V-6011_DCa ad a

MSET ENGINEERING CORPORATION SDN BHD

DOCUMENT TITLE: DESIGN CALCULATION DATE: 11.01.2015

DOC. REF. NO.: MSET/M2-251/V-6011/DC REVISION: 02

SUBJECT: TITLE PAGE JOB NO: M2-251

SERIAL NO.: 002

DESIGN CALCULATION

Fuel Gas Scrubber TAG NO: V-6011

PROJECT NAME: E6 Development Project

CLIENT NAME: VME Process

02 11.01.15 Issued for Approval Mohd Faizal Yahasliza Azahar 01 10.12.14 Issued for Review Muhd Faizal Yahasliza Azahar

Rev. No.

Date Description of Revision Prepared

by Reviewed

by Approved

by





SERIAL NO.: M2-234/001

DESIGN DATA

ITEM NO. FUEL GAS SCRUBBER

DESIGN CODE ASME SEC.VIII DIV.1, 2013 EDITION +

DEP 31.22. 20.31

DESIGN PRESSURE (barg) (Int./Ext.) 18/FV

TEMPERATURE (⁰C) (Max./Min) 50/0

OPERATING PRESSURE (barg) (Max) 7.1

TEMPERATURE (⁰C) (Max)/(Min) 38.96/24.9

TEST PRESSURE

HYDROTEST (barg) (1.3xMAPxLSR)(note1)

23.754 (Horizontal Position)

PNEUMATIC NO

MAWP (hot & corroded) (barg) 18.283

MAP (new & cold) (barg) 18.363

OUTSIDE DIAMETER / TL TO FACE (mm) 610/2400

TYPE OF HEAD 2:1 ELLIP HEAD/BODY FLANGE

MATERIAL OF CONSTRUCTION (SHELL/HEAD & BODYFLANGE) SA 240 GR. 316/316L & SA 182 F 316/316L

HEAT TREATMENT

NORMALISED NO

PWHT NO

IMPACT TEST NO

MDMT (⁰C) 0

RADIOGRAPHY HEAD: 100%, SHELL: 100%

JOINT EFFICIENCY HEAD:1.0 , SHELL: 1.0

CORROSION ALLOWANCE (mm) 0

CONTENTS HC LIQUID/GAS

ERECTION WEIGHT (kg) 850

CAPACITY (m3) 0.69

PRESSURE VESSEL DESIGN CALCULATION Note: 1.MAP will be used in lieu of MAWP for determining hydro test pressure (As per DEP 31.22.20.31-Gen, Jan 09)





SERIAL NO.: M2-251/001

TABLE OF CONTENT

NO CONTENT PAGE NO.

1 Input Echo 4

2 Flg Calc [Int P] : A1 (flange) 18

3 Flg Calc [Int P] : A1 (blind) 22

4 Internal Pressure Calculations 28

5 External Pressure Calculations 33

6 Element and Detail Weights 37

7 Nozzle Flange MAWP 43

8 Wind Load Calculation 44

9 Earthquake Load Calculation 46

10 Wind / Earthquake Shear, Bending 47

11 Wind Deflection 48

12 Stress due Combined Loads 53

13 Center of Gravity Calculation 60

14 Sup. Lug Calc 61

15 Nozzle Calculation 76

16 Nozzle Schedule 182

17 Nozzle Summary 185

18 MDMT Summary 188

19 Vessel Design Summary 190

20 Attachment 1 : Wind Pressure Calc 193

21 Attachment 2 : Transportation Calc 195

22 Attachment 3 : Lifting Trunnion Calc 235

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Input Echo : Step: 1 1:01a Jan 11,2015

PV Elite Vessel Analysis Program: Input Data

Design Internal Pressure (for test) 18.000 bar

Design Internal Temperature 50 °C

Type of Test UG-99(c)

Test Position Horizontal

Projection of Nozzle from Vessel Top 200.00 mm

Projection of Nozzle from Vessel Bottom 200.00 mm

Minimum Design Metal Temperature 0 °C

Type of Construction Welded

Special Service None

Degree of Radiography RT 1

Miscellaneous Weight Percent 0.0

Use Higher Longitudinal Stresses (Flag) Y

Select t for Internal Pressure (Flag) N

Select t for External Pressure (Flag) N

Select t for Axial Stress (Flag) N

Select Location for Stiff. Rings (Flag) N

Consider Vortex Shedding N

Perform a Corroded Pressure test N

Is this a Heat Exchanger No

User Defined Test Press. (Used if > 0) 0.0000 bar

User defined MAWP 0.0000 bar

User defined MAPnc 0.0000 bar

Load Case 1 NP+EW+WI+FW+BW

Load Case 2 NP+EW+EE+FS+BS

Load Case 3 NP+OW+WI+FW+BW

Load Case 4 NP+OW+EQ+FS+BS

Load Case 5 NP+HW+HI

Load Case 6 NP+HW+HE

4

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Input Echo : Step: 1 1:01a Jan 11,2015 Load Case 7 IP+OW+WI+FW+BW

Load Case 8 IP+OW+EQ+FS+BS

Load Case 9 EP+OW+WI+FW+BW

Load Case 10 EP+OW+EQ+FS+BS

Load Case 11 HP+HW+HI

Load Case 12 HP+HW+HE

Load Case 13 IP+WE+EW

Load Case 14 IP+WF+CW

Load Case 15 IP+VO+OW

Load Case 16 IP+VE+EW

Load Case 17 NP+VO+OW

Load Case 18 FS+BS+IP+OW

Load Case 19 FS+BS+EP+OW

Wind Design Code User Defined

Wind Profile Height mm Pressure kPa

10000.0000 0.7500

0.0000 0.0000

0.0000 0.0000

0.0000 0.0000

0.0000 0.0000

0.0000 0.0000

0.0000 0.0000

0.0000 0.0000

Damping Factor (Beta) for Wind (Ope) 0.0100

Damping Factor (Beta) for Wind (Empty) 0.0000

Damping Factor (Beta) for Wind (Filled) 0.0000

Seismic Design Code G Loading

Seismic Importance Factor 1.000

G Loading Coefficient Gx 0.500

G Loading Coefficient Gz 0.500

5

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Input Echo : Step: 1 1:01a Jan 11,2015 G Loading Coefficient Gy -2.000

Percent Seismic for Test 0.000

Design Nozzle for M.A.W.P. (maximum) Y

Consider MAP New and Cold in Noz. Design N

Consider External Loads for Nozzle Des. Y

Use ASME VIII-1 Appendix 1-9 N

Material Database Year Current w/Addenda or Code Year

Configuration Directives:

Do not use Nozzle MDMT Interpretation VIII-1 01-37 No

Use Table G instead of exact equation for "A" Yes

Shell Head Joints are Tapered Yes

Compute "K" in corroded condition No

Use Code Case 2286 No

Use the MAWP to compute the MDMT Yes

Using Metric Material Databases, ASME II D No

Complete Listing of Vessel Elements and Details:

Element From Node 10

Element To Node 20

Element Type Elliptical

Description Head

Distance "FROM" to "TO" 38.000 mm

Element Outside Diameter 610.00 mm

Element Thickness 5.0000 mm

Internal Corrosion Allowance 0.0000 mm

Nominal Thickness 8.0000 mm

External Corrosion Allowance 0.0000 mm

Design Internal Pressure 18.000 bar

6

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Input Echo : Step: 1 1:01a Jan 11,2015 Design Temperature Internal Pressure 50 °C

Design External Pressure 1.0342 bar

Design Temperature External Pressure 50 °C

Effective Diameter Multiplier 1.2

Material Name SA-240 316L

Allowable Stress, Ambient 115.15 MPa

Allowable Stress, Operating 115.15 MPa

Allowable Stress, Hydrotest 155.14 MPa

Material Density 8027.2 kg/m³

P Number Thickness 0.0000 mm

Yield Stress, Operating 165.40 MPa

External Pressure Chart Name HA-4

UNS Number S31603

Product Form Plate

Efficiency, Longitudinal Seam 1.0

Efficiency, Circumferential Seam 1.0

Elliptical Head Factor 2.0


Detail Type Liquid

Detail ID LIQUID

Dist. from "FROM" Node / Offset dist -150.00 mm

Height/Length of Liquid 188.00 mm

Liquid Density 909.98 kg/m³


Detail Type Nozzle

Detail ID N3

Dist. from "FROM" Node / Offset dist 0.0000 mm

Nozzle Diameter 2.0 in.

Nozzle Schedule 80S

Nozzle Class 150

Layout Angle 90.0

7

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Input Echo : Step: 1 1:01a Jan 11,2015 Blind Flange (Y/N) N

Weight of Nozzle ( Used if > 0 ) 51.995 N

Grade of Attached Flange GR 2.2

Nozzle Matl SA-312 TP316L

--------------------------------------------------------------------


Element To Node 30

Element Type Cylinder

Description Shell


Element Outside Diameter 610.00 mm




External Corrosion Allowance 0.0000 mm


Design Temperature Internal Pressure 50 °C




Material Name SA-240 316L

Efficiency, Longitudinal Seam 1.0

Efficiency, Circumferential Seam 1.0


Detail Type Liquid

Detail ID LIQUID


Height/Length of Liquid 900.00 mm

Liquid Density 910.00 kg/m³

8

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Input Echo : Step: 1 1:01a Jan 11,2015 Element From Node 20

Detail Type Nozzle

Detail ID N1



Nozzle Schedule None

Nozzle Class 600

Layout Angle 270.0

Blind Flange (Y/N) N



Nozzle Matl SA-182 F316


Detail Type Nozzle

Detail ID N5




Nozzle Class 150

Layout Angle 270.0






Detail Type Nozzle

Detail ID N6




Nozzle Class 150

9

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Input Echo : Step: 1 1:01a Jan 11,2015 Layout Angle 90.0






Detail Type Nozzle

Detail ID K1




Nozzle Class 150

Layout Angle 315.0






Detail Type Nozzle

Detail ID K2A



Nozzle Schedule 80S

Nozzle Class 150

Layout Angle 0.0






10

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Input Echo : Step: 1 1:01a Jan 11,2015 Detail Type Nozzle

Detail ID K2B



Nozzle Schedule 80S

Nozzle Class 150

Layout Angle 0.0






Detail Type Nozzle

Detail ID K3A



Nozzle Schedule 80S

Nozzle Class 150

Layout Angle 135.0






Detail Type Nozzle

Detail ID K3B



Nozzle Schedule 80S

Nozzle Class 150

Layout Angle 135.0

11






Detail Type Nozzle

Detail ID K4A




Nozzle Class 150

Layout Angle 315.0






Detail Type Nozzle

Detail ID K4B




Nozzle Class 150

Layout Angle 315.0






Detail Type Nozzle

12

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Input Echo : Step: 1 1:01a Jan 11,2015 Detail ID K5A



Nozzle Schedule 80S

Nozzle Class 150

Layout Angle 30.0






Detail Type Nozzle

Detail ID K5B



Nozzle Schedule 80S

Nozzle Class 150

Layout Angle 30.0






Detail Type Nozzle

Detail ID HH



Nozzle Schedule 80S

Nozzle Class 150

Layout Angle 250.0

Blind Flange (Y/N) Y

13

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Input Echo : Step: 1 1:01a Jan 11,2015 Weight of Nozzle ( Used if > 0 ) 185.10 N




Detail Type Lug

Detail ID LUG


Number of Lugs 2

Dist. from OD to Lug Cntrline(dlug) 128.00 mm

Height of Gusset Plates (hgp) 306.00 mm

Force Bearing Width (wfb) 204.00 mm

Weight of Lug 150.00 N

Lug Start Angle (degrees) 0.0


Detail Type Weight

Detail ID MIST ELIMINATOR


Miscellaneous Weight 980.60 N

Offset from Element Centerline 0.0000 mm

--------------------------------------------------------------------


Element To Node 40

Element Type Flange

Description Body Flange


Flange Inside Diameter (OD for Blinds) 593.60 mm




14

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Input Echo : Step: 1 1:01a Jan 11,2015 External Corrosion Allowance 0.0000 mm






Material Name SA-182 F316

Allowable Stress, Ambient 137.90 MPa

Allowable Stress, Operating 137.90 MPa

Allowable Stress, Hydrotest 186.17 MPa

Material Density 8027.2 kg/m³

P Number Thickness 0.0000 mm

Yield Stress, Operating 217.74 MPa

External Pressure Chart Name HA-2

UNS Number S31600

Class / Thickness / Grade :: > 5

Product Form Forgings

Perform Flange Stress Calculation (Y/N) Y

Weight of ANSI B16.5/B16.47 Flange 0.0000 N

Class of ANSI B16.5/B16.47 Flange

Grade of ANSI B16.5/B16.47 Flange

--------------------------------------------------------------------


Element To Node 50

Element Type Flange

Description Blind


Flange Inside Diameter (OD for Blinds) 812.80 mm




15

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Input Echo : Step: 1 1:01a Jan 11,2015 External Corrosion Allowance 0.0000 mm






Material Name SA-182 F316

Perform Flange Stress Calculation (Y/N) Y

Weight of ANSI B16.5/B16.47 Flange 0.0000 N

Class of ANSI B16.5/B16.47 Flange

Grade of ANSI B16.5/B16.47 Flange


Detail Type Nozzle

Detail ID N2




Nozzle Class 150

Layout Angle 180.0






Detail Type Nozzle

Detail ID N4




Nozzle Class 150

Layout Angle 0.0

16





PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013

17

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Flg Calc [Int P] : A1 (flange) Flng: 11 1:01a Jan 11,2015

Flange Input Data Values Description: A1 (flange) :

Body Flange

Description of Flange Geometry (Type) Integral Weld Neck

Design Pressure P 18.00 bar

Design Temperature 50 °C

Internal Corrosion Allowance ci 0.0000 mm

External Corrosion Allowance ce 0.0000 mm

Use Corrosion Allowance in Thickness Calcs. No

Flange Inside Diameter B 593.600 mm

Flange Outside Diameter A 812.800 mm

Flange Thickness t 47.7520 mm

Thickness of Hub at Small End go 8.0000 mm

Thickness of Hub at Large End g1 34.9240 mm

Length of Hub h 104.6480 mm

Flange Material SA-182 F316

Flange Material UNS number S31600

Flange Allowable Stress At Temperature Sfo 137.90 MPa

Flange Allowable Stress At Ambient Sfa 137.90 MPa

Bolt Material SA-193 B7

Bolt Allowable Stress At Temperature Sb 172.38 MPa

Bolt Allowable Stress At Ambient Sa 172.38 MPa

Diameter of Bolt Circle C 749.300 mm

Nominal Bolt Diameter a 31.7500 mm

Type of Threads TEMA Thread Series

Number of Bolts 20

Flange Face Outside Diameter Fod 692.150 mm

18

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Flg Calc [Int P] : A1 (flange) Flng: 11 1:01a Jan 11,2015 Flange Face Inside Diameter Fid 593.600 mm

Flange Facing Sketch 1, Code Sketch 1a

Gasket Outside Diameter Go 685.800 mm

Gasket Inside Diameter Gi 628.650 mm

Gasket Factor m 0.0000

Gasket Design Seating Stress y 0.00 MPa

Column for Gasket Seating 2, Code Column II

Gasket Thickness tg 3.1750 mm

ANSI Flange Class 150

ANSI Flange Grade GR 2.2

ASME Code, Section VIII, Division 1, 2010, 2011a

Hub Small End Required Thickness due to Internal Pressure:

= (P*(D/2+Ca))/(S*E-0.6*P) per UG-27 (c)(1)

= (18.00*(593.6000/2+0.0000))/(137.90*1.00-0.6*18.00)+Ca

= 3.9053 mm

Hub Small End Hub MAWP:

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (137.90 * 1.00 * 8.0000 )/(296.8000 + 0.6 * 8.0000 )

= 36.573 bar

Corroded Flange ID, Bcor = B+2*Fcor 593.600 mm

Corroded Large Hub, g1Cor = g1-ci 34.924 mm

Corroded Small Hub, g0Cor = go-ci 8.000 mm

Code R Dimension, R = (C-B)/2 - g1 42.926 mm

Gasket Contact Width, N = (Go - Gi) / 2 28.575 mm

Basic Gasket Width, bo = N / 2 14.287 mm

19

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Flg Calc [Int P] : A1 (flange) Flng: 11 1:01a Jan 11,2015 Effective Gasket Width, b = Cb sqrt(bo) 9.525 mm

Gasket Reaction Diameter, G = Go (Self-Energizing) 685.800 mm

Basic Flange and Bolt Loads:

Hydrostatic End Load due to Pressure [H]:

= 0.785 * G² * Peq

= 0.785 * 685.8000² * 18.000

= 664941.500 N

Contact Load on Gasket Surfaces [Hp]:

= 2 * b * Pi * G * m * P

= 2 * 9.5250 * 3.1416 * 685.8000 * 0.0000 * 18.00

= 0.000 N

Hydrostatic End Load at Flange ID [Hd]:

= Pi * Bcor² * P / 4

= 3.1416 * 593.6000² *18.0000/4

= 498168.531 N

Pressure Force on Flange Face [Ht]:

= H - Hd

= 664941 - 498168

= 166773.000 N

Operating Bolt Load [Wm1]:

= max( H + Hp + H'p, 0 )

= max( 664941 + 0 + 0 , 0 )

= 664941.500 N

Gasket Seating Bolt Load [Wm2]:

= y * b * Pi * G + yPart * bPart * lp

= 0.00*9.5250*3.141*685.800+0.00*0.0000*0.00

= 0.000 N

Required Bolt Area [Am]:

= Maximum of Wm1/Sb, Wm2/Sa

= Maximum of 664941/172 , 0/172

= 3857.857 mm²

20

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Flg Calc [Int P] : A1 (flange) Flng: 11 1:01a Jan 11,2015

ASME Maximum Circumferential Spacing between Bolts per App. 2 eq. (3) [Bsmax]:

= 2a + 6t/(m + 0.5)

= 2 * 31.750 + 6 * 47.752/(0.00 + 0.5)

= 636.524 mm

Actual Circumferential Bolt Spacing [Bs]:

= C * sin( pi / n )

= 749.300 * sin( 3.142/20 )

= 117.216 mm

ASME Moment Multiplier for Bolt Spacing per App. 2 eq. (7) [Bsc]:

= max( sqrt( Bs/( 2a + t )), 1 )

= max( sqrt( 117.216/( 2 * 31.750 + 47.752 )), 1 )

= 1.0265

Bolting Information for TEMA Imperial Thread Series (Non Mandatory):

-----------------------------------------------------------------------------

Minimum Actual Maximum

-----------------------------------------------------------------------------

Bolt Area, mm² 3857.857 11987.072

Radial distance bet. hub and bolts 44.450 42.926

Radial distance bet. bolts and the edge 31.750 31.750

Circumferential spacing between bolts 71.450 117.216 636.524

-----------------------------------------------------------------------------

Flange Design Bolt Load, Gasket Seating [W]:

= Sa * ( Am + Ab ) / 2

= 172.38 * ( 3857.8567 + 11987.0723 )/2

= 1365518.75 N

Gasket Load for the Operating Condition [HG]:

= Wm1 - H

= 664941 - 664941

21

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Flg Calc [Int P] : A1 (flange) Flng: 11 1:01a Jan 11,2015 = 0.00 N

Moment Arm Calculations:

Distance to Gasket Load Reaction [hg]:

= (C - G ) / 2

= ( 749.3000 - 685.8000 )/2

= 31.7500 mm

Distance to Face Pressure Reaction [ht]:

= ( R + g1 + hg ) / 2

= ( 42.9260 + 34.9240 + 31.7500 )/2

= 54.8000 mm

Distance to End Pressure Reaction [hd]:

= R + ( g1 / 2 )

= 42.9260 + ( 34.9240/2.0 )

= 60.3880 mm

Summary of Moments for Internal Pressure:

Loading Force Distance Bolt Corr Moment

End Pressure, Md 498169. 60.3880 1.0265 30892. N-m

Face Pressure, Mt 166773. 54.8000 1.0265 9385. N-m

Gasket Load, Mg 0. 31.7500 1.0265 0. N-m

Gasket Seating, Matm 1365519. 31.7500 1.0265 44520. N-m

Total Moment for Operation, Mop 40277. N-m

Total Moment for Gasket seating, Matm 44520. N-m

Note: User choose not to perform Stress Calculations on this ANSI Flange.

Pressure rating of the flange will be used to check code compliance.

Estimated Finished Weight of Flange at given Thk. 127.6 kgm

Estimated Unfinished Weight of Forging at given Thk 296.2 kgm


22

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Flg Calc [Int P] : A1 (blind) Flng: 12 1:01a Jan 11,2015

Flange Input Data Values Description: A1 (blind) :

Blind

Description of Flange Geometry (Type) Blind

Design Pressure P 18.00 bar

Design Temperature 50 °C

Internal Corrosion Allowance ci 0.0000 mm

External Corrosion Allowance ce 0.0000 mm

Use Corrosion Allowance in Thickness Calcs. Yes

Flange Outside Diameter A 812.800 mm

Flange Thickness t 68.0000 mm


Flange Material UNS number S31600

Flange Allowable Stress At Temperature Sfo 137.90 MPa

Flange Allowable Stress At Ambient Sfa 137.90 MPa


Bolt Allowable Stress At Temperature Sb 172.38 MPa

Bolt Allowable Stress At Ambient Sa 172.38 MPa

Diameter of the Load Reaction, Long Span D 0.000 mm

Diameter of the Load Reaction, Short Span d 0.000 mm

Perimeter along the Center of the Bolts L 2353.995 mm

Diameter of Bolt Circle C 749.300 mm

Nominal Bolt Diameter a 31.7500 mm

Type of Threads TEMA Thread Series

Number of Bolts 20

Flange Face Outside Diameter Fod 692.150 mm

23

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Flg Calc [Int P] : A1 (blind) Flng: 12 1:01a Jan 11,2015 Flange Face Inside Diameter Fid 590.550 mm

Flange Facing Sketch 1, Code Sketch 1a

Gasket Outside Diameter Go 685.800 mm

Gasket Inside Diameter Gi 628.650 mm

Gasket Factor m 0.0000

Gasket Design Seating Stress y 0.00 MPa

Column for Gasket Seating 2, Code Column II

Gasket Thickness tg 3.1750 mm

Evaluate Patterned Holes in Blind Cover Yes

Hole Diameter D1 77.200 mm

Hole Diameter D2 77.200 mm

Edge Distance to D1 163.000 mm

Edge Distance to D2 163.000 mm

Pitch Distance 410.000 mm

Checking Multiple Openings on Flat Head per ASME Sec. VIII Div. 1 UG-39

Head dia = 749.30 Opening dia, d1 = 77.20 d2 = 77.20 mm

UG-39(e)(1) Spacing 410.00 is >= 2*Avg. dia. 154.40 OK.


Gasket Contact Width, N = (Go - Gi) / 2 28.575 mm

Basic Gasket Width, bo = N / 2 14.287 mm

Effective Gasket Width, b = Cb sqrt(bo) 9.525 mm

Gasket Reaction Diameter, G = Go (Self-Energizing) 685.800 mm

24

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Flg Calc [Int P] : A1 (blind) Flng: 12 1:01a Jan 11,2015 Basic Flange and Bolt Loads:

Hydrostatic End Load due to Pressure [H]:

= 0.785 * G² * Peq

= 0.785 * 685.8000² * 18.000

= 664941.500 N

Contact Load on Gasket Surfaces [Hp]:

= 2 * b * Pi * G * m * P

= 2 * 9.5250 * 3.1416 * 685.8000 * 0.0000 * 18.00

= 0.000 N

Operating Bolt Load [Wm1]:

= max( H + Hp + H'p, 0 )

= max( 664941 + 0 + 0 , 0 )

= 664941.500 N

Gasket Seating Bolt Load [Wm2]:

= y * b * Pi * G + yPart * bPart * lp

= 0.00*9.5250*3.141*685.800+0.00*0.0000*0.00

= 0.000 N

Required Bolt Area [Am]:

= Maximum of Wm1/Sb, Wm2/Sa

= Maximum of 664941/172 , 0/172

= 3857.857 mm²

ASME Maximum Circumferential Spacing between Bolts per App. 2 eq. (3) [Bsmax]:

= 2a + 6t/(m + 0.5)

= 2 * 31.750 + 6 * 68.000/(0.00 + 0.5)

= 879.500 mm

Actual Circumferential Bolt Spacing [Bs]:

= C * sin( pi / n )

= 749.300 * sin( 3.142/20 )

= 117.216 mm

25

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Flg Calc [Int P] : A1 (blind) Flng: 12 1:01a Jan 11,2015 ASME Moment Multiplier for Bolt Spacing per App. 2 eq. (7) [Bsc]:

= max( sqrt( Bs/( 2a + t )), 1 )

= max( sqrt( 117.216/( 2 * 31.750 + 68.000 )), 1 )

= 1.0000

Bolting Information for TEMA Imperial Thread Series (Non Mandatory):

-----------------------------------------------------------------------------

Minimum Actual Maximum

-----------------------------------------------------------------------------

Bolt Area, mm² 3857.857 11987.072

Radial distance bet. bolts and the edge 31.750 31.750

Circumferential spacing between bolts 71.450 117.216 879.500

-----------------------------------------------------------------------------

Flange Design Bolt Load, Gasket Seating [W]:

= Sa * ( Am + Ab ) / 2

= 172.38 * ( 3857.8567 + 11987.0723 )/2

= 1365518.75 N

Gasket Load for the Operating Condition [HG]:

= Wm1

= 664941.50 N

Moment Arm Calculations:

Distance to Gasket Load Reaction [hg]:

= (C - G ) / 2

= ( 749.3000 - 685.8000 )/2

= 31.7500 mm

Tangential Flange Stress, Flat Head (UG-34), Operating [STo]:

= 2 * ( 1.9 * Wm1 * hG * Bsc/(t² * G) + C * Z * Peq * G²/t² )

= 2*(1.9*664941*31.7500*1.0000/(68.0000²*685.8000)+

0.30*1.0000*18.00*685.8000²/68.0000²)

= 135.17 MPa Doubled per UG-39(d)(2).

26

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Flg Calc [Int P] : A1 (blind) Flng: 12 1:01a Jan 11,2015

Tangential Flange Stress, Flat Head (UG-34), Seating [STa]:

= 2 * 1.9 * W * hG * Bcor / (t² * G)

= 2*1.9*1365518*31.7500*1.000/(68.0000²*685.8000)

= 51.96 MPa Doubled per UG-39(d)(2).

Bolt Stress, Operating [BSo]:

= ( Wm1 / Ab )

= (664941/11987.0723)

= 55.48 MPa

Bolt Stress, Seating [BSa]:

= ( Wm2 / Ab )

= (0/11987.0723)

= 0.00 MPa

Flange Stress Analysis Results:

Operating Gasket Seating

Actual Allowed Actual Allowed

---------------------------------------------------------------------

Tangential Flange 135. 138. 52. 138. MPa

Bolting 55. 172. 0. 172. MPa

---------------------------------------------------------------------

Reqd. Blind Flange Thickness at Center 67.323 mm

Reqd. Blind Flange Thickness at Gasket 29.514 mm

Estimated M.A.W.P. ( Operating ) 18.4 bar

Estimated Finished Weight of Flange at given Thk. 283.2 kgm

Estimated Unfinished Weight of Forging at given Thk 283.2 kgm

SA-182 F316, Min Metal Temp without impact per UHA-51: -196 °C


27

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Internal Pressure Calculations : Step: 5 1:01a Jan 11,2015

Element Thickness, Pressure, Diameter and Allowable Stress :

| | Int. Press | Nominal | Total Corr| Element | Allowable |

From| To | + Liq. Hd | Thickness | Allowance | Diameter | Stress(SE)|

| | bar | mm | mm | mm | MPa |

---------------------------------------------------------------------------

Head| 18.097 | 8.0000 | ... | 610.00 | 115.15 |

Shell| 18.080 | 8.0000 | ... | 610.00 | 115.15 |

Body Flang| 18.000 | 8.0000 | ... | 593.60 | 137.90 |

Blind| 18.000 | 8.0000 | ... | 812.80 | 137.90 |

Element Required Thickness and MAWP :

| | Design | M.A.W.P. | M.A.P. | Minimum | Required |

From| To | Pressure | Corroded | New & Cold | Thickness | Thickness |

| | bar | bar | bar | mm | mm |

----------------------------------------------------------------------------

Head| 18.0000 | 19.0593 | 19.1564 | 5.00000 | 4.72737 |

Shell| 18.0000 | 30.4379 | 30.5182 | 8.00000 | 4.75991 |

Body Flang| 18.0000 | 18.3984 | 18.9983 | 47.7520 | No Calc |

Blind| 18.0000 | 18.3635 | 18.3635 | 68.0000 | 67.3228 |

Minimum 18.283 18.363

Note : The M.A.W.P is Governed by a Standard Flange !

Flange MAWP including Static Pressure: 18.283 = 18.398 - 0.115 bar

Internal Pressure Calculation Results :


Elliptical Head From 10 To 20 SA-240 316L at 50 °C

28


Head

Longitudinal Joint: Full Radiography per UW-11(a) Type 1

Circumferential Joint: Full Radiography per UW-11(a) Type 1

Material UNS Number: S31603

Required Thickness due to Internal Pressure [tr]:

= (P*Do*K)/(2*S*E+2*P*(K-0.1)) per Appendix 1-4 (c)

= (18.097*610.0000*1.000)/(2*115.15*1.00+2*18.097*(1.000-0.1))

= 4.7274 + 0.0000 = 4.7274 mm

Max. Allowable Working Pressure at given Thickness, corroded [MAWP]:

Less Operating Hydrostatic Head Pressure of 0.097 bar

= (2*S*E*t)/(K*Do-2*t*(K-0.1)) per Appendix 1-4 (c)

= (2*115.15*1.00*5.0000)/(1.000*610.0000-2*5.0000*(1.00-0.1))

= 19.156 - 0.097 = 19.059 bar

Maximum Allowable Pressure, New and Cold [MAPNC]:

= (2*S*E*t)/(K*Do-2*t*(K-0.1)) per Appendix 1-4 (c)

= (2*115.15*1.00*5.0000)/(1.000*610.0000-2*5.0000*(1.000-0.1))

= 19.156 bar

Actual stress at given pressure and thickness, corroded [Sact]:

= (P*(K*Do-2*t*(K-0.1)))/(2*E*t)

= (18.097*(1.000*610.0000-2*5.0000*(1.000-0.1)))/(2*1.00*5.0000)

= 108.779 MPa

Straight Flange Required Thickness:

= (P*Ro)/(S*E+0.4*P) + ca per Appendix 1-1 (a)(1)

= (18.097*305.0000)/(115.15*1.00+0.4*18.097)+0.000

= 4.764 mm

29


Straight Flange Maximum Allowable Working Pressure:


= (S*E*t)/(Ro-0.4*t) per Appendix 1-1 (a)(1)

= (115.15 * 1.00 * 8.0000 )/(305.0000 - 0.4 * 8.0000 )

= 30.518 - 0.084 = 30.434 bar

Percent Elongation per UHA-44 (75*tnom/Rf)*(1-Rf/Ro) 5.715 %

Note: Please Check Requirements of Table UHA-44 for Elongation limits.

SA-240 316L, Min Metal Temp without impact per UHA-51: -196 °C

Cylindrical Shell From 20 To 30 SA-240 316L at 50 °C

Shell

Longitudinal Joint: Full Radiography per UW-11(a) Type 1

Circumferential Joint: Full Radiography per UW-11(a) Type 1



= (P*Ro) / (S*E+0.4*P) per Appendix 1-1 (a)(1)

= (18.080*305.0000)/(115.15*1.00+0.4*18.080)

= 4.7599 + 0.0000 = 4.7599 mm



= (S*E*t)/(Ro-0.4*t) per Appendix 1-1 (a)(1)

= (115.15*1.00*8.0000)/(305.0000-0.4*8.0000)

= 30.518 - 0.080 = 30.438 bar

Maximum Allowable Pressure, New and Cold [MAPNC]:

30

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Internal Pressure Calculations : Step: 5 1:01a Jan 11,2015 = (S*E*t)/(Ro-0.4*t) per Appendix 1-1 (a)(1)

= (115.15*1.00*8.0000)/(305.0000-0.4*8.0000)

= 30.518 bar

Actual stress at given pressure and thickness, corroded [Sact]:

= (P*(Ro-0.4*t))/(E*t)

= (18.080*((305.0000-0.4*8.0000))/(1.00*8.0000)

= 68.218 MPa

Percent Elongation per UHA-44 (50*tnom/Rf)*(1-Rf/Ro) 1.329 %

Note: Please Check Requirements of Table UHA-44 for Elongation limits.


Hydrostatic Test Pressure Results:

Pressure per UG99b = 1.3 * M.A.W.P. * Sa/S 23.768 bar

Pressure per UG99b[34] = 1.3 * Design Pres * Sa/S 23.400 bar

Pressure per UG99c = 1.3 * M.A.P. - Head(Hyd) 23.754 bar

Pressure per UG100 = 1.1 * M.A.W.P. * Sa/S 20.112 bar

Pressure per PED = 1.43 * MAWP 26.145 bar

Horizontal Test performed per: UG-99c

Please note that Nozzle, Shell, Head, Flange, etc MAWPs are all considered

when determining the hydrotest pressure for those test types that are based

on the MAWP of the vessel.

Stresses on Elements due to Test Pressure:

From To Stress Allowable Ratio Pressure

----------------------------------------------------------------------

Head 143.1 155.1 0.923 23.81

31

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Internal Pressure Calculations : Step: 5 1:01a Jan 11,2015 Shell 89.8 155.1 0.579 23.81

----------------------------------------------------------------------

Elements Suitable for Internal Pressure.


32

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- External Pressure Calculations : Step: 6 1:01a Jan 11,2015

External Pressure Calculation Results :


Elliptical Head From 10 to 20 Ext. Chart: HA-4 at 50 °C

Head

Elastic Modulus from Chart: HA-4 at 50 °C : 0.192E+06 MPa

Results for Maximum Allowable External Pressure (MAEP):

Tca OD D/t Factor A B

5.000 610.00 122.00 0.0011384 65.13

EMAP = B/(K0*D/t) = 65.1257/(0.9000 *122.0000 ) = 5.9304 bar

Results for Required Thickness (Tca):

Tca OD D/t Factor A B

1.613 610.00 378.29 0.0003672 35.22

EMAP = B/(K0*D/t) = 35.2184/(0.9000 *378.2888 ) = 1.0343 bar

Check the requirements of UG-33(a)(1) using P = 1.67 * External Design

pressure for this head.



= (P*Do*K)/(2*S*E+2*P*(K-0.1)) per Appendix 1-4 (c)

= (1.727*610.0000*1.000)/(2*115.15*1.00+2*1.727*(1.000-0.1))

= 0.4569 + 0.0000 = 0.4569 mm


= ((2*S*E*t)/(K*Do-2*t*(K-0.1)))/1.67 per Appendix 1-4 (c)

33

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- External Pressure Calculations : Step: 6 1:01a Jan 11,2015 = ((2*115.15*1.00*5.0000)/(1.000*610.0000-2*5.0000*(1.00-0.1)))/1.67

= 11.471 bar

Maximum Allowable External Pressure [MAEP]:

= min( MAEP, MAWP )

= min( 5.93 , 11.4709 )

= 5.930 bar

Thickness requirements per UG-33(a)(1) do not govern the required

thickness of this head.

Cylindrical Shell From 20 to 30 Ext. Chart: HA-4 at 50 °C

Shell

Elastic Modulus from Chart: HA-4 at 50 °C : 0.192E+06 MPa

Results for Maximum Allowable External Pressure (MAEP):

Tca OD SLEN D/t L/D Factor A B

8.000 610.00 2297.00 76.25 3.7656 0.0004912 47.12

EMAP = (4*B)/(3*(D/t)) = (4*47.1178 )/(3*76.2500 ) = 8.2380 bar

Results for Required Thickness (Tca):


3.448 610.00 2297.00 176.90 3.7656 0.0001431 13.72

EMAP = (4*B)/(3*(D/t)) = (4*13.7243 )/(3*176.9043 ) = 1.0343 bar

Results for Maximum Stiffened Length (Slen):


8.000 610.00 66104.80 76.25 50.0000 0.0001932 18.54

EMAP = (4*B)/(3*(D/t)) = (4*18.5364 )/(3*76.2500 ) = 3.2409 bar

External Pressure Calculations

34

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- External Pressure Calculations : Step: 6 1:01a Jan 11,2015

| | Section | Outside | Corroded | Factor | Factor |

From| To | Length | Diameter | Thickness | A | B |

| | mm | mm | mm | | MPa |

---------------------------------------------------------------------------

10| 20| No Calc | 610.000 | 5.00000 | 0.0011384 | 65.1257 |

20| 30| 2297.00 | 610.000 | 8.00000 | 0.00049120 | 47.1178 |

30| 40| No Calc | ... | 47.7520 | No Calc | No Calc |

40| 50| No Calc | ... | 68.0000 | No Calc | No Calc |


| | External | External | External | External |

From| To | Actual T. | Required T.|Des. Press. | M.A.W.P. |

| | mm | mm | bar | bar |

----------------------------------------------------------------

10| 20| 5.00000 | 1.61252 | 1.03420 | 5.93044 |

20| 30| 8.00000 | 3.44819 | 1.03420 | 8.23798 |

30| 40| 47.7520 | No Calc | 1.03420 | No Calc |

40| 50| 68.0000 | 37.6682 | 1.03420 | No Calc |

Minimum 5.930


| | Actual Len.| Allow. Len.| Ring Inertia | Ring Inertia |

From| To | Bet. Stiff.| Bet. Stiff.| Required | Available |

| | mm | mm | mm**4 | mm**4 |

-------------------------------------------------------------------

10| 20| No Calc | No Calc | No Calc | No Calc |

20| 30| 2297.00 | 66104.8 | No Calc | No Calc |



35

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- External Pressure Calculations : Step: 6 1:01a Jan 11,2015 Elements Suitable for External Pressure.


36

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Element and Detail Weights : Step: 7 1:01a Jan 11,2015

Element and Detail Weights

| | Element | Element | Corroded | Corroded | Extra due |

From| To | Metal Wgt. | ID Volume |Metal Wgt. | ID Volume | Misc % |

| | kgm | m³ | kgm | m³ | kgm |

---------------------------------------------------------------------------

10| 20| 33.0736 | 0.039026 | 33.0736 | 0.039026 | 1.65368 |

20| 30| 268.288 | 0.61226 | 268.288 | 0.61226 | 13.4144 |

30| 40| 127.648 | 0.042183 | 127.648 | 0.042183 | 6.38241 |

40| 50| 283.228 | ... | 283.228 | ... | 14.1614 |

---------------------------------------------------------------------------

Total 712 0.69 712 0.69 35

Weight of Details

| | Weight of | X Offset, | Y Offset, |

From|Type| Detail | Dtl. Cent. |Dtl. Cent. | Description

| | kgm | mm | mm |

-------------------------------------------------

10|Liqd| 35.5072 | ... | -75.0000 | LIQUID

10|Nozl| 5.56748 | ... | -150.000 | N3

20|Liqd| 226.965 | ... | 450.000 | LIQUID

20|Nozl| 8.73081 | 322.400 | 1187.00 | N1

20|Nozl| 7.18497 | 322.400 | 1812.00 | N5

20|Nozl| 7.18497 | 322.400 | 162.000 | N6

20|Nozl| 7.18497 | 322.400 | 1812.00 | K1

20|Nozl| 8.15833 | 341.450 | 962.000 | K2A

20|Nozl| 8.15833 | 341.450 | 162.000 | K2B

20|Nozl| 8.15833 | 341.450 | 712.000 | K3A

20|Nozl| 8.15833 | 341.450 | 162.000 | K3B

20|Nozl| 7.18497 | 322.400 | 1002.00 | K4A

20|Nozl| 7.18497 | 322.400 | 162.000 | K4B

37

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Element and Detail Weights : Step: 7 1:01a Jan 11,2015 20|Nozl| 8.15833 | 341.450 | 962.000 | K5A

20|Nozl| 8.15833 | 341.450 | 512.000 | K5B

20|Nozl| 19.8200 | 354.150 | 162.000 | HH

20|Lugs| 32.1232 | ... | 1924.00 | LUG

20|Wght| 100.000 | ... | 2100.00 | MIST ELIMINATOR

40|Nozl| 7.18497 | ... | 2460.00 | N2

40|Nozl| 6.61229 | ... | 2460.00 | N4

Total Weight of Each Detail Type

Total Weight of Liquid 262.5

Total Weight of Nozzles 132.8

Total Weight of Lugs 32.1

Total Weight of Weights 100.0

---------------------------------------------------------------

Sum of the Detail Weights 527.4 kgm

Weight Summation

Fabricated Shop Test Shipping Erected Empty Operating

------------------------------------------------------------------------------

747.8 912.8 747.8 912.8 747.8 912.8

... 693.0 ... ... ... 262.5

132.8 ... 132.8 ... ... ...

32.1 ... 32.1 ... ... ...

... ... ... ... ... 100.0

... ... ... ... ... ...

... ... ... ... 132.8 ...

... ... ... ... 32.1 ...

------------------------------------------------------------------------------

912.8 1605.8 912.8 912.8 912.8 1275.2 kgm

38


Miscellaneous Weight Percent: 5.0 %

Note that the above value for the miscellaneous weight percent has

been applied to the shells/heads/flange/tubesheets/tubes etc. in the

weight calculations for metallic components.

Note: The shipping total has been modified because some items have

been specified as being installed in the shop.

Weight Summary

Fabricated Wt. - Bare Weight W/O Removable Internals 912.8 kgm

Shop Test Wt. - Fabricated Weight + Water ( Full ) 1605.8 kgm

Shipping Wt. - Fab. Wt + Rem. Intls.+ Shipping App. 912.8 kgm

Erected Wt. - Fab. Wt + Rem. Intls.+ Insul. (etc) 912.8 kgm

Ope. Wt. no Liq - Fab. Wt + Intls. + Details + Wghts. 912.8 kgm

Operating Wt. - Empty Wt + Operating Liq. Uncorroded 1275.2 kgm

Field Test Wt. - Empty Weight + Water (Full) 1605.8 kgm

Mass of the Upper 1/3 of the Vertical Vessel 636.4 kgm

Outside Surface Areas of Elements

| | Surface |

From| To | Area |

| | mm² |

----------------------------

10| 20| 484863. |

20| 30| 4.233E+06 |

30| 40| 582175. |

40| 50| 692506. |

-----------------------------

Total 5992808.500 mm²

39



| To | Total Ele.| Total. Ele.|Total. Ele.| Total Dtl.| Oper. Wgt. |

From| To | Empty Wgt.| Oper. Wgt.|Hydro. Wgt.| Offset Mom.| No Liquid |

| | kgm | kgm | kgm | N-m | kgm |

---------------------------------------------------------------------------

10| 20| 40.2947 | 75.8019 | 79.2965 | ... | 40.2947 |

20|Lugs| 316.782 | 578.916 | 807.345 | 299.889 | 396.954 |

Lugs| 30| 78.3459 | 143.176 | 199.671 | 74.1678 | 98.1739 |

30| 40| 134.031 | 134.031 | 176.188 | ... | 134.031 |

40| 50| 311.187 | 311.187 | 311.187 | ... | 311.187 |

Cumulative Vessel Weight

| | Cumulative Ope | Cumulative | Cumulative |

From| To | Wgt. No Liquid | Oper. Wgt. | Hydro. Wgt. |

| | kgm | kgm | kgm |

-------------------------------------------------------

10| 20| ... | ... | ... |

20|Lugs| -40.2947 | -75.8019 | -79.2965 |

Lugs| 30| 543.391 | 588.394 | 687.045 |

30| 40| 445.217 | 445.217 | 487.375 |

40| 50| 311.187 | 311.187 | 311.187 |

Note: The cumulative operating weights no liquid in the column above

are the cumulative operating weights minus the operating liquid

weight minus any weights absent in the empty condition.

Cumulative Vessel Moment

| | Cumulative | Cumulative |Cumulative |

From| To | Empty Mom. | Oper. Mom. |Hydro. Mom.|

40

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Element and Detail Weights : Step: 7 1:01a Jan 11,2015 | | N-m | N-m | N-m |

-------------------------------------------------

10| 20| ... | ... | ... |

20|Lugs| 299.889 | 299.889 | 299.889 |

Lugs| 30| 74.1678 | 74.1678 | 74.1678 |

30| 40| ... | ... | ... |

40| 50| ... | ... | ... |


41

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Flange MAWP : Step: 8 1:01a Jan 11,2015

Nozzle Flange MAWP Results :

Nozzle ----- Flange Rating

Description Operating Ambient Temperature Class Grade|Group

bar bar °C

----------------------------------------------------------------------------

N3 18.4 19.0 50 150 GR 2.2

N1 96.2 99.3 50 600 GR 2.2

N5 18.4 19.0 50 150 GR 2.2

N6 18.4 19.0 50 150 GR 2.2

K1 18.4 19.0 50 150 GR 2.2

K2A 18.4 19.0 50 150 GR 2.2

K2B 18.4 19.0 50 150 GR 2.2

K3A 18.4 19.0 50 150 GR 2.2

K3B 18.4 19.0 50 150 GR 2.2

K4A 18.4 19.0 50 150 GR 2.2

K4B 18.4 19.0 50 150 GR 2.2

K5A 18.4 19.0 50 150 GR 2.2

K5B 18.4 19.0 50 150 GR 2.2

HH 18.4 19.0 50 150 GR 2.2

N2 18.4 19.0 50 150 GR 2.2

N4 18.4 19.0 50 150 GR 2.2

----------------------------------------------------------------------------

Minimum Rating 18.4 19.0 bar

Note: ANSI Ratings are per ANSI/ASME B16.5 2009 Metric Edition


42

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Natural Frequency Calculation : Step: 9 1:01a Jan 11,2015

The Natural Frequencies for the vessel have been computed iteratively

by solving a system of matrices. These matrices describe the mass

and the stiffness of the vessel. This is the generalized eigenvalue/

eigenvector problem and is referenced in some mathematical texts.

The Natural Frequency for the Vessel (Empty.) is 81.2720 Hz.

The Natural Frequency for the Vessel (Ope...) is 64.8727 Hz.


43

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Wind Load Calculation : Step: 10 1:01a Jan 11,2015

Note: Using the User Defined Wind Profile ...

Wind Vibration Calculations

This evaluation is based on work by Kanti Mahajan and Ed Zorilla

Nomenclature

Cf - Correction factor for natural frequency

D - Average internal diameter of vessel mm

Df - Damping Factor < 0.75 Unstable, > 0.95 Stable

Dr - Average internal diameter of top half of vessel mm

f - Natural frequency of vibration (Hertz)

f1 - Natural frequency of bare vessel based on a unit value of (D/L²)(104)

L - Total height of structure mm

Lc - Total length of conical section(s) of vessel mm

tb - Uncorroded plate thickness at bottom of vessel mm

V30 - Design Wind Speed provided by user km/hr

Vc - Critical wind velocity km/hr

Vw - Maximum wind speed at top of structure km/hr

W - Total corroded weight of structure N

Ws - Cor. vessel weight excl. weight of parts which do not effect stiff. N

Z - Maximum amplitude of vibration at top of vessel mm

Dl - Logarithmic decrement ( taken as 0.03 for Welded Structures )

Vp - Vib. Chance, <= 0.314E-05 (High); 0.314E-05 < 0.393E-05 (Probable)

P30 - wind pressure 30 feet above the base

Check other Conditions and Basic Assumptions:

#1 - Total Cone Length / Total Length < 0.5

0.000/2467.400 = 0.000

44

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Wind Load Calculation : Step: 10 1:01a Jan 11,2015 #2 - ( D / L² ) * 104 < 8.0 (English Units)

- ( 2.02/8.10² ) * 104 = 307.689 [Geometry Violation]

Compute the vibration possibility. If Vp > 0.393E-05 no chance. [Vp]:

= W / ( L * Dr²)

= 12504/( 2467.40 * 606.011² )

= 0.13800E-04

Since Vp is > 0.393E-05 no further vibration analysis is required !

Wind Loads on Masses/Equipment/Piping

ID Wind Area Elevation Pressure Force

mm² mm kPa N

-------------------------------------------------------------------------

MIST ELIMINAT 0.00 2138.00 0.75 0.00


Wind Load Calculation

| | Wind | Wind | Wind | Wind | Element |

From| To | Height | Diameter | Area | Pressure | Wind Load |

| | mm | mm | mm² | kPa | N |

---------------------------------------------------------------------------

10| 20| 109.385 | 732.000 | 116927. | 0.75000 | 87.6934 |

20| 30| 1292.50 | 732.000 | 1.617E+06 | 0.75000 | 1212.71 |

30| 40| 2473.20 | 712.320 | 108558. | 0.75000 | 81.4163 |

40| 50| 2583.40 | 975.360 | 66324.5 | 0.75000 | 49.7422 |


45

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Earthquake Load Calculation : Step: 11 1:01a Jan 11,2015

Earthquake Loading Specified in G's

Horizontal Acceleration factor (GX) 0.500

Horizontal Acceleration factor (GZ) 0.500

Vertical Acceleration factor (GY) -2.000


Earthquake Load Calculation

| | Earthquake | Earthquake | Element | Element |

From| To | Height | Weight | Ope Load | Emp Load |

| | mm | N | N | N |

--------------------------------------------------------------

10| 20| 19.0000 | 743.314 | 525.602 | 279.399 |

20|Lugs| 1809.00 | 5676.85 | 4014.14 | 2196.53 |

Lugs| 30| 2028.00 | 1403.99 | 992.769 | 543.242 |

30| 40| 2323.20 | 1314.30 | 929.353 | 929.353 |

40| 50| 2433.40 | 3051.49 | 2157.73 | 2157.73 |


46

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Wind/Earthquake Shear, Bending : Step: 12 1:01a Jan 11,2015

The following table is for the Operating Case.

Wind/Earthquake Shear, Bending

| | Distance to| Cumulative |Earthquake | Wind | Earthquake |

From| To | Support| Wind Shear | Shear | Bending | Bending |

| | mm | N | N | N-m | N-m |

---------------------------------------------------------------------------

10| 20| 1854.61 | ... | ... | ... | ... |

20|Lugs| 885.500 | 87.6934 | 525.602 | 4.00173 | 23.9849 |

Lugs| 30| 219.000 | 459.308 | 4605.46 | 895.018 | 2467.76 |

30| 40| 514.200 | 131.158 | 3087.09 | 15.4821 | 473.210 |

40| 50| 624.400 | 49.7422 | 2157.73 | 1.69193 | 73.3929 |


47

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Wind Deflection : Step: 13 1:01a Jan 11,2015

Wind Deflection Calculations:

The following table is for the Operating Case.

Wind Deflection

| | Cumulative | Centroid | Elem. End | Elem. Ang. |

From| To | Wind Shear | Deflection |Deflection | Rotation |

| | N | mm | mm | |

--------------------------------------------------------------

10| 20| ... | 0.00030324 |0.00060651 | ... |

20|Lugs| 87.6934 | -0.011117 | ... | ... |

Lugs| 30| 459.308 | -0.011573 |-0.0080331 | -0.00002 |

30| 40| 131.158 | -0.0067998 |-0.0055664 | -0.00002 |

40| 50| 49.7422 | -0.0050160 |-0.0044657 | -0.00002 |

Critical Wind Velocity for Tower Vibration

| | 1st Crit. | 2nd Crit. |

From| To | Wind Speed | Wind Speed |

| | km/hr | km/hr |

-------------------------------------

10| 20| 852.459 | 5327.87 |

20| 30| 852.459 | 5327.87 |

30| 40| 829.541 | 5184.63 |

40| 50| 1135.87 | 7099.17 |

Allowable deflection at the Tower Top (Ope)( 6.000"/100ft. Criteria)

Allowable deflection : 12.337 Actual Deflection : 0.001 mm


48

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Longitudinal Stress Constants : Step: 14 1:01a Jan 11,2015

Longitudinal Stress Constants

| | Metal Area | Metal Area |New & Cold | Corroded |

From| To | New & Cold | Corroded |Sect. Mod. | Sect. Mod. |

| | mm² | mm² | mm ³ | mm ³ |

--------------------------------------------------------------

10| 20| 9503.34 | 9503.34 | 1.426E+06 | 1.426E+06 |

20| 30| 15129.9 | 15129.9 | 2.248E+06 | 2.248E+06 |

30| 40| 15129.9 | 15129.9 | 2.248E+06 | 2.248E+06 |

40| 50| 15129.9 | 15129.9 | 2.248E+06 | 2.248E+06 |


49

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Longitudinal Allowable Stresses : Step: 15 1:01a Jan 11,2015

Longitudinal Allowable Stresses

| | | Hydrotest | | Hydrotest |

From| To | Tensile | Tensile | Compressive | Compressive |

| | MPa | MPa | MPa | MPa |

-------------------------------------------------------------------

10| 20| 138.176 | 186.165 | -88.0035 | -90.1732 |

20|Lugs| 138.176 | 186.165 | -95.5055 | -97.8688 |

Lugs| 30| 138.176 | 186.165 | -95.5055 | -97.8688 |

30| 40| 165.480 | 223.398 | -104.311 | -105.116 |

40| 50| 165.480 | 223.398 | -104.311 | -105.116 |


50

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Longitudinal Stresses Due to . . . Step: 16 1:01a Jan 11,2015

Longitudinal Stress Report

Note: Longitudinal Operating and Empty Stresses are computed in the

corroded condition. Stresses due to loads in the hydrostatic test

cases have been computed in the new and cold condition.

Longitudinal Stresses Due to . . .

| | Long. Str. | Long. Str. |Long. Str. |

From| To | Int. Pres. | Ext. Pres. |Hyd. Pres. |

| | MPa | MPa | MPa |

-------------------------------------------------

10| 20| 53.6478 | -3.18083 | 70.7962 |

20| 30| 33.0573 | -1.99793 | 43.6240 |

30| 40| ... | ... | ... |

40| 50| ... | ... | ... |


| | Wght. Str. | Wght. Str. |Wght. Str. | Wght. Str. | Wght. Str. |

From| To | Empty | Operating |Hydrotest | Emp. Mom. | Opr. Mom. |

| | MPa | MPa | MPa | MPa | MPa |

---------------------------------------------------------------------------

10| 20| ... | ... | ... | ... | ... |

20|Lugs| 0.026118 | 0.049133 | ... | 0.13338 | 0.13338 |

Lugs| 30| -0.35221 | -0.23427 | ... | 0.032988 | 0.032988 |

30| 40| -0.28858 | -0.28858 | ... | ... | ... |

40| 50| -0.20170 | -0.20170 | ... | ... | ... |


| | Wght. Str. | Bend. Str. |Bend. Str. | Bend. Str. | Bend. Str. |

51

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Longitudinal Stresses Due to . . . Step: 16 1:01a Jan 11,2015 From| To | Hyd. Mom. | Oper. Wind |Oper. Equ. | Hyd. Wind | Hyd. Equ. |

| | MPa | MPa | MPa | MPa | MPa |

---------------------------------------------------------------------------

10| 20| ... | ... | ... | ... | ... |

20|Lugs| ... | 0.0017799 | 0.010668 | ... | ... |

Lugs| 30| ... | 0.39809 | 1.09761 | ... | ... |

30| 40| ... | 0.0068861 | 0.21047 | ... | ... |

40| 50| ... | 0.00075253 | 0.032644 | ... | ... |


| | Long. Str. | Long. Str. |Long. Str. | EarthQuake |

From| To | Vortex Ope.| Vortex Emp.|Vortex Tst.| Empty |


--------------------------------------------------------------

10| 20| ... | ... | ... | ... |

20|Lugs| ... | ... | ... | 0.0056709 |

Lugs| 30| ... | ... | ... | 0.22624 |

30| 40| ... | ... | ... | 0.21047 |

40| 50| ... | ... | ... | 0.032644 |


| | Long. Str. | Long. Str. |

From| To | Y Forces W | Y ForceS S |

| | MPa | MPa |

-------------------------------------

10| 20| ... | 0.15645 |

20|Lugs| ... | 0.84874 |

Lugs| 30| ... | -0.76276 |

30| 40| ... | -0.57716 |

40| 50| ... | -0.40341 |

52

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Longitudinal Stresses Due to . . . Step: 16 1:01a Jan 11,2015 Long. Stresses due to User Forces and Moments

| |Wind For/Mom| Eqk For/Mom|Wnd For/Mom| Eqk For/Mom|

From| To | Corroded | Corroded | No Corr. | No Corr. |


--------------------------------------------------------------

10| 20| ... | ... | ... | ... |

20|Lugs| ... | ... | ... | ... |

Lugs| 30| ... | ... | ... | ... |

30| 40| ... | ... | ... | ... |

40| 50| ... | ... | ... | ... |


53

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Stress due to Combined Loads : Step: 17 1:01a Jan 11,2015

Stress Combination Load Cases for Vertical Vessels:

Load Case Definition Key

IP = Longitudinal Stress due to Internal Pressure

EP = Longitudinal Stress due to External Pressure

HP = Longitudinal Stress due to Hydrotest Pressure

NP = No Pressure

EW = Longitudinal Stress due to Weight (No Liquid)

OW = Longitudinal Stress due to Weight (Operating)

HW = Longitudinal Stress due to Weight (Hydrotest)

WI = Bending Stress due to Wind Moment (Operating)

EQ = Bending Stress due to Earthquake Moment (Operating)

EE = Bending Stress due to Earthquake Moment (Empty)

HI = Bending Stress due to Wind Moment (Hydrotest)

HE = Bending Stress due to Earthquake Moment (Hydrotest)

WE = Bending Stress due to Wind Moment (Empty) (no CA)

WF = Bending Stress due to Wind Moment (Filled) (no CA)

CW = Longitudinal Stress due to Weight (Empty) (no CA)

VO = Bending Stress due to Vortex Shedding Loads ( Ope )

VE = Bending Stress due to Vortex Shedding Loads ( Emp )

VF = Bending Stress due to Vortex Shedding Loads ( Test No CA. )

FW = Axial Stress due to Vertical Forces for the Wind Case

FS = Axial Stress due to Vertical Forces for the Seismic Case

BW = Bending Stress due to Lat. Forces for the Wind Case, Corroded

BS = Bending Stress due to Lat. Forces for the Seismic Case, Corroded

BN = Bending Stress due to Lat. Forces for the Wind Case, UnCorroded

BU = Bending Stress due to Lat. Forces for the Seismic Case, UnCorroded

General Notes:

Case types HI and HE are in the Un-Corroded condition.

54


Case types WE, WF, and CW are in the Un-Corroded condition.

A blank stress and stress ratio indicates that the corresponding

stress comprising those components that did not contribute to that

type of stress.

An asterisk (*) in the final column denotes overstress.

Analysis of Load Case 1 : NP+EW+WI+FW+BW

From Tensile All. Tens. Comp. All. Comp. Tens. Comp.

Node Stress Stress Stress Stress Ratio Ratio

10 0.00 138.18 0.00 88.00 0.0000 0.0000

20 0.16 138.18 -0.11 95.51 0.0012 0.0011

20 0.08 138.18 -0.78 95.51 0.0006 0.0082

Analysis of Load Case 2 : NP+EW+EE+FS+BS



10 0.16 138.18 88.00 0.0011

20 1.01 138.18 95.51 0.0073

20 138.18 -1.37 95.51 0.0144

Analysis of Load Case 3 : NP+OW+WI+FW+BW



10 0.00 138.18 0.00 88.00 0.0000 0.0000

20 0.18 138.18 -0.09 95.51 0.0013 0.0009

20 0.20 138.18 -0.67 95.51 0.0014 0.0070

Analysis of Load Case 4 : NP+OW+EQ+FS+BS

55

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Stress due to Combined Loads : Step: 17 1:01a Jan 11,2015 From Tensile All. Tens. Comp. All. Comp. Tens. Comp.


10 0.16 138.18 88.00 0.0011

20 1.04 138.18 95.51 0.0075

20 0.13 138.18 -2.13 95.51 0.0010 0.0223

Analysis of Load Case 5 : NP+HW+HI



10 0.00 186.17 0.00 90.17 0.0000 0.0000

20 0.00 186.17 0.00 97.87 0.0000 0.0000

20 0.00 186.17 0.00 97.87 0.0000 0.0000

Analysis of Load Case 6 : NP+HW+HE



10 0.00 186.17 0.00 90.17 0.0000 0.0000

20 0.00 186.17 0.00 97.87 0.0000 0.0000

20 0.00 186.17 0.00 97.87 0.0000 0.0000

Analysis of Load Case 7 : IP+OW+WI+FW+BW



10 53.65 138.18 88.00 0.3883

20 33.24 138.18 95.51 0.2406

20 33.25 138.18 95.51 0.2407

Analysis of Load Case 8 : IP+OW+EQ+FS+BS



10 53.80 138.18 88.00 0.3894

20 34.10 138.18 95.51 0.2468

20 33.19 138.18 95.51 0.2402

56


Analysis of Load Case 9 : EP+OW+WI+FW+BW



10 138.18 -3.18 88.00 0.0361

20 138.18 -2.08 95.51 0.0218

20 138.18 -2.66 95.51 0.0279

Analysis of Load Case 10 : EP+OW+EQ+FS+BS



10 138.18 -3.02 88.00 0.0344

20 138.18 -1.24 95.51 0.0130

20 138.18 -4.13 95.51 0.0432

Analysis of Load Case 11 : HP+HW+HI



10 70.80 186.17 90.17 0.3803

20 43.62 186.17 97.87 0.2343

20 43.62 186.17 97.87 0.2343

Analysis of Load Case 12 : HP+HW+HE



10 70.80 186.17 90.17 0.3803

20 43.62 186.17 97.87 0.2343

20 43.62 186.17 97.87 0.2343

Analysis of Load Case 13 : IP+WE+EW



10 53.65 138.18 88.00 0.3883

57

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Stress due to Combined Loads : Step: 17 1:01a Jan 11,2015 20 33.22 138.18 95.51 0.2404

20 32.74 138.18 95.51 0.2369

Analysis of Load Case 14 : IP+WF+CW



10 53.65 138.18 88.00 0.3883

20 33.11 138.18 95.51 0.2396

20 32.82 138.18 95.51 0.2375

Analysis of Load Case 15 : IP+VO+OW



10 53.65 138.18 88.00 0.3883

20 33.24 138.18 95.51 0.2406

20 32.86 138.18 95.51 0.2378

Analysis of Load Case 16 : IP+VE+EW



10 53.65 138.18 88.00 0.3883

20 33.22 138.18 95.51 0.2404

20 32.74 138.18 95.51 0.2369

Analysis of Load Case 17 : NP+VO+OW



10 0.00 138.18 0.00 88.00 0.0000 0.0000

20 0.18 138.18 -0.08 95.51 0.0013 0.0009

20 138.18 -0.27 95.51 0.0028

Analysis of Load Case 18 : FS+BS+IP+OW


58

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Stress due to Combined Loads : Step: 17 1:01a Jan 11,2015 Node Stress Stress Stress Stress Ratio Ratio

10 53.80 138.18 88.00 0.3894

20 34.09 138.18 95.51 0.2467

20 32.09 138.18 95.51 0.2323

Analysis of Load Case 19 : FS+BS+EP+OW



10 138.18 -3.02 88.00 0.0344

20 138.18 -1.23 95.51 0.0129

20 138.18 -3.03 95.51 0.0317

Absolute Maximum of the all of the Stress Ratio's 0.3894

Governing Element: Head

Governing Load Case 8 : IP+OW+EQ+FS+BS


59

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Center of Gravity Calculation : Step: 18 1:01a Jan 11,2015

Shop/Field Installation Options :

Note : The CG is computed from the first Element From Node

Center of Gravity of Liquid 411.837 mm

Center of Gravity of Nozzles 1114.441 mm

Center of Gravity of Lugs 1962.000 mm

Center of Gravity of Added Weights (Operating) 2138.000 mm

Center of Gravity of Bare Shell New and Cold 1811.575 mm

Center of Gravity of Bare Shell Corroded 1811.575 mm

Vessel CG in the Operating Condition 1480.271 mm

Vessel CG in the Fabricated (Shop/Empty) Condition 1715.449 mm

Vessel CG in the Test Condition 1415.992 mm


60

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:01a Jan 11,2015

Support Lug Calculations: Operating Case

INPUT ECHO OF SUPPORT LUG INPUT

Type of Geometry : Gussets with No Top Plate

Number of Support Lugs Nlug 2

Distance from Vessel OD to Lug Contact Point Dlug 128.0000 mm

Lug Support Force Bearing Width Wfb 204.0000 mm

Lug Material SA-240 316L

Lug Yield Stress 165.40 MPa

Radial Width of bottom Support Lug Plate Wpl 254.0000 mm

Effective Force Bearing Length Lpl 200.0000 mm

Thickness of bottom Support Lug Plate Tpl 20.0000 mm

Distance between Gussets Dgp 154.0000 mm

Mean Width of Gusset Plate Wgp 102.0000 mm

Height of Gusset Plate Hgp 306.0000 mm

Thickness of Gusset Plate Tgp 14.0000 mm

Pad Width along Circumference C11P 200.000 mm

Pad Length along Vessel Axis C22P 380.000 mm

Pad Thickness Tpad 8.000 mm


Bolt Allowable Stress at Design Temperature 172.38 MPa

Thread Series TEMA Metric

Bolt Diameter 24.00 mm

Results for Support Lugs: Description: LUG

Overturning Moment at Support Lug 2468. N-m

Weight Load at the top of one Lug 18285. N

61

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:01a Jan 11,2015 Force on one Lug, Operating Condition [Flug]:

= ( W/Nlug + Mlug/( Rlug * Nlug/2 ) )

= ( 36569/2 + 2467/( 433.00 * 2/2 ))

= 23981.83 N

Bearing Area [Ba]:

= Lpl * Wfb

= 200.000 * 204.000

= 40800.00 mm²

Bending Stress in bottom Plate (Unif. Load) Per Bednar p.156 [Spl2]:

= Beta1 * Flug/Ba * Wfb² / Tpl² per Roark & Young 5th Ed.

= 0.315 * 23981.8/40800.000 * 204.000²/20.000²

= 19.24 MPa

Bottom Plate Required Thickness (Uniform Load) 8.3545 mm

Bottom Plate Required Thickness based on ADM S 3/4 [trAD]:

= 0.71 * Dgp * (( Flug / ( Lpl * Wfb ))/Spa )½

= 0.71*154.00*((23981/(200.00*204.00))/110.267)½

= 7.983 mm

Note: If using the AD Code recommendations, the force bearing width (Wfb) must

be greater than or equal to 1/3 of the bottom plate radial width (Wpl)

plus the pad thickness (Padthk), if there is a pad.

Bottom Support Plate Allowable Stress [Spa]:

= 2/3 * Ylug

= 2/3 * 165

= 110.27 MPa

Gusset Plate Axial Stress ( Force / Gusset Plate Area ) [Sgp]:

= ( Flug/2 )/( Wgp * Tgp )

62

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:01a Jan 11,2015 = ( 23981/2 )/( 102.000 *14.0000 )

= 8.40 MPa

Required Thickness of Gussets per AISC 5.6179 mm

Gusset Plate Allowable Stress [Sga]:

= ( 1-(Klr)²/(2*Cc²))*Fy /( 5/3+3*(Klr)/(8*Cc)-(Klr³)/(8*Cc³)

= ( 1-( 87.43 )²/(2 * 151.74² )) * 165/

( 5/3+3*(87.43 )/(8* 151.74 )-( 87.43³)/(8*151.74³)

= 74.21 MPa

Maximum Compressive Gusset Plate Stress per Bednar [SgpB]:

= Flug*( 3*Dlug-Wpl )/( Tgp* Wpl² * (Sin(Alph_G))² )

= 23981 *( 3*128.000 -254.000 )/( 14.0000 *254.000²*(Sin(45.19 ))² )

= 6.86 MPa

Gusset Plate Allowable Compressive Stress [SgaB]:

= 18000/(1+(1/18000)*( Hgp/Sin(Alph_G)/(0.289*Tgp))² )

= 18000/(1+(1/18000)* (306.000/Sin(45.19 )/(0.289*14.0000 ))² )

= 76.08 MPa

Note :

There was no uplift. Please choose an appropriate bolt

size for this support design.

Input Echo, WRC107/537 Item 1, Description: LUG

Diameter Basis for Vessel Vbasis ID

Cylindrical or Spherical Vessel Cylsph Cylindrical

Internal Corrosion Allowance Cas 0.0000 mm

Vessel Diameter Dv 594.000 mm

Vessel Thickness Tv 8.000 mm

63

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:01a Jan 11,2015 Design Temperature 50.00 °C

Attachment Type Type Rectangular

Parameter C11 C11 92.40 mm

Parameter C22 C22 244.80 mm

Thickness of Reinforcing Pad Tpad 8.000 mm

Pad Parameter C11P C11p 200.000 mm

Pad Parameter C22P C22p 380.000 mm

Design Internal Pressure Dp 18.000 bar

Include Pressure Thrust No

Vessel Centerline Direction Cosine Vx 0.000

Vessel Centerline Direction Cosine Vy 1.000

Vessel Centerline Direction Cosine Vz 0.000

Nozzle Centerline Direction Cosine Nx 1.000

Nozzle Centerline Direction Cosine Ny 0.000

Nozzle Centerline Direction Cosine Nz 0.000

Global Force (SUS) Fx 0.0 N

Global Force (SUS) Fy 18284.9 N

Global Force (SUS) Fz 0.0 N

Global Moment (SUS) Mx 0.0 N-m

Global Moment (SUS) My 0.0 N-m

Global Moment (SUS) Mz 2341.4 N-m

Internal Pressure (SUS) P 18.00 bar


Global Force (OCC) Fx 4309.8 N

Global Force (OCC) Fy 5696.9 N

64

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:01a Jan 11,2015 Global Force (OCC) Fz 0.0 N

Global Moment (OCC) Mx 0.0 N-m

Global Moment (OCC) My 551.9 N-m

Global Moment (OCC) Mz 729.5 N-m

Occasional Internal Pressure (OCC) Pvar 0.00 bar

Use Interactive Control No

WRC107 Version Version March 1979

Include Pressure Stress Indices per Div. 2 No

Compute Pressure Stress per WRC-368 No

WRC 107 Stress Calculation for SUStained loads:

Radial Load P 0.0 N

Circumferential Shear VC 0.0 N

Longitudinal Shear VL 18284.9 N

Circumferential Moment MC 0.0 N-m

Longitudinal Moment ML -2341.4 N-m

Torsional Moment MT 0.0 N-m

Dimensionless Parameters used : Gamma = 19.06

Dimensionless Loads for Cylindrical Shells at Attachment Junction:

-------------------------------------------------------------------

Curves read for 1979 Beta Figure Value Location

-------------------------------------------------------------------

N(PHI) / ( P/Rm ) 0.345 4C 2.411 (A,B)

N(PHI) / ( P/Rm ) 0.345 3C 1.447 (C,D)

M(PHI) / ( P ) 0.222 2C1 0.050 (A,B)

M(PHI) / ( P ) 0.222 1C 0.080 (C,D)

N(PHI) / ( MC/(Rm**2 * Beta) ) 0.210 3A 0.749 (A,B,C,D)

65

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:01a Jan 11,2015 M(PHI) / ( MC/(Rm * Beta) ) 0.250 1A 0.084 (A,B,C,D)

N(PHI) / ( ML/(Rm**2 * Beta) ) 0.290 3B 1.929 (A,B,C,D)

M(PHI) / ( ML/(Rm * Beta) ) 0.268 1B 0.027 (A,B,C,D)

N(x) / ( P/Rm ) 0.287 3C 1.736 (A,B)

N(x) / ( P/Rm ) 0.287 4C 2.636 (C,D)

M(x) / ( P ) 0.298 1C1 0.058 (A,B)

M(x) / ( P ) 0.298 2C ! 0.034 (C,D)

N(x) / ( MC/(Rm**2 * Beta) ) 0.210 4A 1.214 (A,B,C,D)

M(x) / ( MC/(Rm * Beta) ) 0.331 2A 0.035 (A,B,C,D)

N(x) / ( ML/(Rm**2 * Beta) ) 0.290 4B 0.789 (A,B,C,D)

M(x) / ( ML/(Rm * Beta) ) 0.335 2B 0.035 (A,B,C,D)

Note - The ! mark next to the figure name denotes curve value exceeded.

Stress Concentration Factors Kn = 1.00, Kb = 1.00

Stresses in the Vessel at the Attachment Junction

------------------------------------------------------------------------

| Stress Values at

Type of | (MPa )

---------------|--------------------------------------------------------

Stress Load| Au Al Bu Bl Cu Cl Du Dl

---------------|--------------------------------------------------------

Circ. Memb. P | 0 0 0 0 0 0 0 0

Circ. Bend. P | 0 0 0 0 0 0 0 0

Circ. Memb. MC | 0 0 0 0 0 0 0 0

Circ. Bend. MC | 0 0 0 0 0 0 0 0

Circ. Memb. ML | 8 8 -8 -8 0 0 0 0

Circ. Bend. ML | 18 -18 -18 18 0 0 0 0

|

66

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:01a Jan 11,2015 Tot. Circ. Str.| 26.8 -10.0 -26.8 10.0 0.0 0.0 0.0 0.0

------------------------------------------------------------------------

Long. Memb. P | 0 0 0 0 0 0 0 0

Long. Bend. P | 0 0 0 0 0 0 0 0

Long. Memb. MC | 0 0 0 0 0 0 0 0

Long. Bend. MC | 0 0 0 0 0 0 0 0

Long. Memb. ML | 5 5 -5 -5 0 0 0 0

Long. Bend. ML | 18 -18 -18 18 0 0 0 0

|

Tot. Long. Str.| 24.2 -13.5 -24.2 13.5 0.0 0.0 0.0 0.0

------------------------------------------------------------------------

Shear VC | 0 0 0 0 0 0 0 0

Shear VL | 0 0 0 0 -2 -2 2 2

Shear MT | 0 0 0 0 0 0 0 0

|

Tot. Shear| 0.0 0.0 0.0 0.0 -2.3 -2.3 2.3 2.3

------------------------------------------------------------------------

Str. Int. | 26.82 13.46 26.82 13.46 4.67 4.67 4.67 4.67

------------------------------------------------------------------------


Dimensionless Loads for Cylindrical Shells at Pad edge:

-------------------------------------------------------------------


-------------------------------------------------------------------

N(PHI) / ( P/Rm ) 0.597 4C ! 2.658 (A,B)

N(PHI) / ( P/Rm ) 0.597 3C ! 0.987 (C,D)

M(PHI) / ( P ) 0.423 2C1 0.009 (A,B)

M(PHI) / ( P ) 0.423 1C ! 0.062 (C,D)


M(PHI) / ( MC/(Rm * Beta) ) 0.447 1A 0.062 (A,B,C,D)

N(PHI) / ( ML/(Rm**2 * Beta) ) 0.510 3B ! 1.383 (A,B,C,D)


67

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:01a Jan 11,2015

N(x) / ( P/Rm ) 0.516 3C ! 0.987 (A,B)

N(x) / ( P/Rm ) 0.516 4C ! 2.658 (C,D)

M(x) / ( P ) 0.530 1C1 ! 0.014 (A,B)

M(x) / ( P ) 0.530 2C ! 0.032 (C,D)


M(x) / ( MC/(Rm * Beta) ) 0.544 2A ! 0.024 (A,B,C,D)

N(x) / ( ML/(Rm**2 * Beta) ) 0.510 4B ! 0.860 (A,B,C,D)

M(x) / ( ML/(Rm * Beta) ) 0.562 2B ! 0.009 (A,B,C,D)



Stresses in the Vessel at the Edge of Reinforcing Pad

------------------------------------------------------------------------

| Stress Values at

Type of | (MPa )

---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Circ. Memb. P | 0 0 0 0 0 0 0 0

Circ. Bend. P | 0 0 0 0 0 0 0 0

Circ. Memb. MC | 0 0 0 0 0 0 0 0

Circ. Bend. MC | 0 0 0 0 0 0 0 0

Circ. Memb. ML | 7 7 -7 -7 0 0 0 0

Circ. Bend. ML | 8 -8 -8 8 0 0 0 0

|

Tot. Circ. Str.| 16.0 -0.9 -16.0 0.9 0.0 0.0 0.0 0.0

------------------------------------------------------------------------

Long. Memb. P | 0 0 0 0 0 0 0 0

68

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:01a Jan 11,2015 Long. Bend. P | 0 0 0 0 0 0 0 0

Long. Memb. MC | 0 0 0 0 0 0 0 0

Long. Bend. MC | 0 0 0 0 0 0 0 0

Long. Memb. ML | 6 6 -6 -6 0 0 0 0

Long. Bend. ML | 11 -11 -11 11 0 0 0 0

|

Tot. Long. Str.| 18.4 -5.0 -18.4 5.0 0.0 0.0 0.0 0.0

------------------------------------------------------------------------

Shear VC | 0 0 0 0 0 0 0 0

Shear VL | 0 0 0 0 -3 -3 3 3

Shear MT | 0 0 0 0 0 0 0 0

|

Tot. Shear| 0.0 0.0 0.0 0.0 -3.0 -3.0 3.0 3.0

------------------------------------------------------------------------

Str. Int. | 18.38 5.01 18.38 5.01 6.02 6.02 6.02 6.02

------------------------------------------------------------------------

WRC 107 Stress Calculation for OCCasional loads:

Radial Load P 4309.8 N



Circumferential Moment MC -551.9 N-m

Longitudinal Moment ML -729.5 N-m





------------------------------------------------------------------------

| Stress Values at

Type of | (MPa )

---------------|--------------------------------------------------------

69

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:01a Jan 11,2015 Stress Load| Au Al Bu Bl Cu Cl Du Dl

---------------|--------------------------------------------------------

Circ. Memb. P | -2 -2 -2 -2 -1 -1 -1 -1

Circ. Bend. P | -5 5 -5 5 -8 8 -8 8

Circ. Memb. MC | 0 0 0 0 0 0 0 0

Circ. Bend. MC | 0 0 0 0 14 -14 -14 14

Circ. Memb. ML | 2 2 -2 -2 0 0 0 0

Circ. Bend. ML | 5 -5 -5 5 0 0 0 0

|

Tot. Circ. Str.| 1.2 -0.2 -15.6 6.1 5.5 -6.8 -24.1 20.3

------------------------------------------------------------------------

Long. Memb. P | -1 -1 -1 -1 -2 -2 -2 -2

Long. Bend. P | -5 5 -5 5 -3 3 -3 3

Long. Memb. MC | 0 0 0 0 1 1 -1 -1

Long. Bend. MC | 0 0 0 0 4 -4 -4 4

Long. Memb. ML | 1 1 -1 -1 0 0 0 0

Long. Bend. ML | 5 -5 -5 5 0 0 0 0

|

Tot. Long. Str.| 0.1 0.2 -15.0 8.6 0.1 -2.1 -11.6 4.3

------------------------------------------------------------------------

Shear VC | 0 0 0 0 0 0 0 0

Shear VL | 0 0 0 0 0 0 0 0

Shear MT | 0 0 0 0 0 0 0 0

|

Tot. Shear| 0.0 0.0 0.0 0.0 -0.7 -0.7 0.7 0.7

------------------------------------------------------------------------

Str. Int. | 1.15 0.35 15.56 8.57 5.57 6.89 24.15 20.35

------------------------------------------------------------------------




70

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:01a Jan 11,2015 ------------------------------------------------------------------------

| Stress Values at

Type of | (MPa )

---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Circ. Memb. P | -4 -4 -4 -4 -1 -1 -1 -1

Circ. Bend. P | -3 3 -3 3 -25 25 -25 25

Circ. Memb. MC | 0 0 0 0 1 1 -1 -1

Circ. Bend. MC | 0 0 0 0 23 -23 -23 23

Circ. Memb. ML | 2 2 -2 -2 0 0 0 0

Circ. Bend. ML | 2 -2 -2 2 0 0 0 0

|

Tot. Circ. Str.| -3.3 -1.6 -13.3 -1.0 -1.8 0.6 -51.8 45.9

------------------------------------------------------------------------

Long. Memb. P | -1 -1 -1 -1 -4 -4 -4 -4

Long. Bend. P | -5 5 -5 5 -12 12 -12 12

Long. Memb. MC | 0 0 0 0 5 5 -5 -5

Long. Bend. MC | 0 0 0 0 7 -7 -7 7

Long. Memb. ML | 2 2 -2 -2 0 0 0 0

Long. Bend. ML | 3 -3 -3 3 0 0 0 0

|

Tot. Long. Str.| -1.8 2.4 -13.2 5.5 -4.8 5.5 -30.5 10.7

------------------------------------------------------------------------

Shear VC | 0 0 0 0 0 0 0 0

Shear VL | 0 0 0 0 0 0 0 0

Shear MT | 0 0 0 0 0 0 0 0

|

Tot. Shear| 0.0 0.0 0.0 0.0 -0.9 -0.9 0.9 0.9

------------------------------------------------------------------------

Str. Int. | 3.25 3.94 13.25 6.47 5.05 5.69 51.83 45.89

------------------------------------------------------------------------

71

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:01a Jan 11,2015 WRC 107/537 Stress Summations:

Vessel Stress Summation at Attachment Junction

------------------------------------------------------------------------

Type of | Stress Values at

Stress Int. | (MPa )

---------------|--------------------------------------------------------

Location | Au Al Bu Bl Cu Cl Du Dl

---------------|--------------------------------------------------------

Circ. Pm (SUS) | 32 34 32 34 32 34 32 34

Circ. Pm (OCC) | 0 0 0 0 0 0 0 0

Circ. Pm(TOTAL)| 32.5 34.3 32.5 34.3 32.5 34.3 32.5 34.3

Circ. Pl (SUS) | 8 8 -8 -8 0 0 0 0

Circ. Pl (OCC) | 0 0 -4 -4 0 0 -1 -1

Circ. Pl(TOTAL)| 8.9 8.9 -13.2 -13.2 -0.7 -0.7 -1.9 -1.9

Circ. Q (SUS) | 18 -18 -18 18 0 0 0 0

Circ. Q (OCC) | 0 0 -10 10 6 -6 -22 22

Circ. Q (TOTAL)| 19.1 -19.1 -29.2 29.2 6.1 -6.1 -22.2 22.2

------------------------------------------------------------------------

Long. Pm (SUS) | 16 16 16 16 16 16 16 16

Long. Pm (OCC) | 0 0 0 0 0 0 0 0

Long. Pm(TOTAL)| 16.3 16.3 16.3 16.3 16.3 16.3 16.3 16.3

Long. Pl (SUS) | 5 5 -5 -5 0 0 0 0

Long. Pl (OCC) | 0 0 -3 -3 0 0 -3 -3

Long. Pl(TOTAL)| 5.5 5.5 -8.6 -8.6 -1.0 -1.0 -3.7 -3.7

Long. Q (SUS) | 18 -18 -18 18 0 0 0 0

Long. Q (OCC) | 0 0 -11 11 1 -1 -7 7

Long. Q (TOTAL)| 18.8 -18.8 -30.6 30.6 1.1 -1.1 -8.0 8.0

------------------------------------------------------------------------

Shear Pm (SUS) | 0 0 0 0 0 0 0 0

Shear Pm (OCC) | 0 0 0 0 0 0 0 0

Shear Pm(TOTAL)| 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0

Shear Pl (SUS) | 0 0 0 0 -2 -2 2 2

72

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:01a Jan 11,2015 Shear Pl (OCC) | 0 0 0 0 0 0 0 0

Shear Pl(TOTAL)| 0.0 0.0 0.0 0.0 -3.1 -3.1 3.1 3.1

Shear Q (SUS) | 0 0 0 0 0 0 0 0

Shear Q (OCC) | 0 0 0 0 0 0 0 0

Shear Q (TOTAL)| 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0

------------------------------------------------------------------------

Pm (SUS) | 32.5 34.3 32.5 34.3 32.5 34.3 32.5 34.3

------------------------------------------------------------------------

Pm (SUS+OCC) | 32.5 34.3 32.5 34.3 32.5 34.3 32.5 34.3

------------------------------------------------------------------------

Pm+Pl (SUS) | 41.0 42.8 24.1 25.9 32.9 34.6 32.9 34.6

------------------------------------------------------------------------

Pm+Pl (SUS+OCC)| 41.4 43.2 19.4 21.2 32.4 34.2 31.1 32.9

------------------------------------------------------------------------

Pm+Pl+Q (Total)| 60.5 24.2 23.0 50.4 38.4 28.2 10.1 54.9

------------------------------------------------------------------------

------------------------------------------------------------------------

Type of | Max. S.I. S.I. Allowable | Result

Stress Int. | MPa |

---------------|--------------------------------------------------------

Pm (SUS) | 34.34 115.15 | Passed

Pm (SUS+OCC) | 34.34 138.18 | Passed

Pm+Pl (SUS) | 42.75 172.72 | Passed

Pm+Pl (SUS+OCC)| 43.24 207.26 | Passed

Pm+Pl+Q (TOTAL)| 60.51 345.44 | Passed

------------------------------------------------------------------------

WRC 107/537 Stress Summations:

Vessel Stress Summation at Reinforcing Pad Edge

------------------------------------------------------------------------


73

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:01a Jan 11,2015 Stress Int. | (MPa )

---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Circ. Pm (SUS) | 65 67 65 67 65 67 65 67

Circ. Pm (OCC) | 0 0 0 0 0 0 0 0

Circ. Pm(TOTAL)| 65.9 67.7 65.9 67.7 65.9 67.7 65.9 67.7

Circ. Pl (SUS) | 7 7 -7 -7 0 0 0 0

Circ. Pl (OCC) | -2 -2 -7 -7 0 0 -2 -2

Circ. Pl(TOTAL)| 5.1 5.1 -14.7 -14.7 -0.6 -0.6 -3.0 -3.0

Circ. Q (SUS) | 8 -8 -8 8 0 0 0 0

Circ. Q (OCC) | 0 0 -6 6 -1 1 -48 48

Circ. Q (TOTAL)| 7.6 -7.6 -14.6 14.6 -1.2 1.2 -48.8 48.8

------------------------------------------------------------------------

Long. Pm (SUS) | 32 32 32 32 32 32 32 32

Long. Pm (OCC) | 0 0 0 0 0 0 0 0

Long. Pm(TOTAL)| 33.0 33.0 33.0 33.0 33.0 33.0 33.0 33.0

Long. Pl (SUS) | 6 6 -6 -6 0 0 0 0

Long. Pl (OCC) | 0 0 -3 -3 0 0 -9 -9

Long. Pl(TOTAL)| 7.0 7.0 -10.5 -10.5 0.4 0.4 -9.9 -9.9

Long. Q (SUS) | 11 -11 -11 11 0 0 0 0

Long. Q (OCC) | -2 2 -9 9 -5 5 -20 20

Long. Q (TOTAL)| 9.6 -9.6 -21.0 21.0 -5.1 5.1 -20.6 20.6

------------------------------------------------------------------------

Shear Pm (SUS) | 0 0 0 0 0 0 0 0

Shear Pm (OCC) | 0 0 0 0 0 0 0 0

Shear Pm(TOTAL)| 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0

Shear Pl (SUS) | 0 0 0 0 -3 -3 3 3

Shear Pl (OCC) | 0 0 0 0 0 0 0 0

Shear Pl(TOTAL)| 0.0 0.0 0.0 0.0 -3.9 -3.9 3.9 3.9

Shear Q (SUS) | 0 0 0 0 0 0 0 0

Shear Q (OCC) | 0 0 0 0 0 0 0 0

Shear Q (TOTAL)| 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0

74

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:01a Jan 11,2015 ------------------------------------------------------------------------

Pm (SUS) | 65.9 67.7 65.9 67.7 65.9 67.7 65.9 67.7

------------------------------------------------------------------------

Pm (SUS+OCC) | 65.9 67.7 65.9 67.7 65.9 67.7 65.9 67.7

------------------------------------------------------------------------

Pm+Pl (SUS) | 73.5 75.3 58.4 60.2 66.2 68.0 66.2 68.0

------------------------------------------------------------------------

Pm+Pl (SUS+OCC)| 71.1 72.9 51.3 53.1 65.9 67.6 63.4 65.2

------------------------------------------------------------------------

Pm+Pl+Q (Total)| 78.7 65.2 36.7 67.7 64.6 68.9 15.4 113.8

------------------------------------------------------------------------

------------------------------------------------------------------------


Stress Int. | MPa |

---------------|--------------------------------------------------------

Pm (SUS) | 67.75 115.15 | Passed

Pm (SUS+OCC) | 67.75 138.18 | Passed

Pm+Pl (SUS) | 75.30 172.72 | Passed

Pm+Pl (SUS+OCC)| 72.89 207.26 | Passed


------------------------------------------------------------------------


75

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : N3 Nozl: 17 1:01a Jan 11,2015

INPUT VALUES, Nozzle Description: N3 From : 10

Pressure for Reinforcement Calculations P 18.283 bar

Temperature for Internal Pressure Temp 50 °C

Design External Pressure Pext 1.03 bar

Temperature for External Pressure Tempex 50 °C

Shell Material SA-240 316L

Shell Allowable Stress at Temperature S 115.15 MPa

Shell Allowable Stress At Ambient Sa 115.15 MPa

Inside Diameter of Elliptical Head D 600.00 mm

Aspect Ratio of Elliptical Head Ar 2.00

Head Finished (Minimum) Thickness t 5.0000 mm

Head Internal Corrosion Allowance c 0.0000 mm

Head External Corrosion Allowance co 0.0000 mm

Distance from Head Centerline L1 0.0000 mm

User Entered Minimum Design Metal Temperature 0.00 °C

Type of Element Connected to the Shell : Nozzle

Material SA-312 TP316L

Material UNS Number S31603

Material Specification/Type Smls. & wld. pipe

Allowable Stress at Temperature Sn 115.15 MPa

Allowable Stress At Ambient Sna 115.15 MPa

Diameter Basis (for tr calc only) OD

Layout Angle 90.00 deg

Diameter 2.0000 in.

76


Size and Thickness Basis Nominal

Nominal Thickness tn 80S

Flange Material SA-182 F316L

Flange Type Weld Neck Flange

Corrosion Allowance can 0.0000 mm

Joint Efficiency of Shell Seam at Nozzle E1 1.00

Joint Efficiency of Nozzle Neck En 1.00

Outside Projection ho 200.0000 mm

Weld leg size between Nozzle and Pad/Shell Wo 8.0000 mm

Groove weld depth between Nozzle and Vessel Wgnv 5.0000 mm

Pad Material SA-240 316L

Pad Allowable Stress at Temperature Sp 115.15 MPa

Pad Allowable Stress At Ambient Spa 115.15 MPa

Diameter of Pad along vessel surface Dp 170.0000 mm

Thickness of Pad te 8.0000 mm

Weld leg size between Pad and Shell Wp 6.0000 mm

Groove weld depth between Pad and Nozzle Wgpn 8.0000 mm

Reinforcing Pad Width 54.8375 mm

ASME Code Weld Type per UW-16 None

Class of attached Flange 150

Grade of attached Flange GR 2.2

The Pressure Design option was Overall MAWP.

Nozzle Sketch (may not represent actual weld type/configuration)

| |

77

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : N3 Nozl: 17 1:01a Jan 11,2015 | |

| |

| |

| |

__________/|\ |

____/|__________\|_\|

| |

| |

|____________________|

Abutting Nozzle With Pad

Reinforcement CALCULATION, Description: N3

ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45

Actual Outside Diameter Used in Calculation 2.375 in.

Actual Thickness Used in Calculation 0.218 in.

Nozzle input data check completed without errors.

Reqd thk per UG-37(a)of Elliptical Head, Tr [Int. Press]

= (P*K1*D))/(2*S*E-0.2*P) per UG-37(a)(3)

= (18.28*0.900*600.0000)/(2 *115.15*1.00-0.2*18.28)

= 4.2946 mm

Reqd thk per UG-37(a)of Nozzle Wall, Trn [Int. Press]

= (P*Ro)/(S*E+0.4*P) per Appendix 1-1 (a)(1)

= (18.28*30.1625)/(115*1.00+0.4*18.28)

= 0.4760 mm

Required Nozzle thickness under External Pressure per UG-28 : 0.3236 mm

78

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : N3 Nozl: 17 1:01a Jan 11,2015 UG-40, Limits of Reinforcement : [Internal Pressure]

Parallel to Vessel Wall (Diameter Limit) Dl 98.5012 mm

Parallel to Vessel Wall, opening length d 49.2506 mm

Normal to Vessel Wall (Thickness Limit), pad side Tlwp 12.5000 mm

Note : The Pad diameter is greater than the Diameter Limit, the

excess will not be considered .

Note:

Taking a UG-36(c)(3)(a) exemption for nozzle: N3.

This calculation is valid for nozzles that meet all the requirements of

paragraph UG-36. Please check the Code carefully, especially for nozzles

that are not isolated or do not meet Code spacing requirements. To force

the computation of areas for small nozzles go to Tools->Configuration

and check the box to force the UG-37 small nozzle area calculation or

force the Appendix 1-10 computation in Nozzle Design Options.

UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]

Wall Thickness for Internal/External pressures ta = 0.4760 mm

Wall Thickness per UG16(b), tr16b = 1.5000 mm

Wall Thickness, shell/head, internal pressure trb1 = 4.7717 mm

Wall Thickness tb1 = max(trb1, tr16b) = 4.7717 mm

Wall Thickness, shell/head, external pressure trb2 = 0.2695 mm


Wall Thickness per table UG-45 tb3 = 3.4200 mm

Determine Nozzle Thickness candidate [tb]:

= min[ tb3, max( tb1,tb2) ]

= min[ 3.420 , max( 4.772 , 1.500 ) ]

= 3.4200 mm

Minimum Wall Thickness of Nozzle Necks [tUG-45]:

79

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : N3 Nozl: 17 1:01a Jan 11,2015 = max( ta, tb )

= max( 0.4760 , 3.4200 )

= 3.4200 mm

Available Nozzle Neck Thickness = 0.875 * 5.537 = 4.845 mm --> OK

Stresses on Nozzle due to External and Pressure Loads per the ASME

B31.3 Piping Code (see 319.4.4 and 302.3.5):

Sustained : 47.4, Allowable : 115.1 MPa Passed

Expansion : 0.0, Allowable : 240.4 MPa Passed

Occasional : 3.7, Allowable : 153.1 MPa Passed

Shear : 21.4, Allowable : 80.6 MPa Passed

Note : The number of cycles on this nozzle was assumed to be 7000 or less for

the determination of the expansion stress allowable.


SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C

Weld Size Calculations, Description: N3

Intermediate Calc. for nozzle/shell Welds Tmin 5.5372 mm

Intermediate Calc. for pad/shell Welds TminPad 8.0000 mm

Results Per UW-16.1:

Required Thickness Actual Thickness

Nozzle Weld 3.8760 = 0.7 * tmin. 5.6560 = 0.7 * Wo mm

Pad Weld 4.0000 = 0.5*TminPad 4.2420 = 0.7 * Wp mm

NOTE : Skipping the nozzle attachment weld strength calculations.

Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)

(small nozzles) do not require a weld strength check.

80


Maximum Allowable Pressure for this Nozzle at this Location:

Converged Max. Allow. Pressure in Operating case 19.059 bar

Note: The MAWP of this junction was limited by the parent Shell/Head.

The Drop for this Nozzle is : 0.8368 mm

The Cut Length for this Nozzle is, Drop + Ho + H + T : 205.8368 mm

Input Echo, WRC107/537 Item 1, Description: N3 :


Cylindrical or Spherical Vessel Cylsph Spherical


Vessel Diameter Dv 1080.000 mm


Design Temperature -195.57 °C

Vessel Material SA-240 316L

Vessel Cold S.I. Allowable Smc 115.15 MPa

Vessel Hot S.I. Allowable Smh 115.15 MPa

Attachment Type Type Round

WRC107 Attachment Classification Holsol Hollow

Diameter Basis for Nozzle Nbasis OD

Corrosion Allowance for Nozzle Can 0.0000 mm

Nozzle Diameter Dn 60.325 mm

Nozzle Thickness Tn 5.537 mm

Nozzle Material SA-312 TP316L

Nozzle Cold S.I. Allowable SNmc 115.15 MPa

Nozzle Hot S.I. Allowable SNmh 115.15 MPa

81

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : N3 Nozl: 17 1:01a Jan 11,2015 Thickness of Reinforcing Pad Tpad 8.000 mm

Diameter of Reinforcing Pad Dpad 170.000 mm



External Forces and Moments in WRC 107/537 Convention:

Radial Load (SUS) P -1040.0 N

Longitudinal Shear (SUS) (Vl) V1 1040.0 N

Circumferential Shear (SUS) (Vc) V2 1040.0 N

Circumferential Moment (SUS) (Mc) M1 380.0 N-m

Longitudinal Moment (SUS) (Ml) M2 380.0 N-m

Torsional Moment (SUS) Mt 380.0 N-m



Include Pressure Stress Indices per Div. 2 No



Radial Load P -1040.0 N

Circumferential Shear (VC) V2 1040.0 N

Longitudinal Shear (VL) V1 1040.0 N

Circumferential Moment (MC) M1 380.0 N-m

Longitudinal Moment (ML) M2 380.0 N-m


Dimensionless Param: U = 0.36 TAU = 5.00 ( 4.95) RHO = 2.35

Dimensionless Loads for Spherical Shells at Attachment Junction:

------------------------------------------------------------

82

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : N3 Nozl: 17 1:01a Jan 11,2015 Curves read for 1979 Figure Value Location

------------------------------------------------------------

N(x) * T / P SP 3 0.09462 (A,B,C,D)

M(x) / P SP 3 0.05945 (A,B,C,D)

N(x) * T * SQRT(Rm * T ) / MC SM 3 0.24852 (A,B,C,D)

M(x) * SQRT(Rm * T ) / MC SM 3 0.17229 (A,B,C,D)

N(x) * T * SQRT(Rm * T ) / ML SM 3 0.24852 (A,B,C,D)

M(x) * SQRT(Rm * T ) / ML SM 3 0.17229 (A,B,C,D)

N(y) * T / P SP 3 0.24012 (A,B,C,D)

M(y) / P SP 3 0.07626 (A,B,C,D)

N(y) * T * SQRT(Rm * T ) / MC SM 3 0.13148 (A,B,C,D)

M(y) * SQRT(Rm * T ) / MC SM 3 0.31289 (A,B,C,D)

N(y) * T * SQRT(Rm * T ) / ML SM 3 0.13148 (A,B,C,D)

M(y) * SQRT(Rm * T ) / ML SM 3 0.31289 (A,B,C,D)



------------------------------------------------------------------------

| Stress Values at

Type of | (MPa )

---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Rad. Memb. P | 0 0 0 0 0 0 0 0

Rad. Bend. P | 2 -2 2 -2 2 -2 2 -2

Rad. Memb. MC | 0 0 0 0 -6 -6 6 6

Rad. Bend. MC | 0 0 0 0 -27 27 27 -27

Rad. Memb. ML | -6 -6 6 6 0 0 0 0

Rad. Bend. ML | -27 27 27 -27 0 0 0 0

|

Tot. Rad. Str.| -31.4 19.3 37.0 -22.6 -31.4 19.3 37.0 -22.6

83

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : N3 Nozl: 17 1:01a Jan 11,2015 ------------------------------------------------------------------------

Tang. Memb. P | 1 1 1 1 1 1 1 1

Tang. Bend. P | 2 -2 2 -2 2 -2 2 -2

Tang. Memb. MC | 0 0 0 0 -3 -3 3 3

Tang. Bend. MC | 0 0 0 0 -50 50 50 -50

Tang. Memb. ML | -3 -3 3 3 0 0 0 0

Tang. Bend. ML | -50 50 50 -50 0 0 0 0

|

Tot. Tang. Str.| -49.3 45.2 57.9 -47.9 -49.3 45.2 57.9 -47.9

------------------------------------------------------------------------

Shear VC | 0 0 0 0 0 0 0 0

Shear VL | 0 0 0 0 0 0 0 0

Shear MT | 5 5 5 5 5 5 5 5

|

Tot. Shear| 6.0 6.0 4.3 4.3 4.3 4.3 6.0 6.0

------------------------------------------------------------------------

Str. Int. | 51.08 46.52 58.70 48.60 50.24 45.91 59.44 49.23

------------------------------------------------------------------------

Unitless Prm: U = 1.63 TAU = 0.00 ( 14.85) RHO = 0.00 ( 0.90)

Dimensionless Loads for Spherical Shells at Pad edge:

------------------------------------------------------------

Curves read for 1979 Figure Value Location

------------------------------------------------------------

N(x) * T / P SR 2 0.03371 (A,B,C,D)

M(x) / P SR 2 0.01632 (A,B,C,D)

N(x) * T * SQRT(Rm * T ) / MC SR 3 0.03239 (A,B,C,D)

M(x) * SQRT(Rm * T ) / MC SR 3 0.02290 (A,B,C,D)

N(x) * T * SQRT(Rm * T ) / ML SR 3 0.03239 (A,B,C,D)

M(x) * SQRT(Rm * T ) / ML SR 3 0.02290 (A,B,C,D)

N(y) * T / P SR 2 0.01004 (A,B,C,D)

84

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : N3 Nozl: 17 1:01a Jan 11,2015 M(y) / P SR 2 0.00489 (A,B,C,D)

N(y) * T * SQRT(Rm * T ) / MC SR 3 0.00970 (A,B,C,D)

M(y) * SQRT(Rm * T ) / MC SR 3 0.00677 (A,B,C,D)

N(y) * T * SQRT(Rm * T ) / ML SR 3 0.00970 (A,B,C,D)

M(y) * SQRT(Rm * T ) / ML SR 3 0.00677 (A,B,C,D)



------------------------------------------------------------------------

| Stress Values at

Type of | (MPa )

---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Rad. Memb. P | 1 1 1 1 1 1 1 1

Rad. Bend. P | 4 -4 4 -4 4 -4 4 -4

Rad. Memb. MC | 0 0 0 0 -9 -9 9 9

Rad. Bend. MC | 0 0 0 0 -40 40 40 -40

Rad. Memb. ML | -9 -9 9 9 0 0 0 0

Rad. Bend. ML | -40 40 40 -40 0 0 0 0

|

Tot. Rad. Str.| -44.1 28.0 55.0 -33.3 -44.1 28.0 55.0 -33.3

------------------------------------------------------------------------

Tang. Memb. P | 0 0 0 0 0 0 0 0

Tang. Bend. P | 1 -1 1 -1 1 -1 1 -1

Tang. Memb. MC | 0 0 0 0 -2 -2 2 2

Tang. Bend. MC | 0 0 0 0 -11 11 11 -11

Tang. Memb. ML | -2 -2 2 2 0 0 0 0

Tang. Bend. ML | -11 11 11 -11 0 0 0 0

|

Tot. Tang. Str.| -13.0 8.2 16.3 -9.8 -13.0 8.2 16.3 -9.8

------------------------------------------------------------------------

85

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : N3 Nozl: 17 1:01a Jan 11,2015 Shear VC | 0 0 0 0 0 0 0 0

Shear VL | 0 0 0 0 0 0 0 0

Shear MT | 1 1 1 1 1 1 1 1

|

Tot. Shear| 2.5 2.5 0.9 0.9 0.9 0.9 2.5 2.5

------------------------------------------------------------------------

Str. Int. | 44.25 28.26 55.03 33.34 44.08 28.00 55.16 33.56

------------------------------------------------------------------------



------------------------------------------------------------------------



---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Rad. Pm (SUS) | 37 37 37 37 37 37 37 37

Rad. Pl (SUS) | -6 -6 7 7 -6 -6 7 7

Rad. Q (SUS) | -25 25 29 -29 -25 25 29 -29

------------------------------------------------------------------------

Long. Pm (SUS) | 37 37 37 37 37 37 37 37

Long. Pl (SUS) | -2 -2 4 4 -2 -2 4 4

Long. Q (SUS) | -47 47 52 -52 -47 47 52 -52

------------------------------------------------------------------------

Shear Pm (SUS) | 0 0 0 0 0 0 0 0

Shear Pl (SUS) | 0 0 0 0 0 0 0 0

Shear Q (SUS) | 5 5 5 5 5 5 5 5

------------------------------------------------------------------------

Pm (SUS) | 38.0 38.0 38.0 38.0 38.0 38.0 38.0 38.0

------------------------------------------------------------------------

Pm+Pl (SUS) | 36.1 36.1 45.5 45.5 36.1 36.1 45.5 45.5

86


Pm+Pl+Q (Total)| 21.5 84.5 96.7 26.7 19.8 83.9 97.4 28.0

------------------------------------------------------------------------

------------------------------------------------------------------------


Stress Int. | MPa |

---------------|--------------------------------------------------------

Pm (SUS) | 37.99 115.15 | Passed

Pm+Pl (SUS) | 45.49 172.72 | Passed


------------------------------------------------------------------------


Vessel Stress Summation at Reinforcing Pad Edge

------------------------------------------------------------------------



---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Rad. Pm (SUS) | 98 98 98 98 98 98 98 98

Rad. Pl (SUS) | -8 -8 10 10 -8 -8 10 10

Rad. Q (SUS) | -36 36 44 -44 -36 36 44 -44

------------------------------------------------------------------------

Long. Pm (SUS) | 98 98 98 98 98 98 98 98

Long. Pl (SUS) | -2 -2 3 3 -2 -2 3 3

Long. Q (SUS) | -10 10 13 -13 -10 10 13 -13

------------------------------------------------------------------------

Shear Pm (SUS) | 0 0 0 0 0 0 0 0

Shear Pl (SUS) | 0 0 0 0 0 0 0 0

Shear Q (SUS) | 1 1 1 1 1 1 1 1

87


Pm (SUS) | 98.7 98.7 98.7 98.7 98.7 98.7 98.7 98.7

------------------------------------------------------------------------

Pm+Pl (SUS) | 96.4 96.4 109.7 109.7 96.4 96.4 109.7 109.7

------------------------------------------------------------------------

Pm+Pl+Q (Total)| 85.9 127.0 153.8 89.0 85.7 126.8 153.9 89.2

------------------------------------------------------------------------

------------------------------------------------------------------------


Stress Int. | MPa |

---------------|--------------------------------------------------------

Pm (SUS) | 98.75 115.15 | Passed

Pm+Pl (SUS) | 109.68 172.72 | Passed


------------------------------------------------------------------------


88










Inside Diameter of Cylindrical Shell D 594.00 mm

Design Length of Section L 2297.0000 mm

Shell Finished (Minimum) Thickness t 8.0000 mm

Shell Internal Corrosion Allowance c 0.0000 mm

Shell External Corrosion Allowance co 0.0000 mm

Distance from Bottom/Left Tangent 1225.0000 mm



Material SA-182 F316


Material Specification/Type Forgings



Diameter Basis (for tr calc only) ID


Diameter 2.0000 in.

89


Size and Thickness Basis Actual

Actual Thickness tn 16.7640 mm


Flange Type Long Weld Neck







Inside Projection h 0.0000 mm

Weld leg size, Inside Element to Shell Wi 0.0000 mm






| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

90


Insert Nozzle No Pad, no Inside projection



Actual Inside Diameter Used in Calculation 2.000 in.



Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]

= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (18.28*297.0000)/(115*1.00-0.6*18.28)

= 4.7619 mm

Reqd thk per App. 1 of Nozzle Wall, Trn [Int. Press]

= R( exp([P/(SE)] - 1 ) per Appendix 1-2 (a)(1)

= 25.400(exp([18.28/(137.90*1.00]-1)

= 0.3391 mm


UG-40, Limits of Reinforcement : [Internal Pressure]



Normal to Vessel Wall (Thickness Limit), no pad Tlnp 20.0000 mm

Note:



91

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : N1 Nozl: 18 1:01a Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles















= min[ 4.800 , max( 4.762 , 1.500 ) ]

= 4.7619 mm


= max( ta, tb )

= max( 0.3936 , 4.7619 )

= 4.7619 mm

Available Nozzle Neck Thickness = 16.7640 mm --> OK







92























93

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : N1 Nozl: 18 1:01a Jan 11,2015 Vessel Diameter Dv 594.000 mm







Diameter Basis for Nozzle Nbasis ID




Nozzle Material SA-182 F316







Longitudinal Shear (SUS) Vl 1910.0 N

Circumferential Shear (SUS) Vc 1910.0 N

Circumferential Moment (SUS) Mc 440.0 N-m

Longitudinal Moment (SUS) Ml 440.0 N-m




94

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : N1 Nozl: 18 1:01a Jan 11,2015 Include Pressure Stress Indices per Div. 2 No







Longitudinal Moment ML 440.0 N-m




-------------------------------------------------------------------


-------------------------------------------------------------------

N(PHI) / ( P/Rm ) 0.123 4C 6.355 (A,B)

N(PHI) / ( P/Rm ) 0.123 3C 5.191 (C,D)

M(PHI) / ( P ) 0.123 2C1 0.073 (A,B)

M(PHI) / ( P ) 0.123 1C 0.106 (C,D)





N(x) / ( P/Rm ) 0.123 3C 5.191 (A,B)

N(x) / ( P/Rm ) 0.123 4C 6.355 (C,D)

M(x) / ( P ) 0.123 1C1 0.111 (A,B)

M(x) / ( P ) 0.123 2C 0.073 (C,D)




95

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : N1 Nozl: 18 1:01a Jan 11,2015 M(x) / ( ML/(Rm * Beta) ) 0.123 2B 0.064 (A,B,C,D)



------------------------------------------------------------------------

| Stress Values at

Type of | (MPa )

---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Circ. Memb. P | 5 5 5 5 4 4 4 4

Circ. Bend. P | 13 -13 13 -13 18 -18 18 -18

Circ. Memb. MC | 0 0 0 0 -6 -6 6 6

Circ. Bend. MC | 0 0 0 0 -102 102 102 -102

Circ. Memb. ML | -20 -20 20 20 0 0 0 0

Circ. Bend. ML | -46 46 46 -46 0 0 0 0

|

Tot. Circ. Str.| -48.3 17.6 84.6 -33.7 -86.0 81.4 132.2 -111.0

------------------------------------------------------------------------

Long. Memb. P | 4 4 4 4 5 5 5 5

Long. Bend. P | 19 -19 19 -19 13 -13 13 -13

Long. Memb. MC | 0 0 0 0 -9 -9 9 9

Long. Bend. MC | 0 0 0 0 -54 54 54 -54

Long. Memb. ML | -6 -6 6 6 0 0 0 0

Long. Bend. ML | -71 71 71 -71 0 0 0 0

|

Tot. Long. Str.| -53.4 49.4 101.3 -80.8 -46.1 36.7 82.5 -53.0

------------------------------------------------------------------------

Shear VC | 1 1 -1 -1 0 0 0 0

Shear VL | 0 0 0 0 -1 -1 1 1

Shear MT | 4 4 4 4 4 4 4 4

96

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : N1 Nozl: 18 1:01a Jan 11,2015 |

Tot. Shear| 6.7 6.7 3.1 3.1 3.1 3.1 6.7 6.7

------------------------------------------------------------------------

Str. Int. | 58.07 50.79 101.87 81.04 86.26 81.57 133.08 111.82

------------------------------------------------------------------------



------------------------------------------------------------------------



---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Circ. Pm (SUS) | 66 68 66 68 66 68 66 68

Circ. Pl (SUS) | -15 -15 25 25 -2 -2 10 10

Circ. Q (SUS) | -32 32 59 -59 -83 83 121 -121

------------------------------------------------------------------------

Long. Pm (SUS) | 33 33 33 33 33 33 33 33

Long. Pl (SUS) | -2 -2 10 10 -4 -4 14 14

Long. Q (SUS) | -51 51 91 -91 -41 41 67 -67

------------------------------------------------------------------------

Shear Pm (SUS) | 0 0 0 0 0 0 0 0

Shear Pl (SUS) | 1 1 -1 -1 -1 -1 1 1

Shear Q (SUS) | 4 4 4 4 4 4 4 4

------------------------------------------------------------------------

Pm (SUS) | 67.0 68.8 67.0 68.8 67.0 68.8 67.0 68.8

------------------------------------------------------------------------

Pm+Pl (SUS) | 51.8 53.6 92.5 94.3 64.7 66.6 77.7 79.5

------------------------------------------------------------------------

Pm+Pl+Q (Total)| 40.9 91.6 152.1 82.7 20.3 150.3 199.7 44.1

------------------------------------------------------------------------

97


------------------------------------------------------------------------


Stress Int. | MPa |

---------------|--------------------------------------------------------

Pm (SUS) | 68.81 115.15 | Passed

Pm+Pl (SUS) | 94.32 172.72 | Passed


------------------------------------------------------------------------


98

























Diameter 2.0000 in.

99



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

100









= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (18.28*297.0000)/(115*1.00-0.6*18.28)

= 4.7619 mm



= 25.400(exp([18.28/(137.90*1.00]-1)

= 0.3391 mm






Note:



101
















= min[ 4.800 , max( 4.762 , 1.500 ) ]

= 4.7619 mm


= max( ta, tb )

= max( 0.3761 , 4.7619 )

= 4.7619 mm








102























103


























104












-------------------------------------------------------------------


-------------------------------------------------------------------

N(PHI) / ( P/Rm ) 0.113 4C 6.470 (A,B)

N(PHI) / ( P/Rm ) 0.113 3C 5.436 (C,D)

M(PHI) / ( P ) 0.113 2C1 0.080 (A,B)

M(PHI) / ( P ) 0.113 1C 0.113 (C,D)





N(x) / ( P/Rm ) 0.113 3C 5.436 (A,B)

N(x) / ( P/Rm ) 0.113 4C 6.470 (C,D)

M(x) / ( P ) 0.113 1C1 0.118 (A,B)

M(x) / ( P ) 0.113 2C 0.081 (C,D)




105




------------------------------------------------------------------------

| Stress Values at

Type of | (MPa )

---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Circ. Memb. P | 2 2 2 2 2 2 2 2

Circ. Bend. P | 7 -7 7 -7 10 -10 10 -10

Circ. Memb. MC | 0 0 0 0 -5 -5 5 5

Circ. Bend. MC | 0 0 0 0 -98 98 98 -98

Circ. Memb. ML | -18 -18 18 18 0 0 0 0

Circ. Bend. ML | -45 45 45 -45 0 0 0 0

|

Tot. Circ. Str.| -53.2 21.7 74.4 -31.7 -90.6 84.0 117.3 -101.3

------------------------------------------------------------------------

Long. Memb. P | 2 2 2 2 2 2 2 2

Long. Bend. P | 11 -11 11 -11 7 -7 7 -7

Long. Memb. MC | 0 0 0 0 -8 -8 8 8

Long. Bend. MC | 0 0 0 0 -52 52 52 -52

Long. Memb. ML | -5 -5 5 5 0 0 0 0

Long. Bend. ML | -70 70 70 -70 0 0 0 0

|

Tot. Long. Str.| -62.5 56.4 90.3 -74.8 -50.6 39.2 71.9 -49.4

------------------------------------------------------------------------

Shear VC | 1 1 -1 -1 0 0 0 0

Shear VL | 0 0 0 0 -1 -1 1 1

Shear MT | 5 5 5 5 5 5 5 5

106


Tot. Shear| 6.1 6.1 3.9 3.9 3.9 3.9 6.1 6.1

------------------------------------------------------------------------

Str. Int. | 65.47 57.39 91.18 75.12 91.02 84.37 118.10 102.00

------------------------------------------------------------------------



------------------------------------------------------------------------



---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Circ. Pm (SUS) | 66 68 66 68 66 68 66 68

Circ. Pl (SUS) | -15 -15 21 21 -3 -3 8 8

Circ. Q (SUS) | -37 37 53 -53 -87 87 109 -109

------------------------------------------------------------------------

Long. Pm (SUS) | 33 33 33 33 33 33 33 33

Long. Pl (SUS) | -3 -3 7 7 -5 -5 11 11

Long. Q (SUS) | -59 59 82 -82 -44 44 60 -60

------------------------------------------------------------------------

Shear Pm (SUS) | 0 0 0 0 0 0 0 0

Shear Pl (SUS) | 1 1 -1 -1 -1 -1 1 1

Shear Q (SUS) | 5 5 5 5 5 5 5 5

------------------------------------------------------------------------

Pm (SUS) | 67.0 68.8 67.0 68.8 67.0 68.8 67.0 68.8

------------------------------------------------------------------------

Pm+Pl (SUS) | 51.3 53.1 88.4 90.2 63.7 65.5 75.0 76.9

------------------------------------------------------------------------

Pm+Pl+Q (Total)| 44.5 96.2 142.2 78.8 25.5 153.0 184.8 34.5

------------------------------------------------------------------------

107


------------------------------------------------------------------------


Stress Int. | MPa |

---------------|--------------------------------------------------------

Pm (SUS) | 68.81 115.15 | Passed

Pm+Pl (SUS) | 90.18 172.72 | Passed


------------------------------------------------------------------------


108

























Diameter 2.0000 in.

109



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

110









= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (18.28*297.0000)/(115*1.00-0.6*18.28)

= 4.7619 mm



= 25.400(exp([18.28/(137.90*1.00]-1)

= 0.3391 mm






Note:



111
















= min[ 4.800 , max( 4.762 , 1.500 ) ]

= 4.7619 mm


= max( ta, tb )

= max( 0.3761 , 4.7619 )

= 4.7619 mm








112























113


























114












-------------------------------------------------------------------


-------------------------------------------------------------------

N(PHI) / ( P/Rm ) 0.113 4C 6.470 (A,B)

N(PHI) / ( P/Rm ) 0.113 3C 5.436 (C,D)

M(PHI) / ( P ) 0.113 2C1 0.080 (A,B)

M(PHI) / ( P ) 0.113 1C 0.113 (C,D)





N(x) / ( P/Rm ) 0.113 3C 5.436 (A,B)

N(x) / ( P/Rm ) 0.113 4C 6.470 (C,D)

M(x) / ( P ) 0.113 1C1 0.118 (A,B)

M(x) / ( P ) 0.113 2C 0.081 (C,D)




115




------------------------------------------------------------------------

| Stress Values at

Type of | (MPa )

---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Circ. Memb. P | 2 2 2 2 2 2 2 2

Circ. Bend. P | 7 -7 7 -7 10 -10 10 -10

Circ. Memb. MC | 0 0 0 0 -5 -5 5 5

Circ. Bend. MC | 0 0 0 0 -98 98 98 -98

Circ. Memb. ML | -18 -18 18 18 0 0 0 0

Circ. Bend. ML | -45 45 45 -45 0 0 0 0

|

Tot. Circ. Str.| -53.2 21.7 74.4 -31.7 -90.6 84.0 117.3 -101.3

------------------------------------------------------------------------

Long. Memb. P | 2 2 2 2 2 2 2 2

Long. Bend. P | 11 -11 11 -11 7 -7 7 -7

Long. Memb. MC | 0 0 0 0 -8 -8 8 8

Long. Bend. MC | 0 0 0 0 -52 52 52 -52

Long. Memb. ML | -5 -5 5 5 0 0 0 0

Long. Bend. ML | -70 70 70 -70 0 0 0 0

|

Tot. Long. Str.| -62.5 56.4 90.3 -74.8 -50.6 39.2 71.9 -49.4

------------------------------------------------------------------------

Shear VC | 1 1 -1 -1 0 0 0 0

Shear VL | 0 0 0 0 -1 -1 1 1

Shear MT | 5 5 5 5 5 5 5 5

116


Tot. Shear| 6.1 6.1 3.9 3.9 3.9 3.9 6.1 6.1

------------------------------------------------------------------------

Str. Int. | 65.47 57.39 91.18 75.12 91.02 84.37 118.10 102.00

------------------------------------------------------------------------



------------------------------------------------------------------------



---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Circ. Pm (SUS) | 66 68 66 68 66 68 66 68

Circ. Pl (SUS) | -15 -15 21 21 -3 -3 8 8

Circ. Q (SUS) | -37 37 53 -53 -87 87 109 -109

------------------------------------------------------------------------

Long. Pm (SUS) | 33 33 33 33 33 33 33 33

Long. Pl (SUS) | -3 -3 7 7 -5 -5 11 11

Long. Q (SUS) | -59 59 82 -82 -44 44 60 -60

------------------------------------------------------------------------

Shear Pm (SUS) | 0 0 0 0 0 0 0 0

Shear Pl (SUS) | 1 1 -1 -1 -1 -1 1 1

Shear Q (SUS) | 5 5 5 5 5 5 5 5

------------------------------------------------------------------------

Pm (SUS) | 67.0 68.8 67.0 68.8 67.0 68.8 67.0 68.8

------------------------------------------------------------------------

Pm+Pl (SUS) | 51.3 53.1 88.4 90.2 63.7 65.5 75.0 76.9

------------------------------------------------------------------------

Pm+Pl+Q (Total)| 44.5 96.2 142.2 78.8 25.5 153.0 184.8 34.5

------------------------------------------------------------------------

117


------------------------------------------------------------------------


Stress Int. | MPa |

---------------|--------------------------------------------------------

Pm (SUS) | 68.81 115.15 | Passed

Pm+Pl (SUS) | 90.18 172.72 | Passed


------------------------------------------------------------------------


118

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : K1 Nozl: 21 1:01a Jan 11,2015

INPUT VALUES, Nozzle Description: K1 From : 20























Diameter 2.0000 in.

119



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

120



Reinforcement CALCULATION, Description: K1






= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (18.28*297.0000)/(115*1.00-0.6*18.28)

= 4.7619 mm



= 25.400(exp([18.28/(137.90*1.00]-1)

= 0.3391 mm






Note:

Taking a UG-36(c)(3)(a) exemption for nozzle: K1.


121

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : K1 Nozl: 21 1:01a Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles















= min[ 4.800 , max( 4.762 , 1.500 ) ]

= 4.7619 mm


= max( ta, tb )

= max( 0.3761 , 4.7619 )

= 4.7619 mm




Weld Size Calculations, Description: K1

122

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : K1 Nozl: 21 1:01a Jan 11,2015 Intermediate Calc. for nozzle/shell Welds Tmin 8.0000 mm













123

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : K2A Nozl: 22 1:01a Jan 11,2015

INPUT VALUES, Nozzle Description: K2A From : 20























Diameter 3.0000 in.

124



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

125



Reinforcement CALCULATION, Description: K2A






= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (18.28*297.0000)/(115*1.00-0.6*18.28)

= 4.7619 mm



= (18.28*44.4500)/(115*1.00+0.4*18.28)

= 0.7014 mm






Note:

Taking a UG-36(c)(3)(a) exemption for nozzle: K2A.


126

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : K2A Nozl: 22 1:01a Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles















= min[ 4.800 , max( 4.762 , 1.500 ) ]

= 4.7619 mm


= max( ta, tb )

= max( 0.7014 , 4.7619 )

= 4.7619 mm




Weld Size Calculations, Description: K2A

127

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : K2A Nozl: 22 1:01a Jan 11,2015 Intermediate Calc. for nozzle/shell Welds Tmin 7.6200 mm













128

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : K2B Nozl: 23 1:01a Jan 11,2015

INPUT VALUES, Nozzle Description: K2B From : 20























Diameter 3.0000 in.

129



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

130



Reinforcement CALCULATION, Description: K2B






= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (18.28*297.0000)/(115*1.00-0.6*18.28)

= 4.7619 mm



= (18.28*44.4500)/(115*1.00+0.4*18.28)

= 0.7014 mm






Note:

Taking a UG-36(c)(3)(a) exemption for nozzle: K2B.


131

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : K2B Nozl: 23 1:01a Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles















= min[ 4.800 , max( 4.762 , 1.500 ) ]

= 4.7619 mm


= max( ta, tb )

= max( 0.7014 , 4.7619 )

= 4.7619 mm




Weld Size Calculations, Description: K2B

132

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : K2B Nozl: 23 1:01a Jan 11,2015 Intermediate Calc. for nozzle/shell Welds Tmin 7.6200 mm













133

























Diameter 3.0000 in.

134



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

135









= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (18.28*297.0000)/(115*1.00-0.6*18.28)

= 4.7619 mm



= (18.28*44.4500)/(115*1.00+0.4*18.28)

= 0.7014 mm






Note:



136
















= min[ 4.800 , max( 4.762 , 1.500 ) ]

= 4.7619 mm


= max( ta, tb )

= max( 0.7014 , 4.7619 )

= 4.7619 mm





137














138

























Diameter 3.0000 in.

139



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

140









= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (18.28*297.0000)/(115*1.00-0.6*18.28)

= 4.7619 mm



= (18.28*44.4500)/(115*1.00+0.4*18.28)

= 0.7014 mm






Note:



141
















= min[ 4.800 , max( 4.762 , 1.500 ) ]

= 4.7619 mm


= max( ta, tb )

= max( 0.7014 , 4.7619 )

= 4.7619 mm





142














143

























Diameter 2.0000 in.

144



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

145









= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (18.28*297.0000)/(115*1.00-0.6*18.28)

= 4.7619 mm



= 25.400(exp([18.28/(137.90*1.00]-1)

= 0.3391 mm






Note:



146
















= min[ 4.800 , max( 4.762 , 1.500 ) ]

= 4.7619 mm


= max( ta, tb )

= max( 0.3761 , 4.7619 )

= 4.7619 mm





147














148

























Diameter 2.0000 in.

149



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

150









= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (18.28*297.0000)/(115*1.00-0.6*18.28)

= 4.7619 mm



= 25.400(exp([18.28/(137.90*1.00]-1)

= 0.3391 mm






Note:



151
















= min[ 4.800 , max( 4.762 , 1.500 ) ]

= 4.7619 mm


= max( ta, tb )

= max( 0.3761 , 4.7619 )

= 4.7619 mm





152














153

























Diameter 3.0000 in.

154



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

155









= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (18.28*297.0000)/(115*1.00-0.6*18.28)

= 4.7619 mm



= (18.28*44.4500)/(115*1.00+0.4*18.28)

= 0.7014 mm






Note:



156
















= min[ 4.800 , max( 4.762 , 1.500 ) ]

= 4.7619 mm


= max( ta, tb )

= max( 0.7014 , 4.7619 )

= 4.7619 mm





157














158

























Diameter 3.0000 in.

159



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

160









= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (18.28*297.0000)/(115*1.00-0.6*18.28)

= 4.7619 mm



= (18.28*44.4500)/(115*1.00+0.4*18.28)

= 0.7014 mm






Note:



161
















= min[ 4.800 , max( 4.762 , 1.500 ) ]

= 4.7619 mm


= max( ta, tb )

= max( 0.7014 , 4.7619 )

= 4.7619 mm





162














163

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : HH Nozl: 30 1:01a Jan 11,2015

INPUT VALUES, Nozzle Description: HH From : 20























Diameter 4.0000 in.

164



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

165



Reinforcement CALCULATION, Description: HH






= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (18.28*297.0000)/(115*1.00-0.6*18.28)

= 4.7619 mm



= (18.28*57.1500)/(115*1.00+0.4*18.28)

= 0.9018 mm






Weld Strength Reduction Factor [fr1]:

= min( 1, Sn/S )

= min( 1, 115.1/115.1 )

= 1.000

166



= min( 1, Sn/S )

= min( 1, 115.1/115.1 )

= 1.000


= min( fr2, fr4 )

= min( 1.0 , 1.0 )

= 1.000

Results of Nozzle Reinforcement Area Calculations:

AREA AVAILABLE, A1 to A5 MAWP External Mapnc

Area Required Ar 462.763 167.548 NA mm²

Area in Shell A1 314.680 442.346 NA mm²

Area in Nozzle Wall A2 306.318 323.576 NA mm²

Area in Inward Nozzle A3 0.000 0.000 NA mm²

Area in Welds A41+A42+A43 64.000 64.000 NA mm²

Area in Element A5 0.000 0.000 NA mm²

TOTAL AREA AVAILABLE Atot 684.999 829.923 NA mm²

The MAWP Case Governs the Analysis.

Nozzle Angle Used in Area Calculations 90.00 Degs.

The area available without a pad is Sufficient.

Area Required [A]:

= ( d * tr*F + 2 * tn * tr*F * (1-fr1) ) UG-37(c)

= (97.1804*4.7619*1.0+2*8.5598*4.7619*1.0*(1-1.00))

= 462.763 mm²

Reinforcement Areas per Figure UG-37.1

167


Area Available in Shell [A1]:

= d( E1*t - F*tr ) - 2 * tn( E1*t - F*tr ) * ( 1 - fr1 )

= 97.180 ( 1.00 * 8.0000 - 1.0 * 4.762 ) - 2 * 8.560

( 1.00 * 8.0000 - 1.0 * 4.7619 ) * ( 1 - 1.000 )

= 314.680 mm²

Area Available in Nozzle Projecting Outward [A2]:

= ( 2 * tlnp ) * ( tn - trn ) * fr2

= ( 2 * 20.00 ) * ( 8.56 - 0.90 ) * 1.0000

= 306.318 mm²

Area Available in Inward Weld + Outward Weld [A41 + A43]:

= Wo² * fr2 + ( Wi-can/0.707 )² * fr2

= 8.0000² * 1.0000 + ( 0.0000 )² * 1.0000

= 64.000 mm²











= min[ 5.258 , max( 4.762 , 1.500 ) ]

= 4.7619 mm


= max( ta, tb )

168

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : HH Nozl: 30 1:01a Jan 11,2015 = max( 0.9018 , 4.7619 )

= 4.7619 mm




Weld Size Calculations, Description: HH





Weld Strength and Weld Loads per UG-41.1, Sketch (a) or (b)

Weld Load [W]:

= (A-A1+2*tn*fr1*(E1*t-tr))*Sv

= (462.7628 - 314.6804 + 2 * 8.5598 * 1.0000 *

(1.00 * 8.0000 - 4.7619 ) ) * 115

= 23432.33 N

Note: F is always set to 1.0 throughout the calculation.

Weld Load [W1]:

= (A2+A5+A4-(Wi-Can/.707)²*fr2)*Sv

= ( 306.3182 + 0.0000 + 64.0000 - 0.0000 * 1.00 ) * 115

= 42637.22 N

Weld Load [W2]:

= (A2 + A3 + A4 + (2 * tn * t * fr1)) * Sv

169

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : HH Nozl: 30 1:01a Jan 11,2015 = ( 306.3182 + 0.0000 + 64.0000 + ( 136.9568 ) ) * 115

= 58405.98 N

Weld Load [W3]:

= (A2+A3+A4+A5+(2*tn*t*fr1))*S

= ( 306.3182 + 0.0000 + 64.0000 + 0.0000 + ( 136.9568 ) ) * 115

= 58405.98 N

Strength of Connection Elements for Failure Path Analysis

Shear, Outward Nozzle Weld [Sonw]:

= (pi/2) * Dlo * Wo * 0.49 * Snw

= ( 3.1416/2.0 ) * 114.3000 * 8.0000 * 0.49 * 115

= 81034. N

Shear, Nozzle Wall [Snw]:

= (pi *( Dlr + Dlo )/4 ) * ( Thk - Can ) * 0.7 * Sn

= (3.1416 * 52.8701 ) * ( 8.5598 - 0.0000 ) * 0.7 * 115

= 114587. N

Tension, Shell Groove Weld [Tngw]:

= (pi/2) * Dlo * (Wgnvi-Cas) * 0.74 * Sng

= ( 3.1416/2.0 ) * 114.3000 * ( 8.0000 - 0.0000 ) * 0.74 * 115

= 122378. N

Strength of Failure Paths:

PATH11 = ( SONW + SNW ) = ( 81033 + 114587 ) = 195620 N

PATH22 = ( Sonw + Tpgw + Tngw + Sinw )

= ( 81033 + 0 + 122377 + 0 ) = 203411 N

PATH33 = ( Sonw + Tngw + Sinw )

= ( 81033 + 122377 + 0 ) = 203411 N

170

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : HH Nozl: 30 1:01a Jan 11,2015 Summary of Failure Path Calculations:

Path 1-1 = 195620 N , must exceed W = 23432 N or W1 = 42637 N





Nozzle is O.K. for the External Pressure 1.034 bar




171







Shell Material SA-182 F316



Outside Diameter of Bolted Blind Flange D 812.80 mm














Diameter 2.0000 in.

172

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : N2 Nozl: 31 1:01a Jan 11,2015 Size and Thickness Basis Actual

















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

173

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : N2 Nozl: 31 1:01a Jan 11,2015 Insert Nozzle No Pad, no Inside projection








= 25.400(exp([18.28/(137.90*1.00]-1)

= 0.3391 mm




Parallel to Vessel Wall Rn+tn+t 106.8620 mm


Note:








174

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : N2 Nozl: 31 1:01a Jan 11,2015 UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]










= min[ 4.800 , max( 67.850 , 1.500 ) ]

= 4.8000 mm


= max( ta, tb )

= max( 0.3761 , 4.8000 )

= 4.8000 mm







Nozzle Weld 6.0000 = Min per Code 6.3630 = 0.7 * Wo mm



175

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : N2 Nozl: 31 1:01a Jan 11,2015 (small nozzles) do not require a weld strength check.






176







Shell Material SA-182 F316



Outside Diameter of Bolted Blind Flange D 812.80 mm














Diameter 2.0000 in.

177

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : N4 Nozl: 32 1:01a Jan 11,2015 Size and Thickness Basis Actual

















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

178

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : N4 Nozl: 32 1:01a Jan 11,2015 Insert Nozzle No Pad, no Inside projection








= 25.400(exp([18.28/(137.90*1.00]-1)

= 0.3391 mm




Parallel to Vessel Wall Rn+tn+t 106.8620 mm


Note:








179

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : N4 Nozl: 32 1:01a Jan 11,2015 UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]










= min[ 4.800 , max( 67.850 , 1.500 ) ]

= 4.8000 mm


= max( ta, tb )

= max( 0.3548 , 4.8000 )

= 4.8000 mm







Nozzle Weld 6.0000 = Min per Code 6.3630 = 0.7 * Wo mm



180

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Calcs. : N4 Nozl: 32 1:01a Jan 11,2015 (small nozzles) do not require a weld strength check.






181

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Schedule : Step: 50 1:01a Jan 11,2015

Nozzle Schedule:

Nominal Flange Noz. Wall Re-Pad Cut

Description Size Sch/Type O/Dia Thk ODia Thick Length

in. Cls in. mm mm mm mm

------------------------------------------------------------------------------

N3 2.000 80S WNF 2.375 5.537 170.00 8.000 205.84

N1 2.000 600 LWN 3.320 16.764 - - 211.01

N5 2.000 150 LWN 3.060 13.462 - - 210.55

N6 2.000 150 LWN 3.060 13.462 - - 210.55

K1 2.000 150 LWN 3.060 13.462 - - 210.55

K4A 2.000 150 LWN 3.060 13.462 - - 210.55

K4B 2.000 150 LWN 3.060 13.462 - - 210.55

N2 2.000 150 LWN 3.060 13.462 - - 268.05

N4 2.000 150 LWN 3.060 13.462 - - 243.05

K2A 3.000 80S WNF 3.500 7.620 - - 211.35

K2B 3.000 80S WNF 3.500 7.620 - - 211.35

K3A 3.000 80S WNF 3.500 7.620 - - 211.35

K3B 3.000 80S WNF 3.500 7.620 - - 211.35

K5A 3.000 80S WNF 3.500 7.620 - - 211.35

K5B 3.000 80S WNF 3.500 7.620 - - 211.35

HH 4.000 80S WNF 4.500 8.560 - - 213.55

General Notes for the above table:

The Cut Length is the Outside Projection + Inside Projection + Drop +

In Plane Shell Thickness. This value does not include weld gaps,

nor does it account for shrinkage.

In the case of Oblique Nozzles, the Outside Diameter must

be increased. The Re-Pad WIDTH around the nozzle is calculated as follows:

Width of Pad = (Pad Outside Dia. (per above) - Nozzle Outside Dia.)/2

182

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Schedule : Step: 50 1:01a Jan 11,2015

For hub nozzles, the thickness and diameter shown are those of the smaller

and thinner section.

Nozzle Material and Weld Fillet Leg Size Details:

Shl Grve Noz Shl/Pad Pad OD Pad Grve Inside

Nozzle Material Weld Weld Weld Weld Weld

mm mm mm mm mm

------------------------------------------------------------------------------

N3 SA-312 TP316L 5.000 8.000 6.000 8.000 -

N1 SA-182 F316 8.000 8.000 - - -

N5 SA-182 F316 8.000 8.000 - - -

N6 SA-182 F316 8.000 8.000 - - -

K1 SA-182 F316 8.000 8.000 - - -

K4A SA-182 F316 8.000 8.000 - - -

K4B SA-182 F316 8.000 8.000 - - -

N2 SA-182 F316 47.752 9.000 - - -

N4 SA-182 F316 47.752 9.000 - - -

K2A SA-312 TP316L 8.000 8.000 - - -

K2B SA-312 TP316L 8.000 8.000 - - -

K3A SA-312 TP316L 8.000 8.000 - - -

K3B SA-312 TP316L 8.000 8.000 - - -

K5A SA-312 TP316L 8.000 8.000 - - -

K5B SA-312 TP316L 8.000 8.000 - - -

HH SA-312 TP316L 8.000 8.000 - - -

Note: The Outside projections below do not include the flange thickness.

Nozzle Miscellaneous Data:

Elevation/Distance Layout Projection Installed In

Nozzle From Datum Angle Outside Inside Component

mm deg. mm mm

183

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Schedule : Step: 50 1:01a Jan 11,2015 ----------------------------------------------------------------------------

N3 90.00 200.00 0.00 Head

N1 1225.000 270.00 200.00 0.00 Shell

N5 1850.000 270.00 200.00 0.00 Shell

N6 200.000 90.00 200.00 0.00 Shell

K1 1850.000 315.00 200.00 0.00 Shell

K4A 1040.000 315.00 200.00 0.00 Shell

K4B 200.000 315.00 200.00 0.00 Shell

N2 180.00 200.00 0.00 Blind

N4 0.00 175.00 0.00 Blind

K2A 1000.000 0.00 200.00 0.00 Shell

K2B 200.000 0.00 200.00 0.00 Shell

K3A 750.000 135.00 200.00 0.00 Shell

K3B 200.000 135.00 200.00 0.00 Shell

K5A 1000.000 30.00 200.00 0.00 Shell

K5B 550.000 30.00 200.00 0.00 Shell

HH 200.000 250.00 200.00 0.00 Shell


184

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Summary : Step: 51 1:01a Jan 11,2015

Nozzle Calculation Summary:

Description MAWP Ext MAPNC UG45 [tr] Weld Areas or

bar bar Path Stresses

---------------------------------------------------------------------------

N3 19.06 ... ... OK 13.46 OK NoCalc[*]

N1 30.44 ... ... OK 13.46 OK NoCalc[*]

N5 30.44 ... ... OK 13.46 OK NoCalc[*]

N6 30.44 ... ... OK 13.46 OK NoCalc[*]

K1 30.44 ... ... OK 13.46 OK NoCalc[*]

K2A 30.44 ... ... OK 13.46 OK NoCalc[*]

K2B 30.44 ... ... OK 13.46 OK NoCalc[*]

K3A 30.44 ... ... OK 13.46 OK NoCalc[*]

K3B 30.44 ... ... OK 13.46 OK NoCalc[*]

K4A 30.44 ... ... OK 13.46 OK NoCalc[*]

K4B 30.44 ... ... OK 13.46 OK NoCalc[*]

K5A 30.44 ... ... OK 13.46 OK NoCalc[*]

K5B 30.44 ... ... OK 13.46 OK NoCalc[*]

HH 22.46 OK ... OK 13.46 OK Passed

N2 18.36 ... ... OK 13.46 OK NoCalc[*]

N4 18.36 ... ... OK 13.46 OK NoCalc[*]

---------------------------------------------------------------------------

Min. - Nozzles 18.36 N4

Min. Shell&Flgs 18.28

Computed Vessel M.A.W.P. 18.28 bar

[*] - This was a small opening and the areas were not computed or

the MAWP of this connection could not be computed because

the longitudinal bending stress was greater than the hoop stress.

Check the Spatial Relationship between the Nozzles

185

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Summary : Step: 51 1:01a Jan 11,2015

From Node Nozzle Description Y Coordinate, Layout Angle, Dia. Limit

10 N3 0.000 90.000 98.501

20 N1 1225.000 270.000 101.600

20 N5 1850.000 270.000 101.600

20 N6 200.000 90.000 101.600

20 K1 1850.000 315.000 101.600

20 K2A 1000.000 0.000 147.320

20 K2B 200.000 0.000 147.320

20 K3A 750.000 135.000 147.320

20 K3B 200.000 135.000 147.320

20 K4A 1040.000 315.000 101.600

20 K4B 200.000 315.000 101.600

20 K5A 1000.000 30.000 147.320

20 K5B 550.000 30.000 147.320

20 HH 200.000 250.000 194.361

40 N2 0.000 180.000 213.724

40 N4 0.000 0.000 213.724

The nozzle spacing is computed by the following:

= Sqrt( ll² + lc² ) where

ll - Arc length along the inside vessel surface in the long. direction.

lc - Arc length along the inside vessel surface in the circ. direction

If any interferences/violations are found, they will be noted below.

No interference violations have been detected !

Checking Multiple Nozzles on Flat Head per ASME Sec. VIII Div. 1 UG-39

Comparing Nozzles on Element: Blind

186

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Nozzle Summary : Step: 51 1:01a Jan 11,2015 UG-39 Average Nozzle Diameter and Ligament Checks :

Nozzle | Avg. | Head Dia.| Ligament | Min. dn |

Pair Description | dia. | /4 | Width | /4 |

| mm | mm | mm | mm |

-----------------------------------------------------------------

N2 & N4 | 50.800 | 171.45 | 332.28 | 12.700 |

UG-39 Nozzle Spacing and Average Area Checks :

Nozzle | Center | Avg. dia.| Avg. Area | Avg. Area |

Pair Description | Spacing | * 1.25 | Available | Reqd. |

| mm | mm | mm² | mm² |

-------------------------------------------------------------------

N2 & N4 | 410.00 | 63.500 | No Calc | No Calc |

UG-39 Nozzle Diameter and Distance to Edge Checks :

Nozzle | Nozzle | Head Dia. | Distance | Nozzle |

Description | dia. | /2 | from Edge | dia./4 |

| mm | mm | mm | mm |

-------------------------------------------------------------------

N2 | 50.800 | 342.90 | 162.54 | 12.700 |

N4 | 50.800 | 342.90 | 162.54 | 12.700 |

No Multiple Nozzle spacing violations have been detected !


187

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- MDMT Summary : Step: 52 1:01a Jan 11,2015

Minimum Design Metal Temperature Results Summary :

Curve Basic Reduced UG-20(f) Thickness Gov E*

Description MDMT MDMT MDMT ratio Thk

Notes °C °C °C mm

----------------------------------------------------------------------------

Blind [11] -196

Head [16] -196

Shell [16] -196

N3 [15] -196

N1 [15] -196

N5 [15] -196

N6 [15] -196

K1 [15] -196

K2A [15] -196

K2B [15] -196

K3A [15] -196

K3B [15] -196

K4A [15] -196

K4B [15] -196

K5A [15] -196

K5B [15] -196

HH [15] -196

N2 [15] -196

N4 [15] -196

----------------------------------------------------------------------------

Required Minimum Design Metal Temperature 0 °C

Warmest Computed Minimum Design Metal Temperature -196 °C

Notes:

[ ! ] - This was an impact tested material.

[ 1] - Governing Nozzle Weld.

188

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- MDMT Summary : Step: 52 1:01a Jan 11,2015 [ 4] - ANSI Flange MDMT Calcs; Thickness ratio per UCS-66(b)(1)(c).

[ 5] - ANSI Flange MDMT Calcs; Thickness ratio per UCS-66(b)(1)(b).

[ 6] - MDMT Calculations at the Shell/Head Joint.

[ 7] - MDMT Calculations for the Straight Flange.

[ 8] - Cylinder/Cone/Flange Junction MDMT.

[ 9] - Calculations in the Spherical Portion of the Head.

[10] - Calculations in the Knuckle Portion of the Head.

[11] - Calculated (Body Flange) Flange MDMT.

[12] - Calculated Flat Head MDMT per UCS-66.3

[13] - Tubesheet MDMT, shell side, if applicable

[14] - Tubesheet MDMT, tube side, if applicable

[15] - Nozzle Material

[16] - Shell or Head Material

UG-84(b)(2) was not considered.

UCS-66(g) was not considered.

UCS-66(i) was not considered.

Notes:

Impact test temps were not entered in and not considered in the analysis.

UCS-66(i) applies to impact tested materials not by specification and

UCS-66(g) applies to materials impact tested per UG-84.1 General Note (c).

The Basic MDMT includes the (30F) PWHT credit if applicable.


189

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Vessel Design Summary : Step: 53 1:01a Jan 11,2015 Design Code: ASME Code Section VIII Division 1, 2010, 2011a

Diameter Spec : 610.000 mm OD

Vessel Design Length, Tangent to Tangent 2467.40 mm

Distance of Bottom Tangent above Grade 0.00 mm

Specified Datum Line Distance 0.00 mm


Lug Material SA-240 316L

Nozzle Material SA-312 TP316L


Re-Pad Material SA-240 316L

Internal Design Temperature 50 °C

Internal Design Pressure 18.000 bar

External Design Temperature 50 °C

External Design Pressure 1.034 bar

Maximum Allowable Working Pressure 18.283 bar

External Max. Allowable Working Pressure 5.930 bar

Hydrostatic Test Pressure 23.754 bar

Required Minimum Design Metal Temperature 0 °C

Warmest Computed Minimum Design Metal Temperature -196 °C

Wind Design Code User Defined

Earthquake Design Code G-Loading

Element Pressures and MAWP: bar

Element Desc | Design Pres. | External | M.A.W.P | Corrosion

190

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Vessel Design Summary : Step: 53 1:01a Jan 11,2015 | + Stat. head | Pressure | | Allowance

---------------------------------------------------------------------

Head 18.097 1.034 19.059 0.0000

Shell 18.080 1.034 30.438 0.0000

Body Flange 18.000 1.034 18.398 0.0000

Blind 18.000 1.034 18.364 0.0000

Liquid Level: 1088.00 mm Dens.: 910.000 kg/m³ Sp. Gr.: 0.910

Element "To" Elev Length Element Thk R e q d T h k Joint Eff

Type mm mm mm Int. Ext. Long Circ

-----------------------------------------------------------------------

Ellipse 38.0 38.0 8.0 4.7 1.6 1.00 1.00

Cylinder 2247.0 2209.0 8.0 4.8 3.4 1.00 1.00

Body Flg 2399.4 152.4 47.8 No Calc No Calc 1.00 1.00

Body Flg 2467.4 68.0 68.0 67.3 37.7 1.00 1.00

Element thicknesses are shown as Nominal if specified, otherwise are Minimum

Total Wind Shear on Support 1432. N

Total Earthquake Shear on Support 8620. N

Wind Moment on Support 895. N-m

Earthquake Moment on Support 2468. N-m

Note: Wind and Earthquake moments include the effects of user defined

forces and moments if any exist in the job and were specified

to act (compute loads and stresses) during these cases. Also

included are moment effects due to eccentric weights if any are

present in the input.

Weights:

191

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : V-6011 ---------------------------------------- Vessel Design Summary : Step: 53 1:01a Jan 11,2015 Fabricated - Bare W/O Removable Internals 912.8 kgm

Shop Test - Fabricated + Water ( Full ) 1605.8 kgm

Shipping - Fab. + Rem. Intls.+ Shipping App. 912.8 kgm

Erected - Fab. + Rem. Intls.+ Insul. (etc) 912.8 kgm

Empty - Fab. + Intls. + Details + Wghts. 912.8 kgm

Operating - Empty + Operating Liquid (No CA) 1275.2 kgm

Field Test - Empty Weight + Water (Full) 1605.8 kgm


192

Attachment 1

193

(Ref :Recommended Practice for Plannning,Design & Construction Fixed Offshore(API RP 2A‐WSD,

:Design and Engineering Practice‐Shell (DEP) or Petronas Technical Spec.(PTS) 37.81.10.31)

Density of air, ρ = kg/m3

Max. wind Speed at 10m above MSL, μ = m/sShape coefficient, Cs =

Pressure, p = F/A = (ρ/2)μ2 Cs = kg/ms2

= N/m2

= kg/m2

0.7

749.129

749.129

WIND FORCE CALCULATION

76.336

MSET ENGINEERING CORPORATION SDN BHDDATE : 08.12.2014

DOC. REF. NO.: MSET/M2-251/V-6011/DC

SUBJECT: WIND FORCE CALC.

DOCUMENT TITLE: DESIGN CALCULATION

REVISION: 01

JOB NO: M2-251

1.225

41.8

194

Attachment 2

195

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Element and Detail Weights : Step: 7 2:49a Jan 11,2015


| | Element | Element | Corroded | Corroded | Extra due |

From| To | Metal Wgt. | ID Volume |Metal Wgt. | ID Volume | Misc % |

| | kgm | m³ | kgm | m³ | kgm |

---------------------------------------------------------------------------

10| 20| 33.0736 | 0.039026 | 33.0736 | 0.039026 | 1.65368 |

20| 30| 268.288 | 0.61226 | 268.288 | 0.61226 | 13.4144 |

30| 40| 127.648 | 0.042183 | 127.648 | 0.042183 | 6.38241 |

40| 50| 283.228 | ... | 283.228 | ... | 14.1614 |

---------------------------------------------------------------------------

Total 712 0.69 712 0.69 35

Weight of Details

| | Weight of | X Offset, | Y Offset, |

From|Type| Detail | Dtl. Cent. |Dtl. Cent. | Description

| | kgm | mm | mm |

-------------------------------------------------

10|Nozl| 5.56748 | -150.000 | ... | N3

20|Sadl| 44.0970 | 400.000 | 440.500 | Left saddle

20|Sadl| 44.0970 | 1809.00 | 440.500 | Right saddle

20|Nozl| 8.73081 | 1187.00 | 322.400 | N1

20|Nozl| 7.18497 | 1812.00 | 322.400 | N5

20|Nozl| 7.18497 | 162.000 | 322.400 | N6

20|Nozl| 7.18497 | 1812.00 | 322.400 | K1

20|Nozl| 8.15833 | 962.000 | 341.450 | K2A

20|Nozl| 8.15833 | 162.000 | 341.450 | K2B

196

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Element and Detail Weights : Step: 7 2:49a Jan 11,2015 20|Nozl| 8.15833 | 712.000 | 341.450 | K3A

20|Nozl| 8.15833 | 162.000 | 341.450 | K3B

20|Nozl| 7.18497 | 1002.00 | 322.400 | K4A

20|Nozl| 7.18497 | 162.000 | 322.400 | K4B

20|Nozl| 8.15833 | 962.000 | 341.450 | K5A

20|Nozl| 8.15833 | 512.000 | 341.450 | K5B

20|Nozl| 19.8200 | 162.000 | 354.150 | HH

20|Wght| 100.000 | 2100.00 | ... | MIST ELIMINATOR

20|Wght| 35.0000 | 1771.00 | ... | LUGS SUPPORT

40|Nozl| 7.18497 | 2460.00 | 431.800 | N2

40|Nozl| 6.61229 | 2460.00 | 431.800 | N4

Total Weight of Each Detail Type

Total Weight of Saddles 88.2

Total Weight of Nozzles 132.8

Total Weight of Weights 135.0

---------------------------------------------------------------

Sum of the Detail Weights 356.0 kgm

Weight Summation

Fabricated Shop Test Shipping Erected Empty Operating

------------------------------------------------------------------------------

747.8 968.8 747.8 968.8 747.8 1003.8

88.2 693.0 88.2 ... 88.2 ...

132.8 35.0 132.8 ... ... ...

... ... ... ... ... 135.0

197

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Element and Detail Weights : Step: 7 2:49a Jan 11,2015 ... ... ... ... ... -35.0

... ... ... ... 132.8 ...

... ... ... ... 35.0 ...

------------------------------------------------------------------------------

968.8 1696.9 968.8 1003.8 1003.8 1103.8 kgm

Miscellaneous Weight Percent: 5.0 %

Note that the above value for the miscellaneous weight percent has

been applied to the shells/heads/flange/tubesheets/tubes etc. in the

weight calculations for metallic components.

Note: The shipping total has been modified because some items have

been specified as being installed in the shop.

Weight Summary

Fabricated Wt. - Bare Weight W/O Removable Internals 968.8 kgm

Shop Test Wt. - Fabricated Weight + Water ( Full ) 1696.9 kgm

Shipping Wt. - Fab. Wt + Rem. Intls.+ Shipping App. 968.8 kgm

Erected Wt. - Fab. Wt + Rem. Intls.+ Insul. (etc) 1003.8 kgm

Ope. Wt. no Liq - Fab. Wt + Intls. + Details + Wghts. 1003.8 kgm

Operating Wt. - Empty Wt + Operating Liq. Uncorroded 1103.8 kgm

Oper. Wt. + CA - Corr Wt. + Operating Liquid 1103.8 kgm

Field Test Wt. - Empty Weight + Water (Full) 1696.9 kgm

Note: The Corroded Weight and thickness are used in the Horizontal

Vessel Analysis (Ope Case) and Earthquake Load Calculations.

198

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Element and Detail Weights : Step: 7 2:49a Jan 11,2015

Outside Surface Areas of Elements

| | Surface |

From| To | Area |

| | mm² |

----------------------------

10| 20| 484863. |

20| 30| 4.233E+06 |

30| 40| 582175. |

40| 50| 692506. |

-----------------------------

Total 5992808.500 mm²


199

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Wind Load Calculation : Step: 9 2:49a Jan 11,2015

Note: Using the User Defined Wind Profile ...

Wind Loads on Masses/Equipment/Piping

ID Wind Area Elevation Pressure Force

mm² mm kPa N

-------------------------------------------------------------------------

MIST ELIMINAT 0.00 2100.00 0.75 0.00

LUGS SUPPORT 0.00 1771.00 0.75 0.00

Wind Load Calculation

| | Wind | Wind | Wind | Wind | Element |

From| To | Height | Diameter | Area | Pressure | Wind Load |

| | mm | mm | mm² | kPa | N |

---------------------------------------------------------------------------

10| 20| 600.000 | 732.000 | 102075. | 0.75000 | 76.5547 |

20| 30| 600.000 | 732.000 | 1.617E+06 | 0.75000 | 1212.71 |

30| 40| 600.000 | 712.320 | 108558. | 0.75000 | 81.4163 |

40| 50| 600.000 | 975.360 | 66324.5 | 0.75000 | 49.7422 |


200

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Earthquake Load Calculation : Step: 10 2:49a Jan 11,2015

Earthquake Loading Specified in G's

Horizontal Acceleration factor (GX) 0.500

Horizontal Acceleration factor (GZ) 0.500

Vertical Acceleration factor (GY) -2.000

Note: Loads are distributed evenly among all elements for horizontal

geometries.

Earthquake Load Calculation

| | Earthquake | Earthquake | Element |

From| To | Height | Weight | Ope Load |

| | mm | N | N |

-------------------------------------------------

10| 20| 300.000 | 1804.03 | 902.016 |

20|Sadl| 297.000 | 1804.03 | 902.016 |

Sadl| 30| 297.000 | 1804.03 | 902.016 |

20| 30| 297.000 | 1804.03 | 902.016 |

30| 40| 296.800 | 1804.03 | 902.016 |

40| 50| 406.400 | 1804.03 | 902.016 |


201

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 2:49a Jan 11,2015

ASME Horizontal Vessel Analysis: Stresses for the Left Saddle

(per ASME Sec. VIII Div. 2 based on the Zick method.)

Horizontal Vessel Stress Calculations : Operating Case

Note: Wear Pad Width (200.00) is less than 1.56*sqrt(rm*t)

and less than 2a. The wear plate will be ignored.

Minimum Wear Plate Width to be considered in analysis [b1]:

= min( b + 1.56*sqrt( Rm * t ), 2a )

= min( 150.000 + 1.56*sqrt( 301.0000 * 8.0000 ), 2 * 438.000 )

= 226.5513 mm

Input and Calculated Values:

Vessel Mean Radius Rm 301.00 mm

Stiffened Vessel Length per 4.15.6 L 2247.00 mm

Distance from Saddle to Vessel tangent a 438.00 mm

Saddle Width b 150.00 mm

Saddle Bearing Angle theta 120.00 degrees

Inside Depth of Head h2 150.00 mm

Shell Allowable Stress used in Calculation 115.15 MPa

Head Allowable Stress used in Calculation 115.15 MPa

Circumferential Efficiency in Plane of Saddle 1.00

Circumferential Efficiency at Mid-Span 1.00

202


Saddle Force Q, Operating Case 20847.71 N

Horizontal Vessel Analysis Results: Actual Allowable

-------------------------------------------------------------------

Long. Stress at Top of Midspan -0.84 -386.09 MPa

Long. Stress at Top of Midspan 0.84 115.15 MPa

Long. Stress at Bottom of Midspan 0.84 115.15 MPa

Long. Stress at Top of Saddles 8.61 115.15 MPa

Long. Stress at Bottom of Saddles -4.77 -386.09 MPa

Long. Stress at Bottom of Saddles 4.77 115.15 MPa

Tangential Shear in Shell 5.68 69.09 MPa

Circ. Stress at Horn of Saddle 30.55 143.93 MPa

Circ. Compressive Stress in Shell 0.87 115.15 MPa

Intermediate Results: Saddle Reaction Q due to Wind or Seismic

Saddle Reaction Force due to Wind Ft [Fwt]:

= Ftr * ( Ft/Num of Saddles + Z Force Load ) * B / E

= 3.00 * ( 1420.4/2 + 0 ) * 600.0000/521.3474

= 2452.1 N

Saddle Reaction Force due to Wind Fl or Friction [Fwl]:

= max( Fl, Friction Load, Sum of X Forces) * B / Ls

= max( 263.02 , 0.00 , 0 ) * 600.0000/1409.0000

= 112.0 N

Saddle Reaction Force due to Earthquake Fl or Friction [Fsl]:

203

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 2:49a Jan 11,2015 = max( Fl, Friction Force, Sum of X Forces ) * B / Ls

= max( 5412.10 , 0.00 , 0 ) * 600.0000/1409.0000

= 2304.7 N

Saddle Reaction Force due to Earthquake Ft [Fst]:


= 3.00 * ( 5412/2 + 0 ) * 600.0000/521.3474

= 9342.9 N

Load Combination Results for Q + Wind or Seismic [Q]:

= Saddle Load + Max( Fwl, Fwt, Fsl, Fst )

= 11504 + Max( 112 , 2452 , 2304 , 9342 )

= 20847.7 N

Summary of Loads at the base of this Saddle:

Vertical Load (including saddle weight) 21280.13 N

Transverse Shear Load Saddle 2706.05 N

Longitudinal Shear Load Saddle 5412.10 N

Formulas and Substitutions for Horizontal Vessel Analysis:

Note: Wear Plate is Welded to the Shell, k = 0.1

The Computed K values from Table 4.15.1:

K1 = 0.1066 K2 = 1.1707 K3 = 0.8799 K4 = 0.4011

K5 = 0.7603 K6 = 0.0529 K7 = 0.0529 K8 = 0.3405

K9 = 0.2711 K10 = 0.0581 K1* = 0.1923

Note: Dimension a is greater than or equal to Rm / 2.

204


Moment per Equation 4.15.3 [M1]:

= -Q*a [1 - (1- a/L + (R²-h2²)/(2a*L))/(1+(4h2)/3L)]

= -20847*438.00[1-(1-438.00/2247.00+(301.000²-150.000²)/

(2*438.00*2247.00))/(1+(4*150.00)/(3*2247.00))]

= -2091.5 N-m


= Q*L/4(1+2(R²-h2²)/(L²))/(1+(4h2)/( 3L))-4a/L

= 20847*2247/4(1+2(301²-150²)/(2247²))/(1+(4*150)/

(3*2247))-4*438/2247

= 1913.6 N-m

Longitudinal Stress at Top of Shell (4.15.6) [Sigma1]:

= P * Rm/(2t) - M2/(pi*Rm²t)

= 0.000 * 301.000/(2*8.000 ) - 1913.6/(pi*301.0²*8.000 )

= -0.84 MPa

Longitudinal Stress at Bottom of Shell (4.15.7) [Sigma2]:

= P * Rm/(2t) + M2/(pi * Rm² * t)

= 0.000 * 301.000/(2 * 8.000 ) + 1913.6/(pi * 301.0² * 8.000 )

= 0.84 MPa

Longitudinal Stress at Top of Shell at Support (4.15.10) [Sigma*3]:

= P * Rm/(2t) - M1/(K1*pi*Rm²t)

= 0.000*301.000/(2*8.000)--2091.5/(0.1066*pi*301.0²*8.000)

= 8.61 MPa

Longitudinal Stress at Bottom of Shell at Support (4.15.11) [Sigma*4]:

205

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 2:49a Jan 11,2015 = P * Rm/(2t) + M1/(K1* * pi * Rm² * t)

= 0.000*301.000/(2*8.000)+-2091.5/(0.1923*pi*301.0²*8.000)

= -4.77 MPa

Maximum Shear Force in the Saddle (4.15.5) [T]:

= Q(L-2a)/(L+(4*h2/3))

= 20847 ( 2247.00 - 2 * 438.00 )/(2247.00 + ( 4 * 150.00/3))

= 11680.5 N

Shear Stress in the shell no rings, not stiffened (4.15.14) [tau2]:

= K2 * T / ( Rm * t )

= 1.1707 * 11680.51/( 301.0000 * 8.0000 )

= 5.68 MPa

Decay Length (4.15.22) [x1,x2]:

= 0.78 * sqrt( Rm * t )

= 0.78 * sqrt( 301.000 * 8.000 )

= 38.276 mm

Circumferential Stress in shell, no rings (4.15.23) [sigma6]:

= -K5 * Q * k / ( t * ( b + X1 + X2 ) )

= -0.7603 * 20847 * 0.1/( 8.000 * ( 150.00 + 38.28 + 38.28 ) )

= -0.87 MPa

Circ. Comp. Stress at Horn of Saddle, L<8Rm (4.15.25) [sigma7*]:

= -Q/(4*t*(b+X1+X2)) - 12*K7*Q*Rm/(L*t²)

= -20847/(4*8.000 *(150.000 +38.276 +38.276 )) -

12 * 0.053 * 20847 * 301.000/(2247.000 * 8.000²)

= -30.55 MPa

206


Effective reinforcing plate width (4.15.1) [B1]:

= min( b + 1.56 * sqrt( Rm * t ), 2a )

= min( 150.00 + 1.56 * sqrt( 301.000 * 8.000 ), 2 * 438.000 )

= 226.55 mm

Free Un-Restrained Thermal Expansion between the Saddles [Exp]:

= Alpha * Ls * ( Design Temperature - Ambient Temperature )

= 0.155E-04 * 1409.000 * ( 40.0 - 21.1 )

= 0.413 mm

Results for Vessel Ribs, Web and Base:

Baseplate Length Bplen 580.0000 mm

Baseplate Thickness Bpthk 10.0000 mm

Baseplate Width Bpwid 150.0000 mm

Number of Ribs ( inc. outside ribs ) Nribs 2

Rib Thickness Ribtk 10.0000 mm

Web Thickness Webtk 10.0000 mm

Web Location Webloc Center

Moment of Inertia of Saddle - Lateral Direction

Y A AY Io

Shell 4. 2208. 8833. 47111.

Wearplate 12. 1600. 19200. 238933.

Web 150. 2690. 404845. 77150032.

BasePlate 290. 1500. 435000. 126162376.

Totals 457. 7998. 867878. 203598448.

207

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 2:49a Jan 11,2015 Value C1 = Sumof(Ay)/Sumof(A) = 109. mm

Value I = Sumof(Io) - C1*Sumof(Ay) = 109427280. mm**4

Value As = Sumof(A) - Ashell = 5790. mm²

K1 = (1+Cos(beta)-.5*Sin(beta)² )/(pi-beta+Sin(beta)*Cos(beta)) = 0.2035

Fh = K1 * Q = 0.2035 * 20847.715 = 4242.9629 N

Tension Stress, St = ( Fh/As ) = 0.7329 MPa

Allowed Stress, Sa = 0.6 * Yield Str = 148.9320 MPa

d = B - R*Sin(theta) / theta = 346.3830 mm

Bending Moment, M = Fh * d = 1470.2858 N-m

Bending Stress, Sb = ( M * C1 / I ) = 1.4575 MPa

Allowed Stress, Sa = 2/3 * Yield Str = 165.4800 MPa

Minimum Thickness of Baseplate per Moss :

= ( 3 * ( Q + Saddle_Wt ) * BasePlateWidth / ( 4 * BasePlateLength *

AllStress ))½

= ( 3 * (20847 + 432 ) * 150.00/( 4 * 580.000 * 165.480 ))½

= 4.995 mm

Calculation of Axial Load, Intermediate Values and Compressive Stress

Effective Baseplate Length [e]:

= ( Bplen - Clearance ) / ( Nribs - 1)

= ( 580.0000 - 25.4 )/( 2 - 1 ) = 554.6000 mm

208

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 2:49a Jan 11,2015 Baseplate Pressure Area [Ap]:

= e * Bpwid / 2

= 554.6000 * 150.0000/2 = 41595.0000 mm²

Axial Load [P]:

= Ap * Bp

= 41595.0 * 0.24 = 9967.4 N

Area of the Rib and Web [Ar]:

= ( Bpwid - Clearance - Webtk ) * Ribtk + e/2 * Webtk

= ( 150.000 - 25.4 - 10.000 ) * 10.000 + 554.6000/2 * 10.000

= 3919.000 mm²

Compressive Stress [Sc]:

= P/Ar

= 9967.4/3918.9998 = 2.5436 MPa

Check of Outside Ribs:

Inertia of Saddle, Outer Ribs - Longitudinal Direction

Y A AY Ay² Io

Rib 75.0 1273.0 95475.0 0.0 2156899.5

Web 75.0 2773.0 207975.0 0.0 46216.6

Values 75.0 4046.0 303450.0 0.0 2203116.2

Bending Moment [Rm]:

= Fl /( 2 * Bplen ) * e * rl / 2

= 5412.1/( 2 * 580.00 ) * 554.600 * 439.50/2

= 568.843 N-m

209

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 2:49a Jan 11,2015 KL/R < Cc ( 18.5365 < 126.0993 ) per AISC E2-1

Sca = (1-(Klr)²/(2*Cc²))*Fy/(5/3+3*(Klr)/(8*Cc)-(Klr³)/(8*Cc³)

Sca = ( 1-( 18.54 )²/(2 * 126.10² )) * 248/

( 5/3+3*(18.54 )/(8* 126.10 )-( 18.54³)/(8*126.10³)

Sca = 142.64 MPa

AISC Unity Check on Outside Ribs ( must be <= 1.0 )

Check = Sc/Sca + (Rm/Z)/Sba

Check = 2.54/142.64 + (568.84/29374.883 )/165.48

Check = 0.13

ASME Horizontal Vessel Analysis: Stresses for the Right Saddle





= min( b + 1.56*sqrt( Rm * t ), 2a )

= min( 150.000 + 1.56*sqrt( 301.0000 * 8.0000 ), 2 * 438.000 )

= 226.5513 mm





210

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 2:49a Jan 11,2015 Saddle Width b 150.00 mm






Saddle Force Q, Operating Case 29445.79 N


-------------------------------------------------------------------

Long. Stress at Top of Midspan -1.86 -386.09 MPa




Long. Stress at Bottom of Saddles -4.38 -386.09 MPa








= 3.00 * ( 1420.4/2 + 0 ) * 600.0000/521.3474

= 2452.1 N

211




= max( 263.02 , 0.00 , 0 ) * 600.0000/1409.0000

= 112.0 N

Saddle Reaction Force due to Earthquake Fl or Friction [Fsl]:

= max( Fl, Friction Force, Sum of X Forces ) * B / Ls

= max( 5412.10 , 0.00 , 0 ) * 600.0000/1409.0000

= 2304.7 N

Saddle Reaction Force due to Earthquake Ft [Fst]:


= 3.00 * ( 5412/2 + 0 ) * 600.0000/521.3474

= 9342.9 N



= 20102 + Max( 112 , 2452 , 2304 , 9342 )

= 29445.8 N







212



K1 = 0.1066 K2 = 1.1707 K3 = 0.8799 K4 = 0.4011

K5 = 0.7603 K6 = 0.0529 K7 = 0.0529 K8 = 0.3405

K9 = 0.2711 K10 = 0.0581 K1* = 0.1923



= -Q*a [1 - (1- a/L + (R²-h2²)/(2a*L))/(1+(4h2)/3L)]

= -29445*438.00[1-(1-438.00/2247.00+(301.000²-0.000²)/

(2*438.00*2247.00))/(1+(4*0.00)/(3*2247.00))]

= -1921.2 N-m


= Q*L/4(1+2(R²-h2²)/(L²))/(1+(4h2)/( 3L))-4a/L

= 29445*2247/4(1+2(301²-0²)/(2247²))/(1+(4*0)/

(3*2247))-4*438/2247

= 4239.3 N-m


= P * Rm/(2t) - M2/(pi*Rm²t)

= 0.000 * 301.000/(2*8.000 ) - 4239.3/(pi*301.0²*8.000 )

= -1.86 MPa


= P * Rm/(2t) + M2/(pi * Rm² * t)

= 0.000 * 301.000/(2 * 8.000 ) + 4239.3/(pi * 301.0² * 8.000 )

= 1.86 MPa

213



= P * Rm/(2t) - M1/(K1*pi*Rm²t)

= 0.000*301.000/(2*8.000)--1921.2/(0.1066*pi*301.0²*8.000)

= 7.91 MPa


= P * Rm/(2t) + M1/(K1* * pi * Rm² * t)

= 0.000*301.000/(2*8.000)+-1921.2/(0.1923*pi*301.0²*8.000)

= -4.38 MPa


= Q(L-2a)/(L+(4*h2/3))

= 29445 ( 2247.00 - 2 * 438.00 )/(2247.00 + ( 4 * 0.00/3))

= 17966.3 N


= K2 * T / ( Rm * t )

= 1.1707 * 17966.26/( 301.0000 * 8.0000 )

= 8.74 MPa


= 0.78 * sqrt( Rm * t )

= 0.78 * sqrt( 301.000 * 8.000 )

= 38.276 mm


= -K5 * Q * k / ( t * ( b + X1 + X2 ) )

= -0.7603 * 29445 * 0.1/( 8.000 * ( 150.00 + 38.28 + 38.28 ) )

214

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 2:49a Jan 11,2015 = -1.24 MPa


= -Q/(4*t*(b+X1+X2)) - 12*K7*Q*Rm/(L*t²)

= -29445/(4*8.000 *(150.000 +38.276 +38.276 )) -

12 * 0.053 * 29445 * 301.000/(2247.000 * 8.000²)

= -43.15 MPa


= min( b + 1.56 * sqrt( Rm * t ), 2a )

= min( 150.00 + 1.56 * sqrt( 301.000 * 8.000 ), 2 * 438.000 )

= 226.55 mm

Results for Vessel Ribs, Web and Base









Y A AY Io

Shell 4. 2208. 8833. 47111.

Wearplate 12. 1600. 19200. 238933.

Web 150. 2690. 404845. 77150032.

215

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 2:49a Jan 11,2015 BasePlate 290. 1500. 435000. 126162376.

Totals 457. 7998. 867878. 203598448.

Value C1 = Sumof(Ay)/Sumof(A) = 109. mm




Fh = K1 * Q = 0.2035 * 29445.795 = 5992.8584 N









AllStress ))½

= ( 3 * (29445 + 432 ) * 150.00/( 4 * 580.000 * 165.480 ))½

= 5.918 mm



216

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 2:49a Jan 11,2015 = ( Bplen - Clearance ) / ( Nribs - 1)

= ( 580.0000 - 25.4 )/( 2 - 1 ) = 554.6000 mm

Baseplate Pressure Area [Ap]:

= e * Bpwid / 2

= 554.6000 * 150.0000/2 = 41595.0000 mm²

Axial Load [P]:

= Ap * Bp

= 41595.0 * 0.34 = 14078.1 N



= ( 150.000 - 25.4 - 10.000 ) * 10.000 + 554.6000/2 * 10.000

= 3919.000 mm²


= P/Ar

= 14078.1/3918.9998 = 3.5926 MPa



Y A AY Ay² Io

Rib 75.0 1273.0 95475.0 0.0 2156899.5

Web 75.0 2773.0 207975.0 0.0 46216.6

Values 75.0 4046.0 303450.0 0.0 2203116.2


= Fl /( 2 * Bplen ) * e * rl / 2

217

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 2:49a Jan 11,2015 = 5412.1/( 2 * 580.00 ) * 554.600 * 439.50/2

= 568.843 N-m

KL/R < Cc ( 18.5365 < 126.0993 ) per AISC E2-1


Sca = ( 1-( 18.54 )²/(2 * 126.10² )) * 248/

( 5/3+3*(18.54 )/(8* 126.10 )-( 18.54³)/(8*126.10³)

Sca = 142.64 MPa



Check = 3.59/142.64 + (568.84/29374.883 )/165.48

Check = 0.14


218

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 2:49a Jan 11,2015

ASME Horizontal Vessel Analysis: Stresses for the Left Saddle


Horizontal Vessel Stress Calculations : Test Case




= min( b + 1.56*sqrt( Rm * t ), 2a )

= min( 150.000 + 1.56*sqrt( 301.0000 * 8.0000 ), 2 * 438.000 )

= 226.5513 mm







Inside Depth of Head h2 150.00 mm





219


Saddle Force Q, Test Case, no Ext. Forces 5084.59 N


-------------------------------------------------------------------











= 3.00 * ( 468.7/2 + 0 ) * 600.0000/521.3474

= 809.2 N



= max( 263.02 , 0.00 , 0 ) * 600.0000/1409.0000

= 37.0 N



= 4275 + Max( 36 , 809 , 0 , 0 )

220

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 2:49a Jan 11,2015 = 5084.6 N





Hydrostatic Test Pressure at center of Vessel: 23.783 bar




K1 = 0.1066 K2 = 1.1707 K3 = 0.8799 K4 = 0.4011

K5 = 0.7603 K6 = 0.0529 K7 = 0.0529 K8 = 0.3405

K9 = 0.2711 K10 = 0.0581 K1* = 0.1923



= -Q*a [1 - (1- a/L + (R²-h2²)/(2a*L))/(1+(4h2)/3L)]

= -5084*438.00[1-(1-438.00/2247.00+(301.000²-150.000²)/

(2*438.00*2247.00))/(1+(4*150.00)/(3*2247.00))]

= -510.1 N-m


= Q*L/4(1+2(R²-h2²)/(L²))/(1+(4h2)/( 3L))-4a/L

= 5084*2247/4(1+2(301²-150²)/(2247²))/(1+(4*150)/

221

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 2:49a Jan 11,2015 (3*2247))-4*438/2247

= 466.7 N-m


= P * Rm/(2t) - M2/(pi*Rm²t)

= 23.783 * 301.000/(2*8.000 ) - 466.7/(pi*301.0²*8.000 )

= 44.54 MPa


= P * Rm/(2t) + M2/(pi * Rm² * t)

= 23.783 * 301.000/(2 * 8.000 ) + 466.7/(pi * 301.0² * 8.000 )

= 44.95 MPa


= P * Rm/(2t) - M1/(K1*pi*Rm²t)

= 23.783*301.000/(2*8.000)--510.1/(0.1066*pi*301.0²*8.000)

= 46.85 MPa


= P * Rm/(2t) + M1/(K1* * pi * Rm² * t)

= 23.783*301.000/(2*8.000)+-510.1/(0.1923*pi*301.0²*8.000)

= 43.58 MPa


= Q(L-2a)/(L+(4*h2/3))

= 5084 ( 2247.00 - 2 * 438.00 )/(2247.00 + ( 4 * 150.00/3))

= 2848.8 N


222

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 2:49a Jan 11,2015 = K2 * T / ( Rm * t )

= 1.1707 * 2848.78/( 301.0000 * 8.0000 )

= 1.39 MPa


= 0.78 * sqrt( Rm * t )

= 0.78 * sqrt( 301.000 * 8.000 )

= 38.276 mm


= -K5 * Q * k / ( t * ( b + X1 + X2 ) )

= -0.7603 * 5084 * 0.1/( 8.000 * ( 150.00 + 38.28 + 38.28 ) )

= -0.21 MPa


= -Q/(4*t*(b+X1+X2)) - 12*K7*Q*Rm/(L*t²)

= -5084/(4*8.000 *(150.000 +38.276 +38.276 )) -

12 * 0.053 * 5084 * 301.000/(2247.000 * 8.000²)

= -7.45 MPa


= min( b + 1.56 * sqrt( Rm * t ), 2a )

= min( 150.00 + 1.56 * sqrt( 301.000 * 8.000 ), 2 * 438.000 )

= 226.55 mm

Results for Vessel Ribs, Web and Base:




223

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 2:49a Jan 11,2015 Number of Ribs ( inc. outside ribs ) Nribs 2





Y A AY Io

Shell 4. 2208. 8833. 47111.

Wearplate 12. 1600. 19200. 238933.

Web 150. 2690. 404845. 77150032.

BasePlate 290. 1500. 435000. 126162376.

Totals 457. 7998. 867878. 203598448.





Fh = K1 * Q = 0.2035 * 5084.591 = 1034.8246 N






224

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 2:49a Jan 11,2015 Allowed Stress, Sa = 2/3 * Yield Str = 165.4800 MPa



AllStress ))½

= ( 3 * (5084 + 432 ) * 150.00/( 4 * 580.000 * 165.480 ))½

= 2.543 mm




= ( 580.0000 - 25.4 )/( 2 - 1 ) = 554.6000 mm


= e * Bpwid / 2

= 554.6000 * 150.0000/2 = 41595.0000 mm²

Axial Load [P]:

= Ap * Bp

= 41595.0 * 0.06 = 2431.0 N



= ( 150.000 - 25.4 - 10.000 ) * 10.000 + 554.6000/2 * 10.000

= 3919.000 mm²


= P/Ar

225

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 2:49a Jan 11,2015 = 2431.0/3918.9998 = 0.6204 MPa



Y A AY Ay² Io

Rib 75.0 1273.0 95475.0 0.0 2156899.5

Web 75.0 2773.0 207975.0 0.0 46216.6

Values 75.0 4046.0 303450.0 0.0 2203116.2


= Fl /( 2 * Bplen ) * e * rl / 2

= 86.8/( 2 * 580.00 ) * 554.600 * 439.50/2

= 9.123 N-m

KL/R < Cc ( 18.5365 < 126.0993 ) per AISC E2-1


Sca = ( 1-( 18.54 )²/(2 * 126.10² )) * 248/

( 5/3+3*(18.54 )/(8* 126.10 )-( 18.54³)/(8*126.10³)

Sca = 142.64 MPa



Check = 0.62/142.64 + (9.12/29374.883 )/165.48

Check = 0.01

ASME Horizontal Vessel Analysis: Stresses for the Right Saddle


226

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 2:49a Jan 11,2015 Note: Wear Pad Width (200.00) is less than 1.56*sqrt(rm*t)



= min( b + 1.56*sqrt( Rm * t ), 2a )

= min( 150.000 + 1.56*sqrt( 301.0000 * 8.0000 ), 2 * 438.000 )

= 226.5513 mm











Saddle Force Q, Test Case, no Ext. Forces 12308.55 N


-------------------------------------------------------------------




227

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 2:49a Jan 11,2015 Long. Stress at Bottom of Saddles 42.92 155.14 MPa







= 3.00 * ( 468.7/2 + 0 ) * 600.0000/521.3474

= 809.2 N



= max( 263.02 , 0.00 , 0 ) * 600.0000/1409.0000

= 37.0 N



= 11499 + Max( 36 , 809 , 0 , 0 )

= 12308.6 N





Hydrostatic Test Pressure at center of Vessel: 23.783 bar

228





K1 = 0.1066 K2 = 1.1707 K3 = 0.8799 K4 = 0.4011

K5 = 0.7603 K6 = 0.0529 K7 = 0.0529 K8 = 0.3405

K9 = 0.2711 K10 = 0.0581 K1* = 0.1923



= -Q*a [1 - (1- a/L + (R²-h2²)/(2a*L))/(1+(4h2)/3L)]

= -12308*438.00[1-(1-438.00/2247.00+(301.000²-0.000²)/

(2*438.00*2247.00))/(1+(4*0.00)/(3*2247.00))]

= -803.1 N-m


= Q*L/4(1+2(R²-h2²)/(L²))/(1+(4h2)/( 3L))-4a/L

= 12308*2247/4(1+2(301²-0²)/(2247²))/(1+(4*0)/

(3*2247))-4*438/2247

= 1772.0 N-m


= P * Rm/(2t) - M2/(pi*Rm²t)

= 23.783 * 301.000/(2*8.000 ) - 1772.0/(pi*301.0²*8.000 )

= 43.97 MPa

229

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 2:49a Jan 11,2015 Longitudinal Stress at Bottom of Shell (4.15.7) [Sigma2]:

= P * Rm/(2t) + M2/(pi * Rm² * t)

= 23.783 * 301.000/(2 * 8.000 ) + 1772.0/(pi * 301.0² * 8.000 )

= 45.53 MPa


= P * Rm/(2t) - M1/(K1*pi*Rm²t)

= 23.783*301.000/(2*8.000)--803.1/(0.1066*pi*301.0²*8.000)

= 48.06 MPa


= P * Rm/(2t) + M1/(K1* * pi * Rm² * t)

= 23.783*301.000/(2*8.000)+-803.1/(0.1923*pi*301.0²*8.000)

= 42.92 MPa


= Q(L-2a)/(L+(4*h2/3))

= 12308 ( 2247.00 - 2 * 438.00 )/(2247.00 + ( 4 * 0.00/3))

= 7510.0 N


= K2 * T / ( Rm * t )

= 1.1707 * 7510.02/( 301.0000 * 8.0000 )

= 3.65 MPa


= 0.78 * sqrt( Rm * t )

= 0.78 * sqrt( 301.000 * 8.000 )

= 38.276 mm

230



= -K5 * Q * k / ( t * ( b + X1 + X2 ) )

= -0.7603 * 12308 * 0.1/( 8.000 * ( 150.00 + 38.28 + 38.28 ) )

= -0.52 MPa


= -Q/(4*t*(b+X1+X2)) - 12*K7*Q*Rm/(L*t²)

= -12308/(4*8.000 *(150.000 +38.276 +38.276 )) -

12 * 0.053 * 12308 * 301.000/(2247.000 * 8.000²)

= -18.04 MPa


= min( b + 1.56 * sqrt( Rm * t ), 2a )

= min( 150.00 + 1.56 * sqrt( 301.000 * 8.000 ), 2 * 438.000 )

= 226.55 mm

Results for Vessel Ribs, Web and Base









231

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 2:49a Jan 11,2015 Y A AY Io

Shell 4. 2208. 8833. 47111.

Wearplate 12. 1600. 19200. 238933.

Web 150. 2690. 404845. 77150032.

BasePlate 290. 1500. 435000. 126162376.

Totals 457. 7998. 867878. 203598448.





Fh = K1 * Q = 0.2035 * 12308.552 = 2505.0576 N









AllStress ))½

= ( 3 * (12308 + 432 ) * 150.00/( 4 * 580.000 * 165.480 ))½

= 3.865 mm

232





= ( 580.0000 - 25.4 )/( 2 - 1 ) = 554.6000 mm


= e * Bpwid / 2

= 554.6000 * 150.0000/2 = 41595.0000 mm²

Axial Load [P]:

= Ap * Bp

= 41595.0 * 0.14 = 5884.8 N



= ( 150.000 - 25.4 - 10.000 ) * 10.000 + 554.6000/2 * 10.000

= 3919.000 mm²


= P/Ar

= 5884.8/3918.9998 = 1.5017 MPa



Y A AY Ay² Io

Rib 75.0 1273.0 95475.0 0.0 2156899.5

Web 75.0 2773.0 207975.0 0.0 46216.6

233

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 2:49a Jan 11,2015 Values 75.0 4046.0 303450.0 0.0 2203116.2


= Fl /( 2 * Bplen ) * e * rl / 2

= 86.8/( 2 * 580.00 ) * 554.600 * 439.50/2

= 9.123 N-m

KL/R < Cc ( 18.5365 < 126.0993 ) per AISC E2-1


Sca = ( 1-( 18.54 )²/(2 * 126.10² )) * 248/

( 5/3+3*(18.54 )/(8* 126.10 )-( 18.54³)/(8*126.10³)

Sca = 142.64 MPa



Check = 1.50/142.64 + (9.12/29374.883 )/165.48

Check = 0.01


234

Attachment 3

235

Input Echo, Leg & Lug Item 1, Description: Trunnion

Design Internal Pressure 0.00 barDesign Temperature for Attachment TEMP 40.00 CVessel Outside Diameter OD 609.600 mm.Vessel Wall Thickness Ts 8.0000 mm.Vessel Corrosion Allowance Cas 0.0000 mm.Vessel Material SA-240 316LVessel Material UNS Number S31603Vessel Allowable Stress at Design S 115.23 MPaAnalysis Type: Trunnion

Empty Weight of Vessel Wemp 9810.00 N .Operating Weight of Vessel (vertical load ) W 0.00 N .

Trunnion Material SA-312 TP316LTrunnion Material UNS Number S31603Trunnion Yield Stress SY 171.23 MPaTrunnion Outside Diameter TOD 88.900 mm.Trunnion Thickness TTHK 7.6200 mm.Trunnion Length TL 232.0000 mm.Bail/Sling Width TT 25.4000 mm.Pad Outside Diameter POD 154.000 mm.Pad Thickness PTHK 8.0000 mm.Ring Outside Diameter Rod 172.00 mm.Ring Thickness Rthk 8.00 mm.Trunnion Type HollowLift Orientation VerticalImpact Factor Impfac 2.00

Force Along Vessel Axis Fax 4905.00 N .Force Normal to Vessel Fn 2832.00 N .Force Tangential to Vessel Ft 491.00 N .Perform WRC-107 Analysis on the Trunnion Yes

Occasional Load Factor (AISC A5.2) Occfac 1.00

Results for Trunnions, Description : Trunnion

Trunnion Lifting Load [Tlf]:= ((Fa^2 + Ft^2)^1/2)= ((4905.00 ^2 + 491.00 ^2)^1/2) * 2.00= 9859.03 N .

Z = pi * (TOD^4 - TID^4) / (32.0 * TOD)= 3.14 * ( 88.90 ^4 - 73.66 ^4) / (32.0 * 88.90 )= 36466.53 mm.^3

Trunnion Bending Moment [Tmom]:= (TL - 0.5 * TT)/1.001* Tlf= ( 232.00 - 0.5 * 25.40 )/1.001 * 9859.03= 2162.96 N-m .

Trunnion Calculated Bending Stress [SBC]:= TMOM * 1.001/ Z= 2162.96 *1.001/ 36466.53= 59.34 MPa [Passed] SBC < Min(0.66* SY* Occfac, .75* SY) (113.01)

Trunnion Cross Section Area [Txsa]:= pi / 4 * (TOD^2- TID^2)= 3.14 /4 * ( 88.90^2- 73.66^2)= 1945.76 mm^2

Trunnion Calculated Shear Stress [SSC]:= Tlf / Txsa= 9859.03 / 1945.76= 5.07 MPa [Passed] SSC < 0.4 * SY * Occfac (68.49)

Trunnion Unity Check [UCHK]:= SBC / SBA + SSC / SSA= 59.34 / 113.01 + 5.07 / 68.49= 0.60 [Passed] UCHK, Must be less than 1.

Trunnion Bearing Contact Area [Tbca]:= TOD * TT= 88.90 * 25.40= 2258.06 mm^2

236

Trunnion Bearing Stress [SBEC]:= Tlf / Tbca= 9859.03 / 2258.06= 4.37 MPa [Passed] SBEC < Min(0.75* SY* Occfac, 0.9* SY) (128.42)

Results of WRC-107 Analysis on the trunnion:

Note: This following Stress Analysis assumes that the Trunnionpasses through the pad and is welded to the shell via a groove weld.Additionally the re-pad is welded to the shell at the outsideedge via a fillet weld.

WRC 107 Stress Calculation for OCCasional loads:Radial Load P -5664.0 N .Circumferential Shear VC 982.0 N .Longitudinal Shear VL 9810.0 N .Circumferential Moment MC 215.4 N-m .Longitudinal Moment ML 2152.2 N-m .Torsional Moment MT 0.0 N-m .


Dimensionless Loads for Cylindrical Shells at Attachment Junction:-------------------------------------------------------------------Curves read for 1979 Beta Figure Value Location-------------------------------------------------------------------N(PHI) / ( P/Rm ) 0.128 4C 3.402 (A,B)N(PHI) / ( P/Rm ) 0.128 3C 3.034 (C,D)M(PHI) / ( P ) 0.128 2C1 0.098 (A,B)M(PHI) / ( P ) 0.128 1C 0.133 (C,D)N(PHI) / ( MC/(Rm**2 * Beta) ) 0.128 3A 0.528 (A,B,C,D)M(PHI) / ( MC/(Rm * Beta) ) 0.128 1A 0.098 (A,B,C,D)N(PHI) / ( ML/(Rm**2 * Beta) ) 0.128 3B 1.817 (A,B,C,D)M(PHI) / ( ML/(Rm * Beta) ) 0.128 1B 0.049 (A,B,C,D)

N(x) / ( P/Rm ) 0.128 3C 3.034 (A,B)N(x) / ( P/Rm ) 0.128 4C 3.402 (C,D)M(x) / ( P ) 0.128 1C1 0.135 (A,B)M(x) / ( P ) 0.128 2C 0.098 (C,D)N(x) / ( MC/(Rm**2 * Beta) ) 0.128 4A 0.763 (A,B,C,D)M(x) / ( MC/(Rm * Beta) ) 0.128 2A 0.055 (A,B,C,D)N(x) / ( ML/(Rm**2 * Beta) ) 0.128 4B 0.501 (A,B,C,D)M(x) / ( ML/(Rm * Beta) ) 0.128 2B 0.079 (A,B,C,D)


Stresses in the Vessel at the Attachment Junction------------------------------------------------------------------------

| Stress Values atType of | (MPa )

---------------|--------------------------------------------------------Stress Load| Au Al Bu Bl Cu Cl Du Dl---------------|--------------------------------------------------------Circ. Memb. P | 3 3 3 3 3 3 3 3Circ. Bend. P | 12 -12 12 -12 17 -17 17 -17Circ. Memb. MC | 0 0 0 0 0 0 0 0Circ. Bend. MC | 0 0 0 0 -12 12 12 -12Circ. Memb. ML | -20 -20 20 20 0 0 0 0Circ. Bend. ML | -63 63 63 -63 0 0 0 0

|Tot. Circ. Str.| -67.1 33.7 100.9 -51.7 7.8 -1.9 34.5 -26.3------------------------------------------------------------------------Long. Memb. P | 3 3 3 3 3 3 3 3Long. Bend. P | 17 -17 17 -17 13 -13 13 -13Long. Memb. MC | 0 0 0 0 0 0 0 0Long. Bend. MC | 0 0 0 0 -7 7 7 -7Long. Memb. ML | -5 -5 5 5 0 0 0 0Long. Bend. ML | -102 102 102 -102 0 0 0 0

|Tot. Long. Str.| -87.0 82.7 130.0 -111.6 8.9 -2.8 25.0 -15.3------------------------------------------------------------------------

Shear VC | 0 0 0 0 0 0 0 0Shear VL | 0 0 0 0 -4 -4 4 4Shear MT | 0 0 0 0 0 0 0 0

|Tot. Shear| 0.4 0.4 -0.4 -0.4 -4.4 -4.4 4.4 4.4

------------------------------------------------------------------------

237

Str. Int. | 86.99 82.67 130.00 111.57 12.78 8.83 36.23 27.80------------------------------------------------------------------------


Dimensionless Loads for Cylindrical Shells at Pad edge:-------------------------------------------------------------------Curves read for 1979 Beta Figure Value Location-------------------------------------------------------------------N(PHI) / ( P/Rm ) 0.224 4C 5.002 (A,B)N(PHI) / ( P/Rm ) 0.224 3C 3.009 (C,D)M(PHI) / ( P ) 0.224 2C1 0.030 (A,B)M(PHI) / ( P ) 0.224 1C ! 0.062 (C,D)N(PHI) / ( MC/(Rm**2 * Beta) ) 0.224 3A 1.538 (A,B,C,D)M(PHI) / ( MC/(Rm * Beta) ) 0.224 1A 0.074 (A,B,C,D)N(PHI) / ( ML/(Rm**2 * Beta) ) 0.224 3B 3.604 (A,B,C,D)M(PHI) / ( ML/(Rm * Beta) ) 0.224 1B 0.022 (A,B,C,D)

N(x) / ( P/Rm ) 0.224 3C 3.009 (A,B)N(x) / ( P/Rm ) 0.224 4C 5.002 (C,D)M(x) / ( P ) 0.224 1C1 0.060 (A,B)M(x) / ( P ) 0.224 2C ! 0.032 (C,D)N(x) / ( MC/(Rm**2 * Beta) ) 0.224 4A 3.085 (A,B,C,D)M(x) / ( MC/(Rm * Beta) ) 0.224 2A 0.035 (A,B,C,D)N(x) / ( ML/(Rm**2 * Beta) ) 0.224 4B 1.536 (A,B,C,D)M(x) / ( ML/(Rm * Beta) ) 0.224 2B 0.034 (A,B,C,D)



Stresses in the Vessel at the Edge of Reinforcing Pad------------------------------------------------------------------------

| Stress Values atType of | (MPa )

---------------|--------------------------------------------------------Stress Load| Au Al Bu Bl Cu Cl Du Dl---------------|--------------------------------------------------------Circ. Memb. P | 11 11 11 11 7 7 7 7Circ. Bend. P | 15 -15 15 -15 32 -32 32 -32Circ. Memb. MC | 0 0 0 0 -2 -2 2 2Circ. Bend. MC | 0 0 0 0 -22 22 22 -22Circ. Memb. ML | -47 -47 47 47 0 0 0 0Circ. Bend. ML | -65 65 65 -65 0 0 0 0

|Tot. Circ. Str.| -86.0 13.9 141.1 -21.8 15.7 -5.7 64.2 -46.0------------------------------------------------------------------------Long. Memb. P | 7 7 7 7 11 11 11 11Long. Bend. P | 31 -31 31 -31 16 -16 16 -16Long. Memb. MC | 0 0 0 0 -4 -4 4 4Long. Bend. MC | 0 0 0 0 -10 10 10 -10Long. Memb. ML | -20 -20 20 20 0 0 0 0Long. Bend. ML | -102 102 102 -102 0 0 0 0

|Tot. Long. Str.| -84.1 57.5 162.1 -107.1 14.2 1.1 43.2 -11.4------------------------------------------------------------------------

Shear VC | 0 0 0 0 0 0 0 0Shear VL | 0 0 0 0 -5 -5 5 5Shear MT | 0 0 0 0 0 0 0 0

|Tot. Shear| 0.5 0.5 -0.5 -0.5 -5.1 -5.1 5.1 5.1

------------------------------------------------------------------------Str. Int. | 86.17 57.52 162.10 107.13 20.13 12.20 65.38 46.69

------------------------------------------------------------------------

SUMMARY OF RESULTS:

Trunnion unity check value: 0.5991

Actual Allowable Pass/FailBending Stress (MPa ) 59.34 113.01 PassShear Stress (MPa ) 5.07 68.49 PassBearing Stress (MPa ) 4.37 128.42 Pass

Vessel Maximum Stress Intensity Comparison:At Nozzle Edge: 130.00 Allowable: 1.5 * S: 172.85 MPa [Passed]At Pad Edge : 162.10 Allowable: 1.5 * S: 172.85 MPa [Passed]

238


239

V-6011_DCa ad a

Documents

Transcript of V-6011_DCa ad a