S-6011_DC asdasd asda dad a

MSET ENGINEERING CORPORATION SDN BHD

DOCUMENT TITLE: DESIGN CALCULATION DATE: 11.01.2015

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

SUBJECT: TITLE PAGE JOB NO: M2-251

SERIAL NO.: M2-251/002

DESIGN CALCULATION

Fuel Gas Filter Coalescer TAG NO: S-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






DESIGN DATA

ITEM NO. FUEL GAS FILTER COALESCER

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) (In / Out) 7 / 6.8

TEMPERATURE (⁰C) (In / Out) 24.8-38.9 / 24.7-38.8

TEST PRESSURE

HYDROTEST (barg) (1.3xMAPxLSR)(note1) (UG-99c)

24.625 (Horizontal Position)

PNEUMATIC NO

MAWP (hot & corroded) (barg) 18.347

MAP (new & cold) (barg) 18.998

OUTSIDE DIAMETER / SEAM TO SEAM (mm) 219.1/3120

TYPE OF HEAD 2:1 ELLIP HEAD/BODY FLANGE

MATERIAL OF CONSTRUCTION (SHELL & HEAD) SA 312 TP 316/316L & SA 403 WP 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) 390

CAPACITY (m3) 0.11

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)






TABLE OF CONTENT

NO CONTENT PAGE NO.

1 Input Echo 4

2 Flg Calc [Int P] : A1 (flange) 20

3 Flg Calc [Int P] : A1 (blind) 25

4 Internal Pressure Calculations 29

5 External Pressure Calculations 33

6 Element and Detail Weights 37

7 Nozzle Flange MAWP 42

8 Wind Load Calculation 44

9 Earthquake Load Calculation 45

10 Wind / Earthquake Shear, Bending 47

11 Wind Deflection 49

12 Stress due Combined Loads 55

13 Center of Gravity Calculation 61

14 Sup. Lug Calc 62

15 Nozzle Calculation 78

16 Nozzle Schedule 213

17 Nozzle Summary 217

18 MDMT Summary 220

19 Vessel Design Summary 222

20 Attachment 1 : Wind Pressure Calc 225

21 Attachment 2 : Transportation Calc 227

22 Attachment 3 : Trunnion Calc 266

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p 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 : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p 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 : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p 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 Yes

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" 55.000 mm

Element Outside Diameter 219.07 mm

Element Thickness 7.1565 mm

Internal Corrosion Allowance 0.0000 mm

Nominal Thickness 8.1788 mm

External Corrosion Allowance 0.0000 mm

Design Internal Pressure 18.000 bar

6

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p 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-403 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 Smls. & wld. fittings

Efficiency, Longitudinal Seam 1.0

Efficiency, Circumferential Seam 1.0

Elliptical Head Factor 2.0


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

Blind Flange (Y/N) N

Weight of Nozzle ( Used if > 0 ) 0.0000 N

Grade of Attached Flange GR 2.2

Nozzle Matl SA-312 TP316L

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

7

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Element From Node 20

Element To Node 30

Element Type Cylinder

Description Shell


Element Outside Diameter 219.07 mm






Design Temperature Internal Pressure 50 °C




Material Name SA-312 TP316L








UNS Number S31603

Product Form Smls. & wld. pipe

Efficiency, Longitudinal Seam 1.0

Efficiency, Circumferential Seam 1.0


Detail Type Liquid

Detail ID LIQUID (LOWER)


Height/Length of Liquid 650.00 mm

8

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Liquid Density 803.23 kg/m³


Detail Type Nozzle

Detail ID N1



Nozzle Schedule None

Nozzle Class 150

Layout Angle 0.0




Nozzle Matl SA-182 F316


Detail Type Nozzle

Detail ID N2




Nozzle Class 150

Layout Angle 285.0






Detail Type Nozzle

Detail ID N4



9

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Nozzle Schedule None

Nozzle Class 150

Layout Angle 90.0






Detail Type Nozzle

Detail ID N5




Nozzle Class 150

Layout Angle 345.0






Detail Type Nozzle

Detail ID N6




Nozzle Class 150

Layout Angle 90.0





10

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015


Detail Type Nozzle

Detail ID K1A



Nozzle Schedule 80S

Nozzle Class 150

Layout Angle 20.0






Detail Type Nozzle

Detail ID K1B



Nozzle Schedule 80S

Nozzle Class 150

Layout Angle 20.0






Detail Type Nozzle

Detail ID K2A




11

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Nozzle Class 150

Layout Angle 315.0






Detail Type Nozzle

Detail ID K2B




Nozzle Class 150

Layout Angle 315.0






Detail Type Nozzle

Detail ID K3A



Nozzle Schedule 80S

Nozzle Class 150

Layout Angle 225.0





12

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Element From Node 20

Detail Type Nozzle

Detail ID K3B



Nozzle Schedule 80S

Nozzle Class 150

Layout Angle 225.0






Detail Type Nozzle

Detail ID K4A



Nozzle Schedule 80S

Nozzle Class 150

Layout Angle 165.0






Detail Type Nozzle

Detail ID K4B



Nozzle Schedule 80S

Nozzle Class 150

13

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Layout Angle 165.0






Detail Type Nozzle

Detail ID K6A




Nozzle Class 150

Layout Angle 340.0






Detail Type Nozzle

Detail ID K6B




Nozzle Class 150

Layout Angle 340.0






14

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Detail Type Nozzle

Detail ID K7A



Nozzle Schedule 80S

Nozzle Class 150

Layout Angle 225.0






Detail Type Nozzle

Detail ID K7B



Nozzle Schedule 80S

Nozzle Class 150

Layout Angle 225.0






Detail Type Nozzle

Detail ID K8A



Nozzle Schedule 80S

Nozzle Class 150

Layout Angle 165.0

15

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Blind Flange (Y/N) N





Detail Type Nozzle

Detail ID K8B



Nozzle Schedule 80S

Nozzle Class 150

Layout Angle 165.0






Detail Type Nozzle

Detail ID K5A



Nozzle Schedule 80S

Nozzle Class 150

Layout Angle 30.0






Detail Type Nozzle

16

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Detail ID K5B



Nozzle Schedule 80S

Nozzle Class 150

Layout Angle 30.0






Detail Type Lug

Detail ID LUG


Number of Lugs 2

Dist. from OD to Lug Cntrline(dlug) 600.00 mm

Height of Gusset Plates (hgp) 250.00 mm

Force Bearing Width (wfb) 200.00 mm

Weight of Lug 133.44 N

Lug Start Angle (degrees) 0.0


Detail Type Weight

Detail ID FILTER


Miscellaneous Weight 980.60 N

Offset from Element Centerline 0.0000 mm


Detail Type Weight

Detail ID LIQUID (UPPER)


17

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Miscellaneous Weight 156.90 N

Offset from Element Centerline 0.0000 mm

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


Element To Node 40

Element Type Flange

Description Body Flange (DN200)


Flange Inside Diameter (OD for Blinds) 345.00 mm










Material Name SA-182 F316L








UNS Number S31603

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

18

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 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 (DN200)


Flange Inside Diameter (OD for Blinds) 345.00 mm










Material Name SA-182 F316L

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

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

19

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Flg Calc [Int P] : A1 (flange) Flng: 3 1:14p Jan 11,2015

Flange Input Data Values Description: A1 (flange) :

Body Flange (DN200)

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 202.692 mm

Flange Outside Diameter A 345.000 mm

Flange Thickness t 28.4480 mm

Thickness of Hub at Small End go 7.1564 mm

Thickness of Hub at Large End g1 20.6184 mm

Length of Hub h 73.1520 mm

Flange Material SA-182 F316L

Flange Material UNS number S31603

Flange Allowable Stress At Temperature Sfo 115.15 MPa

Flange Allowable Stress At Ambient Sfa 115.15 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 298.500 mm

Nominal Bolt Diameter a 19.0500 mm

Type of Threads TEMA Thread Series

Number of Bolts 8

Flange Face Outside Diameter Fod 269.748 mm

20

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Flg Calc [Int P] : A1 (flange) Flng: 3 1:14p Jan 11,2015 Flange Face Inside Diameter Fid 202.692 mm

Flange Facing Sketch 1, Code Sketch 1a

Gasket Outside Diameter Go 263.652 mm

Gasket Inside Diameter Gi 233.426 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*(202.6920/2+0.0000))/(115.15*1.00-0.6*18.00)+Ca

= 1.5995 mm

Hub Small End Hub MAWP:

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

= (115.15 * 1.00 * 7.1564 )/(101.3460 + 0.6 * 7.1564 )

= 77.993 bar

Corroded Flange ID, Bcor = B+2*Fcor 202.692 mm

Corroded Large Hub, g1Cor = g1-ci 20.618 mm

Corroded Small Hub, g0Cor = go-ci 7.156 mm

Code R Dimension, R = (C-B)/2 - g1 27.286 mm

Gasket Contact Width, N = (Go - Gi) / 2 15.113 mm

Basic Gasket Width, bo = N / 2 7.557 mm

21

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Flg Calc [Int P] : A1 (flange) Flng: 3 1:14p Jan 11,2015 Effective Gasket Width, b = Cb sqrt(bo) 6.927 mm

Gasket Reaction Diameter, G = Go (Self-Energizing) 263.652 mm

Basic Flange and Bolt Loads:

Hydrostatic End Load due to Pressure [H]:

= 0.785 * G² * Peq

= 0.785 * 263.6520² * 18.000

= 98276.719 N

Contact Load on Gasket Surfaces [Hp]:

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

= 2 * 6.9270 * 3.1416 * 263.6520 * 0.0000 * 18.00

= 0.000 N

Hydrostatic End Load at Flange ID [Hd]:

= Pi * Bcor² * P / 4

= 3.1416 * 202.6920² *18.0000/4

= 58084.695 N

Pressure Force on Flange Face [Ht]:

= H - Hd

= 98276 - 58084

= 40192.023 N

Operating Bolt Load [Wm1]:

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

= max( 98276 + 0 + 0 , 0 )

= 98276.719 N

Gasket Seating Bolt Load [Wm2]:

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

= 0.00*6.9270*3.141*263.652+0.00*0.0000*0.00

= 0.000 N

Required Bolt Area [Am]:

= Maximum of Wm1/Sb, Wm2/Sa

= Maximum of 98276/172 , 0/172

= 570.182 mm²

22

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Flg Calc [Int P] : A1 (flange) Flng: 3 1:14p Jan 11,2015

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

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

= 2 * 19.050 + 6 * 28.448/(0.00 + 0.5)

= 379.476 mm

Actual Circumferential Bolt Spacing [Bs]:

= C * sin( pi / n )

= 298.500 * sin( 3.142/8 )

= 114.231 mm

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

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

= max( sqrt( 114.231/( 2 * 19.050 + 28.448 )), 1 )

= 1.3102

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

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

Minimum Actual Maximum

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

Bolt Area, mm² 570.182 1558.706

Radial distance bet. hub and bolts 28.575 27.286

Radial distance bet. bolts and the edge 20.637 23.250

Circumferential spacing between bolts 44.450 114.231 379.476

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

Flange Design Bolt Load, Gasket Seating [W]:

= Sa * ( Am + Ab ) / 2

= 172.38 * ( 570.1817 + 1558.7064 )/2

= 183467.95 N

Gasket Load for the Operating Condition [HG]:

= Wm1 - H

= 98276 - 98276

23

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Flg Calc [Int P] : A1 (flange) Flng: 3 1:14p Jan 11,2015 = 0.00 N

Moment Arm Calculations:

Distance to Gasket Load Reaction [hg]:

= (C - G ) / 2

= ( 298.5000 - 263.6520 )/2

= 17.4240 mm

Distance to Face Pressure Reaction [ht]:

= ( R + g1 + hg ) / 2

= ( 27.2856 + 20.6184 + 17.4240 )/2

= 32.6640 mm

Distance to End Pressure Reaction [hd]:

= R + ( g1 / 2 )

= 27.2856 + ( 20.6184/2.0 )

= 37.5948 mm

Summary of Moments for Internal Pressure:

Loading Force Distance Bolt Corr Moment

End Pressure, Md 58085. 37.5948 1.3102 2862. N-m

Face Pressure, Mt 40192. 32.6640 1.3102 1721. N-m

Gasket Load, Mg 0. 17.4240 1.3102 0. N-m

Gasket Seating, Matm 183468. 17.4240 1.3102 4190. N-m

Total Moment for Operation, Mop 4583. N-m

Total Moment for Gasket seating, Matm 4190. 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. 19.5 kgm

Estimated Unfinished Weight of Forging at given Thk 49.9 kgm


24

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Flg Calc [Int P] : A1 (blind) Flng: 4 1:14p Jan 11,2015

Flange Input Data Values Description: A1 (blind) :

Blind Flange (DN200)

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 345.000 mm

Flange Thickness t 28.4480 mm

Flange Material SA-182 F316L

Flange Material UNS number S31603

Flange Allowable Stress At Temperature Sfo 115.15 MPa

Flange Allowable Stress At Ambient Sfa 115.15 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 937.765 mm

Diameter of Bolt Circle C 298.500 mm

Nominal Bolt Diameter a 19.0500 mm

Type of Threads TEMA Thread Series

Number of Bolts 8

Flange Face Outside Diameter Fod 269.748 mm

25

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Flg Calc [Int P] : A1 (blind) Flng: 4 1:14p Jan 11,2015 Flange Face Inside Diameter Fid 184.150 mm

Flange Facing Sketch 1, Code Sketch 1a

Gasket Outside Diameter Go 263.652 mm

Gasket Inside Diameter Gi 233.426 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


Gasket Contact Width, N = (Go - Gi) / 2 15.113 mm

Basic Gasket Width, bo = N / 2 7.557 mm

Effective Gasket Width, b = Cb sqrt(bo) 6.927 mm

Gasket Reaction Diameter, G = Go (Self-Energizing) 263.652 mm

Basic Flange and Bolt Loads:

Hydrostatic End Load due to Pressure [H]:

= 0.785 * G² * Peq

= 0.785 * 263.6520² * 18.000

= 98276.719 N

Contact Load on Gasket Surfaces [Hp]:

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

= 2 * 6.9270 * 3.1416 * 263.6520 * 0.0000 * 18.00

= 0.000 N

Operating Bolt Load [Wm1]:

26

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Flg Calc [Int P] : A1 (blind) Flng: 4 1:14p Jan 11,2015 = max( H + Hp + H'p, 0 )

= max( 98276 + 0 + 0 , 0 )

= 98276.719 N

Gasket Seating Bolt Load [Wm2]:

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

= 0.00*6.9270*3.141*263.652+0.00*0.0000*0.00

= 0.000 N

Required Bolt Area [Am]:

= Maximum of Wm1/Sb, Wm2/Sa

= Maximum of 98276/172 , 0/172

= 570.182 mm²

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

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

= 2 * 19.050 + 6 * 28.448/(0.00 + 0.5)

= 379.476 mm

Actual Circumferential Bolt Spacing [Bs]:

= C * sin( pi / n )

= 298.500 * sin( 3.142/8 )

= 114.231 mm

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

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

= max( sqrt( 114.231/( 2 * 19.050 + 28.448 )), 1 )

= 1.3102

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

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

Minimum Actual Maximum

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

Bolt Area, mm² 570.182 1558.706

Radial distance bet. bolts and the edge 20.637 23.250

27

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Flg Calc [Int P] : A1 (blind) Flng: 4 1:14p Jan 11,2015 Circumferential spacing between bolts 44.450 114.231 379.476

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

Flange Design Bolt Load, Gasket Seating [W]:

= Sa * ( Am + Ab ) / 2

= 172.38 * ( 570.1817 + 1558.7064 )/2

= 183467.95 N

Gasket Load for the Operating Condition [HG]:

= Wm1

= 98276.72 N

Moment Arm Calculations:

Distance to Gasket Load Reaction [hg]:

= (C - G ) / 2

= ( 298.5000 - 263.6520 )/2

= 17.4240 mm

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. 21.3 kgm

Estimated Unfinished Weight of Forging at given Thk 21.3 kgm


28

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Internal Pressure Calculations : Step: 5 1:14p 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| 18.051 | 8.1788 | ... | 219.07 | 115.15 |

Shell| 18.051 | 8.1788 | ... | 219.07 | 115.15 |

Body Flang| 18.000 | 8.1788 | ... | 345.00 | 115.15 |

Blind Flan| 18.000 | ... | ... | 345.00 | 115.15 |

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 | 79.8661 | 79.9173 | 7.15645 | 1.69354 |

Shell| 18.0000 | 77.1854 | 77.2366 | 7.15645 | 1.70673 |

Body Flang| 18.0000 | 18.3984 | 18.9983 | 28.4480 | No Calc |

Blind Flan| 18.0000 | 18.3984 | 18.9983 | 28.4480 | No Calc |

Minimum 18.347 18.998

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

Flange MAWP including Static Pressure: 18.347 = 18.398 - 0.051 bar

Internal Pressure Calculation Results :


Elliptical Head From 10 To 20 SA-403 316L at 50 °C

29


Head

Longitudinal Joint: Seamless

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

Material UNS Number: S31603

Required Thickness due to Internal Pressure [tr]:

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

= (18.051*219.0750*1.000)/(2*115.15*1.00+2*18.051*(1.000-0.1))

= 1.6935 + 0.0000 = 1.6935 mm

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

Less Operating Hydrostatic Head Pressure of 0.051 bar

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

= (2*115.15*1.00*7.1565)/(1.000*219.0750-2*7.1565*(1.00-0.1))

= 79.917 - 0.051 = 79.866 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*7.1565)/(1.000*219.0750-2*7.1565*(1.000-0.1))

= 79.917 bar

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

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

= (18.051*(1.000*219.0750-2*7.1565*(1.000-0.1)))/(2*1.00*7.1565)

= 26.009 MPa

Straight Flange Required Thickness:

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

= (18.051*109.5375)/(115.15*1.00+0.4*18.051)+0.000

= 1.707 mm

30


Straight Flange Maximum Allowable Working Pressure:


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

= (115.15 * 1.00 * 8.1788 )/(109.5375 - 0.4 * 8.1788 )

= 88.610 - 0.051 = 88.559 bar

SA-403 316L, Min Metal Temp without impact per UHA-51: -196 °C

Cylindrical Shell From 20 To 30 SA-312 TP316L at 50 °C

Shell

Longitudinal Joint: Seamless

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



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

= (18.051*109.5375)/(115.15*1.00+0.4*18.051)

= 1.7067 + 0.0000 = 1.7067 mm




= (115.15*1.00*7.1565)/(109.5375-0.4*7.1565)

= 77.237 - 0.051 = 77.185 bar

Maximum Allowable Pressure, New and Cold [MAPNC]:


= (115.15*1.00*7.1565)/(109.5375-0.4*7.1565)

= 77.237 bar

31


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

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

= (18.051*((109.5375-0.4*7.1565))/(1.00*7.1565)

= 26.911 MPa

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

Hydrostatic Test Pressure Results:

Pressure per UG99b = 1.3 * M.A.W.P. * Sa/S 23.851 bar

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

Pressure per UG99c = 1.3 * M.A.P. - Head(Hyd) 24.625 bar

Pressure per UG100 = 1.1 * M.A.W.P. * Sa/S 20.182 bar

Pressure per PED = 1.43 * MAWP 26.236 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 35.5 155.1 0.229 24.65

Shell 36.7 155.1 0.237 24.65

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

Elements Suitable for Internal Pressure.


32

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- External Pressure Calculations : Step: 6 1:14p 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

7.156 219.07 30.61 0.0045370 83.75

EMAP = B/(K0*D/t) = 83.7457/(0.9000 *30.6122 ) = 30.3922 bar

Results for Required Thickness (Tca):

Tca OD D/t Factor A B

0.579 219.07 378.29 0.0003671 35.22

EMAP = B/(K0*D/t) = 35.2178/(0.9000 *378.2943 ) = 1.0343 bar

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

pressure for this head.



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

= (1.727*219.0750*1.000)/(2*115.15*1.00+2*1.727*(1.000-0.1))

= 0.1641 + 0.0000 = 0.1641 mm


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

33

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- External Pressure Calculations : Step: 6 1:14p Jan 11,2015 = ((2*115.15*1.00*7.1565)/(1.000*219.0750-2*7.1565*(1.00-0.1)))/1.67

= 47.855 bar

Maximum Allowable External Pressure [MAEP]:

= min( MAEP, MAWP )

= min( 30.39 , 47.8547 )

= 30.392 bar

Thickness requirements per UG-33(a)(1) 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

7.156 219.07 3192.06 30.61 14.5706 0.0011983 65.86

EMAP = (4*B)/(3*(D/t)) = (4*65.8589 )/(3*30.6122 ) = 28.6811 bar

Results for Required Thickness (Tca):


1.939 219.07 3192.06 112.96 14.5706 0.0000914 8.76

EMAP = (4*B)/(3*(D/t)) = (4*8.7631 )/(3*112.9565 ) = 1.0342 bar

Results for Maximum Stiffened Length (Slen):


7.156 219.07 88373.64 30.61 50.0000 0.0011797 65.64

EMAP = (4*B)/(3*(D/t)) = (4*65.6350 )/(3*30.6122 ) = 28.5836 bar

External Pressure Calculations

34

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- External Pressure Calculations : Step: 6 1:14p Jan 11,2015

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

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

| | mm | mm | mm | | MPa |

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

10| 20| No Calc | 219.075 | 7.15645 | 0.0045370 | 83.7457 |

20| 30| 3192.06 | 219.075 | 7.15645 | 0.0011983 | 65.8589 |

30| 40| No Calc | ... | 28.4480 | No Calc | No Calc |

40| 50| No Calc | ... | 28.4480 | 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| 7.15645 | 1.50000 | 1.03420 | 30.3922 |

20| 30| 7.15645 | 1.93946 | 1.03420 | 28.6811 |

30| 40| 28.4480 | No Calc | 1.03420 | No Calc |

40| 50| 28.4480 | No Calc | 1.03420 | No Calc |

Minimum 28.681


| | 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| 3192.06 | 88373.6 | No Calc | No Calc |



35

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- External Pressure Calculations : Step: 6 1:14p Jan 11,2015 Elements Suitable for External Pressure.


36

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Element and Detail Weights : Step: 7 1:14p 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| 5.97865 | 0.0029355 | 5.97865 | 0.0029355 | 0.29893 |

20| 30| 137.032 | 0.10276 | 137.032 | 0.10276 | 6.85162 |

30| 40| 19.5277 | 0.0032789 | 19.5277 | 0.0032789 | 0.97638 |

40| 50| 21.3476 | ... | 21.3476 | ... | 1.06738 |

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

Total 183 0.11 183 0.11 9

Weight of Details

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

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

| | kgm | mm | mm |

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

10|Nozl| 3.82814 | ... | -51.1905 | N3

20|Liqd| 17.1931 | ... | 325.000 | LIQUID (LOWER)

20|Nozl| 7.18497 | 127.781 | 1200.00 | N1

20|Nozl| 7.18497 | 127.781 | 2920.00 | N2

20|Nozl| 7.18497 | 127.781 | 1425.00 | N4

20|Nozl| 7.18497 | 127.781 | 3000.00 | N5

20|Nozl| 7.18497 | 127.781 | 200.000 | N6

20|Nozl| 8.15833 | 146.831 | 770.000 | K1A

20|Nozl| 8.15833 | 146.831 | 170.000 | K1B

20|Nozl| 7.18496 | 127.781 | 1010.00 | K2A

20|Nozl| 7.18496 | 127.781 | 170.000 | K2B

20|Nozl| 8.15833 | 146.831 | 570.000 | K3A

20|Nozl| 8.15833 | 146.831 | 170.000 | K3B

37

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Element and Detail Weights : Step: 7 1:14p Jan 11,2015 20|Nozl| 8.15833 | 146.831 | 750.000 | K4A

20|Nozl| 8.15833 | 146.831 | 350.000 | K4B

20|Nozl| 7.18496 | 127.781 | 1895.00 | K6A

20|Nozl| 7.18496 | 127.781 | 1445.00 | K6B

20|Nozl| 8.15833 | 146.831 | 1795.00 | K7A

20|Nozl| 8.15833 | 146.831 | 1445.00 | K7B

20|Nozl| 8.15833 | 146.831 | 1950.00 | K8A

20|Nozl| 8.15833 | 146.831 | 1550.00 | K8B

20|Nozl| 8.15833 | 146.831 | 1850.00 | K5A

20|Nozl| 8.15833 | 146.831 | 1500.00 | K5B

20|Lugs| 28.5768 | ... | 2692.00 | LUG

20|Wght| 100.000 | ... | 1700.00 | FILTER

20|Wght| 16.0000 | ... | 1908.00 | LIQUID (UPPER)

Total Weight of Each Detail Type

Total Weight of Liquid 17.2

Total Weight of Nozzles 166.4

Total Weight of Lugs 28.6

Total Weight of Weights 116.0

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

Sum of the Detail Weights 328.2 kgm

Weight Summation

Fabricated Shop Test Shipping Erected Empty Operating

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

193.1 388.1 193.1 388.1 193.1 388.1

... 108.9 ... ... ... 17.2

166.4 ... 166.4 ... ... ...

28.6 ... 28.6 ... ... ...

... ... ... ... ... 116.0

38

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Element and Detail Weights : Step: 7 1:14p Jan 11,2015 ... ... ... ... ... ...

... ... ... ... 166.4 ...

... ... ... ... 28.6 ...

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

388.1 497.0 388.1 388.1 388.1 521.2 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 388.1 kgm

Shop Test Wt. - Fabricated Weight + Water ( Full ) 497.0 kgm

Shipping Wt. - Fab. Wt + Rem. Intls.+ Shipping App. 388.1 kgm

Erected Wt. - Fab. Wt + Rem. Intls.+ Insul. (etc) 388.1 kgm

Ope. Wt. no Liq - Fab. Wt + Intls. + Details + Wghts. 388.1 kgm

Operating Wt. - Empty Wt + Operating Liq. Uncorroded 521.2 kgm

Field Test Wt. - Empty Weight + Water (Full) 497.0 kgm

Mass of the Upper 1/3 of the Vertical Vessel 102.1 kgm

Outside Surface Areas of Elements

| | Surface |

From| To | Area |

| | mm² |

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

39

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Element and Detail Weights : Step: 7 1:14p Jan 11,2015 10| 20| 91207.0 |

20| 30| 2.167E+06 |

30| 40| 148106. |

40| 50| 124315. |

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

Total 2530993.000 mm²


| 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| 10.1057 | 10.1057 | 13.0394 | ... | 10.1057 |

20|Lugs| 252.132 | 361.718 | 336.627 | 182.714 | 347.572 |

Lugs| 30| 54.3161 | 77.9237 | 72.5184 | 39.3614 | 74.8763 |

30| 40| 20.5040 | 20.5040 | 23.7810 | ... | 20.5040 |

40| 50| 22.4150 | 22.4150 | 22.4150 | ... | 22.4150 |

Cumulative Vessel Weight

| | Cumulative Ope | Cumulative | Cumulative |

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

| | kgm | kgm | kgm |

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

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

20|Lugs| -10.1057 | -10.1057 | -13.0394 |

Lugs| 30| 117.795 | 120.843 | 118.714 |

30| 40| 42.9191 | 42.9191 | 46.1960 |

40| 50| 22.4150 | 22.4150 | 22.4150 |

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

are the cumulative operating weights minus the operating liquid

40

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Element and Detail Weights : Step: 7 1:14p Jan 11,2015 weight minus any weights absent in the empty condition.

Cumulative Vessel Moment

| | Cumulative | Cumulative |Cumulative |

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

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

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

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

20|Lugs| 182.714 | 182.714 | 182.714 |

Lugs| 30| 39.3614 | 39.3614 | 39.3614 |

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

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


41

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Flange MAWP : Step: 8 1:14p 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 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

N5 18.4 19.0 50 150 GR 2.2

N6 18.4 19.0 50 150 GR 2.2

K1A 18.4 19.0 50 150 GR 2.2

K1B 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

K6A 18.4 19.0 50 150 GR 2.2

K6B 18.4 19.0 50 150 GR 2.2

K7A 18.4 19.0 50 150 GR 2.2

K7B 18.4 19.0 50 150 GR 2.2

K8A 18.4 19.0 50 150 GR 2.2

K8B 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

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

Minimum Rating 18.4 19.0 bar

42

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Flange MAWP : Step: 8 1:14p Jan 11,2015 Note: ANSI Ratings are per ANSI/ASME B16.5 2009 Metric Edition


43

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Natural Frequency Calculation : Step: 9 1:14p 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 11.6100 Hz.

The Natural Frequency for the Vessel (Ope...) is 11.3756 Hz.


44

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Wind Load Calculation : Step: 10 1:14p 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

0.000/3305.048 = 0.000

45

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Wind Load Calculation : Step: 10 1:14p Jan 11,2015 #2 - ( D / L² ) * 104 < 8.0 (English Units)

- ( 0.72/10.84² ) * 104 = 60.973 [Geometry Violation]

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

= W / ( L * Dr²)

= 5111/( 3305.05 * 204.762² )

= 0.36885E-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

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

FILTER 0.00 1755.00 0.75 0.00

LIQUID (UPPER 0.00 1963.00 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| 62.0931 | 262.890 | 26506.0 | 0.75000 | 19.8791 |

20| 30| 1666.19 | 262.890 | 820217. | 0.75000 | 615.148 |

30| 40| 3276.99 | 245.715 | 24964.6 | 0.75000 | 18.7230 |

40| 50| 3342.01 | 245.715 | 6990.09 | 0.75000 | 5.24244 |


46

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Earthquake Load Calculation : Step: 11 1:14p 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| 27.5000 | 99.0967 | 70.0719 | 70.0719 |

20|Lugs| 2622.00 | 3547.01 | 2508.11 | 1748.26 |

Lugs| 30| 2898.50 | 764.119 | 540.314 | 376.621 |

30| 40| 3225.80 | 201.063 | 142.173 | 142.173 |

40| 50| 3290.82 | 219.802 | 155.423 | 155.423 |


47

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Wind/Earthquake Shear, Bending : Step: 12 1:14p 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| 2618.25 | ... | ... | ... | ... |

20|Lugs| 1283.50 | 19.8791 | 70.0719 | 0.074501 | 0.26261 |

Lugs| 30| 276.500 | 152.876 | 907.982 | 655.864 | 3060.82 |

30| 40| 603.800 | 23.9655 | 297.596 | 1.55896 | 25.2343 |

40| 50| 668.824 | 5.24244 | 155.423 | 0.074598 | 2.21161 |


48

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Wind Deflection : Step: 13 1:14p 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| ... | 0.010864 | 0.021727 | ... |

20|Lugs| 19.8791 | -0.39317 | ... | ... |

Lugs| 30| 152.876 | -0.42107 | -0.31128 |-0.00039289 |

30| 40| 23.9655 | -0.29111 | -0.27093 |-0.00039289 |

40| 50| 5.24244 | -0.26528 | -0.25963 |-0.00039289 |

Critical Wind Velocity for Tower Vibration

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

From| To | Wind Speed | Wind Speed |

| | km/hr | km/hr |

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

10| 20| 53.6847 | 335.529 |

20| 30| 53.6847 | 335.529 |

30| 40| 50.1773 | 313.608 |

40| 50| 50.1773 | 313.608 |

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

Allowable deflection : 16.525 Actual Deflection : 0.022 mm


49

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Longitudinal Stress Constants : Step: 14 1:14p 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| 4764.49 | 4764.49 | 244454. | 244454. |

20| 30| 4764.49 | 4764.49 | 244454. | 244454. |

30| 40| 4764.49 | 4764.49 | 244454. | 244454. |

40| 50| 4764.49 | 4764.49 | 244454. | 244454. |


50

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Longitudinal Allowable Stresses : Step: 15 1:14p Jan 11,2015

Longitudinal Allowable Stresses

| | | Hydrotest | | Hydrotest |

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

| | MPa | MPa | MPa | MPa |

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

10| 20| 138.176 | 186.165 | -109.117 | -111.814 |

20|Lugs| 138.176 | 186.165 | -109.117 | -111.814 |

Lugs| 30| 138.176 | 186.165 | -109.117 | -111.814 |

30| 40| 138.176 | 186.165 | -109.117 | -111.814 |

40| 50| 138.176 | 186.165 | -109.117 | -111.814 |


51

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Longitudinal Stresses Due to . . . Step: 16 1:14p 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| 12.5173 | -0.81833 | 17.1242 |

20| 30| 12.5173 | -0.81833 | 17.1242 |

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| 0.020801 | 0.020801 | ... | 0.74720 | 0.74720 |

Lugs| 30| -0.24246 | -0.21334 | ... | 0.16097 | 0.16097 |

30| 40| -0.088341 | -0.088341 | ... | ... | ... |

40| 50| -0.046137 | -0.046137 | ... | ... | ... |


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

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PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Longitudinal Stresses Due to . . . Step: 16 1:14p Jan 11,2015 From| To | Hyd. Mom. | Oper. Wind |Oper. Equ. | Hyd. Wind | Hyd. Equ. |

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

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

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

20|Lugs| ... | 0.00030467 | 0.0010739 | ... | ... |

Lugs| 30| ... | 2.68212 | 12.5171 | ... | ... |

30| 40| ... | 0.0063753 | 0.10319 | ... | ... |

40| 50| ... | 0.00030506 | 0.0090443 | ... | ... |


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

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


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

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

20|Lugs| ... | ... | ... | 0.0010739 |

Lugs| 30| ... | ... | ... | 8.71229 |

30| 40| ... | ... | ... | 0.10319 |

40| 50| ... | ... | ... | 0.0090443 |


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

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

| | MPa | MPa |

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

10| 20| ... | 0.041602 |

20|Lugs| ... | 1.53066 |

Lugs| 30| ... | -0.49746 |

30| 40| ... | -0.17668 |

40| 50| ... | -0.092274 |

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PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Longitudinal Stresses Due to . . . Step: 16 1:14p 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| ... | ... | ... | ... |


54

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Stress due to Combined Loads : Step: 17 1:14p 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.

55


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 0.00 109.12 0.0000 0.0000

20 0.77 138.18 -0.73 109.12 0.0056 0.0067

20 2.60 138.18 -3.09 109.12 0.0188 0.0283

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



10 0.04 138.18 109.12 0.0003

20 2.30 138.18 109.12 0.0166

20 8.13 138.18 -9.61 109.12 0.0589 0.0881

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



10 0.00 138.18 0.00 109.12 0.0000 0.0000

20 0.77 138.18 -0.73 109.12 0.0056 0.0067

20 2.63 138.18 -3.06 109.12 0.0190 0.0280

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

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PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Stress due to Combined Loads : Step: 17 1:14p Jan 11,2015 From Tensile All. Tens. Comp. All. Comp. Tens. Comp.


10 0.04 138.18 109.12 0.0003

20 2.30 138.18 109.12 0.0166

20 11.97 138.18 -13.39 109.12 0.0866 0.1227

Analysis of Load Case 5 : NP+HW+HI



10 0.00 186.17 0.00 111.81 0.0000 0.0000

20 0.00 186.17 0.00 111.81 0.0000 0.0000

20 0.00 186.17 0.00 111.81 0.0000 0.0000

Analysis of Load Case 6 : NP+HW+HE



10 0.00 186.17 0.00 111.81 0.0000 0.0000

20 0.00 186.17 0.00 111.81 0.0000 0.0000

20 0.00 186.17 0.00 111.81 0.0000 0.0000

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



10 12.52 138.18 109.12 0.0906

20 13.29 138.18 109.12 0.0962

20 15.15 138.18 109.12 0.1096

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



10 12.56 138.18 109.12 0.0909

20 14.82 138.18 109.12 0.1072

20 24.48 138.18 -0.87 109.12 0.1772 0.0080

57


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



10 138.18 -0.82 109.12 0.0075

20 138.18 -1.55 109.12 0.0142

20 1.81 138.18 -3.87 109.12 0.0131 0.0355

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



10 138.18 -0.78 109.12 0.0071

20 1.48 138.18 -0.02 109.12 0.0107 0.0001

20 11.15 138.18 -14.21 109.12 0.0807 0.1302

Analysis of Load Case 11 : HP+HW+HI



10 17.12 186.17 111.81 0.0920

20 17.12 186.17 111.81 0.0920

20 17.12 186.17 111.81 0.0920

Analysis of Load Case 12 : HP+HW+HE



10 17.12 186.17 111.81 0.0920

20 17.12 186.17 111.81 0.0920

20 17.12 186.17 111.81 0.0920

Analysis of Load Case 13 : IP+WE+EW



10 12.52 138.18 109.12 0.0906

58

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Stress due to Combined Loads : Step: 17 1:14p Jan 11,2015 20 13.29 138.18 109.12 0.0961

20 12.44 138.18 109.12 0.0900

Analysis of Load Case 14 : IP+WF+CW



10 12.52 138.18 109.12 0.0906

20 12.54 138.18 109.12 0.0907

20 12.30 138.18 109.12 0.0890

Analysis of Load Case 15 : IP+VO+OW



10 12.52 138.18 109.12 0.0906

20 13.29 138.18 109.12 0.0961

20 12.46 138.18 109.12 0.0902

Analysis of Load Case 16 : IP+VE+EW



10 12.52 138.18 109.12 0.0906

20 13.29 138.18 109.12 0.0961

20 12.44 138.18 109.12 0.0900

Analysis of Load Case 17 : NP+VO+OW



10 0.00 138.18 0.00 109.12 0.0000 0.0000

20 0.77 138.18 -0.73 109.12 0.0056 0.0067

20 138.18 -0.37 109.12 0.0034

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


59

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Stress due to Combined Loads : Step: 17 1:14p Jan 11,2015 Node Stress Stress Stress Stress Ratio Ratio

10 12.56 138.18 109.12 0.0909

20 14.82 138.18 109.12 0.1072

20 11.97 138.18 109.12 0.0866

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



10 138.18 -0.78 109.12 0.0071

20 1.48 138.18 -0.01 109.12 0.0107 0.0001

20 138.18 -1.69 109.12 0.0155

Absolute Maximum of the all of the Stress Ratio's 0.1772

Governing Element: Shell

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


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PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Center of Gravity Calculation : Step: 18 1:14p Jan 11,2015

Shop/Field Installation Options :

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

Center of Gravity of Liquid 380.000 mm

Center of Gravity of Nozzles 1256.373 mm

Center of Gravity of Lugs 2747.000 mm

Center of Gravity of Added Weights (Operating) 1783.690 mm

Center of Gravity of Bare Shell New and Cold 1928.210 mm

Center of Gravity of Bare Shell Corroded 1928.210 mm

Vessel CG in the Operating Condition 1675.404 mm

Vessel CG in the Fabricated (Shop/Empty) Condition 1700.429 mm

Vessel CG in the Test Condition 1784.015 mm


61

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p 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 600.0000 mm

Lug Support Force Bearing Width Wfb 200.0000 mm

Lug Material SA-240 316L

Lug Yield Stress 165.40 MPa

Radial Width of bottom Support Lug Plate Wpl 250.0000 mm

Effective Force Bearing Length Lpl 120.0000 mm

Thickness of bottom Support Lug Plate Tpl 10.0000 mm

Distance between Gussets Dgp 90.0000 mm

Mean Width of Gusset Plate Wgp 102.0000 mm

Height of Gusset Plate Hgp 250.0000 mm

Thickness of Gusset Plate Tgp 15.0000 mm

Pad Width along Circumference C11P 160.000 mm

Pad Length along Vessel Axis C22P 300.000 mm

Pad Thickness Tpad 8.000 mm


Bolt Allowable Stress at Design Temperature 172.38 MPa

Thread Series TEMA Metric

Bolt Diameter 20.00 mm

Results for Support Lugs: Description: LUG

Overturning Moment at Support Lug 3061. N-m

Weight Load at the top of one Lug 7247. N

62

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 Force on one Lug, Operating Condition [Flug]:

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

= ( 14493/2 + 3060/( 709.54 * 2/2 ))

= 11558.71 N

Force on one lug in the Empty Condition [Flugemp]:

= ( -Wemp/Nlug + Mlugemp/( Rlug * Nlug/2 ) )

= ( -3524/2 + 2130/( 709.54 * 2/2 ))

= 1238.85 N

Bottom Support Plate Bending Stress (Point Load) [Spl]:

= ( Flugemp/2*Dgp/2)/((Wpl/6)*Tpl²) (Uplift Condition)

= ( 1238/2*90.000/2)/((250.00/6)*10.0000²)

= 6.69 MPa

Bottom Plate Required Thickness (Point Load) 2.4632 mm

Bottom Plate required thickness for Uplift per ADM S 3/4 [trUpl]:

= 0.72 * sqrt( Flugemp * Dgp / ( ( Wpl - dt ) * Spa ) )

= 0.72 * sqrt( 1238.9 * 90.00/( ( 250.00 - 23.17 ) * 110.267 ) )

= 1.52 mm

Bearing Area [Ba]:

= Lpl * Wfb

= 120.000 * 200.000

= 24000.00 mm²

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

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

= 0.157 * 11558.7/24000.000 * 200.000²/10.000²

= 30.21 MPa

Bottom Plate Required Thickness (Uniform Load) 5.2346 mm

63


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

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

= 0.71*90.00*((11558/(120.00*200.00))/110.267)½

= 4.223 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 )

= ( 11558/2 )/( 102.000 *15.0000 )

= 3.78 MPa

Required Thickness of Gussets per AISC 3.8494 mm

Gusset Plate Allowable Stress [Sga]:

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

= ( 1-( 66.67 )²/(2 * 151.74² )) * 165/

( 5/3+3*(66.67 )/(8* 151.74 )-( 66.67³)/(8*151.74³)

= 82.07 MPa

Maximum Compressive Gusset Plate Stress per Bednar [SgpB]:

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

= 11558 *( 3*600.000 -250.000 )/( 15.0000 *250.000²*(Sin(40.18 ))² )

= 45.90 MPa

64

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 Gusset Plate Allowable Compressive Stress [SgaB]:

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

= 18000/(1+(1/18000)* (250.000/Sin(40.18 )/(0.289*15.0000 ))² )

= 85.96 MPa

Determine the required bolt area due to Uplift [Abr]:

= Flugemp / Sabolt

= 1238.854/172.375

= 7.19 mm²

The Area available in a single bolt : 217.051 mm² [OK]

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 204.762 mm

Vessel Thickness Tv 7.156 mm

Design Temperature 50.00 °C

Attachment Type Type Rectangular

Parameter C11 C11 54.00 mm

Parameter C22 C22 200.00 mm

Thickness of Reinforcing Pad Tpad 8.000 mm

Pad Parameter C11P C11p 160.000 mm

Pad Parameter C22P C22p 300.000 mm

Design Internal Pressure Dp 18.000 bar

Include Pressure Thrust No

65

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 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 7246.6 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 4349.7 N-m

Internal Pressure (SUS) P 18.00 bar


Global Force (OCC) Fx 1708.0 N

Global Force (OCC) Fy 4312.1 N

Global Force (OCC) Fz 0.0 N

Global Moment (OCC) Mx 0.0 N-m

Global Moment (OCC) My 1025.2 N-m

Global Moment (OCC) Mz 2588.3 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

66


WRC 107 Stress Calculation for SUStained loads:

Radial Load P 0.0 N

Circumferential Shear VC 0.0 N

Longitudinal Shear VL 7246.6 N

Circumferential Moment MC 0.0 N-m

Longitudinal Moment ML -4349.7 N-m

Torsional Moment MT 0.0 N-m

Dimensionless Parameters used : Gamma = 7.25

Dimensionless Loads for Cylindrical Shells at Attachment Junction:

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

Curves read for 1979 Beta Figure Value Location

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

N(PHI) / ( P/Rm ) 0.693 4C ! 0.973 (A,B)

N(PHI) / ( P/Rm ) 0.693 3C ! 0.668 (C,D)

M(PHI) / ( P ) 0.417 2C1 0.041 (A,B)

M(PHI) / ( P ) 0.417 1C 0.064 (C,D)

N(PHI) / ( MC/(Rm**2 * Beta) ) 0.380 3A ! 0.292 (A,B,C,D)

M(PHI) / ( MC/(Rm * Beta) ) 0.491 1A 0.082 (A,B,C,D)

N(PHI) / ( ML/(Rm**2 * Beta) ) 0.588 3B ! 0.760 (A,B,C,D)

M(PHI) / ( ML/(Rm * Beta) ) 0.532 1B ! 0.022 (A,B,C,D)

N(x) / ( P/Rm ) 0.565 3C ! 0.668 (A,B)

N(x) / ( P/Rm ) 0.565 4C ! 0.973 (C,D)

M(x) / ( P ) 0.588 1C1 ! 0.052 (A,B)

M(x) / ( P ) 0.588 2C ! 0.034 (C,D)

N(x) / ( MC/(Rm**2 * Beta) ) 0.380 4A ! 0.602 (A,B,C,D)

M(x) / ( MC/(Rm * Beta) ) 0.684 2A ! 0.042 (A,B,C,D)

N(x) / ( ML/(Rm**2 * Beta) ) 0.588 4B ! 0.331 (A,B,C,D)

M(x) / ( ML/(Rm * Beta) ) 0.718 2B ! 0.040 (A,B,C,D)

67


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 | 21 21 -21 -21 0 0 0 0

Circ. Bend. ML | 43 -43 -43 43 0 0 0 0

|

Tot. Circ. Str.| 64.9 -21.5 -64.9 21.5 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 | 16 16 -16 -16 0 0 0 0

Long. Bend. ML | 58 -58 -58 58 0 0 0 0

|

Tot. Long. Str.| 74.2 -41.8 -74.2 41.8 0.0 0.0 0.0 0.0

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

Shear VC | 0 0 0 0 0 0 0 0

Shear VL | 0 0 0 0 -1 -1 1 1

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PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 Shear MT | 0 0 0 0 0 0 0 0

|

Tot. Shear| 0.0 0.0 0.0 0.0 -1.2 -1.2 1.2 1.2

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

Str. Int. | 74.22 41.80 74.22 41.80 2.39 2.39 2.39 2.39

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

WARNING: Ratio of Pad Radius/Rm (0.755) is not between 0.01 and 0.571.


Dimensionless Loads for Cylindrical Shells at Pad edge:

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


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

N(PHI) / ( P/Rm ) 1.343 4C ! 1.591 (A,B)

N(PHI) / ( P/Rm ) 1.343 3C ! 0.884 (C,D)

M(PHI) / ( P ) 0.957 2C1 ! 0.015 (A,B)

M(PHI) / ( P ) 0.957 1C ! 0.055 (C,D)

N(PHI) / ( MC/(Rm**2 * Beta) ) 0.931 3A ! 0.554 (A,B,C,D)

M(PHI) / ( MC/(Rm * Beta) ) 1.017 1A ! 0.066 (A,B,C,D)

N(PHI) / ( ML/(Rm**2 * Beta) ) 1.148 3B ! 1.113 (A,B,C,D)

M(PHI) / ( ML/(Rm * Beta) ) 1.093 1B ! 0.012 (A,B,C,D)

N(x) / ( P/Rm ) 1.162 3C ! 0.884 (A,B)

N(x) / ( P/Rm ) 1.162 4C ! 1.591 (C,D)

M(x) / ( P ) 1.195 1C1 ! 0.030 (A,B)

M(x) / ( P ) 1.195 2C ! 0.030 (C,D)

N(x) / ( MC/(Rm**2 * Beta) ) 0.931 4A ! 1.587 (A,B,C,D)

M(x) / ( MC/(Rm * Beta) ) 1.258 2A ! 0.032 (A,B,C,D)

N(x) / ( ML/(Rm**2 * Beta) ) 1.148 4B ! 0.568 (A,B,C,D)

M(x) / ( ML/(Rm * Beta) ) 1.278 2B ! 0.023 (A,B,C,D)

69

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 Note - The ! mark next to the figure name denotes curve value exceeded.


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 | 45 45 -45 -45 0 0 0 0

Circ. Bend. ML | 53 -53 -53 53 0 0 0 0

|

Tot. Circ. Str.| 99.0 -7.4 -99.0 7.4 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 | 33 33 -33 -33 0 0 0 0

Long. Bend. ML | 86 -86 -86 86 0 0 0 0

|

Tot. Long. Str.| 120.3 -53.1 -120.3 53.1 0.0 0.0 0.0 0.0

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

Shear VC | 0 0 0 0 0 0 0 0

Shear VL | 0 0 0 0 -1 -1 1 1

Shear MT | 0 0 0 0 0 0 0 0

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PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 |

Tot. Shear| 0.0 0.0 0.0 0.0 -1.7 -1.7 1.7 1.7

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

Str. Int. | 120.35 53.09 120.35 53.09 3.38 3.38 3.38 3.38

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

WRC 107 Stress Calculation for OCCasional loads:

Radial Load P 1708.0 N



Circumferential Moment MC -1025.2 N-m

Longitudinal Moment ML -2588.3 N-m





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

| Stress Values at

Type of | (MPa )

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


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

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

Circ. Bend. P | -1 1 -1 1 -2 2 -2 2

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

Circ. Bend. MC | 0 0 0 0 40 -40 -40 40

Circ. Memb. ML | 12 12 -12 -12 0 0 0 0

Circ. Bend. ML | 25 -25 -25 25 0 0 0 0

|

Tot. Circ. Str.| 35.8 -11.9 -41.4 13.6 38.5 -36.9 -45.5 41.3

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

71

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 Long. Memb. P | 0 0 0 0 0 0 0 0

Long. Bend. P | -2 2 -2 2 -1 1 -1 1

Long. Memb. MC | 0 0 0 0 4 4 -4 -4

Long. Bend. MC | 0 0 0 0 15 -15 -15 15

Long. Memb. ML | 9 9 -9 -9 0 0 0 0

Long. Bend. ML | 34 -34 -34 34 0 0 0 0

|

Tot. Long. Str.| 41.2 -23.2 -47.2 26.5 17.1 -10.0 -22.1 11.1

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

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. | 41.16 23.23 47.18 26.52 38.49 36.96 45.54 41.27

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

WARNING: Ratio of Pad Radius/Rm (0.755) is not between 0.01 and 0.571.



Stresses in the Vessel at the Edge of Reinforcing Pad

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

| Stress Values at

Type of | (MPa )

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


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

Circ. Memb. P | -3 -3 -3 -3 -1 -1 -1 -1

Circ. Bend. P | -2 2 -2 2 -11 11 -11 11

Circ. Memb. MC | 0 0 0 0 5 5 -5 -5

72

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 Circ. Bend. MC | 0 0 0 0 73 -73 -73 73

Circ. Memb. ML | 27 27 -27 -27 0 0 0 0

Circ. Bend. ML | 31 -31 -31 31 0 0 0 0

|

Tot. Circ. Str.| 52.4 -5.1 -65.4 3.8 65.8 -59.7 -92.0 77.9

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

Long. Memb. P | -1 -1 -1 -1 -3 -3 -3 -3

Long. Bend. P | -5 5 -5 5 -6 6 -6 6

Long. Memb. MC | 0 0 0 0 16 16 -16 -16

Long. Bend. MC | 0 0 0 0 28 -28 -28 28

Long. Memb. ML | 20 20 -20 -20 0 0 0 0

Long. Bend. ML | 51 -51 -51 51 0 0 0 0

|

Tot. Long. Str.| 63.6 -27.6 -79.6 35.6 35.7 -9.7 -55.0 14.7

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

Shear VC | 0 0 0 0 0 0 0 0

Shear VL | 0 0 0 0 -1 -1 1 1

Shear MT | 0 0 0 0 0 0 0 0

|

Tot. Shear| 0.0 0.0 0.0 0.0 -1.0 -1.0 1.0 1.0

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

Str. Int. | 63.63 27.60 79.59 35.59 65.87 59.76 92.01 77.94

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

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

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

73

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 Circ. Pm (SUS) | 11 13 11 13 11 13 11 13

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

Circ. Pm(TOTAL)| 11.3 13.1 11.3 13.1 11.3 13.1 11.3 13.1

Circ. Pl (SUS) | 21 21 -21 -21 0 0 0 0

Circ. Pl (OCC) | 11 11 -13 -13 0 0 -2 -2

Circ. Pl(TOTAL)| 33.6 33.6 -35.6 -35.6 0.8 0.8 -2.1 -2.1

Circ. Q (SUS) | 43 -43 -43 43 0 0 0 0

Circ. Q (OCC) | 23 -23 -27 27 37 -37 -43 43

Circ. Q (TOTAL)| 67.0 -67.0 -70.7 70.7 37.7 -37.7 -43.4 43.4

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

Long. Pm (SUS) | 5 5 5 5 5 5 5 5

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

Long. Pm(TOTAL)| 5.7 5.7 5.7 5.7 5.7 5.7 5.7 5.7

Long. Pl (SUS) | 16 16 -16 -16 0 0 0 0

Long. Pl (OCC) | 8 8 -10 -10 3 3 -5 -5

Long. Pl(TOTAL)| 25.2 25.2 -26.5 -26.5 3.5 3.5 -5.5 -5.5

Long. Q (SUS) | 58 -58 -58 58 0 0 0 0

Long. Q (OCC) | 32 -32 -36 36 13 -13 -16 16

Long. Q (TOTAL)| 90.2 -90.2 -94.9 94.9 13.6 -13.6 -16.6 16.6

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

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 -1 -1 1 1

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

Shear Pl(TOTAL)| 0.0 0.0 0.0 0.0 -1.9 -1.9 1.9 1.9

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

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

Pm (SUS) | 11.3 13.1 11.3 13.1 11.3 13.1 11.3 13.1

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

Pm (SUS+OCC) | 11.3 13.1 11.3 13.1 11.3 13.1 11.3 13.1

74

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 ------------------------------------------------------------------------

Pm+Pl (SUS) | 33.0 34.8 10.5 10.5 11.6 13.3 11.6 13.3

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

Pm+Pl (SUS+OCC)| 45.0 46.8 24.3 22.5 13.0 14.6 9.8 11.5

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

Pm+Pl+Q (Total)| 121.0 59.4 115.7 74.0 49.9 24.0 34.4 54.5

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

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

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

Stress Int. | MPa |

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

Pm (SUS) | 13.12 115.15 | Passed

Pm (SUS+OCC) | 13.12 138.18 | Passed

Pm+Pl (SUS) | 34.84 172.72 | Passed

Pm+Pl (SUS+OCC)| 46.77 207.26 | Passed

Pm+Pl+Q (TOTAL)| 121.04 345.44 | Passed

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


Vessel Stress Summation at Reinforcing Pad Edge

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



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


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

Circ. Pm (SUS) | 24 26 24 26 24 26 24 26

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

Circ. Pm(TOTAL)| 24.9 26.7 24.9 26.7 24.9 26.7 24.9 26.7

Circ. Pl (SUS) | 45 45 -45 -45 0 0 0 0

Circ. Pl (OCC) | 23 23 -30 -30 3 3 -7 -7

75

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 Circ. Pl(TOTAL)| 69.4 69.4 -76.6 -76.6 3.0 3.0 -7.0 -7.0

Circ. Q (SUS) | 53 -53 -53 53 0 0 0 0

Circ. Q (OCC) | 28 -28 -34 34 62 -62 -84 84

Circ. Q (TOTAL)| 81.9 -81.9 -87.8 87.8 62.8 -62.8 -85.0 85.0

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

Long. Pm (SUS) | 12 12 12 12 12 12 12 12

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

Long. Pm(TOTAL)| 12.4 12.4 12.4 12.4 12.4 12.4 12.4 12.4

Long. Pl (SUS) | 33 33 -33 -33 0 0 0 0

Long. Pl (OCC) | 18 18 -22 -22 12 12 -20 -20

Long. Pl(TOTAL)| 51.6 51.6 -55.6 -55.6 13.0 13.0 -20.2 -20.2

Long. Q (SUS) | 86 -86 -86 86 0 0 0 0

Long. Q (OCC) | 45 -45 -57 57 22 -22 -34 34

Long. Q (TOTAL)| 132.3 -132.3 -144.3 144.3 22.7 -22.7 -34.8 34.8

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

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 -1 -1 1 1

Shear Pl (OCC) | 0 0 0 0 -1 -1 1 1

Shear Pl(TOTAL)| 0.0 0.0 0.0 0.0 -2.7 -2.7 2.7 2.7

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) | 24.9 26.7 24.9 26.7 24.9 26.7 24.9 26.7

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

Pm (SUS+OCC) | 24.9 26.7 24.9 26.7 24.9 26.7 24.9 26.7

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

Pm+Pl (SUS) | 70.7 72.5 21.2 21.2 25.1 26.9 25.1 26.9

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

Pm+Pl (SUS+OCC)| 94.3 96.1 51.7 49.9 29.7 31.0 26.1 27.9

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

76

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 Pm+Pl+Q (Total)| 196.4 82.5 187.5 101.1 90.9 36.2 67.4 104.7

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

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


Stress Int. | MPa |

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

Pm (SUS) | 26.69 115.15 | Passed

Pm (SUS+OCC) | 26.69 138.18 | Passed

Pm+Pl (SUS) | 72.47 172.72 | Passed

Pm+Pl (SUS+OCC)| 96.13 207.26 | Passed


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


77

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N3 Nozl: 23 1:14p Jan 11,2015

INPUT VALUES, Nozzle Description: N3 From : 10

Pressure for Reinforcement Calculations P 18.347 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-403 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 204.76 mm

Aspect Ratio of Elliptical Head Ar 2.00

Head Finished (Minimum) Thickness t 7.1565 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.

78


Size and Thickness Basis Nominal

Nominal Thickness tn 80S

Flange Material SA-182 F316

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 150.0000 mm

Weld leg size between Nozzle and Pad/Shell Wo 6.0000 mm

Groove weld depth between Nozzle and Vessel Wgnv 7.1564 mm

Inside Projection h 0.0000 mm

Weld leg size, Inside Element to Shell Wi 0.0000 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)

| |

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| \ | |

| \ | |

|____________\|__|

79


Insert Nozzle No Pad, no Inside projection

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)

= (18.35*0.900*204.7621)/(2 *115.15*1.00-0.2*18.35)

= 1.4707 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)

= (18.35*30.1625)/(115*1.00+0.4*18.35)

= 0.4776 mm

Required Nozzle thickness under External Pressure per UG-28 : 0.2876 mm

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), no pad Tlnp 13.8430 mm

Note:

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

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

80

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N3 Nozl: 23 1:14p Jan 11,2015 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 = 0.4776 mm

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

Wall Thickness, shell/head, internal pressure trb1 = 1.6342 mm

Wall Thickness tb1 = max(trb1, tr16b) = 1.6342 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( 1.634 , 1.500 ) ]

= 1.6342 mm

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

= max( ta, tb )

= max( 0.4776 , 1.6342 )

= 1.6342 mm

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

SA-403 316L, 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

81


Results Per UW-16.1:

Required Thickness Actual Thickness

Nozzle Weld 3.8760 = 0.7 * tmin. 4.2420 = 0.7 * Wo 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.

Maximum Allowable Pressure for this Nozzle at this Location:

Converged Max. Allow. Pressure in Operating case 79.866 bar

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

The Drop for this Nozzle is : 2.4093 mm

The Cut Length for this Nozzle is, Drop + Ho + H + T : 159.5657 mm


82







Shell Material SA-312 TP316L



Inside Diameter of Cylindrical Shell D 202.72 mm

Design Length of Section L 3192.0637 mm

Shell Finished (Minimum) Thickness t 7.1565 mm

Shell Internal Corrosion Allowance c 0.0000 mm

Shell External Corrosion Allowance co 0.0000 mm

Distance from Bottom/Left Tangent 1255.0001 mm



Material SA-182 F316


Material Specification/Type Forgings



Diameter Basis (for tr calc only) ID


Diameter 2.0000 in.

83


Size and Thickness Basis Actual

Actual Thickness tn 13.4620 mm


Flange Type Long Weld Neck














| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

84





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)

= (18.35*101.3587)/(115*1.00-0.6*18.35)

= 1.6309 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([18.35/(137.90*1.00]-1)

= 0.3402 mm






Note:



85















= min[ 4.800 , max( 1.631 , 1.500 ) ]

= 1.6309 mm


= max( ta, tb )

= max( 0.3761 , 1.6309 )

= 1.6309 mm

Available Nozzle Neck Thickness = 13.4620 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 : 15.2, Allowable : 137.9 MPa Passed

Expansion : 0.0, Allowable : 329.5 MPa Passed

Occasional : 1.4, Allowable : 183.4 MPa Passed

Shear : 8.3, Allowable : 96.5 MPa Passed

86

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N1 Nozl: 24 1:14p Jan 11,2015 Note : The number of cycles on this nozzle was assumed to be 7000 or less for

the determination of the expansion stress allowable.


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














Input Echo, WRC107/537 Item 1, Description: N1 :





87

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N1 Nozl: 24 1:14p Jan 11,2015 Vessel Thickness Tv 7.156 mm

Design Temperature -195.57 °C

Vessel Material SA-312 TP316L

Vessel Cold S.I. Allowable Smc 115.15 MPa

Vessel Hot S.I. Allowable Smh 115.15 MPa

Attachment Type Type Round

Diameter Basis for Nozzle Nbasis ID

Corrosion Allowance for Nozzle Can 0.0000 mm

Nozzle Diameter Dn 50.800 mm

Nozzle Thickness Tn 13.462 mm

Nozzle Material SA-182 F316

Nozzle Cold S.I. Allowable SNmc 137.90 MPa

Nozzle Hot S.I. Allowable SNmh 137.90 MPa



External Forces and Moments in WRC 107/537 Convention:

Radial Load (SUS) P -1040.0 N

Longitudinal Shear (SUS) Vl 1040.0 N

Circumferential Shear (SUS) Vc 1040.0 N

Circumferential Moment (SUS) Mc 380.0 N-m

Longitudinal Moment (SUS) Ml 380.0 N-m

Torsional Moment (SUS) Mt 380.0 N-m




88

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N1 Nozl: 24 1:14p Jan 11,2015 Compute Pressure Stress per WRC-368 No


Radial Load P -1040.0 N




Longitudinal Moment ML 380.0 N-m




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


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

N(PHI) / ( P/Rm ) 0.324 4C 2.100 (A,B)

N(PHI) / ( P/Rm ) 0.324 3C 1.445 (C,D)

M(PHI) / ( P ) 0.324 2C1 0.034 (A,B)

M(PHI) / ( P ) 0.324 1C 0.058 (C,D)

N(PHI) / ( MC/(Rm**2 * Beta) ) 0.324 3A 0.631 (A,B,C,D)


N(PHI) / ( ML/(Rm**2 * Beta) ) 0.324 3B 1.569 (A,B,C,D)

M(PHI) / ( ML/(Rm * Beta) ) 0.324 1B 0.025 (A,B,C,D)

N(x) / ( P/Rm ) 0.324 3C 1.445 (A,B)

N(x) / ( P/Rm ) 0.324 4C 2.100 (C,D)

M(x) / ( P ) 0.324 1C1 0.059 (A,B)

M(x) / ( P ) 0.324 2C 0.033 (C,D)

N(x) / ( MC/(Rm**2 * Beta) ) 0.324 4A 1.280 (A,B,C,D)

M(x) / ( MC/(Rm * Beta) ) 0.324 2A 0.039 (A,B,C,D)

N(x) / ( ML/(Rm**2 * Beta) ) 0.324 4B 0.614 (A,B,C,D)

M(x) / ( ML/(Rm * Beta) ) 0.324 2B 0.042 (A,B,C,D)

89




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

| Stress Values at

Type of | (MPa )

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


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

Circ. Memb. P | 2 2 2 2 2 2 2 2

Circ. Bend. P | 4 -4 4 -4 7 -7 7 -7

Circ. Memb. MC | 0 0 0 0 -9 -9 9 9

Circ. Bend. MC | 0 0 0 0 -105 105 105 -105

Circ. Memb. ML | -23 -23 23 23 0 0 0 0

Circ. Bend. ML | -32 32 32 -32 0 0 0 0

|

Tot. Circ. Str.| -49.0 8.2 63.0 -10.5 -106.2 91.5 124.4 -101.6

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

Long. Memb. P | 2 2 2 2 2 2 2 2

Long. Bend. P | 7 -7 7 -7 4 -4 4 -4

Long. Memb. MC | 0 0 0 0 -19 -19 19 19

Long. Bend. MC | 0 0 0 0 -51 51 51 -51

Long. Memb. ML | -9 -9 9 9 0 0 0 0

Long. Bend. ML | -55 55 55 -55 0 0 0 0

|

Tot. Long. Str.| -55.5 41.2 73.8 -51.5 -63.2 31.0 77.1 -33.2

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

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

|

90

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N1 Nozl: 24 1:14p Jan 11,2015 Tot. Shear| 6.8 6.8 4.4 4.4 4.4 4.4 6.8 6.8

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

Str. Int. | 59.77 42.56 75.36 51.99 106.69 91.80 125.36 102.30

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



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



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


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

Circ. Pm (SUS) | 25 26 25 26 25 26 25 26

Circ. Pl (SUS) | -20 -20 26 26 -7 -7 11 11

Circ. Q (SUS) | -28 28 36 -36 -98 98 113 -113

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

Long. Pm (SUS) | 12 12 12 12 12 12 12 12

Long. Pl (SUS) | -7 -7 11 11 -16 -16 21 21

Long. Q (SUS) | -48 48 62 -62 -47 47 55 -55

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

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) | 25.1 26.9 25.1 26.9 25.1 26.9 25.1 26.9

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

Pm+Pl (SUS) | 6.3 7.3 51.4 53.2 21.4 23.3 37.0 38.7

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

Pm+Pl+Q (Total)| 45.1 56.0 91.7 56.1 81.8 118.7 150.3 75.5

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

91

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N1 Nozl: 24 1:14p Jan 11,2015 ------------------------------------------------------------------------


Stress Int. | MPa |

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

Pm (SUS) | 26.94 115.15 | Passed

Pm+Pl (SUS) | 53.24 172.72 | Passed


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


92

























Diameter 2.0000 in.

93



















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____________/| |

| \ | |

| \ | |

|____________\|__|

94









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

= (18.35*101.3587)/(115*1.00-0.6*18.35)

= 1.6309 mm



= 25.400(exp([18.35/(137.90*1.00]-1)

= 0.3402 mm






Note:



95















= min[ 4.800 , max( 1.631 , 1.500 ) ]

= 1.6309 mm


= max( ta, tb )

= max( 0.3761 , 1.6309 )

= 1.6309 mm








96























97


























98











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


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

N(PHI) / ( P/Rm ) 0.324 4C 2.100 (A,B)

N(PHI) / ( P/Rm ) 0.324 3C 1.445 (C,D)

M(PHI) / ( P ) 0.324 2C1 0.034 (A,B)

M(PHI) / ( P ) 0.324 1C 0.058 (C,D)





N(x) / ( P/Rm ) 0.324 3C 1.445 (A,B)

N(x) / ( P/Rm ) 0.324 4C 2.100 (C,D)

M(x) / ( P ) 0.324 1C1 0.059 (A,B)

M(x) / ( P ) 0.324 2C 0.033 (C,D)





99




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

| Stress Values at

Type of | (MPa )

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


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

Circ. Memb. P | 2 2 2 2 2 2 2 2

Circ. Bend. P | 4 -4 4 -4 7 -7 7 -7

Circ. Memb. MC | 0 0 0 0 -9 -9 9 9

Circ. Bend. MC | 0 0 0 0 -105 105 105 -105

Circ. Memb. ML | -23 -23 23 23 0 0 0 0

Circ. Bend. ML | -32 32 32 -32 0 0 0 0

|

Tot. Circ. Str.| -49.0 8.2 63.0 -10.5 -106.2 91.5 124.4 -101.6

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

Long. Memb. P | 2 2 2 2 2 2 2 2

Long. Bend. P | 7 -7 7 -7 4 -4 4 -4

Long. Memb. MC | 0 0 0 0 -19 -19 19 19

Long. Bend. MC | 0 0 0 0 -51 51 51 -51

Long. Memb. ML | -9 -9 9 9 0 0 0 0

Long. Bend. ML | -55 55 55 -55 0 0 0 0

|

Tot. Long. Str.| -55.5 41.2 73.8 -51.5 -63.2 31.0 77.1 -33.2

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

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

|

100


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

Str. Int. | 59.77 42.56 75.36 51.99 106.69 91.80 125.36 102.30

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



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



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


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

Circ. Pm (SUS) | 25 26 25 26 25 26 25 26

Circ. Pl (SUS) | -20 -20 26 26 -7 -7 11 11

Circ. Q (SUS) | -28 28 36 -36 -98 98 113 -113

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

Long. Pm (SUS) | 12 12 12 12 12 12 12 12

Long. Pl (SUS) | -7 -7 11 11 -16 -16 21 21

Long. Q (SUS) | -48 48 62 -62 -47 47 55 -55

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

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) | 25.1 26.9 25.1 26.9 25.1 26.9 25.1 26.9

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

Pm+Pl (SUS) | 6.3 7.3 51.4 53.2 21.4 23.3 37.0 38.7

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

Pm+Pl+Q (Total)| 45.1 56.0 91.7 56.1 81.8 118.7 150.3 75.5

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

101



Stress Int. | MPa |

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

Pm (SUS) | 26.94 115.15 | Passed

Pm+Pl (SUS) | 53.24 172.72 | Passed


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


102

























Diameter 2.0000 in.

103



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

104









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

= (18.35*101.3587)/(115*1.00-0.6*18.35)

= 1.6309 mm



= 25.400(exp([18.35/(137.90*1.00]-1)

= 0.3402 mm






Note:



105















= min[ 4.800 , max( 1.631 , 1.500 ) ]

= 1.6309 mm


= max( ta, tb )

= max( 0.3761 , 1.6309 )

= 1.6309 mm








106























107


























108











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


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

N(PHI) / ( P/Rm ) 0.324 4C 2.100 (A,B)

N(PHI) / ( P/Rm ) 0.324 3C 1.445 (C,D)

M(PHI) / ( P ) 0.324 2C1 0.034 (A,B)

M(PHI) / ( P ) 0.324 1C 0.058 (C,D)





N(x) / ( P/Rm ) 0.324 3C 1.445 (A,B)

N(x) / ( P/Rm ) 0.324 4C 2.100 (C,D)

M(x) / ( P ) 0.324 1C1 0.059 (A,B)

M(x) / ( P ) 0.324 2C 0.033 (C,D)





109




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

| Stress Values at

Type of | (MPa )

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


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

Circ. Memb. P | 2 2 2 2 2 2 2 2

Circ. Bend. P | 4 -4 4 -4 7 -7 7 -7

Circ. Memb. MC | 0 0 0 0 -9 -9 9 9

Circ. Bend. MC | 0 0 0 0 -105 105 105 -105

Circ. Memb. ML | -23 -23 23 23 0 0 0 0

Circ. Bend. ML | -32 32 32 -32 0 0 0 0

|

Tot. Circ. Str.| -49.0 8.2 63.0 -10.5 -106.2 91.5 124.4 -101.6

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

Long. Memb. P | 2 2 2 2 2 2 2 2

Long. Bend. P | 7 -7 7 -7 4 -4 4 -4

Long. Memb. MC | 0 0 0 0 -19 -19 19 19

Long. Bend. MC | 0 0 0 0 -51 51 51 -51

Long. Memb. ML | -9 -9 9 9 0 0 0 0

Long. Bend. ML | -55 55 55 -55 0 0 0 0

|

Tot. Long. Str.| -55.5 41.2 73.8 -51.5 -63.2 31.0 77.1 -33.2

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

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

|

110


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

Str. Int. | 59.77 42.56 75.36 51.99 106.69 91.80 125.36 102.30

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



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



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


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

Circ. Pm (SUS) | 25 26 25 26 25 26 25 26

Circ. Pl (SUS) | -20 -20 26 26 -7 -7 11 11

Circ. Q (SUS) | -28 28 36 -36 -98 98 113 -113

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

Long. Pm (SUS) | 12 12 12 12 12 12 12 12

Long. Pl (SUS) | -7 -7 11 11 -16 -16 21 21

Long. Q (SUS) | -48 48 62 -62 -47 47 55 -55

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

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) | 25.1 26.9 25.1 26.9 25.1 26.9 25.1 26.9

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

Pm+Pl (SUS) | 6.3 7.3 51.4 53.2 21.4 23.3 37.0 38.7

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

Pm+Pl+Q (Total)| 45.1 56.0 91.7 56.1 81.8 118.7 150.3 75.5

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

111



Stress Int. | MPa |

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

Pm (SUS) | 26.94 115.15 | Passed

Pm+Pl (SUS) | 53.24 172.72 | Passed


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


112

























Diameter 2.0000 in.

113



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

114









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

= (18.35*101.3587)/(115*1.00-0.6*18.35)

= 1.6309 mm



= 25.400(exp([18.35/(137.90*1.00]-1)

= 0.3402 mm






Note:



115















= min[ 4.800 , max( 1.631 , 1.500 ) ]

= 1.6309 mm


= max( ta, tb )

= max( 0.3761 , 1.6309 )

= 1.6309 mm








116























117


























118











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


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

N(PHI) / ( P/Rm ) 0.324 4C 2.100 (A,B)

N(PHI) / ( P/Rm ) 0.324 3C 1.445 (C,D)

M(PHI) / ( P ) 0.324 2C1 0.034 (A,B)

M(PHI) / ( P ) 0.324 1C 0.058 (C,D)





N(x) / ( P/Rm ) 0.324 3C 1.445 (A,B)

N(x) / ( P/Rm ) 0.324 4C 2.100 (C,D)

M(x) / ( P ) 0.324 1C1 0.059 (A,B)

M(x) / ( P ) 0.324 2C 0.033 (C,D)





119




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

| Stress Values at

Type of | (MPa )

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


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

Circ. Memb. P | 2 2 2 2 2 2 2 2

Circ. Bend. P | 4 -4 4 -4 7 -7 7 -7

Circ. Memb. MC | 0 0 0 0 -9 -9 9 9

Circ. Bend. MC | 0 0 0 0 -105 105 105 -105

Circ. Memb. ML | -23 -23 23 23 0 0 0 0

Circ. Bend. ML | -32 32 32 -32 0 0 0 0

|

Tot. Circ. Str.| -49.0 8.2 63.0 -10.5 -106.2 91.5 124.4 -101.6

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

Long. Memb. P | 2 2 2 2 2 2 2 2

Long. Bend. P | 7 -7 7 -7 4 -4 4 -4

Long. Memb. MC | 0 0 0 0 -19 -19 19 19

Long. Bend. MC | 0 0 0 0 -51 51 51 -51

Long. Memb. ML | -9 -9 9 9 0 0 0 0

Long. Bend. ML | -55 55 55 -55 0 0 0 0

|

Tot. Long. Str.| -55.5 41.2 73.8 -51.5 -63.2 31.0 77.1 -33.2

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

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

|

120


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

Str. Int. | 59.77 42.56 75.36 51.99 106.69 91.80 125.36 102.30

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



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



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


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

Circ. Pm (SUS) | 25 26 25 26 25 26 25 26

Circ. Pl (SUS) | -20 -20 26 26 -7 -7 11 11

Circ. Q (SUS) | -28 28 36 -36 -98 98 113 -113

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

Long. Pm (SUS) | 12 12 12 12 12 12 12 12

Long. Pl (SUS) | -7 -7 11 11 -16 -16 21 21

Long. Q (SUS) | -48 48 62 -62 -47 47 55 -55

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

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) | 25.1 26.9 25.1 26.9 25.1 26.9 25.1 26.9

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

Pm+Pl (SUS) | 6.3 7.3 51.4 53.2 21.4 23.3 37.0 38.7

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

Pm+Pl+Q (Total)| 45.1 56.0 91.7 56.1 81.8 118.7 150.3 75.5

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

121



Stress Int. | MPa |

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

Pm (SUS) | 26.94 115.15 | Passed

Pm+Pl (SUS) | 53.24 172.72 | Passed


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


122

























Diameter 2.0000 in.

123



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

124









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

= (18.35*101.3587)/(115*1.00-0.6*18.35)

= 1.6309 mm



= 25.400(exp([18.35/(137.90*1.00]-1)

= 0.3402 mm






Note:



125















= min[ 4.800 , max( 1.631 , 1.500 ) ]

= 1.6309 mm


= max( ta, tb )

= max( 0.3761 , 1.6309 )

= 1.6309 mm








126























127


























128











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


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

N(PHI) / ( P/Rm ) 0.324 4C 2.100 (A,B)

N(PHI) / ( P/Rm ) 0.324 3C 1.445 (C,D)

M(PHI) / ( P ) 0.324 2C1 0.034 (A,B)

M(PHI) / ( P ) 0.324 1C 0.058 (C,D)





N(x) / ( P/Rm ) 0.324 3C 1.445 (A,B)

N(x) / ( P/Rm ) 0.324 4C 2.100 (C,D)

M(x) / ( P ) 0.324 1C1 0.059 (A,B)

M(x) / ( P ) 0.324 2C 0.033 (C,D)





129




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

| Stress Values at

Type of | (MPa )

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


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

Circ. Memb. P | 2 2 2 2 2 2 2 2

Circ. Bend. P | 4 -4 4 -4 7 -7 7 -7

Circ. Memb. MC | 0 0 0 0 -9 -9 9 9

Circ. Bend. MC | 0 0 0 0 -105 105 105 -105

Circ. Memb. ML | -23 -23 23 23 0 0 0 0

Circ. Bend. ML | -32 32 32 -32 0 0 0 0

|

Tot. Circ. Str.| -49.0 8.2 63.0 -10.5 -106.2 91.5 124.4 -101.6

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

Long. Memb. P | 2 2 2 2 2 2 2 2

Long. Bend. P | 7 -7 7 -7 4 -4 4 -4

Long. Memb. MC | 0 0 0 0 -19 -19 19 19

Long. Bend. MC | 0 0 0 0 -51 51 51 -51

Long. Memb. ML | -9 -9 9 9 0 0 0 0

Long. Bend. ML | -55 55 55 -55 0 0 0 0

|

Tot. Long. Str.| -55.5 41.2 73.8 -51.5 -63.2 31.0 77.1 -33.2

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

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

|

130


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

Str. Int. | 59.77 42.56 75.36 51.99 106.69 91.80 125.36 102.30

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



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



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


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

Circ. Pm (SUS) | 25 26 25 26 25 26 25 26

Circ. Pl (SUS) | -20 -20 26 26 -7 -7 11 11

Circ. Q (SUS) | -28 28 36 -36 -98 98 113 -113

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

Long. Pm (SUS) | 12 12 12 12 12 12 12 12

Long. Pl (SUS) | -7 -7 11 11 -16 -16 21 21

Long. Q (SUS) | -48 48 62 -62 -47 47 55 -55

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

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) | 25.1 26.9 25.1 26.9 25.1 26.9 25.1 26.9

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

Pm+Pl (SUS) | 6.3 7.3 51.4 53.2 21.4 23.3 37.0 38.7

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

Pm+Pl+Q (Total)| 45.1 56.0 91.7 56.1 81.8 118.7 150.3 75.5

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

131



Stress Int. | MPa |

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

Pm (SUS) | 26.94 115.15 | Passed

Pm+Pl (SUS) | 53.24 172.72 | Passed


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


132

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K1A Nozl: 29 1:14p Jan 11,2015

INPUT VALUES, Nozzle Description: K1A From : 20























Diameter 3.0000 in.

133



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

134



Reinforcement CALCULATION, Description: K1A






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

= (18.35*101.3587)/(115*1.00-0.6*18.35)

= 1.6309 mm



= (18.35*44.4500)/(115*1.00+0.4*18.35)

= 0.7039 mm






Note:

Taking a UG-36(c)(3)(a) exemption for nozzle: K1A.


135

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K1A Nozl: 29 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles














= min[ 4.800 , max( 1.631 , 1.500 ) ]

= 1.6309 mm


= max( ta, tb )

= max( 0.7039 , 1.6309 )

= 1.6309 mm



Weld Size Calculations, Description: K1A



136

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K1A Nozl: 29 1:14p Jan 11,2015 Required Thickness Actual Thickness











137

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K1B Nozl: 30 1:14p Jan 11,2015

INPUT VALUES, Nozzle Description: K1B From : 20























Diameter 3.0000 in.

138



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

139



Reinforcement CALCULATION, Description: K1B






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

= (18.35*101.3587)/(115*1.00-0.6*18.35)

= 1.6309 mm



= (18.35*44.4500)/(115*1.00+0.4*18.35)

= 0.7039 mm






Note:

Taking a UG-36(c)(3)(a) exemption for nozzle: K1B.


140

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K1B Nozl: 30 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles














= min[ 4.800 , max( 1.631 , 1.500 ) ]

= 1.6309 mm


= max( ta, tb )

= max( 0.7039 , 1.6309 )

= 1.6309 mm



Weld Size Calculations, Description: K1B



141

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K1B Nozl: 30 1:14p Jan 11,2015 Required Thickness Actual Thickness











142

























Diameter 2.0000 in.

143



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

144









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

= (18.35*101.3587)/(115*1.00-0.6*18.35)

= 1.6309 mm



= 25.400(exp([18.35/(137.90*1.00]-1)

= 0.3402 mm






Note:



145















= min[ 4.800 , max( 1.631 , 1.500 ) ]

= 1.6309 mm


= max( ta, tb )

= max( 0.3761 , 1.6309 )

= 1.6309 mm






146














147

























Diameter 2.0000 in.

148



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

149









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

= (18.35*101.3587)/(115*1.00-0.6*18.35)

= 1.6309 mm



= 25.400(exp([18.35/(137.90*1.00]-1)

= 0.3402 mm






Note:



150















= min[ 4.800 , max( 1.631 , 1.500 ) ]

= 1.6309 mm


= max( ta, tb )

= max( 0.3761 , 1.6309 )

= 1.6309 mm






151














152

























Diameter 3.0000 in.

153



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

154









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

= (18.35*101.3587)/(115*1.00-0.6*18.35)

= 1.6309 mm



= (18.35*44.4500)/(115*1.00+0.4*18.35)

= 0.7039 mm






Note:



155















= min[ 4.800 , max( 1.631 , 1.500 ) ]

= 1.6309 mm


= max( ta, tb )

= max( 0.7039 , 1.6309 )

= 1.6309 mm






156












157

























Diameter 3.0000 in.

158



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

159









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

= (18.35*101.3587)/(115*1.00-0.6*18.35)

= 1.6309 mm



= (18.35*44.4500)/(115*1.00+0.4*18.35)

= 0.7039 mm






Note:



160















= min[ 4.800 , max( 1.631 , 1.500 ) ]

= 1.6309 mm


= max( ta, tb )

= max( 0.7039 , 1.6309 )

= 1.6309 mm






161












162

























Diameter 3.0000 in.

163



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

164









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

= (18.35*101.3587)/(115*1.00-0.6*18.35)

= 1.6309 mm



= (18.35*44.4500)/(115*1.00+0.4*18.35)

= 0.7039 mm






Note:



165















= min[ 4.800 , max( 1.631 , 1.500 ) ]

= 1.6309 mm


= max( ta, tb )

= max( 0.7039 , 1.6309 )

= 1.6309 mm






166












167

























Diameter 3.0000 in.

168



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

169









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

= (18.35*101.3587)/(115*1.00-0.6*18.35)

= 1.6309 mm



= (18.35*44.4500)/(115*1.00+0.4*18.35)

= 0.7039 mm






Note:



170















= min[ 4.800 , max( 1.631 , 1.500 ) ]

= 1.6309 mm


= max( ta, tb )

= max( 0.7039 , 1.6309 )

= 1.6309 mm






171












172

























Diameter 2.0000 in.

173



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

174









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

= (18.35*101.3587)/(115*1.00-0.6*18.35)

= 1.6309 mm



= 25.400(exp([18.35/(137.90*1.00]-1)

= 0.3402 mm






Note:



175















= min[ 4.800 , max( 1.631 , 1.500 ) ]

= 1.6309 mm


= max( ta, tb )

= max( 0.3761 , 1.6309 )

= 1.6309 mm






176














177

























Diameter 2.0000 in.

178



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

179









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

= (18.35*101.3587)/(115*1.00-0.6*18.35)

= 1.6309 mm



= 25.400(exp([18.35/(137.90*1.00]-1)

= 0.3402 mm






Note:



180















= min[ 4.800 , max( 1.631 , 1.500 ) ]

= 1.6309 mm


= max( ta, tb )

= max( 0.3761 , 1.6309 )

= 1.6309 mm






181














182

























Diameter 3.0000 in.

183



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

184









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

= (18.35*101.3587)/(115*1.00-0.6*18.35)

= 1.6309 mm



= (18.35*44.4500)/(115*1.00+0.4*18.35)

= 0.7039 mm






Note:



185















= min[ 4.800 , max( 1.631 , 1.500 ) ]

= 1.6309 mm


= max( ta, tb )

= max( 0.7039 , 1.6309 )

= 1.6309 mm






186












187

























Diameter 3.0000 in.

188



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

189









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

= (18.35*101.3587)/(115*1.00-0.6*18.35)

= 1.6309 mm



= (18.35*44.4500)/(115*1.00+0.4*18.35)

= 0.7039 mm






Note:



190















= min[ 4.800 , max( 1.631 , 1.500 ) ]

= 1.6309 mm


= max( ta, tb )

= max( 0.7039 , 1.6309 )

= 1.6309 mm






191












192

























Diameter 3.0000 in.

193



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

194









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

= (18.35*101.3587)/(115*1.00-0.6*18.35)

= 1.6309 mm



= (18.35*44.4500)/(115*1.00+0.4*18.35)

= 0.7039 mm






Note:



195















= min[ 4.800 , max( 1.631 , 1.500 ) ]

= 1.6309 mm


= max( ta, tb )

= max( 0.7039 , 1.6309 )

= 1.6309 mm






196












197

























Diameter 3.0000 in.

198



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

199









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

= (18.35*101.3587)/(115*1.00-0.6*18.35)

= 1.6309 mm



= (18.35*44.4500)/(115*1.00+0.4*18.35)

= 0.7039 mm






Note:



200















= min[ 4.800 , max( 1.631 , 1.500 ) ]

= 1.6309 mm


= max( ta, tb )

= max( 0.7039 , 1.6309 )

= 1.6309 mm






201












202

























Diameter 3.0000 in.

203



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

204









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

= (18.35*101.3587)/(115*1.00-0.6*18.35)

= 1.6309 mm



= (18.35*44.4500)/(115*1.00+0.4*18.35)

= 0.7039 mm






Note:



205















= min[ 4.800 , max( 1.631 , 1.500 ) ]

= 1.6309 mm


= max( ta, tb )

= max( 0.7039 , 1.6309 )

= 1.6309 mm






206












207

























Diameter 3.0000 in.

208



















| |

| |

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

209









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

= (18.35*101.3587)/(115*1.00-0.6*18.35)

= 1.6309 mm



= (18.35*44.4500)/(115*1.00+0.4*18.35)

= 0.7039 mm






Note:



210















= min[ 4.800 , max( 1.631 , 1.500 ) ]

= 1.6309 mm


= max( ta, tb )

= max( 0.7039 , 1.6309 )

= 1.6309 mm






211












212

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Schedule : Step: 42 1:14p 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 - - 159.57

N1 2.000 150 LWN 3.060 13.462 - - 214.90

N2 2.000 150 LWN 3.060 13.462 - - 214.90

N4 2.000 150 LWN 3.060 13.462 - - 214.90

N5 2.000 150 LWN 3.060 13.462 - - 214.90

N6 2.000 150 LWN 3.060 13.462 - - 214.90

K2A 2.000 150 LWN 3.060 13.462 - - 214.90

K2B 2.000 150 LWN 3.060 13.462 - - 214.90

K6A 2.000 150 LWN 3.060 13.462 - - 214.90

K6B 2.000 150 LWN 3.060 13.462 - - 214.90

K1A 3.000 80S WNF 3.500 7.620 - - 217.42

K1B 3.000 80S WNF 3.500 7.620 - - 217.42

K3A 3.000 80S WNF 3.500 7.620 - - 217.42

K3B 3.000 80S WNF 3.500 7.620 - - 217.42

K4A 3.000 80S WNF 3.500 7.620 - - 217.42

K4B 3.000 80S WNF 3.500 7.620 - - 217.42

K7A 3.000 80S WNF 3.500 7.620 - - 217.42

K7B 3.000 80S WNF 3.500 7.620 - - 217.42

K8A 3.000 80S WNF 3.500 7.620 - - 217.42

K8B 3.000 80S WNF 3.500 7.620 - - 217.42

K5A 3.000 80S WNF 3.500 7.620 - - 217.42

K5B 3.000 80S WNF 3.500 7.620 - - 217.42

General Notes for the above table:

The Cut Length is the Outside Projection + Inside Projection + Drop +

213

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Schedule : Step: 42 1:14p Jan 11,2015 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

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 7.156 6.000 - - -

N1 SA-182 F316 7.156 9.000 - - -

N2 SA-182 F316 7.156 9.000 - - -

N4 SA-182 F316 7.156 9.000 - - -

N5 SA-182 F316 7.156 9.000 - - -

N6 SA-182 F316 7.156 9.000 - - -

K2A SA-182 F316 7.156 9.000 - - -

K2B SA-182 F316 7.156 9.000 - - -

K6A SA-182 F316 7.156 9.000 - - -

K6B SA-182 F316 7.156 9.000 - - -

K1A SA-312 TP316L 3.289 9.000 - - -

K1B SA-312 TP316L 7.156 9.000 - - -

K3A SA-312 TP316L 7.156 8.000 - - -

K3B SA-312 TP316L 7.156 8.000 - - -

K4A SA-312 TP316L 7.156 8.000 - - -

K4B SA-312 TP316L 7.156 8.000 - - -

K7A SA-312 TP316L 7.156 8.000 - - -

K7B SA-312 TP316L 7.156 8.000 - - -

214

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Schedule : Step: 42 1:14p Jan 11,2015 K8A SA-312 TP316L 7.156 8.000 - - -

K8B SA-312 TP316L 7.156 8.000 - - -

K5A SA-312 TP316L 7.156 8.000 - - -

K5B SA-312 TP316L 7.156 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

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

N3 90.00 150.00 0.00 Head

N1 1200.000 0.00 200.00 0.00 Shell

N2 2920.000 285.00 200.00 0.00 Shell

N4 1425.000 90.00 200.00 0.00 Shell

N5 3000.000 345.00 200.00 0.00 Shell

N6 200.000 90.00 200.00 0.00 Shell

K2A 1010.000 315.00 200.00 0.00 Shell

K2B 170.000 315.00 200.00 0.00 Shell

K6A 1895.000 340.00 200.00 0.00 Shell

K6B 1445.000 340.00 200.00 0.00 Shell

K1A 770.000 20.00 200.00 0.00 Shell

K1B 170.000 20.00 200.00 0.00 Shell

K3A 570.000 225.00 200.00 0.00 Shell

K3B 170.000 225.00 200.00 0.00 Shell

K4A 750.000 165.00 200.00 0.00 Shell

K4B 350.000 165.00 200.00 0.00 Shell

K7A 1795.000 225.00 200.00 0.00 Shell

K7B 1445.000 225.00 200.00 0.00 Shell

K8A 1950.000 165.00 200.00 0.00 Shell

K8B 1550.000 165.00 200.00 0.00 Shell

215

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Schedule : Step: 42 1:14p Jan 11,2015 K5A 1850.000 30.00 200.00 0.00 Shell

K5B 1500.000 30.00 200.00 0.00 Shell


216

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Summary : Step: 43 1:14p Jan 11,2015

Nozzle Calculation Summary:

Description MAWP Ext MAPNC UG45 [tr] Weld Areas or

bar bar Path Stresses

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

N3 79.87 ... ... OK 1.63 OK NoCalc[*]

N1 77.19 ... ... OK 1.63 OK NoCalc[*]

N2 77.19 ... ... OK 1.63 OK NoCalc[*]

N4 77.19 ... ... OK 1.63 OK NoCalc[*]

N5 77.19 ... ... OK 1.63 OK NoCalc[*]

N6 77.19 ... ... OK 1.63 OK NoCalc[*]

K1A 77.19 ... ... OK 1.63 OK NoCalc[*]

K1B 77.19 ... ... OK 1.63 OK NoCalc[*]

K2A 77.19 ... ... OK 1.63 OK NoCalc[*]

K2B 77.19 ... ... OK 1.63 OK NoCalc[*]

K3A 77.19 ... ... OK 1.63 OK NoCalc[*]

K3B 77.19 ... ... OK 1.63 OK NoCalc[*]

K4A 77.19 ... ... OK 1.63 OK NoCalc[*]

K4B 77.19 ... ... OK 1.63 OK NoCalc[*]

K6A 77.19 ... ... OK 1.63 OK NoCalc[*]

K6B 77.19 ... ... OK 1.63 OK NoCalc[*]

K7A 77.19 ... ... OK 1.63 OK NoCalc[*]

K7B 77.19 ... ... OK 1.63 OK NoCalc[*]

K8A 77.19 ... ... OK 1.63 OK NoCalc[*]

K8B 77.19 ... ... OK 1.63 OK NoCalc[*]

K5A 77.19 ... ... OK 1.63 OK NoCalc[*]

K5B 77.19 ... ... OK 1.63 OK NoCalc[*]

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

Min. - Nozzles 77.19 K5B

Min. Shell&Flgs 18.35

Computed Vessel M.A.W.P. 18.35 bar

217

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Summary : Step: 43 1:14p Jan 11,2015

[*] - 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

From Node Nozzle Description Y Coordinate, Layout Angle, Dia. Limit

10 N3 0.000 90.000 98.501

20 N1 1255.000 0.000 101.600

20 N2 2975.000 285.000 101.600

20 N4 1480.000 90.000 101.600

20 N5 3055.000 345.000 101.600

20 N6 255.000 90.000 101.600

20 K1A 825.000 20.000 147.320

20 K1B 225.000 20.000 147.320

20 K2A 1065.000 315.000 101.600

20 K2B 225.000 315.000 101.600

20 K3A 625.000 225.000 147.320

20 K3B 225.000 225.000 147.320

20 K4A 805.000 165.000 147.320

20 K4B 405.000 165.000 147.320

20 K6A 1950.000 340.000 101.600

20 K6B 1500.000 340.000 101.600

20 K7A 1850.000 225.000 147.320

20 K7B 1500.000 225.000 147.320

20 K8A 2005.000 165.000 147.320

20 K8B 1605.000 165.000 147.320

20 K5A 1905.000 30.000 147.320

20 K5B 1555.000 30.000 147.320

The nozzle spacing is computed by the following:

218

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Summary : Step: 43 1:14p Jan 11,2015 = 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.


219

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- MDMT Summary : Step: 44 1:14p 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

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

Head [16] -196

Shell [16] -196

N3 [15] -196

N1 [15] -196

N2 [15] -196

N4 [15] -196

N5 [15] -196

N6 [15] -196

K1A [15] -196

K1B [15] -196

K2A [15] -196

K2B [15] -196

K3A [15] -196

K3B [15] -196

K4A [15] -196

K4B [15] -196

K6A [15] -196

K6B [15] -196

K7A [15] -196

K7B [15] -196

K8A [15] -196

K8B [15] -196

K5A [15] -196

K5B [15] -196

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

Required Minimum Design Metal Temperature 0 °C

220

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- MDMT Summary : Step: 44 1:14p Jan 11,2015 Warmest Computed Minimum Design Metal Temperature -196 °C

Notes:

[ ! ] - This was an impact tested material.

[ 1] - Governing Nozzle Weld.

[ 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.


221

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Vessel Design Summary : Step: 45 1:14p Jan 11,2015 Design Code: ASME Code Section VIII Division 1, 2010, 2011a

Diameter Spec : 219.075 mm OD

Vessel Design Length, Tangent to Tangent 3305.05 mm

Distance of Bottom Tangent above Grade 0.00 mm

Specified Datum Line Distance 55.00 mm


Head Material SA-403 316L

Lug Material SA-240 316L


Nozzle Material SA-312 TP316L

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 18.347 bar

External Max. Allowable Working Pressure 28.681 bar

Hydrostatic Test Pressure 24.625 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

222

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Vessel Design Summary : Step: 45 1:14p Jan 11,2015 | + Stat. head | Pressure | | Allowance

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

Head 18.051 1.034 79.866 0.0000

Shell 18.051 1.034 77.185 0.0000

Body Flange (DN200) 18.000 1.034 18.398 0.0000

Blind Flange (DN200) 18.000 1.034 18.398 0.0000

Liquid Level: 650.00 mm Dens.: 803.232 kg/m³ Sp. Gr.: 0.804

Element "To" Elev Length Element Thk R e q d T h k Joint Eff

Type mm mm mm Int. Ext. Long Circ

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

Ellipse 0.0 55.0 8.2 1.7 1.5 1.00 1.00

Cylinder 3120.0 3120.0 8.2 1.7 1.9 1.00 1.00

Body Flg 3221.6 101.6 28.4 No Calc No Calc 1.00 1.00

Body Flg 3250.0 28.4 28.4 No Calc No Calc 1.00 1.00

Element thicknesses are shown as Nominal if specified, otherwise are Minimum

Total Wind Shear on Support 659. N

Total Earthquake Shear on Support 3416. N

Wind Moment on Support 656. N-m

Earthquake Moment on Support 3061. 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:

223

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Vessel Design Summary : Step: 45 1:14p Jan 11,2015 Fabricated - Bare W/O Removable Internals 388.1 kgm

Shop Test - Fabricated + Water ( Full ) 497.0 kgm

Shipping - Fab. + Rem. Intls.+ Shipping App. 388.1 kgm

Erected - Fab. + Rem. Intls.+ Insul. (etc) 388.1 kgm

Empty - Fab. + Intls. + Details + Wghts. 388.1 kgm

Operating - Empty + Operating Liquid (No CA) 521.2 kgm

Field Test - Empty Weight + Water (Full) 497.0 kgm


224

Attachment 1

225

(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/S-6011/DC

SUBJECT: WIND FORCE CALC.

DOCUMENT TITLE: DESIGN CALCULATION

REVISION: 0

JOB NO: M2-251

1.225

41.8

226

Attachment 2

227

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Element and Detail Weights : Step: 7 1:45p 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| 5.97865 | 0.0029355 | 5.97865 | 0.0029355 | 0.29893 |

20| 30| 137.032 | 0.10276 | 137.032 | 0.10276 | 6.85162 |

30| 40| 19.5277 | 0.0032789 | 19.5277 | 0.0032789 | 0.97638 |

40| 50| 21.3476 | ... | 21.3476 | ... | 1.06738 |

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

Total 183 0.11 183 0.11 9

Weight of Details

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

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

| | kgm | mm | mm |

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

10|Nozl| 3.82814 | -51.1905 | ... | N3

20|Sadl| 11.2964 | 350.000 | 192.612 | Left saddle

20|Sadl| 11.2964 | 2770.00 | 192.612 | Right saddle

20|Nozl| 7.18497 | 1200.00 | 127.781 | N1

20|Nozl| 7.18497 | 2920.00 | 127.781 | N2

20|Nozl| 7.18497 | 1425.00 | 127.781 | N4

20|Nozl| 7.18497 | 3000.00 | 127.781 | N5

20|Nozl| 7.18497 | 200.000 | 127.781 | N6

20|Nozl| 8.15833 | 770.000 | 146.831 | K1A

20|Nozl| 8.15833 | 170.000 | 146.831 | K1B

20|Nozl| 7.18496 | 1010.00 | 127.781 | K2A

228

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Element and Detail Weights : Step: 7 1:45p Jan 11,2015 20|Nozl| 7.18496 | 170.000 | 127.781 | K2B

20|Nozl| 8.15833 | 570.000 | 146.831 | K3A

20|Nozl| 8.15833 | 170.000 | 146.831 | K3B

20|Nozl| 8.15833 | 750.000 | 146.831 | K4A

20|Nozl| 8.15833 | 350.000 | 146.831 | K4B

20|Nozl| 7.18496 | 1895.00 | 127.781 | K6A

20|Nozl| 7.18496 | 1445.00 | 127.781 | K6B

20|Nozl| 8.15833 | 1795.00 | 146.831 | K7A

20|Nozl| 8.15833 | 1445.00 | 146.831 | K7B

20|Nozl| 8.15833 | 1950.00 | 146.831 | K8A

20|Nozl| 8.15833 | 1550.00 | 146.831 | K8B

20|Nozl| 8.15833 | 1850.00 | 146.831 | K5A

20|Nozl| 8.15833 | 1500.00 | 146.831 | K5B

20|Wght| 100.000 | 1700.00 | ... | FILTER

20|Wght| 16.0000 | 1908.00 | ... | LIQUID (UPPER)

20|Wght| 30.0000 | 2567.00 | ... | LUGS

Total Weight of Each Detail Type

Total Weight of Saddles 22.6

Total Weight of Nozzles 166.4

Total Weight of Weights 146.0

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

Sum of the Detail Weights 335.0 kgm

Weight Summation

Fabricated Shop Test Shipping Erected Empty Operating

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

193.1 382.1 193.1 382.1 193.1 412.1

229

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Element and Detail Weights : Step: 7 1:45p Jan 11,2015 22.6 108.9 22.6 ... 22.6 ...

166.4 30.0 166.4 ... ... ...

... ... ... ... ... 146.0

... ... ... ... ... -30.0

... ... ... ... 166.4 ...

... ... ... ... 30.0 ...

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

382.1 521.0 382.1 412.1 412.1 528.1 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 382.1 kgm

Shop Test Wt. - Fabricated Weight + Water ( Full ) 521.0 kgm

Shipping Wt. - Fab. Wt + Rem. Intls.+ Shipping App. 382.1 kgm

Erected Wt. - Fab. Wt + Rem. Intls.+ Insul. (etc) 412.1 kgm

Ope. Wt. no Liq - Fab. Wt + Intls. + Details + Wghts. 412.1 kgm

Operating Wt. - Empty Wt + Operating Liq. Uncorroded 528.1 kgm

Oper. Wt. + CA - Corr Wt. + Operating Liquid 528.1 kgm

Field Test Wt. - Empty Weight + Water (Full) 521.0 kgm

Note: The Corroded Weight and thickness are used in the Horizontal

230

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Element and Detail Weights : Step: 7 1:45p Jan 11,2015 Vessel Analysis (Ope Case) and Earthquake Load Calculations.

Outside Surface Areas of Elements

| | Surface |

From| To | Area |

| | mm² |

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

10| 20| 91207.0 |

20| 30| 2.167E+06 |

30| 40| 148106. |

40| 50| 124315. |

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

Total 2530993.000 mm²


231

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Wind Load Calculation : Step: 9 1:45p Jan 11,2015

Note: Using the User Defined Wind Profile ...

Platform Load Calculations

ID Wind Area Elevation Pressure Force Cf

mm² mm kPa N

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

Wind Loads on Masses/Equipment/Piping

ID Wind Area Elevation Pressure Force

mm² mm kPa N

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

FILTER 0.00 1700.00 0.75 0.00

LIQUID (UPPER 0.00 1908.00 0.75 0.00

LUGS 0.00 2567.00 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| 300.000 | 262.890 | 24498.2 | 0.75000 | 18.3732 |

20| 30| 300.000 | 262.890 | 820217. | 0.75000 | 615.148 |

30| 40| 300.000 | 245.715 | 24964.6 | 0.75000 | 18.7230 |

40| 50| 300.000 | 245.715 | 6990.09 | 0.75000 | 5.24244 |

232

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Wind Load Calculation : Step: 9 1:45p Jan 11,2015 PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013

233

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Earthquake Load Calculation : Step: 10 1:45p 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| 102.381 | 863.036 | 431.518 |

20|Sadl| 102.381 | 863.036 | 431.518 |

Sadl| 30| 102.381 | 863.036 | 431.518 |

20| 30| 102.381 | 863.036 | 431.518 |

30| 40| 102.381 | 863.036 | 431.518 |

40| 50| 102.381 | 863.036 | 431.518 |


234

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p 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 (120.00) 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( 100.000 + 1.56*sqrt( 105.9593 * 7.1565 ), 2 * 106.000 )

= 142.9579 mm

Input and Calculated Values:

Vessel Mean Radius Rm 105.96 mm

Stiffened Vessel Length per 4.15.6 L 3175.00 mm

Distance from Saddle to Vessel tangent a 106.00 mm

Saddle Width b 100.00 mm

Saddle Bearing Angle theta 120.00 degrees

Inside Depth of Head h2 51.19 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

Saddle Force Q, Operating Case 13801.04 N

235


Horizontal Vessel Analysis Results: Actual Allowable

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

Long. Stress at Top of Midspan -23.44 -977.24 MPa

Long. Stress at Top of Midspan 23.44 115.15 MPa

Long. Stress at Bottom of Midspan 50.09 115.15 MPa

Long. Stress at Top of Saddles 15.57 115.15 MPa

Long. Stress at Bottom of Saddles 12.09 115.15 MPa

Tangential Shear in Shell 19.47 69.09 MPa

Circ. Stress at Horn of Saddle 24.74 143.93 MPa

Circ. Compressive Stress in Shell 1.03 115.15 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 * ( 657.5/2 + 0 ) * 300.0000/183.5269

= 1612.1 N

Saddle Reaction Force due to Wind Fl or Friction [Fwl]:

= max( Fl, Friction Load, Sum of X Forces) * B / Ls

= max( 33.92 , 0.00 , 0 ) * 300.0000/2420.0002

= 4.2 N

Saddle Reaction Force due to Earthquake Fl or Friction [Fsl]:

= max( Fl, Friction Force, Sum of X Forces ) * B / Ls

= max( 2589.11 , 0.00 , 0 ) * 300.0000/2420.0002

= 321.0 N

Saddle Reaction Force due to Earthquake Ft [Fst]:

236

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015 = Ftr * ( Ft/Num of Saddles + Z Force Load ) * B / E

= 3.00 * ( 2589/2 + 0 ) * 300.0000/183.5269

= 6348.4 N

Load Combination Results for Q + Wind or Seismic [Q]:

= Saddle Load + Max( Fwl, Fwt, Fsl, Fst )

= 7452 + Max( 4 , 1612 , 320 , 6348 )

= 13801.0 N

Summary of Loads at the base of this Saddle:

Vertical Load (including saddle weight) 13911.82 N

Transverse Shear Load Saddle 1294.55 N

Longitudinal Shear Load Saddle 2589.11 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.

Moment per Equation 4.15.3 [M1]:

= -Q*a [1 - (1- a/L + (R²-h2²)/(2a*L))/(1+(4h2)/3L)]

= -13801*106.00[1-(1-106.00/3175.00+(105.959²-51.191²)/

(2*106.00*3175.00))/(1+(4*51.19)/(3*3175.00))]

= -60.3 N-m

237

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015 Moment per Equation 4.15.4 [M2]:

= Q*L/4(1+2(R²-h2²)/(L²))/(1+(4h2)/( 3L))-4a/L

= 13801*3175/4(1+2(105²-51²)/(3175²))/(1+(4*51)/

(3*3175))-4*105/3175

= 9283.2 N-m

Longitudinal Stress at Top of Shell (4.15.6) [Sigma1]:

= P * Rm/(2t) - M2/(pi*Rm²t)

= 18.000 * 105.959/(2*7.156 ) - 9283.2/(pi*106.0²*7.156 )

= -23.44 MPa

Longitudinal Stress at Bottom of Shell (4.15.7) [Sigma2]:

= P * Rm/(2t) + M2/(pi * Rm² * t)

= 18.000 * 105.959/(2 * 7.156 ) + 9283.2/(pi * 106.0² * 7.156 )

= 50.09 MPa

Longitudinal Stress at Top of Shell at Support (4.15.10) [Sigma*3]:

= P * Rm/(2t) - M1/(K1*pi*Rm²t)

= 18.000*105.959/(2*7.156)--60.3/(0.1066*pi*106.0²*7.156)

= 15.57 MPa

Longitudinal Stress at Bottom of Shell at Support (4.15.11) [Sigma*4]:

= P * Rm/(2t) + M1/(K1* * pi * Rm² * t)

= 18.000*105.959/(2*7.156)+-60.3/(0.1923*pi*106.0²*7.156)

= 12.09 MPa

Maximum Shear Force in the Saddle (4.15.5) [T]:

= Q(L-2a)/(L+(4*h2/3))

= 13801 ( 3175.00 - 2 * 106.00 )/(3175.00 + ( 4 * 51.19/3))

= 12608.5 N

238

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015 Shear Stress in the shell no rings, not stiffened (4.15.14) [tau2]:

= K2 * T / ( Rm * t )

= 1.1707 * 12608.48/( 105.9593 * 7.1565 )

= 19.47 MPa

Decay Length (4.15.22) [x1,x2]:

= 0.78 * sqrt( Rm * t )

= 0.78 * sqrt( 105.959 * 7.156 )

= 21.479 mm

Circumferential Stress in shell, no rings (4.15.23) [sigma6]:

= -K5 * Q * k / ( t * ( b + X1 + X2 ) )

= -0.7603 * 13801 * 0.1/( 7.156 * ( 100.00 + 21.48 + 21.48 ) )

= -1.03 MPa

Circ. Comp. Stress at Horn of Saddle, L>=8Rm (4.15.24) [sigma7]:

= -Q/(4*t*(b+X1+X2)) - 3*K7*Q/(2*t²)

= -13801/(4*7.156 *(100.000 +21.479 +21.479 )) -

3*0.0529 *13801/(2*7.156²)

= -24.74 MPa

Effective reinforcing plate width (4.15.1) [B1]:

= min( b + 1.56 * sqrt( Rm * t ), 2a )

= min( 100.00 + 1.56 * sqrt( 105.959 * 7.156 ), 2 * 106.000 )

= 142.96 mm

Free Un-Restrained Thermal Expansion between the Saddles [Exp]:

= Alpha * Ls * ( Design Temperature - Ambient Temperature )

= 0.156E-04 * 2420.000 * ( 50.0 - 21.1 )

= 1.093 mm

239

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015 Results for Vessel Ribs, Web and Base:

Baseplate Length Bplen 210.0000 mm

Baseplate Thickness Bpthk 8.0000 mm

Baseplate Width Bpwid 100.0000 mm

Number of Ribs ( inc. outside ribs ) Nribs 2

Rib Thickness Ribtk 8.0000 mm

Web Thickness Webtk 8.0000 mm

Web Location Webloc Center

Moment of Inertia of Saddle - Lateral Direction

Y A AY Io

Shell 4. 1161. 4154. 19819.

Wearplate 12. 1200. 14588. 187335.

Web 126. 1743. 219723. 34594160.

BasePlate 239. 800. 191200. 45701020.

Totals 381. 4904. 429664. 80502336.

Value C1 = Sumof(Ay)/Sumof(A) = 88. mm

Value I = Sumof(Io) - C1*Sumof(Ay) = 42855068. mm**4

Value As = Sumof(A) - Ashell = 3743. mm²

K1 = (1+Cos(beta)-.5*Sin(beta)² )/(pi-beta+Sin(beta)*Cos(beta)) = 0.2035

Fh = K1 * Q = 0.2035 * 13801.044 = 2808.8120 N

Tension Stress, St = ( Fh/As ) = 0.7505 MPa

Allowed Stress, Sa = 0.6 * Yield Str = 148.9320 MPa

d = B - R*Sin(theta) / theta = 260.7126 mm

Bending Moment, M = Fh * d = 732.5896 N-m

240


Bending Stress, Sb = ( M * C1 / I ) = 1.4974 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 * (13801 + 110 ) * 100.00/( 4 * 210.000 * 165.480 ))½

= 5.480 mm

Calculation of Axial Load, Intermediate Values and Compressive Stress

Effective Baseplate Length [e]:

= ( Bplen - Clearance ) / ( Nribs - 1)

= ( 210.0000 - 25.4 )/( 2 - 1 ) = 184.6000 mm

Baseplate Pressure Area [Ap]:

= e * Bpwid / 2

= 184.6000 * 100.0000/2 = 9229.9990 mm²

Axial Load [P]:

= Ap * Bp

= 9230.0 * 0.66 = 6065.9 N

Area of the Rib and Web [Ar]:

= ( Bpwid - Clearance - Webtk ) * Ribtk + e/2 * Webtk

= ( 100.000 - 25.4 - 8.000 ) * 8.000 + 184.6000/2 * 8.000

= 1271.200 mm²

Compressive Stress [Sc]:

= P/Ar

241

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015 = 6065.9/1271.2000 = 4.7722 MPa

Check of Outside Ribs:

Inertia of Saddle, Outer Ribs - Longitudinal Direction

Y A AY Ay² Io

Rib 50.0 634.4 31720.0 0.0 443558.7

Web 50.0 738.4 36920.0 0.0 7876.3

Values 50.0 1372.8 68640.0 0.0 451434.9

Bending Moment [Rm]:

= Fl /( 2 * Bplen ) * e * rl / 2

= 2589.1/( 2 * 210.00 ) * 184.600 * 290.61/2

= 165.422 N-m

KL/R < Cc ( 15.4214 < 126.0993 ) per AISC E2-1

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

Sca = ( 1-( 15.42 )²/(2 * 126.10² )) * 248/

( 5/3+3*(15.42 )/(8* 126.10 )-( 15.42³)/(8*126.10³)

Sca = 143.88 MPa

AISC Unity Check on Outside Ribs ( must be <= 1.0 )

Check = Sc/Sca + (Rm/Z)/Sba

Check = 4.77/143.88 + (165.42/9028.698 )/165.48

Check = 0.14

ASME Horizontal Vessel Analysis: Stresses for the Right Saddle




242



= min( b + 1.56*sqrt( Rm * t ), 2a )

= min( 100.000 + 1.56*sqrt( 105.9593 * 7.1565 ), 2 * 106.000 )

= 142.9579 mm











Saddle Force Q, Operating Case 14208.82 N


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

Long. Stress at Top of Midspan -25.49 -977.24 MPa







243

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015 Circ. Compressive Stress in Shell 1.06 115.15 MPa




= 3.00 * ( 657.5/2 + 0 ) * 300.0000/183.5269

= 1612.1 N



= max( 33.92 , 0.00 , 0 ) * 300.0000/2420.0002

= 4.2 N

Saddle Reaction Force due to Earthquake Fl or Friction [Fsl]:

= max( Fl, Friction Force, Sum of X Forces ) * B / Ls

= max( 2589.11 , 0.00 , 0 ) * 300.0000/2420.0002

= 321.0 N

Saddle Reaction Force due to Earthquake Ft [Fst]:


= 3.00 * ( 2589/2 + 0 ) * 300.0000/183.5269

= 6348.4 N



= 7860 + Max( 4 , 1612 , 320 , 6348 )

= 14208.8 N



244

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015 Transverse Shear Load Saddle 1294.55 N





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)]

= -14208*106.00[1-(1-106.00/3175.00+(105.959²-0.000²)/

(2*106.00*3175.00))/(1+(4*0.00)/(3*3175.00))]

= -25.2 N-m


= Q*L/4(1+2(R²-h2²)/(L²))/(1+(4h2)/( 3L))-4a/L

= 14208*3175/4(1+2(105²-0²)/(3175²))/(1+(4*0)/

(3*3175))-4*105/3175

= 9801.2 N-m


= P * Rm/(2t) - M2/(pi*Rm²t)

= 18.000 * 105.959/(2*7.156 ) - 9801.2/(pi*106.0²*7.156 )

= -25.49 MPa

245

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015 Longitudinal Stress at Bottom of Shell (4.15.7) [Sigma2]:

= P * Rm/(2t) + M2/(pi * Rm² * t)

= 18.000 * 105.959/(2 * 7.156 ) + 9801.2/(pi * 106.0² * 7.156 )

= 52.14 MPa


= P * Rm/(2t) - M1/(K1*pi*Rm²t)

= 18.000*105.959/(2*7.156)--25.2/(0.1066*pi*106.0²*7.156)

= 14.26 MPa


= P * Rm/(2t) + M1/(K1* * pi * Rm² * t)

= 18.000*105.959/(2*7.156)+-25.2/(0.1923*pi*106.0²*7.156)

= 12.81 MPa


= Q(L-2a)/(L+(4*h2/3))

= 14208 ( 3175.00 - 2 * 106.00 )/(3175.00 + ( 4 * 0.00/3))

= 13260.1 N

Shear Stress in the shell no rings, not stiffened (4.15.14) [tau2]:

= K2 * T / ( Rm * t )

= 1.1707 * 13260.07/( 105.9593 * 7.1565 )

= 20.47 MPa


= 0.78 * sqrt( Rm * t )

= 0.78 * sqrt( 105.959 * 7.156 )

= 21.479 mm


246

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015 = -K5 * Q * k / ( t * ( b + X1 + X2 ) )

= -0.7603 * 14208 * 0.1/( 7.156 * ( 100.00 + 21.48 + 21.48 ) )

= -1.06 MPa


= -Q/(4*t*(b+X1+X2)) - 3*K7*Q/(2*t²)

= -14208/(4*7.156 *(100.000 +21.479 +21.479 )) -

3*0.0529 *14208/(2*7.156²)

= -25.47 MPa


= min( b + 1.56 * sqrt( Rm * t ), 2a )

= min( 100.00 + 1.56 * sqrt( 105.959 * 7.156 ), 2 * 106.000 )

= 142.96 mm

Results for Vessel Ribs, Web and Base









Y A AY Io

Shell 4. 1161. 4154. 19819.

Wearplate 12. 1200. 14588. 187335.

Web 126. 1743. 219723. 34594160.

247

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015 BasePlate 239. 800. 191200. 45701020.

Totals 381. 4904. 429664. 80502336.





Fh = K1 * Q = 0.2035 * 14208.821 = 2891.8035 N









AllStress ))½

= ( 3 * (14208 + 110 ) * 100.00/( 4 * 210.000 * 165.480 ))½

= 5.559 mm




= ( 210.0000 - 25.4 )/( 2 - 1 ) = 184.6000 mm

248



= e * Bpwid / 2

= 184.6000 * 100.0000/2 = 9229.9990 mm²

Axial Load [P]:

= Ap * Bp

= 9230.0 * 0.68 = 6245.1 N



= ( 100.000 - 25.4 - 8.000 ) * 8.000 + 184.6000/2 * 8.000

= 1271.200 mm²


= P/Ar

= 6245.1/1271.2000 = 4.9132 MPa



Y A AY Ay² Io

Rib 50.0 634.4 31720.0 0.0 443558.7

Web 50.0 738.4 36920.0 0.0 7876.3

Values 50.0 1372.8 68640.0 0.0 451434.9


= Fl /( 2 * Bplen ) * e * rl / 2

= 2589.1/( 2 * 210.00 ) * 184.600 * 290.61/2

= 165.422 N-m

KL/R < Cc ( 15.4214 < 126.0993 ) per AISC E2-1

249

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015 Sca = (1-(Klr)²/(2*Cc²))*Fy/(5/3+3*(Klr)/(8*Cc)-(Klr³)/(8*Cc³)

Sca = ( 1-( 15.42 )²/(2 * 126.10² )) * 248/

( 5/3+3*(15.42 )/(8* 126.10 )-( 15.42³)/(8*126.10³)

Sca = 143.88 MPa



Check = 4.91/143.88 + (165.42/9028.698 )/165.48

Check = 0.14


250

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p 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( 100.000 + 1.56*sqrt( 105.9593 * 7.1565 ), 2 * 106.000 )

= 142.9579 mm







Inside Depth of Head h2 51.19 mm





Saddle Force Q, Test Case, no Ext. Forces 2849.23 N

251



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











= 3.00 * ( 217.0/2 + 0 ) * 300.0000/183.5269

= 532.0 N



= max( 33.92 , 0.00 , 0 ) * 300.0000/2420.0002

= 1.4 N



= 2317 + Max( 1 , 532 , 0 , 0 )

= 2849.2 N



252

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015 Transverse Shear Load Saddle 108.49 N


Hydrostatic Test Pressure at center of Vessel: 24.635 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)]

= -2849*106.00[1-(1-106.00/3175.00+(105.959²-51.191²)/

(2*106.00*3175.00))/(1+(4*51.19)/(3*3175.00))]

= -12.5 N-m


= Q*L/4(1+2(R²-h2²)/(L²))/(1+(4h2)/( 3L))-4a/L

= 2849*3175/4(1+2(105²-51²)/(3175²))/(1+(4*51)/

(3*3175))-4*105/3175

= 1916.5 N-m


= P * Rm/(2t) - M2/(pi*Rm²t)

= 24.635 * 105.959/(2*7.156 ) - 1916.5/(pi*106.0²*7.156 )

253

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015 = 10.65 MPa


= P * Rm/(2t) + M2/(pi * Rm² * t)

= 24.635 * 105.959/(2 * 7.156 ) + 1916.5/(pi * 106.0² * 7.156 )

= 25.83 MPa


= P * Rm/(2t) - M1/(K1*pi*Rm²t)

= 24.635*105.959/(2*7.156)--12.5/(0.1066*pi*106.0²*7.156)

= 18.70 MPa


= P * Rm/(2t) + M1/(K1* * pi * Rm² * t)

= 24.635*105.959/(2*7.156)+-12.5/(0.1923*pi*106.0²*7.156)

= 17.98 MPa


= Q(L-2a)/(L+(4*h2/3))

= 2849 ( 3175.00 - 2 * 106.00 )/(3175.00 + ( 4 * 51.19/3))

= 2603.0 N


= K2 * T / ( Rm * t )

= 1.1707 * 2603.02/( 105.9593 * 7.1565 )

= 4.02 MPa


= 0.78 * sqrt( Rm * t )

= 0.78 * sqrt( 105.959 * 7.156 )

= 21.479 mm

254



= -K5 * Q * k / ( t * ( b + X1 + X2 ) )

= -0.7603 * 2849 * 0.1/( 7.156 * ( 100.00 + 21.48 + 21.48 ) )

= -0.21 MPa


= -Q/(4*t*(b+X1+X2)) - 3*K7*Q/(2*t²)

= -2849/(4*7.156 *(100.000 +21.479 +21.479 )) -

3*0.0529 *2849/(2*7.156²)

= -5.11 MPa


= min( b + 1.56 * sqrt( Rm * t ), 2a )

= min( 100.00 + 1.56 * sqrt( 105.959 * 7.156 ), 2 * 106.000 )

= 142.96 mm

Results for Vessel Ribs, Web and Base:









Y A AY Io

Shell 4. 1161. 4154. 19819.

Wearplate 12. 1200. 14588. 187335.

255

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015 Web 126. 1743. 219723. 34594160.

BasePlate 239. 800. 191200. 45701020.

Totals 381. 4904. 429664. 80502336.





Fh = K1 * Q = 0.2035 * 2849.231 = 579.8803 N









AllStress ))½

= ( 3 * (2849 + 110 ) * 100.00/( 4 * 210.000 * 165.480 ))½

= 2.528 mm




256

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015 = ( 210.0000 - 25.4 )/( 2 - 1 ) = 184.6000 mm


= e * Bpwid / 2

= 184.6000 * 100.0000/2 = 9229.9990 mm²

Axial Load [P]:

= Ap * Bp

= 9230.0 * 0.14 = 1252.3 N



= ( 100.000 - 25.4 - 8.000 ) * 8.000 + 184.6000/2 * 8.000

= 1271.200 mm²


= P/Ar

= 1252.3/1271.2000 = 0.9852 MPa



Y A AY Ay² Io

Rib 50.0 634.4 31720.0 0.0 443558.7

Web 50.0 738.4 36920.0 0.0 7876.3

Values 50.0 1372.8 68640.0 0.0 451434.9


= Fl /( 2 * Bplen ) * e * rl / 2

= 11.2/( 2 * 210.00 ) * 184.600 * 290.61/2

= 0.715 N-m

257

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015 KL/R < Cc ( 15.4214 < 126.0993 ) per AISC E2-1


Sca = ( 1-( 15.42 )²/(2 * 126.10² )) * 248/

( 5/3+3*(15.42 )/(8* 126.10 )-( 15.42³)/(8*126.10³)

Sca = 143.88 MPa



Check = 0.99/143.88 + (0.72/9028.698 )/165.48

Check = 0.01

ASME Horizontal Vessel Analysis: Stresses for the Right Saddle





= min( b + 1.56*sqrt( Rm * t ), 2a )

= min( 100.000 + 1.56*sqrt( 105.9593 * 7.1565 ), 2 * 106.000 )

= 142.9579 mm







258






Saddle Force Q, Test Case, no Ext. Forces 3101.89 N


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











= 3.00 * ( 217.0/2 + 0 ) * 300.0000/183.5269

= 532.0 N



= max( 33.92 , 0.00 , 0 ) * 300.0000/2420.0002

= 1.4 N

259

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015 Load Combination Results for Q + Wind or Seismic [Q]:


= 2569 + Max( 1 , 532 , 0 , 0 )

= 3101.9 N



Transverse Shear Load Saddle 108.49 N


Hydrostatic Test Pressure at center of Vessel: 24.635 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)]

= -3101*106.00[1-(1-106.00/3175.00+(105.959²-0.000²)/

(2*106.00*3175.00))/(1+(4*0.00)/(3*3175.00))]

= -5.5 N-m


= Q*L/4(1+2(R²-h2²)/(L²))/(1+(4h2)/( 3L))-4a/L

260

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015 = 3101*3175/4(1+2(105²-0²)/(3175²))/(1+(4*0)/

(3*3175))-4*105/3175

= 2139.7 N-m


= P * Rm/(2t) - M2/(pi*Rm²t)

= 24.635 * 105.959/(2*7.156 ) - 2139.7/(pi*106.0²*7.156 )

= 9.77 MPa


= P * Rm/(2t) + M2/(pi * Rm² * t)

= 24.635 * 105.959/(2 * 7.156 ) + 2139.7/(pi * 106.0² * 7.156 )

= 26.71 MPa


= P * Rm/(2t) - M1/(K1*pi*Rm²t)

= 24.635*105.959/(2*7.156)--5.5/(0.1066*pi*106.0²*7.156)

= 18.44 MPa


= P * Rm/(2t) + M1/(K1* * pi * Rm² * t)

= 24.635*105.959/(2*7.156)+-5.5/(0.1923*pi*106.0²*7.156)

= 18.13 MPa


= Q(L-2a)/(L+(4*h2/3))

= 3101 ( 3175.00 - 2 * 106.00 )/(3175.00 + ( 4 * 0.00/3))

= 2894.8 N


= K2 * T / ( Rm * t )

261

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015 = 1.1707 * 2894.78/( 105.9593 * 7.1565 )

= 4.47 MPa


= 0.78 * sqrt( Rm * t )

= 0.78 * sqrt( 105.959 * 7.156 )

= 21.479 mm


= -K5 * Q * k / ( t * ( b + X1 + X2 ) )

= -0.7603 * 3101 * 0.1/( 7.156 * ( 100.00 + 21.48 + 21.48 ) )

= -0.23 MPa


= -Q/(4*t*(b+X1+X2)) - 3*K7*Q/(2*t²)

= -3101/(4*7.156 *(100.000 +21.479 +21.479 )) -

3*0.0529 *3101/(2*7.156²)

= -5.56 MPa


= min( b + 1.56 * sqrt( Rm * t ), 2a )

= min( 100.00 + 1.56 * sqrt( 105.959 * 7.156 ), 2 * 106.000 )

= 142.96 mm

Results for Vessel Ribs, Web and Base






262

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015 Web Thickness Webtk 8.0000 mm



Y A AY Io

Shell 4. 1161. 4154. 19819.

Wearplate 12. 1200. 14588. 187335.

Web 126. 1743. 219723. 34594160.

BasePlate 239. 800. 191200. 45701020.

Totals 381. 4904. 429664. 80502336.





Fh = K1 * Q = 0.2035 * 3101.894 = 631.3029 N









263

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015 AllStress ))½

= ( 3 * (3101 + 110 ) * 100.00/( 4 * 210.000 * 165.480 ))½

= 2.633 mm




= ( 210.0000 - 25.4 )/( 2 - 1 ) = 184.6000 mm


= e * Bpwid / 2

= 184.6000 * 100.0000/2 = 9229.9990 mm²

Axial Load [P]:

= Ap * Bp

= 9230.0 * 0.15 = 1363.4 N



= ( 100.000 - 25.4 - 8.000 ) * 8.000 + 184.6000/2 * 8.000

= 1271.200 mm²


= P/Ar

= 1363.4/1271.2000 = 1.0726 MPa



Y A AY Ay² Io

Rib 50.0 634.4 31720.0 0.0 443558.7

264

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015 Web 50.0 738.4 36920.0 0.0 7876.3

Values 50.0 1372.8 68640.0 0.0 451434.9


= Fl /( 2 * Bplen ) * e * rl / 2

= 11.2/( 2 * 210.00 ) * 184.600 * 290.61/2

= 0.715 N-m

KL/R < Cc ( 15.4214 < 126.0993 ) per AISC E2-1


Sca = ( 1-( 15.42 )²/(2 * 126.10² )) * 248/

( 5/3+3*(15.42 )/(8* 126.10 )-( 15.42³)/(8*126.10³)

Sca = 143.88 MPa



Check = 1.07/143.88 + (0.72/9028.698 )/165.48

Check = 0.01


265

Attachment 3

266

Input Echo, Leg & Lug Item 1, Description: Trunnion

Design Internal Pressure 0.00 barDesign Temperature for Attachment TEMP 40.00 CVessel Outside Diameter OD 114.300 mm.Vessel Wall Thickness Ts 8.1800 mm.Vessel Corrosion Allowance Cas 0.0000 mm.Vessel Material SA-312 TP316LVessel Material UNS Number S31603Vessel Allowable Stress at Design S 115.23 MPaAnalysis Type: Trunnion

Empty Weight of Vessel Wemp 3826.00 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 Length TL 130.0000 mm.Bail/Sling Width TT 15.0000 mm.Pad Outside Diameter POD 139.000 mm.Pad Thickness PTHK 8.0000 mm.Ring Outside Diameter Rod 140.00 mm.Ring Thickness Rthk 8.00 mm.Trunnion Type SolidLift Orientation SolidImpact Factor Impfac 2.00

Force Along Vessel Axis Fax 3826.00 N .Force Normal to Vessel Fn 2209.00 N .Force Tangential to Vessel Ft 383.00 N .Perform WRC-107 Analysis on the Trunnion No

Occasional Load Factor (AISC A5.2) Occfac 1.00

Results for Trunnions, Description : Trunnion

Trunnion Lifting Load [Tlf]:= ((Fa^2 + Ft^2)^1/2)= ((3826.00 ^2 + 383.00 ^2)^1/2) * 2.00= 7690.24 N .

Z = pi * (TOD^4 - TID^4) / (32.0 * TOD)= 3.14 * ( 88.90 ^4 - 88.90 ^4) / (32.0 * 88.90 )= 68977.13 mm.^3

Trunnion Bending Moment [Tmom]:= (TL - 0.5 * TT)/1.001* Tlf= ( 130.00 - 0.5 * 15.00 )/1.001 * 7690.24= 942.44 N-m .

Trunnion Calculated Bending Stress [SBC]:= TMOM * 1.001/ Z= 942.44 *1.001/ 68977.13= 13.67 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- 88.90^2)= 6207.17 mm^2

Trunnion Calculated Shear Stress [SSC]:= Tlf / Txsa= 7690.24 / 6207.17= 1.24 MPa [Passed] SSC < 0.4 * SY * Occfac (68.49)

Trunnion Unity Check [UCHK]:= SBC / SBA + SSC / SSA= 13.67 / 113.01 + 1.24 / 68.49= 0.14 [Passed] UCHK, Must be less than 1.

Trunnion Bearing Contact Area [Tbca]:= TOD * TT= 88.90 * 15.00= 1333.50 mm^2

267

Trunnion Bearing Stress [SBEC]:= Tlf / Tbca= 7690.24 / 1333.50= 5.77 MPa [Passed] SBEC < Min(0.75* SY* Occfac, 0.9* SY) (128.42)

SUMMARY OF RESULTS:

Trunnion unity check value: 0.1390

Actual Allowable Pass/FailBending Stress (MPa ) 13.67 113.01 PassShear Stress (MPa ) 1.24 68.49 PassBearing Stress (MPa ) 5.77 128.42 Pass


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