Tcp de Plataforma

8/11/2019 Tcp de Plataforma

1/110

Codeware, Inc.

Sarasota, FL, USA

www.codeware.com

COMPRESS Pressure Vessel Design Calculations

Item: Split Stream Dearator

Vessel No: V-1234

Customer: Magaladon Oil Venture

Contract: C-45490-R56

Designer: John Doe

Date: April 1, 2001

You can edit this page by selecting Cover Page settings...in the reportmenu.


2/110

Table of Contents

General Arrangement Drawing..............................................................................................................................1/108

Deficiencies Summary............................................................................................................................................2/108

Nozzle Schedule......................................................................................................................................................4/108

Nozzle Summary.....................................................................................................................................................5/108

Pressure Summary.................................................................................................................................................6/108

Revision History......................................................................................................................................................7/108

Settings Summary...................................................................................................................................................8/108

Radiography Summary.........................................................................................................................................10/108

Thickness Summary.............................................................................................................................................11/108

Weight Summary...................................................................................................................................................12/108

Long Seam Summary...........................................................................................................................................13/108

Hydrostatic Test....................................................................................................................................................14/108

Vacuum Summary.................................................................................................................................................15/108

Ellipsoidal Head #2...............................................................................................................................................16/108

Straight Flange on Ellipsoidal Head #2...............................................................................................................19/108

Cylinder #1.............................................................................................................................................................22/108

Saddle #1...............................................................................................................................................................24/108

Nozzle #2 (N2)........................................................................................................................................................31/108

Copy of Nozzle #2 (N3).........................................................................................................................................45/108

Copy of Copy of Nozzle #2 (N4)...........................................................................................................................59/108

Copy of Copy of Copy of Nozzle #2 (N5).............................................................................................................73/108

Straight Flange on Ellipsoidal Head #1...............................................................................................................87/108

Ellipsoidal Head #1...............................................................................................................................................90/108

Nozzle #1 (N1)........................................................................................................................................................93/108


3/110

General Arrangement Drawing

1/108


4/110

Deficiencies Summary

Deficiencies for Copy of Copy of Copy of Nozzle #2 (N5)Nozzle is located on top of the parent component's longitudinal seam. Move the longitudinal seam or activate theoption switch "Through a Category A Joint" in the nozzle dialog.

Deficiencies for Copy of Copy of Nozzle #2 (N4)Nozzle is located on top of the parent component's longitudinal seam. Move the longitudinal seam or activate theoption switch "Through a Category A Joint" in the nozzle dialog.

Deficiencies for Copy of Nozzle #2 (N3)Nozzle is located on top of the parent component's longitudinal seam. Move the longitudinal seam or activate the

option switch "Through a Category A Joint" in the nozzle dialog.

Deficiencies for Nozzle #2 (N2)Nozzle is located on top of the parent component's longitudinal seam. Move the longitudinal seam or activate the

option switch "Through a Category A Joint" in the nozzle dialog.

Deficiencies for Saddle #1Circumferential stress at the saddle horns is excessive.Compressive stress over saddle is excessive.

Warnings Summary

Warnings for Copy of Copy of Copy of Nozzle #2 (N5)Nozzle reinforcing pad extends over the parent component'slongitudinal seam. This may result in improper fit-up forwelding. Designer review is recommended. (warning)

Warnings for Copy of Copy of Nozzle #2 (N4)Nozzle reinforcing pad extends over the parent component's longitudinal seam. This may result in improper fit-up for

welding. Designer review is recommended. (warning)

Warnings for Copy of Nozzle #2 (N3)Nozzle reinforcing pad extends over the parent component's longitudinal seam. This may result in improper fit-up forwelding. Designer review is recommended. (warning)

Warnings for Ellipsoidal Head #2Internal design temperature varies across this chamber. (warning)External design temperature varies across this chamber. (warning)

External design pressure varies across this chamber. (warning)Check the following component(s): (warning)Cylinder #1 (warning)

Warnings for Nozzle #2 (N2)Nozzle reinforcing pad extends over the parent component's longitudinal seam. This may result in improper fit-up forwelding. Designer review is recommended. (warning)

ASME B16.5 / B16.47 Flange Warnings Summary

2/108


5/110

ASME B16.5 / 16.47 Flanges with Warnings

FlangeApplicableWarnings

Nozzle #2 (N2) 1

Copy of Nozzle #2 (N3) 1

Copy of Copy of Nozzle #2 (N4) 1

Copy of Copy of Copy of Nozzle #2 (N5) 1Nozzle #1 (N1) 1, 2

ASME B16.5 / 16.47 Flange Warnings

No. Warning

1For Class 150 flanges, ASME B16.5 para. 5.4.3 recommends gaskets to be in accordance with NonmandatoryAppendix B, Table B1, Group No. I.

2For Class 150 flanges when temperature exceeds 400 F, care should be taken to avoid imposing severeexternal loads and/or thermal gradients or leakage may develop. ASME B16.5 para. 2.5.2.

3/108


6/110

Nozzle Schedule

Nozzlemark

Service Size MaterialsImpactTested

Normalized Fine Grain Flange Blind

N1 Nozzle #1 NPS 6 Sch 40 (Std)Nozzle SA-106 B Smls pipe No No No NPS 6 Class 150

WN A105No

Pad SA-516 70 No No No

N2 Nozzle #2 NPS 6 Sch 40 (Std)Nozzle SA-106 B Smls pipe No No No NPS 6 Class 150

WN A105No


N3 Copy of Nozzle #2 NPS 6 Sch 40 (Std) Nozzle SA-106 B Smls pipe No No No NPS 6 Class 150WN A105 No


N4 Copy of Copy of Nozzle #2 NPS 6 Sch 40 (Std)Nozzle SA-106 B Smls pipe No No No NPS 6 Class 150

WN A105No


N5 Copy of Copy of Copy of Nozzle #2 NPS 6 Sch 40 (Std)Nozzle SA-106 B Smls pipe No No No NPS 6 Class 150

WN A105No


4/108


7/110

Nozzle Summary

Nozzle

mark

OD

(in)

tn

(in)

Req tn

(in)A1? A2?

ShellReinforcement

Pad Corr

(in)

Aa/A

r(%)

Nom t

(in)

Design t

(in)

User t

(in)

Width

(in)

tpad(in)

N1 6.625 0.28 0.28 Yes Yes 0.5478* 0.524 2 0.5478 0 100.0

N2 6.625 0.28 0.28 Yes Yes 0.5 0.5 2 0.5 0 103.5

N3 6.625 0.28 0.28 Yes Yes 0.5 0.5 2 0.5 0 103.5

N4 6.625 0.28 0.28 Yes Yes 0.5 0.5 2 0.5 0 103.5

N5 6.625 0.28 0.28 Yes Yes 0.5 0.5 2 0.5 0 103.5

tn: Nozzle thickness

Req tn: Nozzle thickness required per UG-45/UG-16

Nom t: Vessel wall thickness

Design t: Required vessel wall thickness due to pressure + corrosion allowance per UG-37

User t: Local vessel wall thickness (near opening)

Aa: Area available per UG-37, governing condition

Ar: Area required per UG-37, governing condition

Corr: Corrosion allowance on nozzle wall* Head minimum thickness after forming

5/108


8/110

Pressure Summary

Pressure Summary for Chamber bounded by Ellipsoidal Head #1 and Ellipsoidal Head #2

Identifier

P

Design

( psi)

T

Design

( F)

MAWP

( psi)

MAP

( psi)

MAEP

( psi)

Te

external

( F)

MDMT

( F)

MDMT

Exemption

Impact

Tested

Ellipsoidal Head #2 100 650 105.57 112.31 15 650 -55 Note 1 No

Straight Flange on Ellipsoidal Head #2 100 650 215.43 229.18 22.31 650 -55 Note 2 No

Cylinder #1 100 311 102.25 102.25 N/A 311 -20 Note 3 No

Straight Flange on Ellipsoidal Head #1 100 650 215.43 229.18 22.31 650 -55 Note 2 No

Ellipsoidal Head #1 100 650 105.57 112.31 15 650 -55 Note 4 No

Saddle #1 100 311 102.25 N/A N/A N/A N/A N/A N/A

Nozzle #1 (N1) 100 650 112.2 118.23 15 650 -20.51Nozzle Note 5 No

Pad Note 6 No

Nozzle #2 (N2) 100 311 102.25 102.25 N/A 311 -20Nozzle Note 5 No

Pad Note 7 No

Copy of Nozzle #2 (N3) 100 311 102.25 102.25 N/A 311 -20Nozzle Note 5 No

Pad Note 7 No

Copy of Copy of Nozzle #2 (N4) 100 311 102.25 102.25 N/A 311 -20Nozzle Note 5 No

Pad Note 7 No

Copy of Copy of Copy of Nozzle #2 (N5) 100 311 102.25 102.25 N/A 311 -20Nozzle Note 5 No

Pad Note 7 No

Chamber design MDMT is -20 FChamber rated MDMT is -20 F @ 102.25 psi

Chamber MAWP hot & corroded is 102.25 psi @ 311 F

Chamber MAP cold & new is 102.25 psi @ 70 F

This pressure chamber is not designed for external pressure.

Notes for MDMT Rating:

Note # Exemption Details

1. Straight Flangegoverns MDMT

2.Material impact test exemption temperature from Fig UCS-66 Curve B = -7 FFig UCS-66.1 MDMT reduction = 72 F, (coincident ratio = 0.4444)

Rated MDMT of -79F is limited to -55F by UCS-66(b)(2)

UCS-66 governing thickness = 0.5 in

3. Material is impact test exempt per UG-20(f) UCS-66 governing thickness = 0.5 in

4. Straight Flangegoverns MDMT

5. Nozzle is impact test exempt to -155 F per UCS-66(b)(3) (coincident ratio = 0.0743).

6.Pad impact test exemption temperature from Fig UCS-66 Curve B = -2.41 FFig UCS-66.1 MDMT reduction = 18.1 F, (coincident ratio = 0.8194) UCS-66 governing thickness = 0.5478 in.

7. Pad is impact test exempt per UG-20(f) UCS-66 governing thickness = 0.5 in.

Design notes are available on the Settings Summarypage.

6/108


9/110

Revision History

No. Date Operator Notes

0 8/18/2014 spineyro New vessel created ASME Section VIII Division 1 [COMPRESS 2014 Build 7400]

7/108


10/110

Settings Summary

COMPRESS 2014 Build 7400

Units: U.S. Customary

Datum Line Location: 0.00" from right seam

Design

ASME Section VIII Division 1, 2013 Edition

Design or Rating: Get Thickness from Pressure

Minimum thickness: 0.0625" per UG-16(b)

Design for cold shut down only: No

Design for lethal service (full radiography required): No

Design nozzles for: Design P, find nozzle MAWP and MAP

Corrosion weight loss: 100% of theoretical loss

UG-23 Stress Increase: 1.20

Skirt/legs stress increase: 1.0

Minimum nozzle projection: 6"Juncture calculations for > 30 only: Yes

Preheat P-No 1 Materials > 1.25" and


11/110

UG-22 Loadings

UG-22(a) Internal or External Design Pressure : Yes

UG-22(b) Weight of the vessel and normal contents under operating or test conditions: Yes

UG-22(c) Superimposed static reactions from weight of attached equipment (external loads): No

UG-22(d)(2) Vessel supports such as lugs, rings, skirts, saddles and legs: Yes

UG-22(f) Wind reactions: No

UG-22(f) Seismic reactions: No

UG-22(j) Test pressure and coincident static head acting during the test: NoNote: UG-22(b),(c) and (f) loads only considered when supports are present.

9/108


12/110

Radiography Summary

Radiography for Chamber bounded by Ellipsoidal Head #1 and Ellipsoidal Head #2

Component

Longitudinal Seam Left Circumferential Seam Right Circumferential Seam

MarkCategory(Fig

UW-3)

Radiography / JointType

Category(Fig

UW-3)


Category(Fig

UW-3)


Ellipsoidal Head #2 N/A Seamless No RT N/A N/A BFull UW-11(a) / Type1

RT1

Cylinder #1 AFull UW-11(a) / Type1

BFull UW-11(a) / Type1

BFull UW-11(a) / Type1

RT1

Ellipsoidal Head #1 N/A Seamless No RT BFull UW-11(a) / Type1

N/A N/A RT1

Nozzle Longitudinal SeamNozzle to Vessel

Circumferential SeamNozzle free end Circumferential

Seam

Nozzle #2 (N2) N/A Seamless No RT D N/A / Type 7 CUW-11(a)(4) exempt /

Type 1N/A

Copy of Nozzle #2 (N3) N/A Seamless No RT D N/A / Type 7 CUW-11(a)(4) exempt /

Type 1N/A

Copy of Copy of Nozzle #2 (N4) N/A Seamless No RT D N/A / Type 7 CUW-11(a)(4) exempt /

Type 1N/A

Copy of Copy of Copy of Nozzle #2 (N5) N/A Seamless No RT D N/A / Type 7 CUW-11(a)(4) exempt /Type 1 N/A

Nozzle #1 (N1) N/A Seamless No RT D N/A / Type 7 CUW-11(a)(4) exempt /Type 1

N/A

Nozzle Flange Longitudinal Seam Flange FaceNozzle to Flange Circumferential

Seam

ASME B16.5/16.47 flange attached to Nozzle #2(N2)

N/A Seamless No RT N/A N/A / Gasketed CUW-11(a)(4) exempt /Type 1

N/A

ASME B16.5/16.47 flange attached to Copy ofNozzle #2 (N3)


N/A

ASME B16.5/16.47 flange attached to Copy ofCopy of Nozzle #2 (N4)


N/A

ASME B16.5/16.47 flange attached to Copy of

Copy of Copy of Nozzle #2 (N5)N/A Seamless No RT N/A N/A / Gasketed C

UW-11(a)(4) exempt /

Type 1N/A

ASME B16.5/16.47 flange attached to Nozzle #1

(N1)N/A Seamless No RT N/A N/A / Gasketed C

UW-11(a)(4) exempt /

Type 1N/A

Chamber bounded by Ellipsoidal Head #1 and Ellipsoidal Head #2 - UG-116(e) Radiography:RT1

10/108


13/110

Thickness Summary

Component

IdentifierMaterial Diameter

(in)

Length

(in)

Nominal t

(in)

Design t

(in)

Total Corrosion

(in)

Joint

ELoad

Ellipsoidal Head #2 SA-516 70 195 ID 49.2978 0.5478* 0.5478 0 1.00 External

Straight Flange on Ellipsoidal Head #2 SA-516 70 195 ID 2 1.125 0.9729 0 1.00 External

Cylinder #1 SA-516 70 196 OD 433 0.5 0.4891 0 1.00 Internal

Straight Flange on Ellipsoidal Head #1 SA-516 70 195 ID 2 1.125 0.9729 0 1.00 External

Ellipsoidal Head #1 SA-516 70 195 ID 49.2978 0.5478* 0.5478 0 1.00 External

Nominal t: Vessel wall nominal thickness

Design t: Required vessel thickness due to governing loading + corrosion

Joint E: Longitudinal seam joint efficiency

* Head minimum thickness after forming

Load

internal: Circumferential stress due to internal pressure governs

external: External pressure governs

Wind: Combined longitudinal stress of pressure + weight + wind governs

Seismic: Combined longitudinal stress of pressure + weight + seismic governs

11/108


14/110

Weight Summary

Component

Weight ( lb) Contributed by Vessel ElementsSurface Area

ft2Metal

New*

Metal

Corroded*Insulation

InsulationSupports

LiningPiping

+ Liquid

OperatingLiquid

Test Liquid

New Corroded New Corroded

Ellipsoidal Head #2 7,055.7 7,055.7 0 0 0 0 0 0 37,192.1 37,192.1 332

Cylinder #1 37,611.1 37,611.1 0 0 0 0 0 0 466,798 466,798 1,851

Ellipsoidal Head #1 7,050.3 7,050.3 0 0 0 0 0 0 37,194.7 37,194.7 332

Saddle #1 3,006 3,006 0 0 0 0 0 0 0 0 223

TOTAL: 54,723 54,723 0 0 0 0 0 0 541,184.8 541,184.8 2,737

* Shells with attached nozzles have weight reduced by material cut out for opening.

Component

Weight ( lb) Contributed by AttachmentsSurface Area

ft2Body FlangesNozzles &Flanges

PackedBeds

TraysTray

SupportsRings &

ClipsVerticalLoads

New Corroded New Corroded

Ellipsoidal Head #2 0 0 0 0 0 0 0 0 0 0

Cylinder #1 0 0 152.3 152.3 0 0 0 0 0 7

Ellipsoidal Head #1 0 0 37.2 37.2 0 0 0 0 0 2

TOTAL: 0 0 189.5 189.5 0 0 0 0 0 9

Vessel operating weight, Corroded: 54,913 lb

Vessel operating weight, New: 54,913 lb

Vessel empty weight, Corroded: 54,913 lb

Vessel empty weight, New: 54,913 lb

Vessel test weight, New: 596,097 lb

Vessel test weight, Corroded: 596,097 lb

Vessel surface area: 2,746 ft2

Vessel center of gravity location - from datum - lift condition

Vessel Lift Weight, New: 54,913 lb

Center of Gravity: 217.7727"

Vessel Capacity

Vessel Capacity** (New): 64,901 US gal

Vessel Capacity** (Corroded): 64,901 US gal

**The vessel capacity does not include volume of nozzle, piping or other attachments.

12/108


15/110

Long Seam Summary

Shell Long Seam Angles

Component Seam 1 Seam 2 Seam 3

Cylinder #1 0 140.6751 281.3501

Shell Plate Lengths

Component

Starting

Angle Plate 1 Plate 2 Plate 3

Cylinder #1 0 240" 240" 134.1813"

*Plate Lengths use the circumference of the vessel based on the mid diameter of the components

Shell Rollout

13/108


16/110

Hydrostatic Test

Shop test pressure determination for Chamber bounded by Ellipsoidal Head #1 and Ellipsoidal Head #2 basedon MAWP per UG-99(b)

Shop hydrostatic test gauge pressure is 132.921 psi at 70 F (the chamber MAWP = 102.247 psi)

The shop test is performed with the vessel in the horizontal position.

IdentifierLocal testpressure

psi

Test liquidstatic head

psi

UG-99(b)stressratio

UG-99(b)pressure

factor

Ellipsoidal Head #2 140.195 7.274 1.0638 1.30

Straight Flange on Ellipsoidal Head #2 140.195 7.274 1.0638 1.30

Cylinder #1 (1) 140.195 7.274 1 1.30

Straight Flange on Ellipsoidal Head #1 140.195 7.274 1.0638 1.30

Ellipsoidal Head #1 140.195 7.274 1.0638 1.30

Copy of Copy of Copy of Nozzle #2 (N5) 133.138 0.217 1 1.30

Copy of Copy of Nozzle #2 (N4) 133.138 0.217 1 1.30

Copy of Nozzle #2 (N3) 133.138 0.217 1 1.30

Nozzle #1 (N1) 136.785 3.864 1 1.30

Nozzle #2 (N2) 133.138 0.217 1 1.30

Notes:

(1) Cylinder #1 limits the UG-99(b) stress ratio.(2) The zero degree angular position is assumed to be up, and the test liquid height is assumed to the top-most

flange.

The field test condition has not been investigated for the Chamber bounded by Ellipsoidal Head #1 and Ellipsoidal

Head #2.

The test temperature of 70 F is warmer than the minimum recommended temperature of 10 F so the brittle fracture

provision of UG-99(h) has been met.

14/108


17/110

Vacuum Summary

Component Line of Support

Elevation

above Datum

(in)

Length Le

(in)

Ellipsoidal Head #2 - 484.2978 N/A

- 1/3 depth of Ellipsoidal Head #2 451.25 N/A

Straight Flange on Ellipsoidal Head #2 Left - 435 469.5

Straight Flange on Ellipsoidal Head #2 Right - 433 469.5

Cylinder #1 Left - 433 469.5

Cylinder #1 Right - 0 469.5

Straight Flange on Ellipsoidal Head #1 Left - 0 469.5

Straight Flange on Ellipsoidal Head #1 Right - -2 469.5

- 1/3 depth of Ellipsoidal Head #1 -18.25 N/A

Ellipsoidal Head #1 - -51.2978 N/A

Note

For main components, the listed value of 'Le' is the largest unsupported length for the component.

15/108


18/110

Ellipsoidal Head #2


Component: Ellipsoidal HeadMaterial Specification: SA-516 70 (II-D p.22, ln. 6)

Straight Flangegoverns MDMT

Internal design pressure: P = 100 psi @ 650 FExternal design pressure: Pe= 15 psi @ 650 F

Static liquid head:

Ps= 0 psi (SG=1, Hs=0" Operating head)Pth= 7.27 psi (SG=1, Hs=201.5" Horizontal test head)

Corrosion allowance: Inner C = 0" Outer C = 0"

Design MDMT = -20F No impact test performedRated MDMT = -55F Material is not normalized

Material is not produced to fine grain practice

PWHT is not performedDo not Optimize MDMT / Find MAWP

Radiography: Category A joints - Seamless No RTHead to shell seam - Full UW-11(a) Type 1

Estimated weight*: new = 7,055.7 lb corr = 7,055.7 lbCapacity*: new = 4,460.3 US gal corr = 4,460.3 US gal

* includes straight flange

Inner diameter = 195"Minimum head thickness = 0.5478"Head ratio D/2h = 2 (new)

Head ratio D/2h = 2 (corroded)Straight flange length Lsf = 2"

Nominal straight flange thickness tsf = 1.125"

Results Summary

The governing condition is external pressure.

Minimum thickness per UG-16 = 0.0625" + 0"= 0.0625"Design thickness due to internal pressure (t) = 0.5189"

Design thickness due to external pressure (te) = 0.5478"Maximum allowable working pressure (MAWP) = 105.57psi

Maximum allowable pressure (MAP) = 112.31psi

Maximum allowable external pressure (MAEP) = 15psi

Design thickness for internal pressure, (Corroded at 650 F) UG-32(d)(1)

t = P*D / (2*S*E - 0.2*P) + Corrosion

= 100*195 / (2*18,800*1 - 0.2*100) + 0= 0.5189"

The head internal pressure design thickness is 0.5189".

16/108


19/110

Maximum allowable working pressure, (Corroded at 650 F) UG-32(d)(1)

P = 2*S*E*t / (D + 0.2*t) - Ps= 2*18,800*1*0.5478 / (195 +0.2*0.5478) - 0= 105.57 psi

The maximum allowable working pressure (MAWP) is 105.57psi.

Maximum allowable pressure, (New at 70 F) UG-32(d)(1)

P = 2*S*E*t / (D + 0.2*t) - Ps= 2*20,000*1*0.5478 / (195 +0.2*0.5478) - 0

= 112.31 psi

The maximum allowable pressure (MAP) is 112.31psi.

Design thickness for external pressure, (Corroded at 650 F) UG-33(d)

Equivalent outside spherical radius (Ro)

Ro = Ko*Do= 0.895*196.0956

= 175.5055 in

A = 0.125 / (Ro/ t)= 0.125 / (175.5055 / 0.547748)

= 0.00039

From Table

CS-2:B =

4,806.1918

psi

Pa = B / (Ro/ t)= 4,806.1918 / (175.5055 / 0.5477)

= 15 psi

t = 0.5477" + Corrosion = 0.5477" + 0" = 0.5477"

Check the external pressure per UG-33(a)(1) UG-32(d)(1)

t = 1.67*Pe*D / (2*S*E - 0.2*1.67*Pe) + Corrosion= 1.67*15*195 / (2*18,800*1 - 0.2*1.67*15) + 0

= 0.1299"

The head external pressure design thickness (te) is 0.5477".

Maximum Allowable External Pressure, (Corroded at 650 F) UG-33(d)

Equivalent outside spherical radius (Ro)

Ro = Ko*Do

= 0.895*196.0956= 175.5055 in

A = 0.125 / (Ro/ t)

= 0.125 / (175.5055 / 0.5478)= 0.00039

From TableCS-2:

B =4,806.6512psi

17/108


20/110

Pa = B / (Ro/ t)= 4,806.6512 / (175.5055 / 0.5478)

= 15.0029 psi

Check the Maximum External Pressure, UG-33(a)(1) UG-32(d)(1)

P = 2*S*E*t / ((D + 0.2*t)*1.67) - Ps2= 2*18,800*1*0.5478 / ((195 +0.2*0.5478)*1.67) - 0

= 63.21 psi

The maximum allowable external pressure (MAEP) is 15psi.

% Extreme fiber elongation - UCS-79(d)

EFE = (75*t / Rf)*(1 - Rf/ Ro)

= (75*1.125 / 33.7125)*(1 - 33.7125 / infinity)

= 2.5028%

The extreme fiber elongation does not exceed 5%.

18/108


21/110

Straight Flange on Ellipsoidal Head #2


Component: Straight Flange

Material specification: SA-516 70 (II-D p. 22, ln. 6)Material impact test exemption temperature from Fig UCS-66 Curve B = -7 F

Fig UCS-66.1 MDMT reduction = 72 F, (coincident ratio = 0.4444)Rated MDMT of -79F is l imited to -55F by UCS-66(b)(2)


Internal design pressure: P = 100 psi @ 650 F

External design pressure: Pe= 15 psi @ 650 F

Static liquid head:

Pth = 7.27 psi (SG = 1, Hs= 201.5", Horizontal testhead)

Corrosion allowance Inner C = 0" Outer C = 0"

Design MDMT = -20 F No impact test performed

Rated MDMT = -55 F Material is not normalizedMaterial is not produced to Fine Grain PracticePWHT is not performed

Radiography: Longitudinal joint - Seamless No RTCircumferential joint - Full UW-11(a) Type 1

Estimated weight New = 392.3 lb corr = 392.3 lb

Capacity New = 258.57 US gal corr = 258.57 US gal

ID = 195"Length

Lc= 2"

t = 1.125"

Design thickness, (at 650 F) UG-27(c)(1)

t = P*R / (S*E - 0.60*P) + Corrosion= 100*97.5 / (18,800*1.00 - 0.60*100) + 0

= 0.5203"

Maximum allowable working pressure, (at 650 F) UG-27(c)(1)

P = S*E*t / (R + 0.60*t) - Ps= 18,800*1.00*1.125 / (97.5 + 0.60*1.125) - 0

= 215.43 psi

Maximum allowable pressure, (at 70 F) UG-27(c)(1)

P = S*E*t / (R + 0.60*t)

= 20,000*1.00*1.125 / (97.5 + 0.60*1.125)= 229.18 psi

19/108


22/110

External Pressure, (Corroded & at 650 F) UG-28(c)

L / Do = 469.5 / 197.25 = 2.3802Do/ t = 197.25 / 0.9729 = 202.7441From table G: A = 0.000186

From tableCS-2:

B = 2,280.8705 psi

Pa = 4*B / (3*(Do/ t))

= 4*2,280.87 / (3*(197.25 / 0.9729))= 15 psi

Design thickness for external pressure Pa= 15 psi

ta = t + Corrosion = 0.9729 + 0 = 0.9729"

Maximum Allowable External Pressure, (Corroded & at 650 F) UG-28(c)

L / Do = 469.5 / 197.25 = 2.3802Do/ t = 197.25 / 1.125 = 175.3333

From table G: A = 0.000239From table

CS-2:B = 2,934.3375 psi

Pa = 4*B / (3*(Do/ t))= 4*2,934.34 / (3*(197.25 / 1.125))

= 22.31 psi


EFE = (50*t / Rf)*(1 - Rf/ Ro)

= (50*1.125 / 98.0625)*(1 - 98.0625 / infinity)

= 0.5736%


Allowable Compressive Stress, Hot and Corroded- ScHC, (table CS-2)

A = 0.125 / (Ro/ t)

= 0.125 / (98.625 / 1.125)

= 0.001426

B = 9,110 psi

S = 18,800 / 1.00 = 18,800 psi

ScHC = min(B, S) = 9,110 psi

Allowable Compressive Stress, Hot and New- ScHN

ScHN = ScHC= 9,110 psi

Allowable Compressive Stress, Cold and New- ScCN, (table CS-2)

A = 0.125 / (Ro/ t)

= 0.125 / (98.625 / 1.125)

= 0.001426

B = 13,615 psi

20/108


23/110

S = 20,000 / 1.00 = 20,000 psi

ScCN = min(B, S) = 13,615 psi

Allowable Compressive Stress, Cold and Corroded- ScCCScCC = ScCN

= 13,615 psi

Allowable Compressive Stress, Vacuum and Corroded- ScVC, (tableCS-2)

A = 0.125 / (Ro/ t)

= 0.125 / (98.625 / 1.125)

= 0.001426

B = 9,110 psi

S = 18,800 / 1.00 = 18,800 psi

ScVC = min(B, S) = 9,110 psi

21/108


24/110

Cylinder #1


Component: Cylinder

Material specification: SA-516 70 (II-D p. 22, ln. 6)Material is impact test exempt per UG-20(f)


Internal design pressure: P = 100 psi @ 311 F

Static liquid head:

Pth = 7.27 psi (SG = 1, Hs= 201.5", Horizontal test

head)

Corrosion allowance Inner C = 0" Outer C = 0"

Design MDMT = -20 F No impact test performed

Rated MDMT = -20 F Material is not normalizedMaterial is not produced to Fine Grain Practice

PWHT is not performed

Radiography: Longitudinal joint - Full UW-11(a) Type 1Left circumferential joint - Full UW-11(a) Type 1

Right circumferential joint - Full UW-11(a) Type 1

Estimated weight New = 37,611.1 lb corr = 37,611.1 lb

Capacity New = 55,980.27 US gal corr = 55,980.27 US gal

OD = 196"

LengthLc

= 433"

t = 0.5"

Design thickness, (at 311 F) Appendix 1-1

t = P*Ro/ (S*E + 0.40*P) + Corrosion

= 100*98 / (20,000*1.00 + 0.40*100) + 0= 0.4891"

Maximum allowable working pressure, (at 311 F) Appendix 1-1

P = S*E*t / (Ro- 0.40*t) - Ps= 20,000*1.00*0.5 / (98 - 0.40*0.5) - 0

= 102.25 psi

Maximum allowable pressure, (at 70 F) Appendix 1-1

P = S*E*t / (Ro- 0.40*t)

= 20,000*1.00*0.5 / (98 - 0.40*0.5)= 102.25 psi


EFE = (50*t / Rf)*(1 - Rf/ Ro)

= (50*0.5 / 97.75)*(1 - 97.75 / infinity)

22/108


25/110

= 0.2558%


Allowable Compressive Stress, Hot and Corroded- ScHC, (table CS-2)

A = 0.125 / (Ro/ t)

= 0.125 / (98 / 0.5)

= 0.000638

B = 9,156 psi

S = 20,000 / 1.00 = 20,000 psi

ScHC = min(B, S) = 9,156 psi

Allowable Compressive Stress, Hot and New- ScHNScHN = ScHC

= 9,156 psi

Allowable Compressive Stress, Cold and New- ScCN, (table CS-2)

A = 0.125 / (Ro/ t)

= 0.125 / (98 / 0.5)= 0.000638

B = 9,196 psi

S = 20,000 / 1.00 = 20,000 psi

ScCN = min(B, S) = 9,196 psi

Allowable Compressive Stress, Cold and Corroded- ScCCScCC = ScCN

= 9,196 psi

Allowable Compressive Stress, Vacuum and Corroded- ScVC, (tableCS-2)

A = 0.125 / (Ro/ t)

= 0.125 / (98 / 0.5)

= 0.000638

B = 9,156 psi

S = 20,000 / 1.00 = 20,000 psi

ScVC = min(B, S) = 9,156 psi

23/108


26/110

Saddle #1

Saddle material:

Saddle construction is: Centered webSaddle allowable stress: Ss= 20,000 psi

Saddle yield stress: Sy= 38,000 psiSaddle distance to datum: 47.0239 in

Tangent to tangent length: L = 437 inSaddle separation: Ls= 377.9522inVessel radius: R = 98 in

Tangent distance left: Al= 10.0239 inTangent distance right: Ar= 49.0239 in

Saddle height: Hs= 110.0478inSaddle contact angle: = 120

Web plate thickness: ts= 0.625 inBase plate length: E = 171.0667inBase plate width: F = 10 in

Base plate thickness: tb= 0.75 inNumber of stiffener ribs: n = 9

Largest stiffener rib spacing: di= 22.6958 in

Stiffener rib thickness: tw= 0.5 inSaddle width: b = 9 inAnchor bolt size & type: 1.25 inch series 8 threaded

Anchor bolt material:Anchor bolt allowable shear: 15,000 psiAnchor bolt corrosion allowance: 0 in

Anchor bolts per saddle: 2Base coefficient of friction: = 0.45

Weight on left saddle: operating corr =23,306 lb, test new =265,973 lb

Weight on right saddle: operating corr =28,601 lb, test new =327,118 lbWeight of saddle pair =3,006 lb

Notes:

(1) Saddle calculations are based on the method presented in "Stresses in Large Cylindrical Pressure Vessels onTwo Saddle Supports" by L.P. Zick.

24/108


27/110

LoadVessel

condition

Bending + pressure between saddles(psi)

Bending + pressure at the saddle(psi)

S1(+)

allow(+)

S1(-)

allow(-)

S2(+)

allow(+)

S2(-)

allow(-)

Weight Operat ing 10,112 20,000 143 9,156 10,035 20,000 66 9,156

Weight Test 15,301 34,200 1,632 9,196 14,421 34,200 752 9,196

LoadVessel

condition

Tangentialshear (psi)

Circumferentialstress (psi)

Stress oversaddle (psi)

Splitting (psi)

S3 allowS4

(horns)

allow(+/-)

S5 allow S6 allow

Weight Operat ing 483 16,000 -4,771 30,000 3,767 16,750 824 13,333

Weight Test 5,521 27,360 -54,572 34,200 43,085 34,200 9,427 34,200

Load Case 1: Weight ,Operating

Longitudinal stress between saddles (Weight ,Operating, left saddle loading and geometry govern)

S1= +- 3*K1*Q*(L / 12) / (*R2*t)

= 3*0.8428*23,306*(437 / 12) / (*97.752*0.5)= 143 psi

Sp= P*R / (2*t)= 102.25*97.5 / (2*0.5)

= 9,969 psi

Maximum tensile stress S1t= S1+ Sp= 10,112psiMaximum compressive stress (shut down) S1c= S1= 143psi

Tensile stress is acceptable (


28/110

Maximum tensile stress S2t= S2+ Sp= 10,035psi

Maximum compressive stress (shut down) S2c= S2= 66psi

Tensile stress is acceptable (


29/110

S6= K8*Q / Ae= 0.2035*28,601 / 7.0611

= 824psi

Stress in saddle is acceptable (


30/110

S3= K2.2*Qshear/ (R*t)

= 1.1707*230,510.18 / (97.75*0.5)= 5,521psi

Tangential shear stress is acceptable ( 34,200 psi)**

Saddle splitting load (right, Weight ,Test)

Area resisting splitting force = Web area + wear plate area

Ae= Heff*ts+ tp*Wp= 11.2978*0.625 + 0*0= 7.0611 in2

S6= K8*Q / Ae= 0.2035*327,118 / 7.0611

= 9,427psi

Stress in saddle is acceptable (


31/110

Bolt shear stress = 13,546.8 / (0.929*1*2) = 7,291 psi

Anchor bolt stress is acceptable (


32/110

The base plate thickness of 0.75 in is adequate.

Foundation bearing check

Sf= Qmax/ (F*E)

= 328,621 / (10*171.0667)= 192 psi

Concrete bearing stress 1,658 psi ; satisfactory.

30/108


33/110

Nozzle #2 (N2)


tw(lower)= 0.25 in

Leg41= 0.3125 in

tw(upper)= 0.25 in

Leg42= 0.375 inLeg43= 0.3125 in

hnew= 1 in

Dp= 10.625 in

te= 0.5 in

Note: round inside edges per UG-76(c)

Location and Orientation

Located on: Cylinder #1

Orientation: 0

Nozzle center line offset to datum line: 413 in

End of nozzle to shell center: 104 in

Passes through a Category A joint: No

Nozzle

Access opening: No

Material specification: SA-106 B Smls pipe (II-D p. 14, ln. 19)

Description: NPS 6 Sch 40 (Std)Inside diameter, new: 6.065 in

Nominal wall thickness: 0.28 in

Corrosion allowance: 0 in

Projection available outside vessel, Lpr: 2.5 in

Internal projection, hnew: 1 in

Projection available outside vessel to flange face, Lf: 6 in

Local vessel minimum thickness: 0.5 in

Liquid static head included: 0 psi

Longitudinal joint efficiency: 1

Reinforcing Pad

Material specification: SA-516 70 (II-D p. 22, ln. 6)

Diameter: 10.625 in

Is split: No

ASME B16.5-2009 Flange

Description: NPS 6 Class 150 WN A105

Bolt Material: SA-193 B7 Bolt


34/110

Blind included: No

Rated MDMT: -55F per UCS-66(b)(1)(b)

Liquid static head: 0 psi

MAWP rating: 226.7 psi@311F

MAP rating: 285 psi@70F

Hydrotest rating: 450 psi@70F

PWHT performed: No

Circumferential joint radiography: Full UW-11(a) Type 1

32/108


35/110


36/110

Outer Normal Limit of reinforcement per UG-40

LH = MIN(2.5*(t - C), 2.5*(tn- Cn) + te)

= MIN(2.5*(0.5 - 0), 2.5*(0.28 - 0) + 0.5)

= 1.2 in

Inner Normal Limit of reinforcement per UG-40

LI = MIN(h, 2.5*(t - C), 2.5*(ti- Cn- C))

= MIN(1, 2.5*(0.5 - 0), 2.5*(0.28 - 0 - 0))= 0.7 in

Nozzle required thickness per UG-27(c)(1)

trn = P*Rn/ (Sn*E - 0.6*P)

= 102.247*3.0325 / (17,100*1 - 0.6*102.247)

= 0.0182 in

Required thickness trfrom UG-37(a)

tr = P*Ro/ (S*E + 0.4*P)

= 102.247*98 / (20,000*1 + 0.4*102.247)

= 0.5 in

Required thickness trper Interpretation VIII-1-07-50

tr = P*Ro/ (S*E + 0.4*P)

= 102.247*98 / (20,000*1 + 0.4*102.247)

= 0.5 in

Area required per UG-37(c)

Allowable stresses: Sn= 17,100, Sv= 20,000, Sp= 20,000 psi

fr1= lesser of 1 or Sn/ Sv= 0.855


fr3= lesser of fr2or Sp/ Sv= 0.855

fr4= lesser of 1 or Sp/ Sv= 1

A = d*tr*F + 2*tn*tr*F*(1 - fr1)

= 6.065*0.5*1 + 2*0.28*0.5*1*(1 - 0.855)

= 3.073in2

Area available from FIG. UG-37.1

A1= larger of the following= 0.0001in2

= d*(E1*t - F*tr) - 2*tn*(E1*t - F*tr)*(1 - fr1)

34/108


37/110

= 6.065*(1*0.5 - 1*0.5) - 2*0.28*(1*0.5 - 1*0.5)*(1 - 0.855)

= 0.0001 in2

= 2*(t + tn)*(E1*t - F*tr) - 2*tn*(E1*t - F*tr)*(1 - fr1)

= 2*(0.5 + 0.28)*(1*0.5 - 1*0.5) - 2*0.28*(1*0.5 - 1*0.5)*(1 - 0.855)

= 0 in2

A2= smaller of the following= 0.5372in2

= 5*(tn- trn)*fr2*t

= 5*(0.28 - 0.0182)*0.855*0.5

= 0.5596 in2

= 2*(tn- trn)*(2.5*tn+ te)*fr2= 2*(0.28 - 0.0182)*(2.5*0.28 + 0.5)*0.855

= 0.5372 in2


= 5*t*ti*fr2= 5*0.5*0.28*0.855

= 0.5985in2

= 5*ti*ti*fr2= 5*0.28*0.28*0.855

= 0.3352in2

= 2*h*ti*fr2= 2*1*0.28*0.855

= 0.4788in2

A41 = Leg2*fr3

= 0.31252*0.855

= 0.0835in2

A42 = Leg2*fr4

= 0.3752*1

= 0.1406in2

A43 = Leg2*fr2

= 0.31252

*0.855= 0.0835in2

A5 = (Dp- d - 2*tn)*te*fr4= (10.625 - 6.065 - 2*0.28)*0.5*1

= 2in2

35/108


38/110

Area = A1+ A2+ A3+ A41+ A42+ A43+ A5= 0.0001 + 0.5372 + 0.3352 + 0.0835 + 0.1406 + 0.0835 + 2

= 3.1801in2

As Area >= A the reinforcement is adequate.

UW-16(d) Weld Check

Inner fillet: tmin = lesser of 0.75 or tnor te= 0.28 in

tc(min) = lesser of 0.25 or 0.7*tmin= 0.196in

tc(actual) = 0.7*Leg = 0.7*0.3125 =0.2188 in

Outer fillet: tmin = lesser of 0.75 or teor t = 0.5 in

tw(min) = 0.5*tmin= 0.25in

tw(actual) = 0.7*Leg = 0.7*0.375 = 0.2625 in

Lower fillet: tmin = lesser of 0.75 or tnor t = 0.28 in


tc(actual) = 0.7*Leg = 0.7*0.3125 = 0.2188in

Upper groove: tmin = lesser of 0.75 or tnor te= 0.28 in


tw(actual) = 0.25 in

Lower groove: tmin = lesser of 0.75 or tnor t = 0.28 in



UG-45 Nozzle Neck Thickness Check

ta UG-27 = P*R / (S*E - 0.6*P) + Corrosion

= 102.247*3.0325 / (17,100*1 - 0.6*102.247) + 0

= 0.0182 in

ta = max[ ta UG-27, ta UG-22]

= max[ 0.0182 , 0 ]

= 0.0182 in

tb1 = P*Ro/ (S*E + 0.4*P) + Corrosion

= 102.247*98 / (20,000*1 + 0.4*102.247) + 0

= 0.5 in

tb1 = max[ tb1, tb UG16]

= max[ 0.5 , 0.0625 ]

= 0.5 in

tb = min[ tb3, tb1]

= min[ 0.245 , 0.5 ]

36/108


39/110

= 0.245 in

tUG-45 = max[ ta, tb]

= max[ 0.0182 , 0.245 ]

= 0.245 in

Available nozzle wall thickness new, tn= 0.875*0.28 = 0.245 in

The nozzle neck thickness is adequate.

Allowable stresses in joints UG-45 and UW-15(c)

Groove weld in tension: 0.74*20,000 = 14,800 psi

Nozzle wall in shear: 0.7*17,100 = 11,970 psi

Inner fil let weld in shear: 0.49*17,100 = 8,379 psi

Outer fi llet weld in shear: 0.49*20,000 = 9,800 psi

Upper groove weld in tension: 0.74*20,000 = 14,800 psi

Lower fillet weld in shear: 0.49*17,100 = 8,379 psi

Strength of welded joints:

(1) Inner fillet weld in shear(/ 2)*Nozzle OD*Leg*Si= (/ 2)*6.625*0.3125*8,379 = 27,248.84 lbf

(2) Outer fillet weld in shear(/ 2)*Pad OD*Leg*So= (/ 2)*10.625*0.375*9,800 = 61,334.69 lbf

(3) Nozzle wall in shear

(/ 2)*Mean nozzle dia*tn*Sn= (/ 2)*6.345*0.28*11,970 = 33,404.4 lbf

(4) Groove weld in tension(/ 2)*Nozzle OD*tw*Sg= (/ 2)*6.625*0.25*14,800 = 38,504.14 lbf

(5) Lower fillet weld in shear(/ 2)*Nozzle OD*Leg*Sl= (/ 2)*6.625*0.3125*8,379 = 27,248.84 lbf

(6) Upper groove weld in tension

(/ 2)*Nozzle OD*tw*Sg= (/ 2)*6.625*0.25*14,800 = 38,504.14 lbf

Loading on welds per UG-41(b)(1)

W = (A - A1+ 2*tn*fr1*(E1*t - F*tr))*Sv= (3.073 - 0.0001 + 2*0.28*0.855*(1*0.5 - 1*0.5))*20,000

= 61,458.87lbf

W1-1 = (A2+ A5+ A41+ A42)*Sv= (0.5372 + 2 + 0.0835 + 0.1406)*20,000

= 55,226lbf

W2-2 = (A2+ A3+ A41+ A43+ 2*tn*t*fr1)*Sv= (0.5372 + 0.3352 + 0.0835 + 0.0835 + 2*0.28*0.5*0.855)*20,000

37/108


40/110

= 25,575.2lbf

W3-3 = (A2+ A3+ A5+ A41+ A42+ A43+ 2*tn*t*fr1)*Sv= (0.5372 + 0.3352 + 2 + 0.0835 + 0.1406 + 0.0835 + 2*0.28*0.5*0.855)*20,000

= 68,387.2lbf

Load for path 1-1 lesser of W or W1-1= 55,226 lbfPath 1-1 through (2) & (3) = 61,334.69 + 33,404.4 = 94,739.09lbfPath 1-1 is stronger than W1-1so it is acceptable per UG-41(b)(1).

Load for path 2-2 lesser of W or W2-2= 25,575.2 lbfPath 2-2 through (1), (4), (5), (6) = 27,248.84 + 38,504.14 + 27,248.84 + 38,504.14 = 131,505.96lbfPath 2-2 is stronger than W2-2so it is acceptable per UG-41(b)(1).

Load for path 3-3 lesser of W or W3-3= 61,458.87 lbfPath 3-3 through (2), (4), (5) = 61,334.69 + 38,504.14 + 27,248.84 = 127,087.67lbfPath 3-3 is stronger than W so it is acceptable per UG-41(b)(2).

38/108


41/110

Reinforcement Calculations for MAP

The vessel wall thickness governs the MAP of this nozzle.

UG-37 Area Calculation Summary (in2)

For P = 102.25 psi @ 70 FThe opening is adequately reinforced

UG-45Nozzle WallThickness

Summary(in)

The nozzlepasses UG-45

Arequired

Aavailable

A1 A2 A3 A5A

weldstreq tmin

3.073 3.1801 0.0001 0.5372 0.3352 2 0.3076 0.245 0.245

UG-41 Weld Failure Path Analysis Summary (lbf)All failurepaths are stronger than the applicable weld loads

Weld loadW

Weld loadW1-1

Path 1-1strength

Weld loadW2-2

Path 2-2strength

Weld loadW3-3

Path 3-3strength

61,458.87 55,226 94,739.09 25,575.2 131,505.96 68,387.2 127,087.67

UW-16 Weld Sizing Summary

Weld descriptionRequired weld

size (in)Actual weld

size (in)Status

Nozzle to pad fillet (Leg41) 0.196 0.2188 weld size is adequate

Pad to shell fillet (Leg42) 0.25 0.2625 weld size is adequate

Nozzle to inside shell fillet (Leg 43) 0.1960.2188

(corroded)weld size is adequate

Nozzle to pad groove (Upper) 0.196 0.25 weld size is adequate

Nozzle to shell groove (Lower) 0.196 0.25 weld size is adequate

Calculations for internal pressure 102.25 psi @ 70 F

Parallel Limit of reinforcement per UG-40

LR = MAX(d, Rn+ (tn- Cn) + (t - C))

= MAX(6.065, 3.0325 + (0.28 - 0) + (0.5 - 0))

= 6.065 in


LH = MIN(2.5*(t - C), 2.5*(tn- Cn) + te)

= MIN(2.5*(0.5 - 0), 2.5*(0.28 - 0) + 0.5)= 1.2 in


LI = MIN(h, 2.5*(t - C), 2.5*(ti- Cn- C))

= MIN(1, 2.5*(0.5 - 0), 2.5*(0.28 - 0 - 0))

= 0.7 in

39/108


42/110


trn = P*Rn/ (Sn*E - 0.6*P)

= 102.247*3.0325 / (17,100*1 - 0.6*102.247)

= 0.0182 in


tr = P*Ro/ (S*E + 0.4*P)

= 102.247*98 / (20,000*1 + 0.4*102.247)

= 0.5 in


tr = P*Ro/ (S*E + 0.4*P)

= 102.247*98 / (20,000*1 + 0.4*102.247)

= 0.5 in







A = d*tr

*F + 2*tn

*tr

*F*(1 - fr1

)

= 6.065*0.5*1 + 2*0.28*0.5*1*(1 - 0.855)

= 3.073in2




= 6.065*(1*0.5 - 1*0.5) - 2*0.28*(1*0.5 - 1*0.5)*(1 - 0.855)

= 0.0001 in2


= 2*(0.5 + 0.28)*(1*0.5 - 1*0.5) - 2*0.28*(1*0.5 - 1*0.5)*(1 - 0.855)

= 0 in2


= 5*(tn- trn)*fr2*t

40/108


43/110

= 5*(0.28 - 0.0182)*0.855*0.5

= 0.5596 in2

= 2*(tn- trn)*(2.5*tn+ te)*fr2= 2*(0.28 - 0.0182)*(2.5*0.28 + 0.5)*0.855

= 0.5372 in2


= 5*t*ti*fr2= 5*0.5*0.28*0.855

= 0.5985in2

= 5*ti*ti*fr2= 5*0.28*0.28*0.855

= 0.3352in2

= 2*h*ti*fr2= 2*1*0.28*0.855

= 0.4788in2

A41 = Leg2*fr3

= 0.31252*0.855

= 0.0835in2

A42 = Leg2*fr4

= 0.3752*1

= 0.1406in2

A43 = Leg2

*fr2= 0.31252*0.855

= 0.0835in2

A5 = (Dp- d - 2*tn)*te*fr4= (10.625 - 6.065 - 2*0.28)*0.5*1

= 2in2

Area = A1+ A2+ A3+ A41+ A42+ A43+ A5

= 0.0001 + 0.5372 + 0.3352 + 0.0835 + 0.1406 + 0.0835 + 2= 3.1801in2


UW-16(d) Weld Check



41/108


44/110

tc(actual) = 0.7*Leg = 0.7*0.3125 =0.2188 in



tw(actual) = 0.7*Leg = 0.7*0.375 = 0.2625 in



tc(actual) = 0.7*Leg = 0.7*0.3125 = 0.2188in









= 102.247*3.0325 / (17,100*1 - 0.6*102.247) + 0

= 0.0182 in


= max[ 0.0182 , 0 ]

= 0.0182 in

tb1 = P*Ro/ (S*E + 0.4*P) + Corrosion= 102.247*98 / (20,000*1 + 0.4*102.247) + 0

= 0.5 in


= max[ 0.5 , 0.0625 ]

= 0.5 in

tb = min[ tb3, tb1]

= min[ 0.245 , 0.5 ]

= 0.245 in


= max[ 0.0182 , 0.245 ]

= 0.245 in



42/108


45/110









(1) Inner fillet weld in shear

(/ 2)*Nozzle OD*Leg*Si= (/ 2)*6.625*0.3125*8,379 = 27,248.84 lbf


(3) Nozzle wall in shear(/ 2)*Mean nozzle dia*tn*Sn= (/ 2)*6.345*0.28*11,970 = 33,404.4 lbf

(4) Groove weld in tension

(/ 2)*Nozzle OD*tw

*Sg

= (/ 2)*6.625*0.25*14,800 = 38,504.14 lbf


(6) Upper groove weld in tension(/ 2)*Nozzle OD*tw*Sg= (/ 2)*6.625*0.25*14,800 = 38,504.14 lbf


W = (A - A1+ 2*tn*fr1*(E1*t - F*tr))*Sv= (3.073 - 0.0001 + 2*0.28*0.855*(1*0.5 - 1*0.5))*20,000

= 61,458.87lbf

W1-1 = (A2+ A5+ A41+ A42)*Sv= (0.5372 + 2 + 0.0835 + 0.1406)*20,000

= 55,226lbf

W2-2 = (A2+ A3+ A41+ A43+ 2*tn*t*fr1)*Sv= (0.5372 + 0.3352 + 0.0835 + 0.0835 + 2*0.28*0.5*0.855)*20,000

= 25,575.2lbf

W3-3 = (A2+ A3+ A5+ A41+ A42+ A43+ 2*tn*t*fr1)*Sv= (0.5372 + 0.3352 + 2 + 0.0835 + 0.1406 + 0.0835 + 2*0.28*0.5*0.855)*20,000

= 68,387.2lbf


43/108


46/110



44/108


47/110

Copy of Nozzle #2 (N3)


tw(lower)= 0.25 in

Leg41= 0.3125 in

tw(upper)= 0.25 in

Leg42= 0.375 inLeg43= 0.3125 in

hnew= 1 in

Dp= 10.625 in

te= 0.5 in




Orientation: 0




Nozzle

Access opening: No











Reinforcing Pad


Diameter: 10.625 in

Is split: No





48/110

Blind included: No






PWHT performed: No


46/108


49/110

Reinforcement Calculations for MAWP

The vessel wall thickness governs the MAWP of this nozzle.




Summary(in)


Arequired

Aavailable

A1 A2 A3 A5A

weldstreq tmin

3.073 3.1801 0.0001 0.5372 0.3352 2 0.3076 0.245 0.245


Weld loadW

Weld loadW1-1

Path 1-1strength

Weld loadW2-2

Path 2-2strength

Weld loadW3-3

Path 3-3strength

61,458.87 55,226 94,739.09 25,575.2 131,505.96 68,387.2 127,087.67




size (in)Status








Fig UCS-66.2 general note (1) applies.

Nozzle is impact test exempt to -155 F per UCS-66(b)(3) (coincident ratio = 0.0743).

Pad is impact test exempt per UG-20(f).

Nozzle UCS-66 governing thk: 0.245 in

Nozzle rated MDMT: -155 F

Pad UCS-66 governing thickness: 0.5 in

Pad rated MDMT: -20 F



= MAX(6.065, 3.0325 + (0.28 - 0) + (0.5 - 0))

= 6.065 in

47/108


50/110


LH = MIN(2.5*(t - C), 2.5*(tn- Cn) + te)

= MIN(2.5*(0.5 - 0), 2.5*(0.28 - 0) + 0.5)

= 1.2 in


LI = MIN(h, 2.5*(t - C), 2.5*(ti- Cn- C))

= MIN(1, 2.5*(0.5 - 0), 2.5*(0.28 - 0 - 0))= 0.7 in


trn = P*Rn/ (Sn*E - 0.6*P)

= 102.247*3.0325 / (17,100*1 - 0.6*102.247)

= 0.0182 in


tr = P*Ro/ (S*E + 0.4*P)

= 102.247*98 / (20,000*1 + 0.4*102.247)

= 0.5 in


tr = P*Ro/ (S*E + 0.4*P)

= 102.247*98 / (20,000*1 + 0.4*102.247)

= 0.5 in







A = d*tr*F + 2*tn*tr*F*(1 - fr1)

= 6.065*0.5*1 + 2*0.28*0.5*1*(1 - 0.855)

= 3.073in2




48/108


51/110

= 6.065*(1*0.5 - 1*0.5) - 2*0.28*(1*0.5 - 1*0.5)*(1 - 0.855)

= 0.0001 in2


= 2*(0.5 + 0.28)*(1*0.5 - 1*0.5) - 2*0.28*(1*0.5 - 1*0.5)*(1 - 0.855)

= 0 in2


= 5*(tn- trn)*fr2*t

= 5*(0.28 - 0.0182)*0.855*0.5

= 0.5596 in2

= 2*(tn- trn)*(2.5*tn+ te)*fr2= 2*(0.28 - 0.0182)*(2.5*0.28 + 0.5)*0.855

= 0.5372 in2


= 5*t*ti*fr2= 5*0.5*0.28*0.855

= 0.5985in2

= 5*ti*ti*fr2= 5*0.28*0.28*0.855

= 0.3352in2

= 2*h*ti*fr2= 2*1*0.28*0.855

= 0.4788in2

A41 = Leg2*fr3

= 0.31252*0.855

= 0.0835in2

A42 = Leg2*fr4

= 0.3752*1

= 0.1406in2

A43 = Leg2*fr2

= 0.31252

*0.855= 0.0835in2

A5 = (Dp- d - 2*tn)*te*fr4= (10.625 - 6.065 - 2*0.28)*0.5*1

= 2in2

49/108


52/110

Area = A1+ A2+ A3+ A41+ A42+ A43+ A5= 0.0001 + 0.5372 + 0.3352 + 0.0835 + 0.1406 + 0.0835 + 2

= 3.1801in2


UW-16(d) Weld Check



tc(actual) = 0.7*Leg = 0.7*0.3125 =0.2188 in



tw(actual) = 0.7*Leg = 0.7*0.375 = 0.2625 in



tc(actual) = 0.7*Leg = 0.7*0.3125 = 0.2188in









= 102.247*3.0325 / (17,100*1 - 0.6*102.247) + 0

= 0.0182 in


= max[ 0.0182 , 0 ]

= 0.0182 in


= 102.247*98 / (20,000*1 + 0.4*102.247) + 0

= 0.5 in


= max[ 0.5 , 0.0625 ]

= 0.5 in

tb = min[ tb3, tb1]

= min[ 0.245 , 0.5 ]

50/108


53/110

= 0.245 in


= max[ 0.0182 , 0.245 ]

= 0.245 in




















W = (A - A1+ 2*tn*fr1*(E1*t - F*tr))*Sv= (3.073 - 0.0001 + 2*0.28*0.855*(1*0.5 - 1*0.5))*20,000

= 61,458.87lbf

W1-1 = (A2+ A5+ A41+ A42)*Sv= (0.5372 + 2 + 0.0835 + 0.1406)*20,000

= 55,226lbf

W2-2 = (A2+ A3+ A41+ A43+ 2*tn*t*fr1)*Sv= (0.5372 + 0.3352 + 0.0835 + 0.0835 + 2*0.28*0.5*0.855)*20,000

51/108


54/110


55/110






Summary(in)


Arequired

Aavailable

A1 A2 A3 A5A

weldstreq tmin

3.073 3.1801 0.0001 0.5372 0.3352 2 0.3076 0.245 0.245


Weld loadW

Weld loadW1-1

Path 1-1strength

Weld loadW2-2

Path 2-2strength

Weld loadW3-3

Path 3-3strength

61,458.87 55,226 94,739.09 25,575.2 131,505.96 68,387.2 127,087.67




size (in)Status










= MAX(6.065, 3.0325 + (0.28 - 0) + (0.5 - 0))

= 6.065 in


LH = MIN(2.5*(t - C), 2.5*(tn- Cn) + te)

= MIN(2.5*(0.5 - 0), 2.5*(0.28 - 0) + 0.5)= 1.2 in


LI = MIN(h, 2.5*(t - C), 2.5*(ti- Cn- C))

= MIN(1, 2.5*(0.5 - 0), 2.5*(0.28 - 0 - 0))

= 0.7 in

53/108


56/110


trn = P*Rn/ (Sn*E - 0.6*P)

= 102.247*3.0325 / (17,100*1 - 0.6*102.247)

= 0.0182 in


tr = P*Ro/ (S*E + 0.4*P)

= 102.247*98 / (20,000*1 + 0.4*102.247)

= 0.5 in


tr = P*Ro/ (S*E + 0.4*P)

= 102.247*98 / (20,000*1 + 0.4*102.247)

= 0.5 in







A = d*tr

*F + 2*tn

*tr

*F*(1 - fr1

)

= 6.065*0.5*1 + 2*0.28*0.5*1*(1 - 0.855)

= 3.073in2




= 6.065*(1*0.5 - 1*0.5) - 2*0.28*(1*0.5 - 1*0.5)*(1 - 0.855)

= 0.0001 in2


= 2*(0.5 + 0.28)*(1*0.5 - 1*0.5) - 2*0.28*(1*0.5 - 1*0.5)*(1 - 0.855)

= 0 in2


= 5*(tn- trn)*fr2*t

54/108


57/110

= 5*(0.28 - 0.0182)*0.855*0.5

= 0.5596 in2

= 2*(tn- trn)*(2.5*tn+ te)*fr2= 2*(0.28 - 0.0182)*(2.5*0.28 + 0.5)*0.855

= 0.5372 in2


= 5*t*ti*fr2= 5*0.5*0.28*0.855

= 0.5985in2

= 5*ti*ti*fr2= 5*0.28*0.28*0.855

= 0.3352in2

= 2*h*ti*fr2= 2*1*0.28*0.855

= 0.4788in2

A41 = Leg2*fr3

= 0.31252*0.855

= 0.0835in2

A42 = Leg2*fr4

= 0.3752*1

= 0.1406in2

A43 = Leg2

*fr2= 0.31252*0.855

= 0.0835in2

A5 = (Dp- d - 2*tn)*te*fr4= (10.625 - 6.065 - 2*0.28)*0.5*1

= 2in2

Area = A1+ A2+ A3+ A41+ A42+ A43+ A5

= 0.0001 + 0.5372 + 0.3352 + 0.0835 + 0.1406 + 0.0835 + 2= 3.1801in2


UW-16(d) Weld Check



55/108


58/110

tc(actual) = 0.7*Leg = 0.7*0.3125 =0.2188 in



tw(actual) = 0.7*Leg = 0.7*0.375 = 0.2625 in



tc(actual) = 0.7*Leg = 0.7*0.3125 = 0.2188in









= 102.247*3.0325 / (17,100*1 - 0.6*102.247) + 0

= 0.0182 in


= max[ 0.0182 , 0 ]

= 0.0182 in


= 0.5 in


= max[ 0.5 , 0.0625 ]

= 0.5 in

tb = min[ tb3, tb1]

= min[ 0.245 , 0.5 ]

= 0.245 in


= max[ 0.0182 , 0.245 ]

= 0.245 in



56/108


59/110














(/ 2)*Nozzle OD*tw

*Sg

= (/ 2)*6.625*0.25*14,800 = 38,504.14 lbf




W = (A - A1+ 2*tn*fr1*(E1*t - F*tr))*Sv= (3.073 - 0.0001 + 2*0.28*0.855*(1*0.5 - 1*0.5))*20,000

= 61,458.87lbf

W1-1 = (A2+ A5+ A41+ A42)*Sv= (0.5372 + 2 + 0.0835 + 0.1406)*20,000

= 55,226lbf

W2-2 = (A2+ A3+ A41+ A43+ 2*tn*t*fr1)*Sv= (0.5372 + 0.3352 + 0.0835 + 0.0835 + 2*0.28*0.5*0.855)*20,000

= 25,575.2lbf

W3-3 = (A2+ A3+ A5+ A41+ A42+ A43+ 2*tn*t*fr1)*Sv= (0.5372 + 0.3352 + 2 + 0.0835 + 0.1406 + 0.0835 + 2*0.28*0.5*0.855)*20,000

= 68,387.2lbf


57/108


60/110


61/110

Copy of Copy of Nozzle #2 (N4)


tw(lower)= 0.25 in

Leg41= 0.3125 in

tw(upper)= 0.25 in

Leg42= 0.375 inLeg43= 0.3125 in

hnew= 1 in

Dp= 10.625 in

te= 0.5 in




Orientation: 0




Nozzle

Access opening: No











Reinforcing Pad


Diameter: 10.625 in

Is split: No





62/110

Blind included: No






PWHT performed: No


60/108


63/110






Summary(in)


Arequired

Aavailable

A1 A2 A3 A5A

weldstreq tmin

3.073 3.1801 0.0001 0.5372 0.3352 2 0.3076 0.245 0.245


Weld loadW

Weld loadW1-1

Path 1-1strength

Weld loadW2-2

Path 2-2strength

Weld loadW3-3

Path 3-3strength

61,458.87 55,226 94,739.09 25,575.2 131,505.96 68,387.2 127,087.67




size (in)Status

















= MAX(6.065, 3.0325 + (0.28 - 0) + (0.5 - 0))

= 6.065 in

61/108


64/110


65/110


66/110

Area = A1+ A2+ A3+ A41+ A42+ A43+ A5= 0.0001 + 0.5372 + 0.3352 + 0.0835 + 0.1406 + 0.0835 + 2

= 3.1801in2


UW-16(d) Weld Check



tc(actual) = 0.7*Leg = 0.7*0.3125 =0.2188 in



tw(actual) = 0.7*Leg = 0.7*0.375 = 0.2625 in



tc(actual) = 0.7*Leg = 0.7*0.3125 = 0.2188in









= 102.247*3.0325 / (17,100*1 - 0.6*102.247) + 0

= 0.0182 in


= max[ 0.0182 , 0 ]

= 0.0182 in


= 102.247*98 / (20,000*1 + 0.4*102.247) + 0

= 0.5 in


= max[ 0.5 , 0.0625 ]

= 0.5 in

tb = min[ tb3, tb1]

= min[ 0.245 , 0.5 ]

64/108


67/110


68/110

= 25,575.2lbf

W3-3 = (A2+ A3+ A5+ A41+ A42+ A43+ 2*tn*t*fr1)*Sv= (0.5372 + 0.3352 + 2 + 0.0835 + 0.1406 + 0.0835 + 2*0.28*0.5*0.855)*20,000

= 68,387.2lbf




66/108


69/110






Summary(in)


Arequired

Aavailable

A1 A2 A3 A5A

weldstreq tmin

3.073 3.1801 0.0001 0.5372 0.3352 2 0.3076 0.245 0.245


Weld loadW

Weld loadW1-1

Path 1-1strength

Weld loadW2-2

Path 2-2strength

Weld loadW3-3

Path 3-3strength

61,458.87 55,226 94,739.09 25,575.2 131,505.96 68,387.2 127,087.67




size (in)Status










= MAX(6.065, 3.0325 + (0.28 - 0) + (0.5 - 0))

= 6.065 in


LH = MIN(2.5*(t - C), 2.5*(tn- Cn) + te)

= MIN(2.5*(0.5 - 0), 2.5*(0.28 - 0) + 0.5)= 1.2 in


LI = MIN(h, 2.5*(t - C), 2.5*(ti- Cn- C))

= MIN(1, 2.5*(0.5 - 0), 2.5*(0.28 - 0 - 0))

= 0.7 in

67/108


70/110


trn = P*Rn/ (Sn*E - 0.6*P)

= 102.247*3.0325 / (17,100*1 - 0.6*102.247)

= 0.0182 in


tr = P*Ro/ (S*E + 0.4*P)

= 102.247*98 / (20,000*1 + 0.4*102.247)

= 0.5 in


tr = P*Ro/ (S*E + 0.4*P)

= 102.247*98 / (20,000*1 + 0.4*102.247)

= 0.5 in







A = d*tr

*F + 2*tn

*tr

*F*(1 - fr1

)

= 6.065*0.5*1 + 2*0.28*0.5*1*(1 - 0.855)

= 3.073in2




= 6.065*(1*0.5 - 1*0.5) - 2*0.28*(1*0.5 - 1*0.5)*(1 - 0.855)

= 0.0001 in2


= 2*(0.5 + 0.28)*(1*0.5 - 1*0.5) - 2*0.28*(1*0.5 - 1*0.5)*(1 - 0.855)

= 0 in2


= 5*(tn- trn)*fr2*t

68/108


71/110

= 5*(0.28 - 0.0182)*0.855*0.5

= 0.5596 in2

= 2*(tn- trn)*(2.5*tn+ te)*fr2= 2*(0.28 - 0.0182)*(2.5*0.28 + 0.5)*0.855

= 0.5372 in2


= 5*t*ti*fr2= 5*0.5*0.28*0.855

= 0.5985in2

= 5*ti*ti*fr2= 5*0.28*0.28*0.855

= 0.3352in2

= 2*h*ti*fr2= 2*1*0.28*0.855

= 0.4788in2

A41 = Leg2*fr3

= 0.31252*0.855

= 0.0835in2

A42 = Leg2*fr4

= 0.3752*1

= 0.1406in2

A43 = Leg2

*fr2= 0.31252*0.855

= 0.0835in2

A5 = (Dp- d - 2*tn)*te*fr4= (10.625 - 6.065 - 2*0.28)*0.5*1

= 2in2

Area = A1+ A2+ A3+ A41+ A42+ A43+ A5

= 0.0001 + 0.5372 + 0.3352 + 0.0835 + 0.1406 + 0.0835 + 2= 3.1801in2


UW-16(d) Weld Check



69/108


72/110

tc(actual) = 0.7*Leg = 0.7*0.3125 =0.2188 in



tw(actual) = 0.7*Leg = 0.7*0.375 = 0.2625 in



tc(actual) = 0.7*Leg = 0.7*0.3125 = 0.2188in









= 102.247*3.0325 / (17,100*1 - 0.6*102.247) + 0

= 0.0182 in


= max[ 0.0182 , 0 ]

= 0.0182 in


= 0.5 in


= max[ 0.5 , 0.0625 ]

= 0.5 in

tb = min[ tb3, tb1]

= min[ 0.245 , 0.5 ]

= 0.245 in


= max[ 0.0182 , 0.245 ]

= 0.245 in



70/108


73/110














(/ 2)*Nozzle OD*tw

*Sg

= (/ 2)*6.625*0.25*14,800 = 38,504.14 lbf




W = (A - A1+ 2*tn*fr1*(E1*t - F*tr))*Sv= (3.073 - 0.0001 + 2*0.28*0.855*(1*0.5 - 1*0.5))*20,000

= 61,458.87lbf

W1-1 = (A2+ A5+ A41+ A42)*Sv= (0.5372 + 2 + 0.0835 + 0.1406)*20,000

= 55,226lbf

W2-2 = (A2+ A3+ A41+ A43+ 2*tn*t*fr1)*Sv= (0.5372 + 0.3352 + 0.0835 + 0.0835 + 2*0.28*0.5*0.855)*20,000

= 25,575.2lbf

W3-3 = (A2+ A3+ A5+ A41+ A42+ A43+ 2*tn*t*fr1)*Sv= (0.5372 + 0.3352 + 2 + 0.0835 + 0.1406 + 0.0835 + 2*0.28*0.5*0.855)*20,000

= 68,387.2lbf


71/108


74/110



72/108


75/110


76/110

Blind included: No






PWHT performed: No


74/108


77/110






Summary(in)


Arequired

Aavailable

A1 A2 A3 A5A

weldstreq tmin

3.073 3.1801 0.0001 0.5372 0.3352 2 0.3076 0.245 0.245


Weld loadW

Weld loadW1-1

Path 1-1strength

Weld loadW2-2

Path 2-2strength

Weld loadW3-3

Path 3-3strength

61,458.87 55,226 94,739.09 25,575.2 131,505.96 68,387.2 127,087.67




size (in)Status

















= MAX(6.065, 3.0325 + (0.28 - 0) + (0.5 - 0))

= 6.065 in

75/108


78/110


79/110


80/110

Area = A1+ A2+ A3+ A41+ A42+ A43+ A5= 0.0001 + 0.5372 + 0.3352 + 0.0835 + 0.1406 + 0.0835 + 2

= 3.1801in2


UW-16(d) Weld Check



tc(actual) = 0.7*Leg = 0.7*0.3125 =0.2188 in



tw(actual) = 0.7*Leg = 0.7*0.375 = 0.2625 in



tc(actual) = 0.7*Leg = 0.7*0.3125 = 0.2188in









= 102.247*3.0325 / (17,100*1 - 0.6*102.247) + 0

= 0.0182 in


= max[ 0.0182 , 0 ]

= 0.0182 in


= 102.247*98 / (20,000*1 + 0.4*102.247) + 0

= 0.5 in


= max[ 0.5 , 0.0625 ]

= 0.5 in

tb = min[ tb3, tb1]

= min[ 0.245 , 0.5 ]

78/108


81/110

= 0.245 in


= max[ 0.0182 , 0.245 ]

= 0.245 in




















W = (A - A1+ 2*tn*fr1*(E1*t - F*tr))*Sv= (3.073 - 0.0001 + 2*0.28*0.855*(1*0.5 - 1*0.5))*20,000

= 61,458.87lbf

W1-1 = (A2+ A5+ A41+ A42)*Sv= (0.5372 + 2 + 0.0835 + 0.1406)*20,000

= 55,226lbf

W2-2 = (A2+ A3+ A41+ A43+ 2*tn*t*fr1)*Sv= (0.5372 + 0.3352 + 0.0835 + 0.0835 + 2*0.28*0.5*0.855)*20,000

79/108


82/110

= 25,575.2lbf

W3-3 = (A2+ A3+ A5+ A41+ A42+ A43+ 2*tn*t*fr1)*Sv= (0.5372 + 0.3352 + 2 + 0.0835 + 0.1406 + 0.0835 + 2*0.28*0.5*0.855)*20,000

= 68,387.2lbf



Load for path 3-3 lesser of W or W3-3= 61,458.87 lbfPath 3-3 through (2), (4), (5

Tcp de Plataforma

Documents

Transcript of Tcp de Plataforma