

Horizontal Unit Gearbox Support Bracket .........................................................................................................9

Driver and Coupling .................................................................................................................................................9

2. LUBRICATING OIL SYSTEM..................................................................................... 9

3. START-UP ................................................................................................................ 13

Compressor Control During Start-Up................................................................................................................14

Run-In of the Compressor ....................................................................................................................................14

4. SERVICING .............................................................................................................. 15

Regular Maintenance .............................................................................................................................................15

5. MAINTENANCE OF THE SEALS AND PROCESS END DISASSEMBLY .............. 16

Tandem Seal Configurations ...............................................................................................................................16

Double Seal Configurations .................................................................................................................................16

Procedure for Disassembling Process End.....................................................................................................16

Vertical units without a driver stand..................................................................................................................17

Vertical units with a driver stand........................................................................................................................17

BMC Units .................................................................................................................................................................17

Tandem Seal Disassembly ...................................................................................................................................19

Impeller/Diffuser Cover Alignment.....................................................................................................................24

Impeller/Diffuser Clearance Calculation ...........................................................................................................27

6. GEARBOX DISASSEMBLY ..................................................................................... 30

7. INSPECTION OF DISASSEMBLED HARDWARE................................................... 44

8. CHECKING AND SETTING HIGH SPEED SHAFT END PLAY............................... 48

9. GEARBOX AND PROCESS END REASSEMBLY.................................................. 50

Gearbox Auxiliary Hardware Installation..........................................................................................................53

10. TROUBLESHOOTING............................................................................................ 54

11. OPERATION........................................................................................................... 57

12. SPARE PARTS....................................................................................................... 58

13. SUNDYNE COMPRESSOR WARRANTY .............................................................. 62

Critical Start-up Checklist ....................................................................................................................................62

Lock-out/Tag-out Guidelines ...............................................................................................................................64

SINGLE SEAL ARRANGEMENT ..........................................................................................................................65

DOUBLE SEAL ARRANGEMENT ........................................................................................................................66

TANDEM SEAL ARRANGEMENT........................................................................................................................67

PHOENIX COMPRESSOR DRAWINGS ...................................................................... 68

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Introduction and Safety

Text Symbols The following symbols may be found in the text of this manual. They have the following meanings:

WARNING: Text accompanied by this symbol indicates that failure to follow directions could result in bodily harm or death.

ELECTRICAL HAZARD: Text accompanied by this symbol indicates that failure to follow directions could result in electrical damage to equipment or electrical shock.

RECOMMENDED: Text accompanied by this symbol indicates recommended usage.

REMINDER: Text accompanied by this symbol indicates a reminder to perform an action.

EQUIPMENT USE ALERT: Text accompanied by this symbol indicates that failure to follow directions could result in damage to equipment.

Equipment and Safety Precautions

Sundyne Corporation manufactures compressors to exacting International Quality Management System Standards (ISO 9001) as certified and audited by Lloyd’s Register Quality Assurance Limited. Genuine parts and accessories are specifically designed and tested for use with these products to ensure continued product quality and performance. Sundyne cannot test all parts and accessories sourced from other vendors; incorrect design and/or fabrication of such parts and accessories may adversely affect the performance and safety features of these products. Failure to properly select, install or use authorized Sundyne pump parts and accessories is considered misuse and damage or failure caused by misuse is not covered by Sundyne’s warranty. Additionally, modification of Sundyne products or removal of original components may impair the safety of these products and their effective operation.

CAUTION Sundyne compressors may handle hazardous, flammable, and/or toxic fluids. Proper personal protective equipment should be worn. Precautions must be taken to prevent physical injury. Residual fluids must be handled and disposed of in accordance with applicable environmental regulations. Note: Safety procedures must be applied

prior to any installation, maintenance, or repair of a Sundyne compressor. Failure to follow safety precautions may lead to injury!

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Wearing Personal Protective Equipment To ensure safety, protective equipment must be worn at all times when installing, performing maintenance, or repairing equipment. The following safety recommendations must be adhered to for optimum safety:

• Safety glasses, with the minimum requirement of side shields, must be worn at all times.

• Steel-toed shoes must be worn when lifting equipment greater than 15 pounds (7 kg) or if pallet jacks or forklifts are operated.

• Hearing protection is strongly recommended at all times when noise levels exceed 85 dB during an eight (8.0) hour period.

Note: Chemical resistant gloves must be used

if chemicals are utilized (refer to Using Chemicals for additional information).

Note: A dust mask respirator must be worn if

chemicals have warning labels regarding fumes, dust, or mists.

When using more than one piece of protective equipment, consider their compatibility. For example, safety glasses will not interfere with hearing protection equipment. Be sure to clean all pieces of personal protective equipment immediately after each use. Using Forklifts Any persons operating a forklift must have an active recognized operator license. Note: Before initializing forklift operation,

verify that the lift is in a safe operating position.

Ensuring Electrical Safety All electrical sources must be powered-off before installation, service, or repair of equipment occurs. Note: Sundyne recommends that a Lock-

out/Tag-out program be followed prior to altering the equipment. Locks or tags must be provided to warn employees that equipment is temporarily unavailable.

Once all work has been completed, the person installing the lock or tag must remove it according to company procedure. Testing Equipment Prior to performing a test on newly installed, maintained, or repaired equipment; all personnel in the immediate area must be warned. Note: Follow company procedures prior to

equipment testing at all times.

Using Chemicals Any chemicals to be used must be accompanied by a relevant material safety data sheet (MSDS), in accordance with government legislation. If applicable, use chemical proof gloves. Note: An eye wash station (or equivalent)

should be available in the event of injury. If any hazardous or flammable chemicals pass through the equipment, a complete decontamination of the equipment is required.

Protection from Falling Fall protection and associated preventative measures are required when working on equipment located six feet or higher from the ground. Note: Follow company fall prevention

procedures prior to working on equipment.

Preventative Machine Guards Preventative guards must remain in place on all equipment. Note: Only remove the guards while

performing maintenance or repair.

Replace the guards immediately after working on the equipment and prior to start up.

EXPLOSION/FIRE HAZARD

Note: Never use an acetylene torch, open flame, or heat to attempt to remove parts that have seized together in Sundyne equipment. Any residual process gas or liquid that is flammable can result in an explosion or fire with potential for serious injury or death.

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Using This Manual: Organization This manual is part of the final data package for the Sundyne LMC/BMC Phoenix compressor. In addition to this manual, the final data package includes such information as the following: Drawings, Sundyne specification sheet with test performance curves, test data, inspection data, material certificates if required; and auxiliary equipment information. When using the specification sheet, section 1 of the final data package, and drawings, last section of final data package, in this manual compare the release date with those in the maintained final data package to ensure that you are using the most current information. This manual explains procedures for the Sundyne compressor, including how to: install it, maintain it, service it, troubleshoot problems; and order parts. Whenever you talk or write to your Sundyne representative, provide your compressor’s unique serial number. This manual contains the following sections: 1. Installation Describes how to install the compressor and how to store it until you install it. 2. Lubricating Oil System Provides the following information: how to prepare the gearbox for start-up; how the lubricating oil

system works; and specifications for gearbox lubricants. 3. Start-up Provides a procedure for starting and controlling the compressor. A critical start-up checklist is

included as Reference A. 4. Servicing Provides procedures for servicing the compressor. 5. Maintenance of the Seals and Process End Disassembly Provides procedures for disassembling the LMC/BMC compressor and its seal housings. 6. Gearbox Disassembly Provides procedures for disassembling & reassembling the gearbox of the compressor. 7. Inspection of Disassembled Hardware Provides procedure for inspecting the disassembled hardware. 8. Checking and Setting High Speed Shaft End Play Provides procedure for checking and setting high speed shaft end play. 9. Gearbox and Process End Reassembly Provides detailed reassembly procedure of gearbox and process end.

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10. Troubleshooting Provides tables for the following: a) Looking up a problem. b) Identifying the possible cause. c) Selecting the corrective action. 11. Operation

Provides general guidelines for controlling a compressor such as surge control, suction throttling, discharge throttling, and speed control.

12. Spare Parts

Contact and reference information. 13. Sundyne Compressor Warranty

Provides a warranty statement for the compressor/gearbox unit. Reference A Critical Start-up Checklist

Reference B Lock-out/Tag-out Guidelines

Reference C Seal Arrangement Drawings for single, double, and tandem configuration

Reference D Phoenix Compressor/Gearbox Drawings 1. Installation This section provides an introduction to the compressor, procedures for inspecting and installing it, and procedures for storing it if you are not installing it immediately. It contains a subsection on each of the following: Introduction: This provides a brief description about the compressor and how it is used. Inspection: As soon as you receive the compressor, inspect it thoroughly. Short-term Storage: If the unit will be installed within 6 months follow these procedures. Long-term Storage: If the unit will not be installed within 6 months follow these procedures. Suction and Discharge Piping: Follow these procedures to set up the piping for suction and discharge. Seal Environment Control System: Follow these procedures to set up the seal environment controls, even if you use the standard system supplied by the factory. Baseplate Grouting: Use this information for applying grouting to the baseplate. Horizontal Unit Gearbox Support Bracket: Follow these procedures to drill and pin the gearbox support bracket on a horizontal unit. Driver and Coupling: Follow these procedures to align the driver and the compressor. Do this after grouting, and before you connect the piping for suction and discharge.

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Introduction to the Sundyne Compressor Sundyne LMC/BMC compressors have a single stage with an integral gearbox. It increases the pressure of a continuous flow gas by applying centrifugal action. Sundyne LMC/BMC compressors are most commonly used in chemical process plants to increase the pressure in a recycle loop. They are also used in refineries, petrochemical plants, and power generation plants. Within these facilities, Sundyne Compressors are used in booster, regeneration, vapor recover, boil-off, and other gas process applications. Sundyne LMC/BMC compressors offer industrial quality in a compact unit that is simple to assemble. It provides high-energy performance and competitive efficiencies. For detailed specifications for Sundyne LMC/BMC compressors, see the specification sheet and bill of materials or consult Sundyne Compressors. For the primary components, see Reference D, compressor /gearbox module drawings. Inspection 1. When you receive the Sundyne LMC/BMC compressor, check for any damage. If you find any, inform

the carrier and Sundyne promptly. 2. Use Outline drawings in the final data package to ensure that all auxiliary items are properly included. 3. Check the gearshaft carefully. Seal drag may cause it not to turn freely at first. This is normal. But if

the gearshaft binds, it may be damaged, or it may need adjusting.

Short-term Storage - 1 day to 6 months 1. If the compressor is to be stored near strong chemicals or salt water, protect it immediately. To do

this, follow steps 5 through 11 from the long-term storage procedures below. 2. Protect the unit from moisture and dust. 3. Make sure that the factory’s shipping covers for the housing flanges and the seal ports are securely

in place. 4. Carefully follow the instructions provided by the manufacturer of the motor or turbine driver.

Long-term Storage - 6 months or more If you store the LMC/BMC compressor for a long period of time, the methods you use are very important. Please contact Sundyne at (303)-425-0800 USA and ask for the Field Service Department for further instructions. 1. Be sure the storage area has: Humidity below 65%; and temperature range from 45° to 85°F (7°C to 29°C). 2. Do not allow contact of airborne chemicals with the internal components of the unit. 3. If the unit is being stored near strong chemicals or salt water, protect it immediately. 4. Protect the unit from moisture and dust. 5. Make sure that the factory’s shipping covers for housing flanges and seal ports are securely in place.

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6. Prevent corrosion to the components of the gearbox and the fluid-end. 7. Store the unit indoors. 8. Keep the room temperature and humidity constant. 9. Use desiccant bags to absorb moisture. Either of the following: 10. Purge the internal components with an inert gas. or 11. Oil flooding of component internals Review Long Term Storage Instructions supplied with Final Data Package. Should you have any

questions, contact the factory in Arvada, Colorado.

After long-term storage, have an authorized Sundyne service engineer inspect all components and supervise any necessary repair to be sure that they work properly. Any components not made by Sundyne (except mechanical seals) must be inspected or replaced as determined by the manufacturer’s authorized personnel, at the purchaser’s expense. Any Field Service work must be clearly stated at the time of purchase to validate an Extended Warranty.

Because storage location and unknown factors at the site or storage are beyond our control, Sundyne does not accept any liability for damage to the equipment during storage, nor do we guarantee the quality of the equipment during and after the storage period. An Extended Warranty will be null and void if the proper equipment preparation is not maintained.

Installing the Suction and Discharge Piping - Guidelines Step 1: Clean the suction line. Step 2: Install a strainer to protect the impeller from damage by mill scale, welding slag, or other

foreign particles. Step 3: Make sure that the piping is aligned with the compressor flanges. Step 4: Support all piping independently of the compressor. Step 5: When you move the piping into place, never use excessive force at the flanged suction and

discharge connections. This could strain the unit. Step 6: Use suction pipe that has a diameter at least as large as the diameter of the suction inlet of

the compressor. Step 7: Make sure that the suction and discharge piping have no unnecessary elbows, bends, and

fittings. These increase the losses caused by friction. Also, be sure that all piping and fittings are large enough to minimize losses caused by friction.

Step 8: Before you connect the piping to the compressor, tighten the hold down-bolts on the

compressor. Step 9: Do not use elbow parts near the suction flange. A straight pipe run of at least 3 times the pipe

diameter is desirable between an elbow and the suction flange.

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Step 10: Use block valves on both suction and discharge pipes to isolate the compressor during shutdown, minimize process leakage, and reduce the likelihood of backflow through the compressor, which can cause reverse rotation.

Seal Environment Control System For the seal used with the compressor, always maintain the environment shown on the specification sheet for your unit. For some arrangements and applications, you may need a system to control the seal environment. For many applications, you can obtain a standard system from the factory. Make sure that the system is installed properly and that the ports are open or plugged, as applicable. See Outline drawing in the Final Data Package. Always be sure to leave port 1 free to drain leakage from the gearbox oil seal and vent the gas seal. You must vent case drain port 1 to atmospheric pressure and allow it to gravity drain properly. Otherwise oil could contaminate the outboard gas seal. This port can be attached to a flare line, but should not have back-pressure in excess of 5 psi. A. GAS BUFFER SYSTEM – A gas buffer system must be used with double gas seals to prevent

process gas leakage out of the compressor. The buffer must be a cooled, dry, filtered gas, which is compatible with the process gas and the compressor metallurgy. The buffer is introduced into seal port 7 at a pressure range of 40 to 80 psi (2.8 to 5.6 kg/cm2) greater than compressor suction pressure (max. of 160 psig – 11.2 kg/cm2) and at an average temperature no higher than 250°F (121°C). Part of the buffer flows across the lower seal into the process gas and part flows across the upper seal and is vented from port 1. A buffer flow of 1.0 to 2.0 scfm (0.028 to 0.056 Nm3/min) must be maintained through the seal cavity, and should be regulated by a valve or orifice on port 2. It is also acceptable to provide a buffer into port 2 and regulate by a valve or orifice out of port 7. The buffer system must be in operation prior to starting the compressor. Refer to compressor specification sheet for specific buffer requirements.

A buffer gas may also be used between tandem seals to reduce process leakage when buffer contamination of the process gas is not permissible. Contact the factory for buffer pressure and flow requirements.

B. LIQUID BUFFER SYSTEM – A liquid buffer system is used with double liquid seals and is functionally identical to a gas buffer. The buffer liquid is introduced into port 7 or 2, allowed to flow through the seal cavity, and out the opposing port. Buffer flow should be 0.5 to 3 gpm (2 to 12 liters/min) with an inlet temperature of 60° to 120°F (16° to 49°C), and inlet pressure a minimum of 20 psi (1.4 kg/cm2) above process suction pressure.

If a closed loop buffer system is used, the buffer must be cooled prior to returning to port 7. Otherwise, heat generated by seal friction will build up in the buffer, resulting in shorter seal life. If an open loop system is used, an orifice or valve on port 2 should be used to regulate flow to proper value.

NOTE The compressor casing of units with double liquid seals must be drained prior to starting.

C. SEAL FLUSH – An optional seal flush system is available for use with single or tandem gas seal

arrangements when the process gas is contaminated with dust, dirt, or any other types of solid particles. A clean, cool gas, either from external sources or cooled, filtered gas throttled from the discharge is introduced into port 5 or 6 at a pressure slightly higher than suction pressure. Thus, only clean gas will contact the seal face minimizing erosion and seal deterioration.

A flush is not required with a double gas seal due to the flushing action of the buffer leakage across the lower seal.

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D. PORT 1 PIPING – Units equipped with gas seals must vent case drain port 1 to atmospheric pressure and allow it to gravity drain properly. Otherwise oil could contaminate the outboard gas seal. This port can be attached to a flare line, but should not have back-pressure in excess of 5 psi.

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Baseplate Grouting A rigid concrete mounting base is recommended for all installations. Use a non-shrink grouting to fill the baseplate grout-fill holes. The concrete foundation should have minimum deflections and freedom from resonant frequencies in the operating range of the equipment being supported. The stand shall be secured in position by one inch diameter bolts. The bolts shall be installed in the foundation with sufficient length to protrude one quarter inch above the nut. The customer shall provide a 4” x 4” x 1/4” steel plate under each leveling screw. BMC UNITS WITH HORIZONTAL STANDS: The base plate should be leveled prior to grouting. Grout shall set for the time limit as determined by the grout manufacturer. LMC UNITS WITH VERTICAL STANDS: The top of the stand (driver mounting surface) should be leveled by shimming under the base prior to grouting. The channels are to be filled with grout through the access holes. The nuts on the foundation bolts should not be tightened until the grout has set as determined by the grout manufacturer. Horizontal Unit Gearbox Support Bracket A gearbox support bracket (BK01AW04) is attached to the gearbox bearing plate and provides support to the gearbox in the horizontally mounted configuration. The bracket is a two-piece slotted hole design attaching the two pieces to provide adjustability in the field during field installation alignment. A shim (1/4” thickness preferred) should be placed under the bracket and alignment completed. The bracket should then be drilled and pinned (3/8” minimum pin diameter) in two locations to prevent possibly shifting of the bracket during operation of the unit.

Driver and Coupling Lock out starting switch on driver prior to working on coupling, following lock-out/tag-out procedure. UNITS WITH VERTICAL OR HORIZONTAL STANDS - ALIGNMENT-- If other than Sundyne supplied couplings are used, they must be flexible disc or gear type couplings capable of tolerating parallel and angular misalignment of .005 inch maximum as well axial end play of .060 inch maximum. Always refer to the coupling manufacturers recommendations for installation and maintenance. The motor and compressor coupling hubs are normally installed at the factory. For alignment specifications, see Coupling Manufacturers Bulletin in the Final Data Package. Align the driver and compressor after grouting and before you connect the suction and discharge piping. After you install the piping, inspect the alignment again. 2. Lubricating Oil System Oil Specification

The oil used in Sundyne gearboxes must meet the specifications presented in Field Engineering Bulletin 40.2.04. In general, an ISO viscosity grade 32 oil will meet these specifications. Before using any oil, you should verify its properties by consulting its manufacturer..

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Field Engineering Bulletin

Sundyne & Sunflo & HMP Gearbox Lubricant Recommendations

EFFECTIVE : MAY 2006 Rev: E

For years the preferred gearbox lubricant for Sundyne pumps and compressors has been automotive automatic transmission fluid (ATF). However, over time the additives in automatic transmission fluid have changed to coincide with the technical improvements in automobile transmissions. The additives in the new formulations of ATF, such as Dexron III, have been found to have negative effects on Sundyne gearboxes and could compromise mechanical integrity and reliability of the equipment. ISO Viscosity Grade 32 or 46 general purpose or synthetic oils are the recommended lubricants for Sundyne gearboxes as shown in Table 1 below. ISO VG 46 lubricants are now recommended for high horsepower gearbox models 33X and 34X with spherical roller bearings and high ambient temperature installations. Gearbox lube oil should be changed twice yearly or more frequently in severe environments which may be detrimental to the lubricant. Oxidized oil is frequently characterized by a darkening and/or thickening of the oil. Operating of gearboxes with oxidized lubricant should be avoided. Synthetic oils possess different characteristics than conventional mineral oils which make them desirable for various extreme conditions such as high and low temperature operation. Synthetic oils offer very low pour points, high temperature oxidation stability and a higher viscosity index. The operation of Sundyne equipment in high or low ambient conditions may require special consideration of gearbox lubricant and/or supplemental protective equipment such as heat exchangers or gearbox heaters. The lubricant chosen must be compatible with gearbox elastomers, Viton and Buna N. Any oil that contains an inert additive such as PTFE, molybdenum disulfide or silicon should not be used in Sundyne gearboxes. Use of lubricants containing inert additives will void the product warranty. Table 1: Use ISO Viscosity Grade 32 Lubricant ** Use ISO Viscosity Grade 46 Lubricant

Models: LMV/BMP-311 LMC/BMC-311F

LMC-BMC-311 LMV/BMP-313 LMC/BMC-313 LMV-322 All Sunflo Gearboxes HMP-3000 HMP-5000

Models: LMV/BMP-331 LMV/BMP-341 LMC/BMC-331F LMC/BMC-341F LMC/BMC-331P LMC/BMC-341P LMV/BMP-333 LMV/BMP-343 LMC/BMC-333 LMC/BMC-343 LMC/BMC-337 LMV-346 BMP-338 LMC/BMC-347 BMP-348

** Use ISO VG 46 lubricant for high ambient temperatures above 40 °C (100 °F).

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Recommended ISO VG 32 gearbox lube oil specifications:

Gravity, API 28 - 37 Pour Point, °C (°F) -7 (20) max. Flash Point, °C (°F) 204 (400) min. Viscosity, cSt at 40°C cSt at 100°C SUS at 100°F SUS at 210°F

28.8 to 35.2 5.2 min. 150 to 180 44 min.

Viscosity Index 95 min. ISO Viscosity Grade 32 Color, ASTM D 1500 1.5 Neutralization Number, Maximum 0.20 Rust Protection, ASTM D 665, A & B Pass Demulsibility, ASTM D 1401 Time to 0 ml emulsion at 54°C (130°F) after 30 min. at 82°C (180°F) after 60 min.

Pass Pass

Foam Limits, ASTM D 892 Sequence 1 Sequence 2 Sequence 3

25/0 max. 50/0 max. 25/0 max.

Note: No other additives are recommended.

Recommended ISO VG 46 gearbox lube oil specifications: Gravity, API 28 - 37 Pour Point, °C (°F) -7 (20) max. Flash Point, °C (°F) 204 (400) min. Viscosity, cSt at 40°C cSt at 100°C SUS at 100°F SUS at 210°F

41.4 to 50.6 6.5 min. 217 to 260 48.8 min.

Viscosity Index 95 min. ISO Viscosity Grade 46 Color, ASTM D 1500 2.0 Neutralization Number, Maximum 0.25 Rust Protection, ASTM D 665, A & B Pass Demulsibility, ASTM D 1401 Time to 0 ml emulsion at 54°C (130°F) after 30 min. at 82°C (180°F) after 60 min.

Pass Pass

Foam Limits, ASTM D 892 Sequence 1 Sequence 2 Sequence 3

25/0 max. 50/0 max. 25/0 max.

Note: No other additives are recommended.

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Lube Oil System The integral Sundyne lube oil system consists of the following major components: gearbox sump, main lube pump, oil heat exchanger (if necessary), and oil filter. Oil is taken from the sump by the lube pump, then passed through internal passages to an external integrally mounted manifold, through the heat exchanger, then through the filter and back into the gearbox to the bearings. After passing through the bearings, the oil drains back to the sump.

The gearbox sump holds approximately seven U.S. quarts (7.4 liters) of oil not including auxiliary piping and heat exchanger. For wet sump gearboxes, fill gearbox within ¼” from top of oil level sight glass. DO NOT overfill gearbox, as this will cause excessive foaming and overheating of the oil.

The main lube pump is a constant displacement gear type pump directly driven by the input shaft.

The standard heat exchanger is a shell and tube water cooled type mounted on the gearbox manifold. Some low speed or low temperature units do not require a heat exchanger. For units having a heat exchanger, cooling water should be provided at 150 psig (11 kg/cm2) maximum pressure. See the specification sheet for cooling water requirements. Coolant flow should be controlled by a hand valve installed in the cooling fluid discharge line to maintain a gearbox sump temperature between 140°F to 200°F (60°C to 93°C). Approximately one hour may be required to stabilize temperature.

The oil filter is a disposable pleated paper element type. Gearbox oil and filter should be changed every six months. Optional Lube Oil System Auxiliaries

A. LUBE OIL PRIMING KIT – A pre-lube system is required on units operating at high speed,

high pressure, or high horsepower conditions. It is also mandatory with the use of certain auxiliary equipment. The kit consists of a motor driven positive displacement pump, check valve, gages, and necessary piping. To start compressor, operate the pre-lube pump at least 30 seconds with a minimum of 7 psig (0.492 kg/cm2) indication prior to starting the main driver.

The pre-lube pump is to shut down only after main driver is at full operating speed.

B. REMOTE HEAT EXCHANGER – Some large water-cooled and all air-cooled heat exchangers are mounted off the gearbox. Except for packaged units, the interconnecting piping is the purchaser’s responsibility. The heat exchanger MUST be mounted lower than the oil filter; otherwise, air pockets may be present in the lube oil lines at start-up, causing oil starvation at the bearings. Equivalent length of piping and fitting must not exceed 20 feet (6m), using minimum of 3/4” (19mm) I.D. tubing or pipe. If greater pipe lengths are required, pipe diameter must be increased accordingly.

C. GEARBOX SUMP HEATER – A sump heater is required when ambient temperatures may fall below the temperature at which the gearbox oil becomes too viscous for proper lube pump operation. Both steam and electric sump heaters are available. The lube oil priming pump must be operated anytime the sump heater is in operation.

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3. Start-up If a Sundyne supplied control panel is to be used with the Sundyne LMC/BMC compressor, use the control panel recommended start-up procedure in addition to the steps below. Before starting the LMC/BMC compressor, complete the following procedure in the order in which the steps are provided: Step 1: Make sure that the driver has been serviced as per manufacturer recommendations. Check motor rotation before installing coupling. Step 2: For the auxiliaries: Check the connections of the utilities; verify that the auxiliary piping

meets the requirements shown in the Outline Drawing. Step 3: Install flushing screens in all field-assembled piping connections. Clean these screens

prior to commissioning. Check frequently for cleanliness and clean as needed. Step 4: Drain any liquids (blow-down) from the compressor and inlet pipe. Step 5: Prime the lubricating system, as follows:

• Fill the oil reservoir with lubricating oil in accordance with the Field Engineering Bulletin Gearbox Lubricant Recommendations.

• Add oil as necessary through the fill opening. • With wet sump compressors, add oil as necessary until the oil level stabilizes at

the top of the bull’s eye in the sight glass. With dry sump, check oil level at reservoir sight glass.

• Start the auxiliary lubricating pump, and run it until the oil reaches the correct pressure and temperature. Add oil as necessary until the oil level stabilizes 3/4 of the way from the bottom of the sight glass.

• Allow lube pump to operate for at least 30 seconds with a minimum of 7 psig (0.492 kg/cm^2) indication prior to starting the main driver.

Step 6: Turn on the cooling water to lubrication systems heat exchanger (if applicable), or turn on

air cooled heat exchanger. Verify high points (e.g. heat exchanger and filters) have been vented.

Step 7: For double seal configurations, the buffer system must be pressurized to the pressure

specified on the spec sheet and on outline drawings prior to pressurizing the unit. Step 8: Charge the compressor with process gas. Step 9: Start compressor, following process control startup procedures. Step 10: Once the gearbox oil temperature has stabilized, adjust cooling water supply until the oil

temperature to the bearings is 120º - 160ºF on units equipped with water cooled heat exchangers. Maximum recommended temperature is 180ºF.

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Compressor Control During Start-Up Single Units:

A. Suction throttling (preferred method). Start compressor with the discharge valve open while throttling the suction valve to bring the compressor to the design operating point.

B. Discharge throttling. Start the compressor with the suction valve completely open

while throttling the discharge valve to bring the compressor to the design operating point.

C. Other Methods – Insure that the compressor does not go into surge (flow too low) or

that the design horsepower is not exceeded (flow too high) while starting or operating the compressor. Check units specification sheet for flow limits

Series Operation:

In series operation, it is necessary to have a bypass from the discharge of the second stage back to the suction of the first stage. A check valve should be placed in the discharge line downstream of the bypass. Typical start-up procedure is as follows: A. Open the suction and discharge block valves and the bypass valve. B. Start the second stage unit and maintain stable operation. C. Start the first stage unit and maintain design flow to both units. D. When sufficient pressure is being produced to overcome system back-pressure, the

check valve will open and the units will be on stream. E. Close the bypass valve, being sure that the flow to the compressor is above the

surge point. Parallel Operation:

Check valves must be placed in the discharge piping of each compressor to prevent back-flow when one unit is started prior to the others. It is advantageous to install separate bypass loops around each compressor for additional operational flexibility.

The first unit may be started as described above for single units. However, prior to starting the second unit, it is preferable that the on-stream unit not be operating near its peak head capability. This will lessen the chance of surging when the second unit is started.

Run-In of the Compressor

If the compressor is to be run-in or mechanically tested under conditions which are considerably different from those that the unit is designed for (such as gas molecular weight, suction pressure, flow rate, etc.) Sundyne should be consulted to insure that the run-in conditions are compatible with the compressor.

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4. Servicing General Requirements To increase the operating life of your compressor and keep it in good operating condition, you should inspect and service it regularly. Measure all of the operating parameters documented in the specific maintenance procedures and log your measurements. Make sure that all major equipment, such as lubricating pumps, heat exchangers, and instrumentation, perform according to the manufacturer’s recommendations. Whenever you find a deviation from specifications, identify its source immediately, and take any corrective steps that are required to bring the unit into manufacturer’s specifications. Regular Maintenance Gearbox Oil Check the level of the oil in the gearbox immediately before and after initial start-up, and regularly while the compressor is running. Be sure to keep the level of the oil within the gearbox design limit. The oil level must be maintained within the MIN/MAX range on the sight glass. You can add oil to the wet sump gearbox while the compressor is running. See tagging information on gearbox for where to add oil during operation. This location is different from the initial fill location. Each must be used for its tagged purpose. Overfilling the gearbox will cause excess foaming and overheating and should be avoided at all times. Oil may be added to the external reservoir of the dry sump gearbox at the fill port. Oil Pressure The correct oil pressure from the main pump of the gearbox depends on the configuration of the bearings and the characteristics of the lubricating oil used. In the normal operation, the oil pressure supplied to the gearbox should be between 18-60 psig (1.2 - 4.2 Kg/cm2 ) (15 psi alarm, 10 psi shutdown). Changing the gearbox oil and filter Change the oil in the reservoir and the oil filter elements every 6 months. SFHC recommended synthetics may go for a longer period of time before an oil change out is required. For dual oil filter units with a transfer valve, vent and fill the idle oil filter before operating the transfer valve. Seal Leakage Seal leakage out of port 1 should be checked periodically. Seals should be replaced if leakage increases to an unacceptable level. With double seals, buffer pressure and usage should be monitored to insure that seals are functioning properly. Driver Inspect the driver to make sure that it performs according to the manufacturer’s specifications. Coupling Inspect the coupling according to the manufacturer’s specifications. Never operate the compressor without first checking the coupling guard. A compressor with a missing or incorrectly installed guard could cause serious or fatal injury.

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5. Maintenance of the Seals and Process End Disassembly This section provides the procedure for disassembling the LMC/BMC compressor and its seal housings for maintenance of the seals. The gearbox assembly is shown in Reference D, gearbox module drawing.

Follow your organization’s Lock-out/Tag-out instructions before working on the compressor. Failure to follow adequate Lockout/Tag-out procedures could cause serious injury. Follow your organization’s procedures for blocking in or isolating the compressor from the process, for depressurizing, and for decontamination before disassembly. Tandem Seal Configurations Depressurize the seal buffer system before depressurizing the compressor, otherwise reverse pressure may cause the inboard seal to fail. Double Seal Configurations The compressor must be depressurized before the seal buffer system is depressurized, otherwise reverse pressure may cause the inboard seal to fail. Item numbers refer to the numbers in Reference D, gearbox module drawings. The following procedures apply to all configurations of the Sundyne LMC/BMC compressors. Refer to the specification sheet to determine the specific configuration and optional equipment included in your unit. Parenthetical numbers in the text correspond to item numbers in the illustrations and parts lists.

Procedure for Disassembling Process End The following replacement parts will be required as a result of compressor disassembly and seal housing removal:

Table 5.1 PART DESCRIPTION ITEM

NUMBER QUANTITY

O-Ring Packing 936B 1 O-Ring Packing 936C 1 O-Ring Packing 936D 1 O-Ring Packing 936E 1 O-Ring Packing 936F 1 O-Ring Packing 936G 1 O-Ring Packing 936H 2 O-Ring Packing 936J 3 Single Seal 60A 1 Double Seal 60A, 60B 2 Tandem Seal 60A, 60B 2 Thermal Barrier Gasket 87A 1

NOTE: An O-Ring repair kit is available. This kit contains the O-Rings required to replace the gearbox and compressor mechanical seals.

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Step 1 Remove the driver and gearbox from the compressor housing as follows:

(3X2 compressor case shown in photo) Vertical units without a driver stand (shown here) Remove attaching hardware and lift driver from gearbox. Remove nuts (914A) from compressor casing studs. Lift the gearbox and seal housing from the compressor casing, taking care not to damage the impeller. Place the gearbox on a suitable support with the impeller inclined upward.

Vertical units with a driver stand Remove bolts (909D) securing the coupling guard. Remove the coupling guard. Disengage both ends of the spacer coupling and remove the floating shaft. Remove nuts (914A) from the compressor casing studs and release the stiffening brackets. Attach the integral turnbuckles to the gearbox bearing plate (102). Using the turnbuckles, lift the gearbox and seal housing from the compressor casing. Exercise care to prevent damage to the impeller. Place the gearbox on a suitable support with the impeller inclined upward.

BMC Units Remove bolts (909D) securing the coupling guard. Remove the coupling guard. Disengage both ends of the spacer coupling and remove the floating shaft. Attach a hoist to the gearbox using eyebolts in the tapped holes on the bearing plate. Eyebolts can also be placed in the gearbox input housing as in above photo. Remove nuts (914A) from the compressor casing studs and disconnect gearbox bracket (BK01AW04) from the main base. Store any shims between the bracket foot and the main base. Remove the gearbox and seal housing from the compressor casing by moving them toward the driver until the impeller clears the compressor casing. Place gearbox on a suitable support with the impeller facing upward.

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NOTE: The gearbox can be worked on while in a horizontal position. However, the diffuser cover must be prevented from falling off when the impeller is removed. If the cover falls from its location severe damage to cover and output shaft (high speed shaft) will occur.

Step 2 Prevent impeller from rotating and

remove impeller bolt (3).

NOTE: Impeller bolt may have either a left-hand or a right-hand thread depending on impeller rotation direction. Left-hand rotation impellers will have a left-hand thread impeller bolt and right-hand rotation impellers will have a right-hand thread impeller bolt.

(full emission impeller shown) Compressors that utilize clockwise impeller rotation when viewed from the inlet, have left hand thread impeller bolts, and counterclockwise rotating impellers have right hand thread bolts.

Step 3 Remove impeller (2). It may be

necessary to pry under the impeller and cover (15) to loosen it from the shaft. Pry on opposite sides of the impeller so that the impeller is removed evenly.

The impeller is dynamically balanced and should be replaced or rebalanced if it shows any sign of damage.

(full emission impeller shown) Step 4 Remove diffuser cover (15) from seal

housing (30).

Use a flat blade screw driver inserted into pry slot of cover (15) to help lift cover from seal housing (30).

(full emission impeller shown)

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Tandem Seal Disassembly

Step 1 Remove the seal rotating face (51a). NOTE: Tandem Seal Arrangement shown here. See Reference C, Seal Arrangement Drawings, for single and double arrangements. Step 2 Remove hex head cap screws (905E),

washers (916A) and remove lower mechanical seal (60A) of the tandem seal arrangement from the seal housing.

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Step 3 Remove spacer sleeve (60A). Step 4 Remove o-ring (936J). Step 5 Remove upper seal rotating face (51C).

Use two small screw drivers to lift up the rotating face.

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Step 6 Remove the hex head cap screws

(905A), lock washers (154AT), flat washers (916AG), and seal washers (916S) from seal housing (30).

Step 7 Install two 3/4” eye-bolts, approximately

180° from each other, through the seal housing flange face.

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Step 8 Use hoist and equal length chain hooks to lift seal housing off the gear box.

Step 9 Turn seal housing (30) over so you can

see the upper Tandem seal, and remove the Thermal Barrier Gasket (87A).

It may help to have to people on hand to help rotate seal housing.

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Step 10 If upper seal from Tandem seal

arrangement requires removal; remove hex head cap screws (905F), and lock washers (916B).

Step 11 Remove upper mechanical seal (60B).

& Carefully inspect the seals for abrasive particles, excessive seal face in the retainer. Replace or rebuild any faulty mechanical seal. Seals may be rebuilt by replacing the carbon seal nose, o-ring, and springs, providing retainer is not damaged or heavily worn. A seal repair kit is available; contact your customer representative or the factory. Replace or lap the seal rotating face if the wear track is rough or worn to a depth greater than .0002-inch.

Step 12 Remove spacer sleeve (50B) from high

speed shaft. Note o-ring (936J) will be lifted off high speed shaft along with spacer sleeve (50B).

Clean and inspect all items for unusual wear or damage. Replace all worn parts.

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Impeller/Diffuser Cover Alignment The following replacement items will be required as a result of compressor disassembly and diffuser removal:

Table 5.2 PART DESCRIPTION ITEM NUMBER QUANTITY Impeller Spacer 158C Series AR O-Ring Packing 936A 1 O-Ring Packing* 936C 1 O-Ring Packing 936E 1 O-Ring Packing 936F 1 O-Ring Packing 936G 1

*Required only if diffuser is removed. Step 1 Remove impeller bolt (3), and impeller (2). Step 2 Inspect impeller and procure a new one if required. Step 3 Inspect diffuser for signs of damage (i.e. gouging in the bowl areas due to erosion or mechanical damage) Step 4 The impeller spacer (158C) is required to align the blade side of the impeller shroud flush with the diffuser cover (15). The impeller spacer (158C) thickness (“D” dimension of Figure 5.1) must be determined and the correct spacer installed during the replacement of any one of the following components: gearbox assembly, gearbox high speed shaft (A130), or high speed shaft bearings (151A or B), impeller (2), seal housing (30), diffuser cover (15).

NOTE: The original clearances for your compressor as shipped from the factory for the impeller and diffuser are recorded and supplied as part of the final data package. Step 5 The Impeller to Diffuser Cover Alignment Procedure Align the impeller (2) with the diffuser cover (15) as follows: The Impeller to Diffuser Cover Alignment Procedure requires multiple assemblies of the stacked rotating elements mounted on the end of the high speed shaft assembly. The procedure is attempted after the gearbox is completely assembled with the shaft end play checked and within its specification of 0.015” +/- 0.002”. This procedure also assumes that all components have been checked and are in good order. If not, then new parts must be procured. The 1st assembly includes only the mating rings, shaft sleeves, impeller spacer (158C), and impeller (2) and is done without any o-rings, mechanical seal, seal housing (30) or diffuser cover (15). The purpose of the 1st assembly is to ensure that all stacked components are compressed and fit tight when the impeller is torqued to specification. A visual and physical check of these stacked components is required to ensure that they cannot be spun in relation to the shaft. The 2nd assembly requires that all components be installed, except the Item #936G O-Ring between the impeller spacer (158C) and impeller (2). The purpose of this assembly is to check the impeller (2)

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shroud height in relation to the diffuser cover (15) and to determine the correct thickness of the impeller spacer (158C). In the 3rd assembly, once the correct impeller spacer (158C) is determined, the impeller spacer (158C), the o-ring (936G) between the impeller spacer (158C) and the impeller (2), and the impeller (2) are assembled for the final time to complete the assembly. 5a. Assemble the gearbox, less the gearbox mechanical seal and mating ring, the process

mechanical seal(s) and mating ring(s), the seal housing (30), the diffuser cover (15), and impeller (2). Ensure end float is within recommended limits; i.e., 0.015” +/- 0.002”.

5b. With the diffuser cover (15) removed from the seal housing (30), set the diffuser cover bottom

side up on a work bench. Set the impeller (2) in the recessed portion of the diffuser cover and measure the distance from the outside flat surface of the diffuser cover to the front or blade side of the impeller shroud as close to the outside edge of the shroud, as possible. The impeller should be recessed into the diffuser cover a minimum of 0.025”. If the dimension is less than 0.025”, contact Sundyne Compressors in Arvada, Colorado.

5c. Place the gearbox upside down on a workbench or gearbox stand so the end of the high speed

shaft (A130) protrudes upward. All checks from this step on, should take place with the high speed shaft resting down on its upper thrust washer or upper thrust tilt pad bearings.

5d. Assemble the seal component stack-up onto the high speed shaft (A130) without using the

mechanical seals, O-Rings, seal housing (30), or diffuser cover (15). With the high speed shaft (A130) extending upward, slide on the gearbox mating ring (51D), and then the following parts:

For double seals, assemble the upper shaft sleeve (50B), the process mating ring (51C), the lower shaft sleeve (50A), the impeller spacer (15C) and the impeller (2). For single seals, assemble the shaft sleeve (50), the process mating ring (51A), the impeller spacer (158C), and the impeller (2). For tandem seals, assemble the upper shaft sleeve (50B), the upper process mating ring (51C), the lower shaft sleeve (50A), the lower process mating ring (51A), the impeller spacer (158C), and the impeller (2). 5e. To install the impeller (2): -Check the shaft OD pilot fits and the impeller bore pilot fits and ensure that they are clean and free of burrs. Clean up, deburr and polish, as needed, to prevent damage to each during assembly. -Heat the impeller in an oven heated to 350ºF for 30-60 minutes. -Apply a very small amount of anti-seize compound onto the shaft pilot fits to ease the installation and removal of the impeller and to prevent galling. -Lower the heated impeller onto the shaft on top of the stacked up parts, place a soft metal washer over the impeller, install the impeller bolt (Item #3), and torque per Table 8.1. A soft metal washer is placed between the impeller and the impeller bolt to prevent damage to the end surfaces of each part. -Allow the impeller to cool. This process can be accelerated by blowing shop air past the heated wheel. 5f. During the cooling process, retorque the impeller bolt (3) 3-4 separate times to 50 ft. Ibs. When

the impeller is cool, retorque one final time per Table 8.1. 5g. Once the impeller is installed and cool, recheck the stacked components to ensure that they are

all tight and cannot rotate in relation to one another.

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NOTE: Steps 5d-5g serve to check that all stacked components are tight and not loose during assembly. There is no way to check these stacked components with the seal housing installed. Since the impeller to shaft fit is not a loose or slip fit, it is possible to assemble the stacked components and achieve the required torque, even though the stacked components could remain loose and free to turn in relation to the shaft. This could lead to component damage if allowed to operate in this condition. 5h. Remove the impeller (2). 5i. Remove all stacked components, except the gearbox mating ring (51D). 5j. Reinstall the same components, only this time, include all O-Rings, mechanical seals, the seal

housing (30), and the impeller spacer (158C). Leave out the 936G O-Ring between the impeller bolt (3) and the impeller. Place a soft metal washer between the impeller bolt and impeller to prevent galling while torquing the impeller bolt.

5k. Before installing the diffuser cover (15), remove the o-ring (936E) from behind the diffuser cover,

then install the diffuser cover, without the o-ring, on to the seal housing (30). 5L. Reinstall the impeller using the same procedure described in step 5e above. 5m. Measure the distance between the top of the impeller shroud and the diffuser cover (15) per

(Figure 5.1). The impeller shroud should extend .000-.030” beyond or above the diffuser cover (with the gearbox upside down). This is the “E” dimension in (Figure 5.1). If the shroud height is measured out of tolerance, determine the correct impeller spacer thickness and replace it with one of the correct size to ensure the proper shroud height (“E” dimension).

Table 5.3

Part Number Thickness SP01AD02XXF 0.018” SP01AD02XXA 0.030” SP01AD02XXG 0.040” SP01AD01XXB 0.050” SP01AD01XXH 0.060” SP01AD01XXC 0.070” SP01AD01XXD 0.090” SP01AD01XXE 0.110” SP01AD01XXJ 0.020”

5n. Remove the impeller (2). 5o. Remove the diffuser cover (15), reinstall the diffuser cover O-Ring (936E) behind the diffuser

cover, and reinstall the diffuser cover, with O-Ring, onto the seal housing. 5p. Install the impeller spacer (158C) with the correct thickness and the o-ring (936G) between the

impeller spacer and the impeller. 5q. Install the impeller (2) as described in step 5 above. 5r. Recheck the alignment of the impeller (2) shroud to the diffuser cover (15); i.e., Dimension “E” in

Figure 5.1.

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5s. When the impeller is completely cooled, remove the impeller bolt (3) and the soft metal washer and then reinstall the impeller bolt, without the soft metal washer and torque per Table 8.1.

5t. Record the thickness of the impeller spacer (158C) and the impeller shroud to diffuser cover

alignment (Dimension “E” in Figure 5.1) for future reference. Impeller/Diffuser Clearance Calculation The clearance between the impeller and diffuser must be checked and, if necessary, adjusted after the replacement of any of the following parts: gearbox assembly, gearbox high speed shaft (A130), gearbox high speed shaft bearings (151A or B), diffuser (13), impeller (2), compressor casing (1), seal housing (30). Step 1 The required impeller to diffuser clearance is 0.035 - 0.055 inches, see (“A”) dimension in (Figure 5.1). This clearance is obtained by installing shim spacers (158A) between the diffuser and compressor casing, see (“B”) dimension in the (Figure 5.1). The recommended procedure for determining shim spacer requirements is as follows: Step 2 Refer to (Figure 5.1). The seals, seal housing, diffuser cover, and impeller must be installed on the gearbox. The diffuser must be bolted into the compressor case (1). Step 3 Using electrical solder, make a ring that is slightly smaller in diameter than the impeller blade diameter. Place the solder ring on the diffuser and center it around the inlet eye. Use tape to hold the solder in place. Step 4 Install the complete compressor assembly and gearbox in to the compressor case and tighten four equally spaced seal housing nuts (914A) onto the case studs. Use the proper torque given in Table 8.1. Then remove the seal housing nuts and carefully lift out the compressor assembly from the compressor case. Step 5 Measure the thickness of the solder ring at points where it contacted the impeller blades and record the average thickness. This is the “A” dimension in (Figure 5.1). This impeller to diffuser clearance must be between 0.035 and 0.055 inch (0.089 and 0.140 mm). Step 6 If the impeller clearance is not within the proper range, calculate the required change in shims. Add or remove diffuser spacers (158A) to adjust the clearance to the correct range.

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Figure 5.1. Compressor Cross-Section and Clearances

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NOTE: The shim spacers are available in sets of five, including one each of: Table 5.4

0.005 inch (0.13 mm) 0.010 inch (0.25 mm) 0.015 inch (0.38 mm) 0.020 inch (0.51 mm) 0.030 inch (0.76 mm)

Step 7 Install the spacers (158A) in compressor case (1). Step 8 Install O-Ring (936C) on the diffuser (13). Step 9 Install diffuser in compressor case and tighten the three screws (906D) per torque Table 8.1.

NOTE: If a PTFE O-Ring (936C) was installed, perform the following steps, (10) through (14) prior to final assembly of the compressor casing to the seal housing (30). If an elastomer O-Ring was used, proceed to Step 15. Step 10 Place casing (1), with diffuser (13) installed, on solid work surface. Step 11 Place three of the compressor casing attaching hex nuts (914A) or other suitable spacers on upper surface of diffuser. Step 12 Lower the gearbox assembly onto the hex nuts. Install four of the compressor casing nuts (914A) and tighten. This step is necessary to compress the PTFE O-Ring (935C) and maintain the proper final impeller-to diffuser clearance. Step 13 Remove the gearbox assembly from the case and remove the hex nuts that were used as spacers. Retorque three screws (906D) to proper torque values. Step 14 Reassemble the compressor with another solder ring and recheck the impeller clearance. Step 15 Record the new diffuser spacers (158A) thickness (“B” dimension) and the impeller to diffuser clearance (“A”) dimension in (Figure 5.1). Remove the compressor assembly from the compressor case and place short strips or coils of electrical solder taped out on the flat portion of the diffuser. Step 16 Reinstall the compressor assembly and retighten the case nuts. Loosen the nuts and remove the assembly. Measure the solder at the flattened portion and record the diffuser to cover clearance (“C” dimension) in (Figure 5.1). This dimension must be within 10% of the as shipped “C” dimension as shown in the final data package.

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Step 17 Reassemble the compressor installing all the O-Rings into the proper positions. Tighten the compressor case nuts to the proper torque listed in Table 8.1. CAUTION: When PTFE O-Rings are being used, special consideration must be taken to allow for cold flow. Retorquing may be required to obtain proper torque value. 6. Gearbox Disassembly Note: In order to disassemble gearbox it is necessary to complete steps 1

through 16 of Maintenance of the Seals and Process End Disassembly.

Step 1 If you have not drained the oil from the gearbox you should do so now! Remove hex head cap screws (905E) and lock washers (916A) from the gearbox seal flange.

Step 2 Remove gearbox seal (60C).

It is helpful to use a small flat blade screw driver to lift the seal flange up from the aluminum gearbox face.

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Step 3 Carefully inspect the seals for abrasive particles, excessive seal face wear and any binding of the carbon seal nose. Replace or rebuild any faulty mechanical seal. Seals may be rebuilt by replacing the carbon seal nose, o-ring, and spring providing the retainer is not damaged or heavily worn.

Step 4 Remove o-ring (936P). Step 5 Remove rotating face (51D).

Use two small flat blade screw drivers to help lift rotating face out of pocket in the gearbox taking care not to damage the gearbox seal o-ring chamfer. Inspect the rotating face for any cracks, chips, or grooves. If any cracks or chips are present replace the rotating face.

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Step 6 Rotate gearbox in holding device so that

the input shaft (A120) is now pointing up. Make certain that the gearbox is steady and held in place by clamps. Remove nuts (914F) and (914E), remove flat washers (916J) and (916H). Next remove bolts (909C) and (909B), and flat washers (916H) and (916J) making sure that the alignment bolts are removed first. Loosen four round hex head socket screws located on the top of the input seal (115).

Failure to loosen these screws will result in damage to either the input seal (115) or the input shaft (A120).

Step 7 Install two 5/8” eye bolts into the top of

the upper gearbox housing (101B). Use hoist to lift the upper gearbox housing (101B) away from the other gearbox housings.

It is a good idea to look into the upper gearbox housing (101B) and watch to see if the input shaft assembly (A120) roller bearing outer race and rollers stay with the upper gearbox housing (101B). If the bearing does stay with the upper gearbox housing (101B), the mechanic should try to keep the bearing from falling out of the upper gearbox housing (101B) by reaching into the housing and holding the bearing in place. After the mechanic rests the upper gearbox housing (101B) on a bench or table remove the outer race and rollers sliding them back onto the input shaft assembly (A120). Remove the input seal (115) from the upper gearbox housing (101B). Inspect seal. If it was leaking or is damaged replace input seal (115) with a new seal.

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Step 8 Remove the input shaft assembly (A120). To accomplish this the mechanic must first lift up the idler shaft assembly (A140) and tilt it away from the input shaft assembly (A120). The mechanic should grasp the input shaft assembly by the top of the shaft and lift straight up and away from the bearing plate (102). The lower outer race and rollers from the input shaft assembly (A120) will be in the bearing plate (102). Pull the outer race and rollers out of the bearing plate (102) and keep with the input shaft assembly (A120).

Step 9 Install two 5/8” eye bolts into the top face

of the bearing plate (102). The mechanic will use these to lift the bearing plate from the lower housing (101A).

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Step 10 a. Remove the sump tube (173). First loosen the nut on the compression fitting (944C) with a wrench.

NOTE: If dry sump design, unit will not have an internal lube pump and sump tube.

Step 10 b. Then hand spin the nut free. Pull the

sump tube (173) out of the compression fitting (944C).

Step 11a. Remove compression fitting (944C).

Loosen the fitting with a wrench.

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Step 11 b. Hand spin the fitting off the 2.0” x 3/4” pipe nipple (944B).

Step 12 Remove the 2.0” x 3/4” pipe nipple

(944B) using a pipe wrench. Be careful the pipe nipple (944B) screws into the aluminum lube pump housing (A160) and do not force the pipe nipple (944B) or you may strip or pull the threads in lube pump assembly (A160).

Step 13 Remove socket head cap screws (905BU), 10-24 x 2.5” long screw, from the lube pump assembly (A160). There are two screws that hold the lube pump in place and two screws that hold the lube pump together. If by chance when removing (905BU) you loosen the shorter screws, replace immediately and move to the next screw on the lube pump assembly (A160). Note: If gearbox is of dry sump configuration, then a spacer is installed instead of the lube pump. The procedure for removing the spacer is the same as for removing the lube pump.

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Spacer with O-ring sealfor dry sump gearbox

O-ring

Step 14 Install two 1/4-20 screws into the top of the lube pump assembly (A160). These screws are used to turn the lube pump assembly (A160) around in the bearing plate (102).

Note: with the dry sump gearbox, a

spacer with O-ring seal is installed instead of the lube pump.

Step 15 a. Using the 1/4-20 screws in step 14,

turn the lube pump assembly around in either CCW or CW rotation so you can see the o-ring (936Z) in the hole in the bearing plate (102) where the 2.0” x 3/4” pipe nipple (944B) was inserted.

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Step 15 b. Remove the o-ring (936Z) after you can

see it through the hole in bearing plate (102). Use a sharp scribe or needle vise and poke the point into the o-ring (936Z) and twist it out of its seat in the lube pump (A160) and through the hole in bearing plate (102). Replace o-ring with new item. Remove the o-ring (936Y) and (936TQ) from the bearing plate (102) replace with new items.

Step 16 Remove the lube pump assembly (A160)

from the bearing plate (102). To achieve this, the mechanic must grasp the top of the lube pump shaft with their fingers and pull straight up and out on that shaft. Remove the pressure relief valve (175) from the top of the bearing plate (102) Inspect the pressure relief valve (175) for any foreign matter. If any particles or sludge is found replace with a new pressure relief valve (175). Remove 1/2” NPT pipe plug (924M) from the top of the bearing plate (102).

(underside of bearing plate shown)

Step 17 Remove the vibration key-phasor probe from the bearing bracket and then remove gearbox bearing plate (102).

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It is a good idea to use a hoist with equal length chains and hooks to facilitate an even lift of the bearing plate (102). If the bearing plate (102) is not lifted evenly it will catch the upper high speed journal bearing (151B) on the high speed shaft (A130) and possibly damage the shaft or the bearing.

Step 18 Remove the bearing plate (102) from the lower gearbox housing (101A). Make certain you use the 5/8” eye bolts to lift

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Step 18 a. Remove and inspect the upper high speed journal bearing (151B) and the upper thrust washer (155B) from the bearing plate (102). First remove hex head cap screws (905N) and lock washers (154E). Next pull high speed journal bearing (151B) from bearing plate (102). Save shim (158). When inspecting the bearing look for rub marks or uneven wear marks. If the bearing has scratches or dings or any unusual wear replace the upper high speed journal bearing with a new item (151B). If the upper high speed journal bearing checks good tag the bearing as upper high speed journal bearing (151B). This will help insure it does not become mixed up with the lower high speed journal bearing. Inspect the thrust washer (155B). If there are any burns or rubs replace the thrust bearing (155B).

Step 19 Remove idler shaft (A140). To do this the

mechanic must lift the high speed shaft (A130) slightly while pulling the idler shaft (A140) up and away from the high speed shaft (A130).

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Step 20 Remove the high speed shaft (A130). Step 21 Remove socket head cap screws

(905AA) from lower idler journal bearing (151C).

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Step 22 Insert a 1/2” square drive 1.0” socket down into the center of the lower idler journal bearing. This socket is used as a spacer/guide for the jack screw. Make certain the 1/2” square drive hole is pointing toward the thrust face of the lower idler journal bearing (151C).

Step 23 Remove lower idler journal bearing. Use

a bearing puller. Thread two screws 1/4-20 into the two top holes in the lower idler journal bearing (151C). Screw the jack bolt on the bearing puller down against the 1.0” socket, and then jack (pull) the bearing out of its location. Inspect the top thrust face and the interior of the lower idler journal bearing. If there are any burns, rubs, deep scratches, replace the bearing with a new item (151C).

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Step 23 (continued) Step 24 Remove socket head cap screws (905M)

and lock washers (154D) from lower high speed journal bearing (151A). Remove thrust washer (155A) by lifting up and off the lower high speed journal bearing (151A). Inspect the thrust washer for any burns, scratches or rubs. If any of these conditions are found, replace the thrust washer with a new item (155A).

Step 25 Remove the lower high speed bearing

(151A) by tapping (with a soft mallet) on the bottom of the bearing. Inspect the lower high speed journal bearing for any rubs, unusual wear marks or scratches. If anything appears abnormal replace the lower high speed journal bearing (151A) with a new item. If the bearing checks out good then tag bearing as lower high speed bearing (151A), so it does not become mixed up with the upper high speed bearing.

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Step 26 Remove the oil filter (185) if applicable. Step 27 Remove the 1/4” NPT socket pipe plugs

(924GB) and (924G) from the lower gearbox housing (101A)

Step 28 Remove o-rings (936TT) and (936T) and

(936YA) from the lower gearbox housing (101A) and replace with new items (936TT), (936T), and (936YA).

Step 29 Remove socket head cap screws

(905AB) from the upper idler journal bearing (151D) located in the upper gearbox housing (101B).

Step 30 Insert a 1/2” square drive 1.0” socket into

the center of the upper idler journal bearing with the 1/2” square drive pointing toward the thrust face of the upper idler journal bearing (151D).

Step 31 Remove the upper idler journal bearing

(151D). Use a bearing puller. Thread two 1/4-20 screws into the top of the upper idler journal bearing. Insert the bearing puller into the upper idler journal bearing with the jack screw located against the 1/2” square drive hole in the socket and pull the upper idler journal bearing (151D) out of its location. Inspect the upper idler journal bearing for any unusual wear, rubs scratches and burns. If any abnormalities are found replace the upper idler journal bearing (151D) with a new item.

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7. Inspection of Disassembled Hardware Step 1 Remove lube jets, then clean and wash all gearbox housings (101B), (102), and (101A)

with solvent and blow dry with clean high pressure air. Step 2 Make certain to flush out all lube passages and blow dry with clean high pressure air.

Reinstall lube jets into housings immediately. Step 3 Inspect all bearing locations for critical size requirements (see Table 7.1). If any

dimensions are found to be out of tolerance replace that housing or bearing. Step 4 Inspect all bearings for damage, if any damage is found replace the bearings with new

items. Step 5 Inspect all shaft bearing surfaces for scratches, burns, dents, or dings. If bearing

surfaces on shafts are burned and/or scared the shaft should be replaced. Scratches nicks or dings on shafting should be lightly stoned and polished to remove high spots.

Step 6 Check shaft run-outs for trueness. Replace shaft if it is bent. Step 7 Inspect all shafts with gears. If gears are missing teeth, or are burned, replace gear or

integral gear shaft as required. If gears show abnormal wear patterns, or have nicks and dings on the gear teeth, lightly stone or hone and polish nicks and dings from gear teeth. If abnormal wear pattern is evident this could indicate a bent shaft.

Step 8 Inspect the bearing thrust faces on the idler shaft (A140). If thrust faces are burned or

scored, replace the shaft. Check the thrust surface on the lower spur gear for abnormalities or replace the shaft assembly.

Step 9 Inspect the thrust face on the lower idler spur gear that is pressed onto the idler shaft

(A140). If the thrust face on this gear is burned or scored replace this gear. If there are nicks or dings in the thrust face lightly stone or hone and polish these areas back to the original surface.

Step 10 Inspect the internal lube pump (A160) o-ring seal groove. If there are any nicks or dings

in this area, polish or hone them back to the original surface. If this cannot be accomplished replace the lube pump (A160). If your gearbox had a catastrophic lube failure due to the lube pump (A160) you should replace the lube pump as a complete assembly.

Step 11 Inspect the gearbox seal. If the carbon seal nose is nicked, scratched, or dinged,

disassemble the seal and try to lap the seal nose back into tolerance. The flatness specification is two light bands or .00002” flatness minimum. If this cannot be achieved replace the carbon seal nose. Check the constant force spring inside the seal retainer. If it is cracked, bent or deformed other than the cone shape, it should be replaced. Contact your customer service representative for part numbers on this seal.

Step 12 Inspect all the sleeves and spacers that were disassembled from the high speed shaft,

Process End. If there are any nicks or dings in the sleeves or spacers lap the locating surfaces back into tolerance. The specification for these sleeves and spacers is two light bands flatness or .00002” flatness and parallel conditions between the faces of the sleeves or spacers of .0003” maximum. If these specifications cannot be maintained then replace the sleeves or spacers with new hardware.

Step 13 Inspect the process seals. If the carbon seal nose is nicked, scratched or dinged,

disassemble the seals and lap the seal nose back into tolerance. Specification for

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flatness on these seal noses are two light bands or .00002” flatness. Install a seal repair kit for the specified seals in your unit. See your Sundyne Compressor Specification Sheet or Recommended Spare Parts List Bill of Materials for the part numbers.

Step 14 Inspect all rotating faces in your unit (process and gearbox). If rotating faces are nicked,

cracked, or have wear rings from seal contact replace them with new hardware. Check the flatness of the rotating faces to factory specifications. Flatness is specified at two light bands or .00002” flatness. The rotating face for the gearbox seal (51D) is to have a matte finish applied. The matte finish is specified as 10-15 Ra micro finish, and still maintaining the flatness of .00002” or two light bands.

Step 15 Inspect the high speed shaft shoulder where the gearbox rotating face locates. Check for

nicks or dings, and raised surfaces on this shoulder. If any abnormalities are found, the shoulder will need to be relapped to factory specification of two light bands flatness or .00002”. If this specification cannot be met replace the high speed shaft (A130).

Step 16 Inspect the high speed shaft (A130) thrust surfaces. If these show abnormal wear, burns,

gouges, deep circular scratches or wear patterns, replace the high speed shaft (A130) with a new assembly.

Step 17 Lubricate all other parts thoroughly with light turbine oil.

Table 7.1 Bearing and Shaft Clearances Item No.

Description Characteristics Critical Size

101B HO06AY01/HO06AY02 Upper, Gearbox Housing

Upper, Input Bearing Bore Ø 4.3311±.0005

Upper, Idler Bearing Bore Ø 3.6255±.0005 102 PL01AY01 Bearing Plate Lower, Input Bearing Liner Ø 4.3311±.0005

Upper High Speed Shaft Bearing Bore

Ø 3.1880±.0005

101A HO05AY01/HO05AY02/HO05AY03 Lower, Gearbox Housing

Lower, High Speed Bearing Bore

Ø 3.1880±.0005

Lower, Idler Bearing Bore Ø 3.6255±.0005 151D BE09AY01A, Upper Idler Bearing Journal Inside Diameter Ø 2.5065±.0005 151C BE09AY02A, Lower Idler Bearing Journal Inside Diameter Ø 1.7545±.0005 151B Upper High Speed Bearing Maximum Bore Diameter Ø 1.5015 151A Lower High Speed Bearing Maximum Bore Diameter Ø 1.5015

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Idler Shaft Upper Bearing (400 HP Gearbox Only) Maximum clearance for replacement: 0.0085 inches (.22 mm)

Lower Idler Bearing & Shaft Clearances Maximum clearance for replacement: 0.0063 inches (.16 mm)

Input Shaft Upper Bearing

Input Shaft Lower Bearing

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Journal Bearing and High-Speed Shaft Clearances Maximum clearance for replacement: 0.0055 inches (.14 mm)

Tilting Pad Thrust Bearing and High-Speed Shaft Clearances Maximum clearance for replacement: 0.0055 inches (.14 mm)

Tilting Pad Radial and High-Speed Shaft Clearances Maximum clearance for replacement: 0.0055 inches (.14 mm)

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8. Checking and Setting High Speed Shaft End Play If a new high speed shaft assembly, lower gearbox housing, upper or lower high speed journal bearings, or thrust washers are installed high speed shaft end play must be measured and reset. NOTE: For accurate checking of shaft end play, all parts must be dry and free of oil. Step 1 Install the lower journal bearing (151A) in to the lower gearbox housing (101A). Install the

hex head cap screws (905M) and the lock washers (154D). Tighten screws (905M) to correct torque specification.

Step 2 Install the upper high speed shaft journal bearing (151B) into the bearing plate (102).

Install the hex head cap screws (905N) and tighten to the specified torque. Step 3 Place both thrust washers (155A) and (155B) (if required) into lower high speed journal

bearing. Place the high speed shaft assembly (A130) into the lower gearbox housing installing it through the lower high speed shaft journal bearing (151A).

Step 4 With the aid of two large diameter alignment bolts (909C), install the bearing plate (102)

without the o-rings (936T), (936TT) and (936YA). Clamp the bearing plate (102) and the lower gearbox housing (101A) together with two “C” clamps or bolts.

Step 5 With the shaft in a vertical position, move the shaft up and down while measuring the

total end play with a dial indicator or depth micrometer. Shaft end play must be .015 +/-.002 inch. If end play is not within this limit, calculate the shim thickness required to place the shaft within the proper end play. Select the required thickness shim using (158) series shim spacer sizes. Do not install shims below the lower bearing.

Step 6 Remove the alignment bolts (909C) and the “C” clamps from the bearing plate (102) and

lower gearbox housing (101A). Now remove the bearing plate (102). Step 7 Remove the upper high speed journal bearing (151B) from the bearing plate (102). Step 8 Place the required shim thickness over the upper high speed journal bearing (151B) and

reinstall the upper high speed journal bearing (151B) into the bearing plate (102). Tighten hex head cap screws. Refer to table 8.1.

Step 9 Repeat steps 3 through 5, and verify high speed shaft (A130) end play. When end play is

within factory specification, repeat step 6. Step 10 Remove the high speed shaft (A130) and the thrust washers (155A). Step 11 Install thrust washer (155A) into lower high speed shaft journal bearing (151A) and install

a thrust washer (155B) into the upper high speed journal bearing (151B) with the flat side (NO GROOVES) towards the high speed journal bearing (151A).

Step 12 Lubricate the upper and lower thrust washer (155A) with light turbine oil and install the

high speed shaft (A130) into and through the lower high speed journal bearing. Step 13 Begin gearbox reassembly. Refer to the detailed Reassembly Procedure. Step 14 Lubricate all assembled parts with light turbine oil as your mechanic proceeds with the

assembly.

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Table 8.1 Torque Values

Gearbox Sundyne Standard Steel Screws & Bolts and NACE Compliant Steel Screws/Bolts (BG Material)

Torque Values Item # Location Size English Metric

905H Oil Filter Manifold 3/8 - 16 x 1/2 22 - 25 ft-lbs 30 - 34 N-m 905L Gearbox Seal 1/4 - 20 x 1/2 75 - 80 in-lbs 8.5 - 9.0 N-m 905M, N Journal Bearings #10 - 24 x 1 35 - 40 in-lbs 4.0 - 4.5 N-m 905T Chemical Barrier Gasket 1/4 - 20 x 5/8 75 - 80 in-lbs 8.5 - 9.0 N-m 909B Gearbox Halves 1/2 - 13 x4 60 - 65 ft-lbs 81 - 88 N-m 909C Gearbox Halves, Alignment 5/8 - 18 x 4 17/64 60 - 65 ft lbs 81 - 88 N-m 906B Sight Glass #8 - 32 x 1/2 10 - 12 in-lbs 1.0 - 1.4 N-m

Pumps & Compressors* Sundyne Standard Steel Screws and Bolts

Torque Values Item # Location Size English Metric

3 Impeller Bolt/Inducer: LMV/BMP-801, 802, 806, 322, 311, 331 1/2 - 20 36 - 40 ft-lbs 49 - 54 N-m LMV/BMP-341, 346 1/2 - 20 65 - 70 ft-lbs 88 - 95 N-m LMV-313, 343, BMP-338, 348 (High

Flow) 3/4 - 10 85 - 90 ft-lbs 115-122 N-m

LMC/BMC 3X1P, 3X1F, 3X3, 3X6P, 3X7 1/2 - 20 36 - 40 ft-lbs 49 - 54 N-m 906D Diffuser Attaching Screws 1/4 - 20 95 - 102 in-lbs 11 - 11.5 N-m 905E Mechanical Seal No. Spacer 1/4 - 20 x 12 95 - 102 in-lbs 11 - 11.5 N-m 905F Throttle Bushing/Mechanical Seal 1/4 - 20 x 12 9 5- 102 in-lbs 11 - 11.5 N-m 905G Double Seal with Spacer 1/4 - 20 x 3/4 95 - 102 in-lbs 11 - 11.5 N-m 914A Case Nuts 3/4 - 10 250 - 275 ft-lbs 340 - 375 N-m 914A Case Nuts 7/8 - 9 300 - 330 ft-lbs 405 - 445 N-m 905A Seal Housing to Gearbox 3/8 - 16 x 1 3/4 35 - 40 ft-lbs 47 - 54 N-m 905P Separator 1/4 - 20 x 5/8 95 - 102 in-lbs 11 - 11.5 N-m

Pumps & Compressors NACE Compliant Steel Screws / Bolts (BG Material)

Torque Values Item # Location Size English Metric

3 Impeller Bolt/Inducer: LMV/BMP-801, 802, 806, 322, 311, 331 1/2 - 20 36 - 40 ft-lbs 49 - 54 N-m LMV/BMP-341, 346 1/2 - 20 65 - 70 ft-lbs 88 - 95 N-m LMV-313, 343, BMP-338, 348 (High

Flow) 3/4 - 10 85- 90 ft-lbs 115 - 122 N-m

LMC/BMC 3X1P, 3X1F, 3X3, 3X6P, 3X7 1/2 - 20 36 - 40 ft-lbs 49 - 54 N-m 906D Diffuser Attaching Screws 1/4 - 20 70 - 75 in-lbs 8.0 - 8.5 N-m 905E Mechanical Seal No. Spacer 1/4 - 20 70 - 75 in-lbs 8.0 - 8.5 N-m 905F Throttle Bushing/Mechanical Seal 1/4 - 20 70 - 75 in-lbs 8.0 - 8.5 N-m 905G Double Seal with Spacer 1/4 - 20 70 - 75 in-lbs 8.0 - 8.5 N-m 914A Case Nuts 3/4 - 10 160 - 200 ft-lbs 217 - 270 N-m 914A Case Nuts 7/8 - 9 225 - 245 ft-lbs 305 - 332 N-m 905A Seal Housing to Gearbox 3/8 - 16 x 1 3/4 27 - 30 ft-lbs 47 - 54 N-m 905P Separator 1/4 - 20 x 5/8 70 - 75 in-lbs 8.0 - 8.5 N-m * When using Teflon® o-rings, allow 15 minutes between torquing for the Teflon® to cold flow. Repeat torquing until there is no change in torque.

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9. Gearbox and Process End Reassembly Step 1 Wash all gearbox housings and be certain the lubrication galleys are open. Step 2 Attach the sight glass (191). Step 3 Put pipe plugs in lower gearbox housing (101A). Step 4 Freeze lower idler journal bearing (151C) in dry ice for 1/2 hour and install into lower

gearbox housing (101A) with socket head cap screws (905AA). Step 5 Install lower high speed journal bearing (151A) and lower thrust washer (155A), no shims

will be used.

NOTE: If the unit includes thermocouples and probes refer to the section of this manual for Gearbox-Auxiliary Hardware Installation for additional instructions. Step 6 Install the high speed shaft assembly (A130). Step 7 Install lube oil pump (A160) with o-ring (936Z) into bearing plate (102). Lubricate o-ring

(936Z) with Vaseline before installing lube pump. Step 8 Install sump tube fitting (944B) and (944C) into the bearing plate (102). Step 9 Install pipe plugs as required and relief valve (175) into bearing plate (102). Step 10 Install upper high speed journal bearing (151B) into bearing plate (102) and upper thrust

washer (155B). Use Vaseline to hold upper thrust washer in place. Step 11 Set high speed shaft (A130) end play.

NOTE: SHIM BEHIND THE UPPER HIGH SPEED JOURNAL BEARING ONLY TO ACHIEVE [.015 +/-.002], see Section 8.

Step 12 Install idler shaft (A140). Pull high speed shaft (A130) up approximately 1.0” to 1.5” and

slide idler shaft (A140) into the lower idler journal bearing (151C) meshing the gear teeth on the lower idler shaft spur gear and the high speed shaft gear.

Step 13 Install o-rings (936YA) and (936T) and (936TT) into the lower gearbox housing (101A).

Step 14 Install the bearing plate (102) onto the lower gearbox housing (101A). Be careful not to knock the upper thrust washer (155B) out of its location. Be careful not to scratch, ding, or dent the upper high speed journal bearing (151B).

Step 15 Install o-rings (936Y) and (936TQ) into the bearing plate (102).

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Step 16 Install lower input shaft roller bearing race into the top of the bearing plate (102) so it locates against the lube pump (A160).

Step 17 Install the sump tube (173) into the sump tube fitting (944C). Step 18 Install input shaft assembly (A120) into lower input shaft roller bearing. Pull up on the

idler shaft (A140) approximately 1.0” to 1.5” and mesh the input shaft assembly (A120) gear with the idler shaft (A140) gear. Make certain that the input shaft assembly (A120) slot fits over the lube pump (A160) drive pin.

Step 19 Freeze upper idler journal bearing (151D) in dry ice for 1/2 hour. Install the upper idler

journal bearing (151D) into the upper gearbox housing (101B). Use socket head cap screws (905AB) to secure the upper idler journal bearing (151D) to the upper gearbox housing (101B).

Step 20 Install the lube jet (174D) into the upper gearbox housing (101B). Step 21 Install the upper gearbox housing (101B) onto the bearing plate (102). Step 22 Install alignment bolts (909C) and fasten gearbox housings together. Use specified

torque value from chart, see Table 8.1. Step 23 Install fasteners (909B) into gearbox housing and tighten. Use specified torque value

from chart, see Table 8.1. Step 24 Install input seal (115) over input shaft assembly (A120) and press into upper gearbox

housing (101B), seating the input seal (115) firmly against the locating shoulder in the upper gearbox housing (101B).

Step 25 Turn the complete gearbox assembly over so the high speed shaft (A130) is pointing

vertically toward the ceiling. Step 26 Install the rotating face (51D) over the high speed shaft (A130) with the chamfer in the

rotating face (51D) toward the high speed shaft shoulder (A130). Step 27 Install the roll pin (918D) into the lower gearbox housing (101A). Use a soft mallet to seat

the roll pin (918D) into place. Step 28 Install the gearbox seal (60C) and the o-ring (936P) onto the lower gearbox housing

(101A). Use socket head cap screws (905E) and lock washer (916A). Step 29 Install o-ring (936H), upper process seal (60B), into seal housing (30). Step 30 Install rotating face (51D) onto high speed shaft (A130). Step 31 Install o-ring (936K), sleeve (50B), onto high speed shaft (A130). Step 32 Install o-ring (936J). Step 33 Install thermal barrier gasket (87A) onto seal housing (30). Step 34 Install seal housing (30) onto lower gearbox housing (101A). Step 35 Install hex head cap screws (905A), lock washers (154AT), flat washers, (916AG), seal

washers (916S), through seal housing (30) and tighten screws to specified torque value.

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Step 36 Install rotating face (51C) over high speed shaft (A130). Step 37 Install o-ring (936J) over high speed shaft (A130). Step 38 Install sleeve (50A) over high speed shaft (A130). Step 39 Install o-ring (936J) over high speed shaft (A130 ASSY). Step 40 Install o-ring (936H), lower process seal (60A) into seal housing (30). Step 41 Install o-rings (936D), (936E), onto cover (15). Step 42 Install cover (15) onto seal housing (30). Step 43 Install rotating face (51A) over high speed shaft (A130). Step 44 Install impeller bolt (3) into high speed shaft (A130). Step 45 Install impeller (2) over impeller bolt (3). Step 46 Install impeller bolt (3). Step 47 Tighten impeller bolt (3) to correct torque specification, see Table 8.1. Step 48 Install initial fill pipe (951D), (947L), (924RF), into upper gearbox housing (101B). Step 49 Install vent pipe (951C), (947D), (186) into upper gearbox housing (101B). Step 50 Install pressure gauge (942F), (177), (193C), into upper gearbox housing (101B). Step 51 Reinstall the assembly of the gearbox/process end into the compressor housing (1). Step 52 Reconnect all lubrication line and electrical connections.

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Gearbox Auxiliary Hardware Installation (as applicable)

Step 1 Thermocouple Wires Install thermocouple wires into the bearing assembly before installing bearings in the lower housing or bearing plate. Refer to job outline drawing for appropriate thermocouple locations. The thermocouples are typically installed in the thrust position of the upper bearing (151B) and in the radial position of the lower bearing (151A).

Step 2 Vibration Probes Install x-y vibration probes in the lower bearing probe bracket attached to bearing (151A). Install keyphasor probe in the upper bearing probe bracket after installation of the bearing plate. Refer to Bentley-Nevada instructions for setting probe gaps.

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10. Troubleshooting

Gearbox and Compressor Many factors affect the performance of your compressor. Among them are suction pressure, temperature, molecular weight, driver speed, flow rate, and discharge control. You need to check all of these when there is a problem with the compressor and when you are analyzing the performance of the system. For details on the performance of the compressor including the performance curve, final data package sections 1 and 2 and specification sheets. Table 10.1 provides information for analyzing gearbox and compressor problems. Table 10.1 Troubleshooting for Gearbox and Compressor Trouble Possible Cause Investigative and Corrective Action The compressor produces no flow and no pressure at start-up

A component of the drive, such as the coupling or the impeller spline, has failed, or an item is missing from the assembly

Disassemble and inspect the component.

The drive shaft rotates in the wrong Direction

Make sure that the drive shaft is rotating in the direction shown by the arrow on the compressor gearbox.

The suction valve or the discharge valve is closed.

Check the valving (see section 3.)Startup instructions).

The head rise is insufficient. The flow is too high. Check the head rise and the flow rate against the performance curve.

The driver shaft is rotating in the wrong direction.

Make sure that the drive shaft is rotating in the direction shown by the arrow on the compressor gearbox.

The suction pressure is low. Check the Sundyne specification sheets.

Recirculation from the discharge to the inlet is excessive.

Check the flow through the external piping, such as the bypass

The molecular weight is not that for which the compressor was designed.

Check the molecular weight against the value given on the specification sheet. Low molecular weight will cause low discharge pressure.

The driver speed is too low. Check the speed against the value listed on the Sundyne specification sheets.

The pressure gauges or the flow meters are in error

Calibrate the instrumentation.

The oil pressure in the gearbox is low. The pressure gauge is faulty. Check the accuracy of the gauge.

The main lubricating pump has failed. Remove the pump and coupling, and check them for damage.

Driver overloaded. Molecular weight higher than values listed on specification sheet

Check actual molecular weight against value listed on specification sheet.

Electrical failure in electric power unit. Check circuit breaker heater size and setting.

Check voltage.

Current for each phase should be balanced within three percent.

Driver overloaded. (continued)

Mechanical failure in driver, gearbox, or compressor.

Disconnect spacer coupling and check for freedom of rotation of compressor, driver, and gearbox shafts.

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Trouble Possible Cause Investigative and Corrective Action Drain oil and remove gearbox oil level sight

glass and inspect bottom of sump for wear particles. Bearings are probably not damaged if no wear particles are present.

Disassemble compressor end and search for any mechanical failure.

Corrosion pitting on surface of diffuser adjacent to impeller blades. Head rise is reduced by this condition.

Disassemble and inspect. Check diffuser bowl area, cover plate and diffuser throat for material buildup. Clean these areas of all obstructions and restore surfaces to a smooth polished finish (use emery cloth) free of all corrosion pitting. Edge of diffuser throat must be sharp. If damage is more severe (i.e. impeller is deformed or has come in contact with diffuser) replace the damaged parts.

High suction pressure. Check specification sheet. Increase suction pressure and corresponding mass flow rate will result in high horsepower consumption.

Excessive discharge pressure pulsation.

Flow rate too low (surge). Increase flow rate through compressor. Add controlled bypass to suction, if necessary.

Defective flow control valve. Check control valve.

Change of gearbox automatic transmission fluid color from normal color to milky pink or yellow.

Gearbox oil contaminated with water or process fluid.

Inspect gearbox heat exchanger for leakage.

Check for excessive compressor seal leakage.

Inspect shaft sleeve “O” rings.

Shaft sleeve rubs on inside diameter of seal.

Gearbox journal bearing failure. Install replacement exchange gearbox or repair gearbox as outlined under “MAINTENANCE.”

Excessive gearbox automatic transmission fluid consumption.

Low speed shaft seal (115) leakage. Check drain port for leakage. Replace shaft seal if required.

High speed shaft mechanical seal (60C) leakage.

Check for fluid leakage from port 1.

Leakage through heat exchanger into cooling fluid.

Pressure test heat exchanger and replace if required.

Excessive oil foaming. High oil level. Shut down the unit and check oil level.

Low gearbox temperature. Adjust coolant to heat exchanger, keeping oil temperature above 140°F. (60°C).

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Compressor Mechanical Seals Table 10.2 provides information on problems with single units, as well as double and tandem seal units. Table 10.2 Troubleshooting for Gearbox and Compressor Trouble Possible Cause Investigative/Corrective Action Leakage around the seal suddenly increases

The system is operating at a low flow rate or a low inlet pressure, causing vibration of the high-speed shaft, bouncing on the face of the seal, and chipping on the nose of the carbon seal.

Make sure that the compressor always operates above the specified minimum flow rate and/or inlet pressure.

The action of the stationary face spring on the seal is rough and sticky

If contamination in the process gas (from entrained solids) causes a sticky seal, there may be need for a seal flush, double seals, or tandem seals.

The seal is worn or damaged. Disassemble the seal and rebuild or replace it by the instructions in Section 5.

The wear pattern on the rotating faces of the seal is not uniform.

Lightly lap the surfaces on the shaft sleeve and the impeller hub that contact the rotating face of the seal, to remove high spots. Install new seal faces. Do not remove more than 0.005 in. (0.12mm) from any surface.

The rotating face of the seal is cracked or broken. This may have been caused by damage at the assembly or by heating due to lack of leakage (cooling) past the seal.

Make sure that the system operates above the specified minimum flow rate at all times.

Check the seal environment to make sure that there is a leakage path of process or buffer fluid across the compressor seal(s) and that there is a differential across the seal(s) to force this leakage. Replace the damaged seal.

The seal faces, seal parts, or o-rings have become chemically attached.

Investigate the properties of the process gas, and replace the components with chemically resistant materials.

The seal on a low-temperature compressor is icing, or there is heavy condensation on the atmospheric side of the seal.

Purge the atmospheric side of the seal with dry nitrogen gas.

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11. Operation Some form of control is required for the majority of SUNDYNE compressor applications. The purpose of control is twofold: 1) to achieve the desired performance as required by process conditions and 2) to protect the compressor from mechanical damage due to surge or overload conditions. This section is a general guideline on controls. A control system should be selected only after completion of a detailed analysis of the specific installation. Surge Control

It is recommended that a surge control system be installed whenever there is any chance that the process flow could decrease appreciably from design flow. In most surge control systems, a flow sensor is placed in the suction line to the compressor. The signal from this sensor is input to a controller which controls a valve in the bypass loop. When the minimum safe flow is reached, this valve opens and the flow through the compressor is kept above the surge point. Again, the recycled gas must be cooled to prevent heat build-up. Both pneumatic and electrical surge control systems are available.

Suction Throttling

Suction throttling is generally the most economical control method with a constant speed drive. Throttling the control valve on the suction side causes a reduction of inlet pressure to the compressor. Although the compressor creates the same compression ratio as if it were unthrottled, the discharge pressure is reduced. The net result is to lower the total head output to the system. The reduction of inlet pressure correspondingly decreases inlet gas density, and thus, power consumption. Suction throttling also has the advantage of slightly lowering the compressor surge point.

Discharge Throttling

Discharge throttling is control by means of a valve placed at the compressor discharge. A constant speed compressor will always operate on its design head-flow curve. For a given system operating point, the compressor will operate at the system flow rate, thus producing more head than the system requires. This excess head is throttled by the discharge valve. Since the throttling occurs downstream of the compressor, there are no power savings by this method. Discharge throttling offers no real advantages over suction throttling, but is nonetheless an acceptable control method.

Speed Control

Speed control is the most efficient means of compressor control. To operate at points below the design head-flow curve, the driver speed may be reduced accordingly. This creates an infinite “family” of head-flow curves on which the compressor may operate. Since consumed horsepower, assuming constant inlet conditions, varies as the cube of the speed, substantial power savings can be realized. Also, the compressor surge point is lowered proportional to the speed decrease. This method is used mainly on turbine driven units although variable speed motors or mechanical drives are available. Since the main lube oil pump in the SUNDYNE compressor is driven by the gearbox input shaft, provision must be made so the speed is not reduced to a point where adequate lube oil pressure is no longer present.

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Flow Bypass

Flow bypass requires a recycle line from the compressor discharge to suction. The compressor is operated at the desired flow or discharge pressure and the excess flow not required by the process is recycled through the bypass. A cooler is required in the loop to cool the recycled gas to normal suction temperature. This method is generally less efficient than other methods discussed, but may be warranted in some special situations.

Other aspects which should be considered in compressor operation are:

Series Compressor Control - Inlet throttling on the first stage is the most practical method of controlling compressor in series. It is necessary to throttle only the first stage, which in turn acts as a throttle for the second stage. Inlet throttling between stages offers no advantages and should be avoided. Efficiency gains by variable speed control of series units will seldom justify its cost and complexity.

Surge control on series units consists of a flow sensor and controller in the suction line of the first stage. This sends a signal to the control valve in a bypass loop around both compressors. It must be determined which compressor surges at the lowest inlet flow to the first unit so the flow controller can be set such that neither compressor will surge. A more complex system which offers maximum machine protection consists of separate bypass loops for each unit which are operated by separate flow controllers. Parallel Compressor Control - The control of two or more compressors operating in parallel would appear to be relatively simple. More than likely, though no two compressors ever operate identically across their flow range. To produce identical discharge pressures, one compressor could be operating at a different flow than the unit in parallel with it. As a result, the control system would have to include a separate flow controller for each unit. Either suction or discharge throttling may be used, but again, suction throttling is the preferred method. If variable speed drivers are used, extreme care must be taken to insure that the speeds can be precisely controlled. In any case, check valves must be installed in the discharge line of each compressor to prevent possible back flow due to any slight imbalance in the characteristics of the compressors. Separate surge control systems for each compressor should be considered for maximum unit protection.

12. Spare Parts

1. General Assemblies, subassemblies and components of the Sundyne compressor are illustrated on

the exploded and cross sectional views in Reference D. Refer to your Sundyne Compressor Specification Sheet for those options applicable to your compressor. The corresponding parts lists, keyed to each part by item number, identify detail parts by part name, quantity and location. A complete bill of materials list for the compressor and gearbox end is included in the final data package. Refer to the unit outline drawing for a list of the major kit bills of material.

2. Recommended Spare Parts Refer to your final data package for recommended spare parts identified for your particular

unit. These are provided as guidelines only.

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3. Repair Kits Seal and O-ring repair kits are not illustrated herein, but may be purchased directly from

Sundyne Corporation. Seal repair kits contain all normal wearing parts (springs, washers, o-rings, carbon faces, etc.) of the compressor or gearbox mechanical seals.

O-ring repair kits contain all o-rings necessary for maintenance or overhaul of the

compressor. The use of these kits reduces maintenance time, prevents assembly mistakes, simplifies stocking and inventory, and reduces delivery time.

4. Ordering Spare Parts When ordering spare parts, give the unit serial number and list each part by the part number

as shown on the Bill of Material which is included with each compressor shipment (preferred method), or list each part by item number (as listed in this manual), part name and compressor model. Specify quantities desired.

Order parts from your Fluid Handling representative or directly from Sundyne Corporation at

one of the following locations. Sundyne Corporation Phone Number: +1-303-940-2989 14845 West 64th Avenue Fax Number: +1-303-940-2826 Arvada, Colorado 80007, USA Sundyne Corporation Europe Phone Number: +011-333-80-38-3300 (13-15 Boulevard Eiffel Fax Number: +011-333-80-38-3366 Zone Industrielle De Dijon-Sud 21600) B.P. 30 21604 Dijon (Longvic) France

Sundyne Nikkiso PHONE: +81-3-3444-6475 27-10, Ebisu 2-Chome, Shibuya-Ku FAX: +81-3-3444-6806 Tokyo 150-0013, Japan

Or visit our Genuine Service and Parts site at www.sundyne.com.

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LMC-341F

TYPICAL RECOMMENDED SPARES LIST

FLUID END ITEMS TYPICAL CLASS (2)

LOC NO. OPTION (1) PART NUMBER DESCRIPTION 1 2 3 3 ALL BO03AD07DB3 BOLT, IMPELLER 0 1 1

87A ALL GK01AW01 GASKET, THERMAL 1 1 2 2 ALL JM01AD87DD6800 IMPELLER,COMPRESSOR 0 0 1

50A DS,TS SL01AD16DD SLEEVE, LOWER 0 1 1 50B,50 DS,TS,SS SL01AD02DD SLEEVE, UPPER 0 1 1

51C DS,TS RJ09AD20RE RING, MATING, UPPER 1 1 2 60A SS,TS SE04AD21F SEAL, LOWER 1 1 2 60B DS,TS SE04AD21F SEAL, UPPER 1 1 2

-- ALL RKORC311FUC O-RING 1 2 2

NOTES: (1) Options: SS = Single Seal, DS = Double Seal, TS = Tandem Seal,

(2) Class 1 = Minimum recommended spare parts necessary to perform a startup and inspection

of a new unit. Class 2 = Minimum recommended spare parts necessary to cover 1-2 years of normal service Class 3 = Minimum recommended spare parts necessary for critical service, or units that will be

installed in remote locations. (3) * Items are alternate items, and should be purchased according to user's preference

(seal kits are available for mechanical seals only). Revised 10/3/00

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LMC-341F

TYPICAL RECOMMENDED SPARES LIST

GEARBOX ITEMS TYPICAL CLASS (2)

LOC NO. OPTION (1) PART NUMBER DESCRIPTION 1 2 3 A160 WS PU04AW02 PUMP, LUBE, REVERSIBLE 0 1 1 115 ALL 20-314 SEAL, ASSY, INPUT 1 1 1 -- AA 22-141 FILTER, OIL, HILCO 2 6 6

125C ALL 21-108 BEARING, INPUT, UPPER 0 1 1 125D ALL 21-108 BEARING, INPUT, LOWER 0 1 1 151A ALL BT20AD0860B BEARING, HIGH SPEED, LOWER 0 0 1 151B ALL BT20AD0860B BEARING, HIGH SPEED, UPPER 0 0 1 151C ALL BE09AY02A BRG, JOURNAL, LOWER IDLER 0 0 1 151D ALL BE09AY01A BRG, JOURNAL, UPPER IDLER 0 0 1 155A AA WA05AA01320 WASHER, THRUST, LOWER 0 0 1 155B AA WA05AA01320 WASHER, THRUST, UPPER 0 0 1 51D ALL RJ09AA21SD RING, MATING 1 1 1 60C ALL SE04AA53A SEAL, ASSY, GEARBOX 1 1 1

936ZG ALL 14-057UC O-RING 2 4 4 936P ALL 14-055UC O-RING 2 4 4 936T ALL 14-324UC O-RING 2 4 4

936TQ ALL 14-324UC O-RING 2 4 4 936TT ALL 14-324UC O-RING 2 4 4 936Y ALL 14-322UC O-RING 2 4 4

936YA ALL 14-322UC O-RING 2 4 4 936ZF ALL 14-323UC O-RING 2 4 4 A130 ALL SH01AY05E1L0 SHAFT, ASSY, HIGH SPEED 0 1 1

NOTES: (1) Options: WS = Wet Sump , AS = As Applicable (2) Class 1 = Minimum recommended spare parts necessary to perform a startup and inspection

of a new unit. Class 2 = Minimum recommended spare parts necessary to cover 1-2 years of normal service Class 3 = Minimum recommended spare parts necessary for critical service, or units that will be

Installed in remote locations. Revised 10/3/00

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13. Sundyne Compressor Warranty Sundyne Compressors warrants to Purchaser for a period of 12 months from the date the line mounted compressor (LMC) is placed in service (not to exceed 18 months after shipment date) that the equipment at the time of shipment is free from defects of material and workmanship. If any defects occur during the warranty period, Sundyne’s sale obligation is limited to alteration, repair, or replacement at Sundyne’s expense, F.O.B. factory, of parts of equipment, which upon Sundyne’s examination prove to be defective. Non-Sundyne equipment and accessories are warranted only to the extent of and by the original manufacturer’s warranty. Sundyne is not liable for damage or wear to equipment caused by abnormal conditions, vibration, improper lubrication, failure to provide proper inlet conditions or flow, corrosives, abrasives, or foreign objects. This warranty is exclusive and in lieu of all other warranties, whether expressed or implied, including any warranty of merchantability or fitness for any purpose. In no event shall Sundyne be liable for consequential or incidental damages. COPYRIGHT All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted in any form or by any means, electronic, mechanical, photocopying, recording or otherwise without the prior permission of Sundyne Compressors.

EUROPEAN UNION MACHINERY DIRECTIVE (CE Mark System) (where applicable) This document incorporates information relevant to the Machinery Directive 89/392/EEC. It should be read prior to the use of any of our equipment. Individual maintenance manuals which also conform to the EU Directive should be read when dealing with specific models. SAFETY WARNING Sundyne Compressors manufactures centrifugal process gas compressors to exacting International Quality Management System Standards (ISO 9001 - 1987) as certified and audited by Lloyd's Register Quality Assurance Limited. Genuine parts and accessories have been specifically designed and tested for use with these products to ensure continued product quality and performance. As Sundyne Compressors cannot test all parts and accessories sourced from other vendors, incorrect design and/or fabrication of such parts and accessories may adversely affect the performance and safety features of these products. Failure to properly select, install or use authorized Sundyne Compressor parts and accessories is considered misuse and damage or failure caused by misuse is not covered by Sundyne’s warranty. Additionally, modification of Sundyne Compressor products or removal of original components may impair the safety of these products and their effective operation. Reference A

Critical Start-up Checklist Know Your Machine Before servicing and starting up the Sundyne line mounted compressor (LMC), carefully review the specification sheet, the outline drawings, the performance curves, and this instruction manual. You should be familiar with the configuration of the compressor before you start and operate it.

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Driver Instructions Carefully follow the installation and starting instructions provided by the manufacturer of the driver. This is included in the final data package. Auxiliaries 1. Check the utility connections. 2. Verify that the auxiliary piping conforms to Sundyne’s drawings. 3. Verify the connections of the switches, the instruments, and the set points. 4. Calibrate the flow instruments and the other transmitters. Environmental Control System Install a system to control the environment of the seal, if required, and verify that port 1 is properly vented. Drain the compressor casing. (Maximum back pressure = 10 psig) Pressurize Fluid Loop Pressurize double seal buffer fluid loop or external seal flush, if required, prior to admitting fluid into compressor casing. Check Driver Rotation Make sure that the gear shaft rotates in the direction indicated by the arrow stamped on the gearbox of the compressor. Start Compressor 1. Suction throttling (preferred method): Start the compressor with the discharge valve open while

throttling the suction valve, to bring the compressor to the design operating point. See specification sheets for the inlet conditions and flow rate.

2. Discharge throttling: Start the compressor with the suction valve completely open while throttling

the discharge valve, to bring the compressor to the design operating point. 3. Variable speed (as applicable): Start the compressor with the suction valve and the discharge

valve open. Check the pressure in the system. If it exceeds the surge point of the compressor (see the specification sheet and the performance curve), you will need a bypass to protect the compressor from surging during ramp-up to speed. Never operate the compressor above the maximum design speed.

Heat Exchanger If a heat exchanger for the gearbox is installed, adjust the cooling flow to keep the temperature of the gearbox sump at 120°-180°F (49°-82°C). Check Check the following items. Each of these parameters significantly affects the performance of the system. Head rise, Flow rate, Power consumption, Inlet pressure, Temperature; and Molecular weight. Coupling There are two types of connections between the motor and gearbox; a splined shaft or a coupling. For splined connections, the splined shaft must be lubricated with the supplied spline grease and the two o-rings installed prior to the mounting the motor. It is recommended that the input shaft be rotated by hand prior to mounting the motor. If the unit has a coupling, be sure coupling gap is correct and bolting between coupling halves is tight. The instruction manual contains coupling set-up information.

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Process Conditions Do process conditions; suction pressure, suction temperature, discharge header pressure, and mole weight agree with specification sheet information? Check with your Sundyne Corporation representative if you must test a different gas than shown on the specification sheet. Auxiliary Lube Pump If you have an auxiliary lubrication pump, unlock the electrical circuit and start it in the “hand” position. Check for oil leaks and recheck the oil level. Piping Connections Are the following bolted/threaded connections tight: a. Compressor flange bolts? b. Seal environment piping and port connections? c. Cooling water connections to heat exchanger? (if applicable) d. Gearbox oil drain plug? e. Compressor case drain plug? Reference B Lock-out/Tag-out Guidelines Follow Your Companies Lock-Out / Tag-Out Procedure When Servicing Sundyne Compressors. Never remove a lock or tag applied by someone else. Additional locks or tags should be applied if multiple groups are working on the equipment. Each responsible work group leader should apply a lock or tag. Always treat conductors and equipment as if they are energized. Reference C Seal Arrangement Drawings for Single, Double and Tandem Configurations

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SINGLE SEAL ARRANGEMENT

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DOUBLE SEAL ARRANGEMENT

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TANDEM SEAL ARRANGEMENT

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Reference D Phoenix Compressor/Gearbox Cross-section Drawing Phoenix Gearbox Module Drawing – GB01AY01

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Phoenix Compressor / Gearbox Cross-Sectional View

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71

PHOENIX GEARBOX MODULE DRAWING – GB01AY01

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73

74

75

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• ANSIMAG • CASTER • GSP • HMD/KONTRO • MASO/SINE • COMPRESSORS • SUNDYNE • SUNFLO •

14845 W. 64th Avenue • Arvada, Colorado 80007 USA • +1-303-425-0800 • FAX: +1-303-425-0896 • www.sundyne.com Sundyne Europe • Dijon (Longvic) France • +33 (0) 3.80.38.33.00 • FAX: +33 (0) 3.80.38.33.66 Sundyne Nikkiso • 27-10, Ebisu 2-Chome, Shibuya-Ku • Tokyo 150-0013, Japan • +81-3-3444-6475 • FAX: +81-3-3444-6806