pipe stress analysis report - portal.cimtas.com

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THTF058 HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION PROJECT CONTRACT Nº THTF-2018-058 UNIT Nº 150 CONTRACTOR DOC No: 54TH58-SS-115-001 SH/OF 1/65 STAR DOCUMENT No. 150-L-ZE-0097001-015 REV 0 PIPE STRESS ANALYSIS REPORT 0 11.06.2020 FOR REVIEW R.A. S.O. S.T. REV. ISSUE DATE REASON FOR ISSUE PREPARED BY CHECKED BY APPROVED BY

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Page 1: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

1/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

PIPE STRESS ANALYSIS REPORT

0 11.06.2020 FOR REVIEW R.A. S.O. S.T.

REV. ISSUE DATE REASON FOR ISSUE PREPARED

BY CHECKED

BY APPROVED

BY

Page 2: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

2/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

REVISION INDEX

Rev. Date Rev. Description

11.06.2020 0 Issued for Review

Page 3: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

3/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

Contents

REVISION INDEX ....................................................................................................................................... 2 

1.1  SCOPE OF WORK ............................................................................................................................................. 4 

2  CALCULATION PROGRAM ............................................................................................................... 4 

3  CODES ................................................................................................................................................ 4 

4  REFERENCES .................................................................................................................................... 4 

5  ASSUMPTIONS, SUPPORT DESCRIPTIONS AND CONCLUSIONS ............................................... 6 

5.1  ASSUMPTIONS ................................................................................................................................................ 6 5.2  SUPPORT DESCRIPTIONS ................................................................................................................................ 7 5.3  CONCLUSIONS ................................................................................................................................................ 8 

6  CALCULATION BASICS .................................................................................................................... 9 

6.1  CALCULATION PROGRAM ................................................................................................................................. 9 6.2  CALCULATION RULE ......................................................................................................................................... 9 

7  SYSTEM DESCRIPTION .................................................................................................................. 10 

7.1  DIMENSIONS AND CALCULATION DATA: ............................................................................................................ 10 7.1.1  Pipe dimensions ................................................................................................................................. 10 7.1.2  Structrual section dimensions ............................................................................................................. 11 

7.2  LINE MASSES ................................................................................................................................................ 11 7.3  COMPONENTS ............................................................................................................................................... 11 

8  LOAD CASES ................................................................................................................................... 12 

8.1  OVERVIEW .................................................................................................................................................... 12 8.2  GLOBAL LOADS ............................................................................................................................................. 12 8.3  SPECIFIC LOADS OF LOAD CASES ................................................................................................................... 12 

9  RESULTS .......................................................................................................................................... 15 

9.1  SPRING DESIGN ............................................................................................................................................ 15 9.2  STRESS EVALUATION SUMMARY ..................................................................................................................... 15 9.1  EXPANSION JOINT RESULTS ........................................................................................................................... 16 9.2  LOADS ON NOZZLES ...................................................................................................................................... 16 9.3  EXTREME LOADS ON SUPPORTS ..................................................................................................................... 16 9.4  LOADS ON SUPPORTS WITH OPERATIONAL CASES ............................................................................................ 17 

10  GRAPHICAL OUTPUTS ................................................................................................................ 42 

10.1  GRAPHICS / PLOTS ........................................................................................................................................ 42 

11  APPENDICES ................................................................................................................................ 65 

11.1  APPENDIX A-DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION .. 65 11.2  APPENDIX B- INTERNAL PRESSURE ANALYSIS ................................................................................................ 65 11.3  APPENDIX C- STRAIGHT PIPE REQUIRED MINIMUM WALL THICKNESS CALCULATION......................................... 65 

Page 4: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

4/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

Scope of work and results

1.1 Scope of work

For the calculation system pipes

3-P150-037-30-BA28P-NI

stress calculation has been carried out, to evaluate the system with regard to dead load, thermal expansion and additional loads. In this calculation, existing pipe lines are only used for consideration of calculation effects to new lines.

This calculation covers the analysis of:

flexibility of the pipe system geometry

stresses in pipes and fittings

pipe displacement

pipe deformations

loads on components

loads on supports

2 Calculation program The pipe stress analysis has been performed by the program Rohr2, Version 32.1.

3 Codes The calculation and the stress analysis were carried out according to ASME B31.3-2016 Edition.

4 References Following documents have been considered in this document. Here after only the document # will be referred for the below items in this document.

# DOC. REV. DESCRIPTION

1 3-P150-037-30-BA28P-NI 0 Isometric

2 6-P150-037-16-BA28P-NI (EXISTING) - 3D Smart Plant model for routing & existing support

3 6-P150-024-04-BA28P-NI (EXISTING) - 3D Smart Plant model for routing & existing support

4 000-L-EE-0020129 3 Piping Material Specification

5 000-L-EE-0020136 3 Piping Support General Specification

6 150-L-ED-0114008 X0A Piping Line List

7 150-L-ZE-0057001-015 0 Pipe Support List

Calculated system overview figure is given below:

Page 5: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

5/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

Page 6: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

6/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

5 Assumptions, support descriptions and conclusions

5.1 Assumptions

After tie in points of the stress analysed lines, existing lines are inserted to stress analyses up to the point of first fix or first guide support. In graphical output section this differences can be seen.

Below assumptions are made regarding earthquake calculations in accordance with DBYBHY-2007,

o Seismic Zone No : 1

o Soil Class : Z4

o Building Importance Factor : 1.5

o Structure Type Coefficient “R” : 4.2

o Spectrum Coefficient S(T) : 2.5

Therefore, the static accelerations to be applied to the piping system are calculated as per following rates;

ax= 3.54 m/s² (0.36 g)

aZ= 1.18 m/s² (0.12 g)

ay= 3.54 m/s² (0.36 g)

Wind and snow loads are neglected.

In this document and it‘s appendices Cordinate System : +Y direction (North), +X direction (East), +Z Direction (Up)

For condition FV@190 C which is stated in “REMARKS” column in the regarding line list; checked only required straight pipe minimum wall thickness and length is assumed the longest straight pipe length (12,3m) as per ASME Sec.VIII Div.1 showed in the Appendix C. For detail see Appendix-C.

Route, dimensions, line numbers of existing line were read from SP3D model; also support types visually viewed from the SP3D model, otherwise please advise.

Valves weights are assumed as showed below table.

Size Check Valve  Gate Valve  Globe Valve 

(kg)  (kg)  (kg) 

3”  50  50  62 

2"  ‐  ‐  36 

Page 7: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

7/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

5.2 Support Descriptions

Supports‘ Degree of Freedoms

NODE  LINE NO  SUPPORT NO  SUPPORT TYPE CO. SYSTEM  ‐X(mm)  +X(mm)  ‐Y(mm)  +Y(mm)  ‐Z(mm)  +Z(mm) 

173  3‐P150‐037‐30‐BA28P‐NI  POS009‐P150‐037‐30  GUIDE  global  No Gap  No Gap  Free  Free  Free  No Gap 

175  3‐P150‐037‐30‐BA28P‐NI  POS010‐P150‐037‐30  GUIDE  global  Free  Free  No Gap  No Gap  Free  No Gap 

81 6‐P150‐024‐04‐BA28P‐NI (EXISTING2)  EXISTING SUPPORT‐2  GUIDE  global  Free  Free  No Gap  No Gap  Free  No Gap 

161  4‐P150‐037‐16‐BA28P‐NI (EXISTING)  EXISTING SUPPORT‐1  GUIDE  global  Free  Free  No Gap  No Gap  Free  No Gap 

167  4‐P150‐037‐16‐BA28P‐NI (EXISTING) POS001‐P150‐037‐16 (EXISTING) 

AXIAL STOP + GUIDE  global  No Gap  No Gap  No Gap  No Gap  Free  No Gap 

177  3‐P150‐037‐30‐BA28P‐NI  POS011‐P150‐037‐30  GUIDE  global  Free  Free  No Gap  No Gap  Free  No Gap 

179  3‐P150‐037‐30‐BA28P‐NI  POS012‐P150‐037‐30  GUIDE  global  Free  Free  No Gap  No Gap  Free  No Gap 

181  3‐P150‐037‐30‐BA28P‐NI  POS004‐P150‐037‐30  GUIDE  global  Free  Free  No Gap  No Gap  Free  No Gap 

183  3‐P150‐037‐30‐BA28P‐NI  POS003‐P150‐037‐30  GUIDE  global  Free  Free  No Gap  No Gap  Free  No Gap 

185  3‐P150‐037‐30‐BA28P‐NI  POS014‐P150‐037‐30 AXIAL STOP + GUIDE  global  No Gap  No Gap  No Gap  No Gap  Free  No Gap 

189  3‐P150‐037‐30‐BA28P‐NI  POS006‐P150‐037‐30 AXIAL STOP + GUIDE  global  No Gap  No Gap  No Gap  No Gap  Free  No Gap 

197  3‐P150‐037‐30‐BA28P‐NI  POS007‐P150‐037‐30  GUIDE  global  Free  Free  No Gap  No Gap  Free  No Gap 

205  3‐P150‐037‐30‐BA28P‐NI  POS001‐P150‐037‐30 AXIAL STOP + GUIDE  global  No Gap  No Gap  No Gap  No Gap  Free  No Gap 

207  3‐P150‐037‐30‐BA28P‐NI  POS008‐P150‐037‐30  GUIDE  global  Free  Free  No Gap  No Gap  Free  No Gap 

211  3‐P150‐037‐30‐BA28P‐NI  POS015‐P150‐037‐30 AXIAL STOP + GUIDE  global  No Gap  No Gap  No Gap  No Gap  Free  No Gap 

Page 8: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

8/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

NODE  LINE NO  SUPPORT NO  SUPPORT TYPE CO. SYSTEM  ‐X(mm)  +X(mm)  ‐Y(mm)  +Y(mm)  ‐Z(mm)  +Z(mm) 

215 6‐P150‐024‐04‐BA28P‐NI (EXISTING2) 

POS001‐P150‐039‐03 (EXISTING) 

AXIAL STOP + GUIDE  global  No Gap  No Gap  No Gap  No Gap  Free  No Gap 

217  3‐P150‐037‐30‐BA28P‐NI  POS013‐P150‐037‐30  GUIDE  global  No Gap  No Gap  Free  Free  Free  No Gap 

223  3‐P150‐037‐30‐BA28P‐NI  POS002‐P150‐037‐30 AXIAL STOP + GUIDE  global  No Gap  No Gap  No Gap  No Gap  Free  No Gap 

225  3‐P150‐037‐30‐BA28P‐NI  POS005‐P150‐037‐30 AXIAL STOP + GUIDE  global  No Gap  No Gap  No Gap  No Gap  Free  No Gap 

Density of steam is assumed as 2,8 kg/m³.

Cordinate System : +Y direction (North), +X direction (East), +Z Direction (Up)

Supports are evaluated based on functionality.

5.3 Conclusions

Sustained, expansion, occasional stress results are under the code limits at all internal pressure design conditions.

Page 9: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

9/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

6 Calculation Basics

6.1 Calculation program

The pipe stresses have been calculated using the program ROHR2, rev. 32.1.

A detailed description of both, the theoretical aspects and its practical application is given in the ROHR2-manual. The program provides solutions for static and dynamic analysis of 3-D pipe systems and gene-ral framework structures.

6.2 Calculation rule

The calculation was carried out acc. to ASME B31.3.

Page 10: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

10/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

7 System description This calculation includes the following lines / drawings:

3-P150-037-30-BA28P-NI 6-P150-024-04-BA28P-NI

(EXISTING2) 4-P150-037-16-BA28P-NI (EXISTING)

The following general parameters were considered:

Density of medium: 735.0 kg/m³, 0.0 kg/m³

Assembly temperature: 18.0 °C

The density of medium is considered for the calculation of the line masses of the pipes. The thermal expansion is calculated due to the difference between assembly temperature and operation temperature.

7.1 Dimensions and calculation data:

7.1.1 Pipe dimensions

Dimension Da [mm]

s [mm]

Material

Insul.thickn. [mm]

Tin-plate [mm]

Calc. temp. [°C]

Calc. pressure [bar(g)]

Page 11: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

11/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

Dimension Da [mm]

s [mm]

Material

Insul.thickn. [mm]

Tin-plate [mm]

Calc. temp. [°C]

Calc. pressure [bar(g)]

NPS2.0 60.33 5.54 SA106B 0.00 0.00 190.0 20.50 NPS3.0 88.90 5.49 SA106B 0.00 0.00 190.0 20.50 NPS4.0 114.30 6.02 SA106B 0.00 0.00 190.0 20.50 NPS6.0 168.27 7.11 SA106B 0.00 0.00 190.0 20.50

7.1.2 Structrual section dimensions

7.2 Line masses

The following table shows the line masses of the pipes consisting of pipe weight and insulation weight. <----------Dimension [mm]----------> <-----------Density [kg/m³]-----------> <------------Line mass [kg/m]------------>

DA S Ins Jack Pipe Ins Jack Med Pipe Ins Med Total168.27 7.11 0 0.0 7750 0 0 0 27.9 0.0 0.0 27.9114.30 6.02 0 0.0 7750 0 0 0 15.9 0.0 0.0 15.9

88.90 5.49 0 0.0 7750 0 0 0 11.1 0.0 0.0 11.160.33 5.54 0 0.0 7750 0 0 0 7.4 0.0 0.0 7.4

Under consideration of the density of the medium from load case Dead weight the following line masses are determined: <----------Dimension [mm]----------> <-----------Density [kg/m³]-----------> <------------Line mass [kg/m]------------>

DA S Ins Jack Pipe Ins Jack Med Pipe Ins Med Total168.27 7.11 0 0.0 7750 0 0 735 27.9 0.0 13.7 41.6114.30 6.02 0 0.0 7750 0 0 735 15.9 0.0 6.0 21.9

88.90 5.49 0 0.0 7750 0 0 735 11.1 0.0 3.5 14.688.90 5.49 0 0.0 7750 0 0 0 11.1 0.0 0.0 11.160.33 5.54 0 0.0 7750 0 0 735 7.4 0.0 1.4 8.8

7.3 Components

The following components are considered by the calculation:

Instruments: Nominal diameter

Design pressure [bar(g)]

Length [mm]

Weight

[kg]

Description

NPS3 64.00 318 62.00 3" GATE VALVE NPS2 16.00 267 36.00 2" GLOBE VALVE NPS3 64.00 272 62.00 3 GLOBE VALVE NPS3 64.00 282 50.00 NPS3 64.00 318 50.00

Flanges: Dimension Norm PN

[bar(g)]Weight

[kg]NPS3 ASME B16.5 300 51.02 6.80NPS2 ASME B16.5 300 51.02 4.08

Page 12: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

12/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

8 Load cases

8.1 Overview

The calculation includes the following load cases (LC):

Loadcase Category Type of Calculation Dead load Primary loads - Dead load Theory 1. order Operation1 Secondary loads - Thermal expansion Nonlinear boundary conditions 1. order Steam Out Con1 Secondary loads - Thermal expansion Nonlinear boundary conditions 1. order Operation2 Secondary loads - Thermal expansion Nonlinear boundary conditions 1. order Earthquake Occasional primary loads - Earthquake

static Theory 1. order

Pressure test Primary loads - Pressure test Theory 1. order

8.2 Global loads

The following global loads are taken into consideration for the different loadcases:

Loadcase axial thermal

expansion

axial expansion due

to operation pressure

Upward bend due to

operation pressure

Acceleration due to gravity

Friction Forces due to

internal pressure

Dead load x x Operation1 x x x x x Steam Out Con1 x x x x x Operation2 x x x x x Earthquake Pressure test x x

8.3 Specific loads of load cases

Dead load

This load case includes loads from internal pressure, and weight from pipe, insulation and medium. In addition loads from internal pressure and forces due to internal pressure at axial expansion joints are taken into consideration.

Dead load Operation data

Operation pressure [bar(g)]

Operation temperature

[°C]

Density medium [kg/m³]

used in Pipeline

20.50 190.0 735.0 4-P150-037-16-BA28P-NI (EXISTING), 3-P150-037-30-BA28P-NI, 6-P150-024-04-BA28P-NI (EXISTING2)

0.00 190.0 0.0 4-P150-037-16-BA28P-NI (EXISTING), 3-P150-037-30-BA28P-NI, 6-P150-024-04-BA28P-NI (EXISTING2)

Page 13: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

13/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

Operation1 Operation data

Operation pressure [bar(g)]

Operation temperature

[°C]

Density medium [kg/m³]

used in Pipeline

20.50 190.0 735.0 4-P150-037-16-BA28P-NI (EXISTING), 3-P150-037-30-BA28P-NI, 6-P150-024-04-BA28P-NI (EXISTING2)

0.00 190.0 0.0 4-P150-037-16-BA28P-NI (EXISTING), 3-P150-037-30-BA28P-NI, 6-P150-024-04-BA28P-NI (EXISTING2)

Steam Out Con1 Operation data

Operation pressure [bar(g)]

Operation temperature

[°C]

Density medium [kg/m³]

used in Pipeline

20.50 190.0 2.8 4-P150-037-16-BA28P-NI (EXISTING), 3-P150-037-30-BA28P-NI, 6-P150-024-04-BA28P-NI (EXISTING2)

0.00 190.0 0.0 4-P150-037-16-BA28P-NI (EXISTING), 3-P150-037-30-BA28P-NI, 6-P150-024-04-BA28P-NI (EXISTING2)

Operation2 Operation data

Operation pressure [bar(g)]

Operation temperature

[°C]

Density medium [kg/m³]

used in Pipeline

20.50 38.0 735.0 4-P150-037-16-BA28P-NI (EXISTING), 3-P150-037-30-BA28P-NI, 6-P150-024-04-BA28P-NI (EXISTING2)

0.00 38.0 0.0 4-P150-037-16-BA28P-NI (EXISTING), 3-P150-037-30-BA28P-NI, 6-P150-024-04-BA28P-NI (EXISTING2)

Earthquake Operation data

Operation pressure [bar(g)]

Operation temperature

[°C]

Density medium [kg/m³]

used in Pipeline

20.50 190.0 735.0 4-P150-037-16-BA28P-NI (EXISTING), 3-P150-037-30-BA28P-NI, 6-P150-024-04-BA28P-NI (EXISTING2)

0.00 190.0 0.0 4-P150-037-16-BA28P-NI (EXISTING), 3-P150-037-30-BA28P-NI, 6-P150-024-04-BA28P-NI (EXISTING2)

Accelerations Acceleration in X: 3.540 m/s². Acceleration in Y: 3.540 m/s². Acceleration in Z: 1.180 m/s². Pressure test

Page 14: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

14/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

Operation data

Operation pressure [bar(g)]

Operation temperature

[°C]

Density medium [kg/m³]

used in Pipeline

76.00 20.0 1000.0 4-P150-037-16-BA28P-NI (EXISTING), 3-P150-037-30-BA28P-NI, 6-P150-024-04-BA28P-NI (EXISTING2)

0.00 20.0 0.0 4-P150-037-16-BA28P-NI (EXISTING), 3-P150-037-30-BA28P-NI, 6-P150-024-04-BA28P-NI (EXISTING2)

Page 15: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

15/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

9 Results

9.1 Spring Design

There is no spring support on the pipelines.

9.2 Stress evaluation summary

ASME B31.3 Ana lysis

Eq. Description Load cases Node S-total [N/mm²]

S-allow. [N/mm²]

Util. [%]

01 SL Sustained loads Dead load 5 37.2 137.4 27.102 SE Secondary loads considering stress

reserves from sustained loads Dead load, Temp. loads

235 92.2 331.4 27.8

03 SOL

Occasional loads Dead load, Earthquake-XYZ

79 69.4 182.7 38.0

04 SLP Primary stresses, category P (pressure test)

Pressure test 5 69.1 241.3 28.6

Figure.: Stress analysis, equation 1

For the lifetime independent equations the allowable loads were determined, based on 7000 load cycles.

The calculation of the allowable and calculated stresses are listed in ROHR2 output ”Stresses”.

Page 16: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

16/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

9.1 Expansion joint results

There is no expansion joint on the pipelines.

9.2 Loads on nozzles

There is no expansion joint on the pipelines. The complete results can be found in the ROHR2 output file “Nozzle loads“.

9.3 Extreme loads on supports

Node Section Line Description CS QX

[kN]QY

[kN] QZ

[kN] MX

[kNm]MY

[kNm]MZ

[kNm]167 ST 4-P150-037-16-BA28P-

NI (EXISTING) POS001-P150-037-16 (EXISTING)

g -1.382 -0.526 -0.635 0.000 0.000 0.000

173 AR 3-P150-037-30-BA28P-NI

POS009-P150-037-30

g -0.877 0.155 -0.986 0.000 0.000 0.000

175 AR 3-P150-037-30-BA28P-NI

POS010-P150-037-30

g -0.304 -0.915 -0.728 0.000 0.000 0.000

177 AR 3-P150-037-30-BA28P-NI

POS011-P150-037-30

g -0.222 0.309 -0.808 0.000 0.000 0.000

179 AR 3-P150-037-30-BA28P-NI

POS012-P150-037-30

g -0.309 -0.747 -1.498 0.000 0.000 0.000

181 AR 3-P150-037-30-BA28P-NI

POS004-P150-037-30

g 1.124 3.116 -0.739 0.000 0.000 0.000

183 AR 3-P150-037-30-BA28P-NI

POS003-P150-037-30

g 1.065 -3.347 -0.553 0.000 0.000 0.000

185 ST 3-P150-037-30-BA28P-NI

POS014-P150-037-30

g -0.284 0.963 2.555 0.000 0.000 0.000

207 AR 3-P150-037-30-BA28P-NI

POS008-P150-037-30

g -0.295 0.650 -0.964 0.000 0.000 0.000

197 AR 3-P150-037-30-BA28P-NI

POS007-P150-037-30

g -0.816 0.235 -3.734 0.000 0.000 0.000

189 ST 3-P150-037-30-BA28P-NI

POS006-P150-037-30

g 2.047 -0.558 -3.898 0.000 0.000 0.000

215 ST 6-P150-024-04-BA28P-NI (EXISTING2)

POS001-P150-039-03 (EXISTING)

g -2.889 -1.495 -3.108 -0.000 -0.000 -0.000

217 AR 3-P150-037-30-BA28P-NI

POS013-P150-037-30

g 2.008 -0.514 -0.970 0.000 0.000 0.000

211 ST 3-P150-037-30-BA28P-NI

POS015-P150-037-30

g 1.441 0.799 -5.143 0.000 0.000 0.000

225 ST 3-P150-037-30-BA28P-NI

POS005-P150-037-30

g -1.105 0.685 -1.091 0.000 0.000 0.000

223 ST 3-P150-037-30-BA28P-NI

POS002-P150-037-30

g -1.156 0.398 0.951 0.000 0.000 0.000

205 ST 3-P150-037-30-BA28P-NI

POS001-P150-037-30

g -0.380 0.221 -2.671 -0.000 -0.000 0.000

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9.4 Loads on supports with operational cases

The support loads are listed below as regard to operational cases.  I N P U T S         ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page      1 

 Commiss.   THTF058                             Date  06/12/20  11:29:14 

 

   CCC   ************************************************************   CCC 

   CCC       Support loads                                              CCC 

   CCC   ************************************************************   CCC 

 

 

    I  N  P  U  T   R  E  C  O  R  D                ANALYSIS OF RESULTS 

    ================================ 

 

 

  COMBINATION OF LOAD CASES CALCULATED BY ROHR2 

 

  with program  ROHR2  Version 32.1 

 

 

   THE CALCULATION IS ONLY CARRIED OUT FOR THE FOLLOWING POINTS: 

 

 

     Line       Point   Pos  Text for section        Coordinate system 

 

       12        167   S     Guide support + axial... 

       13        161   S     EXISTING SUPPORT‐1 

       23        173   S     POS009‐P150‐037‐30 

       23        175   S     POS010‐P150‐037‐30 

       23        177   S     POS011‐P150‐037‐30 

       23        179   S     POS012‐P150‐037‐30 

       21        181   S     POS004‐P150‐037‐30 

       21        183   S     POS003‐P150‐037‐30 

       23        185   S     POS014‐P150‐037‐30 

       23        207   S     POS008‐P150‐037‐30 

       15        197   S     POS007‐P150‐037‐30 

       14        189   S     POS006‐P150‐037‐30 

       18        215   S     Axial stop + guide su... 

       7         81    S     EXISTING SUPPORT‐2 

       23        217   S     POS013‐P150‐037‐30 

       17        211   S     POS015‐P150‐037‐30 

       21        225   S     POS005‐P150‐037‐30 

       21        223   S     POS002‐P150‐037‐30 

       16        205   S     POS001‐P150‐037‐30 

 

 

   THE FOLLOWING LOAD CASES ARE TO BE CONSIDERED: 

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   Lc‐File       Lc‐Array Lc‐Name          calculated at: 

 

   deadl1.erg    G1       Dead load          06/12/20  11:29:06 

   temp1.erg     T1       Operation1         06/12/20  11:29:07 

   temp3.erg     T3       Operation2         06/12/20  11:29:09 

   earthq1.erg   EB00     Earthquake_X       06/12/20  11:29:10 

   earthq1.erg   EB01     Earthquake_Y       06/12/20  11:29:10 

   earthq1.erg   EB02     Earthquake_Z       06/12/20  11:29:10 

   htest1.erg    P1       Pressure test      06/12/20  11:29:12 

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 R E S U L T S       ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page      2 

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                S U P E R P O S I T I O N  S P E C I F I C A T I O N 

 

   Ex‐array XM       Extr.  Dead load        =   FEST   by : 

                        Lc‐array G1       Loadc. Dead load        *   1.00 

   Ex‐array XOP      Extr.  Operation        =   FEST   by : 

                        Lc‐array T1       Loadc. Operation1       *   1.00 

   Ex‐array XOP1     Extr.  Operation1       =   FEST   by : 

                        Lc‐array T3       Loadc. Operation2       *   1.00 

   Lc‐array EQRMS    Loadc. Earthquake‐XYZ   = SRSS     by : 

                        Lc‐array EB00     Loadc. Earthquake_X     *   1.00 

                      + Lc‐array EB01     Loadc. Earthquake_Y     *   1.00 

                      + Lc‐array EB02     Loadc. Earthquake_Z     *   1.00 

   Ex‐array XEQ      Extr.  Earthquake       =   GRWE   by : 

                        Lc‐array EQRMS    Loadc. Earthquake‐XYZ   *   1.00 

   Ex‐array XM1      Extr.  Deadl/Oper.‐Ext. =   SAFE   by : 

                      + Ex‐array XM       Extr.  Dead load        *   1.00 

                      + Ex‐array XOP      Extr.  Operation        *   1.00 

                      + Ex‐array XOP1     Extr.  Operation1       *   1.00 

   Lc‐array OPMAX    Loadc. Deadl/Oper.‐Max  = MAXIMUM  by : 

                        Ex‐array XM1      Extr.  Deadl/Oper.‐Ext. *   1.00 

   Lc‐array OPMIN    Loadc. Deadl/Oper.‐Min  = MINIMUM  by : 

                        Ex‐array XM1      Extr.  Deadl/Oper.‐Ext. *   1.00 

   Ex‐array XXOCC    Extr.  OC(Dead load)    =   SAFR   by : 

                      + Ex‐array XEQ      Extr.  Earthquake       *   1.00 

   Ex‐array XXOCC1   Extr.  Dead load+OC     =   FEST   by : 

                      + Ex‐array XM       Extr.  Dead load        *   1.00 

                      + Ex‐array XXOCC    Extr.  OC(Dead load)    *   1.00 

   Ex‐array XXOCC2   Extr.  OC(Operation)    =   SAFR   by : 

                      + Ex‐array XEQ      Extr.  Earthquake       *   1.00 

   Ex‐array XXOCC3   Extr.  Operation+OC     =   FEST   by : 

                      + Ex‐array XOP      Extr.  Operation        *   1.00 

                      + Ex‐array XXOCC2   Extr.  OC(Operation)    *   1.00 

   Ex‐array XXOCC4   Extr.  OC(Operation1)   =   SAFR   by : 

                      + Ex‐array XEQ      Extr.  Earthquake       *   1.00 

   Ex‐array XXOCC5   Extr.  Operation1+OC    =   FEST   by : 

                      + Ex‐array XOP1     Extr.  Operation1       *   1.00 

                      + Ex‐array XXOCC4   Extr.  OC(Operation1)   *   1.00 

   Ex‐array EXT      Extr.  Extreme val‐Ext  =   SAFE   by : 

                      + Ex‐array XM1      Extr.  Deadl/Oper.‐Ext. *   1.00 

                      + Ex‐array XXOCC1   Extr.  Dead load+OC     *   1.00 

                      + Ex‐array XXOCC3   Extr.  Operation+OC     *   1.00 

                      + Ex‐array XXOCC5   Extr.  Operation1+OC    *   1.00 

   Lc‐array LFMAX    Loadc. Extreme val‐Max  = MAXIMUM  by : 

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                        Ex‐array EXT      Extr.  Extreme val‐Ext  *   1.00 

   Lc‐array LFMIN    Loadc. Extreme val‐Min  = MINIMUM  by : 

                        Ex‐array EXT      Extr.  Extreme val‐Ext  *   1.00 

   Lc‐array LFEXT    Loadc. Extreme value    = EXTREMUM by : 

                        Ex‐array EXT      Extr.  Extreme val‐Ext  *   1.00 

   New page 

   Output of load case arrays: 

                        Lc‐array G1       Loadc. Dead load 

   Output of load case arrays: 

                        Lc‐array T1       Loadc. Operation1 

   Output of load case arrays: 

                        Lc‐array T3       Loadc. Operation2 

   Output of load case arrays: 

                        Lc‐array EB00     Loadc. Earthquake_X 

   Output of load case arrays: 

                        Lc‐array EB01     Loadc. Earthquake_Y 

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   Output of load case arrays: 

                        Lc‐array EB02     Loadc. Earthquake_Z 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

   Output of load case arrays: 

                        Lc‐array LFEXT    Loadc. Extreme value 

   Output of load case arrays: 

                        Lc‐array P1       Loadc. Pressure test 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

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 R E S U L T S       ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page      4 

 Commiss.   THTF058                             Date  06/12/20  11:29:14 

 

 

 

  L i n e      12     P o i n t   167    ST 

  Support in Absolute Coordinate System 

 

  Guide support + axial stop 

   POS001‐P150‐037‐16 (EXISTING) 

 

  LoadCase               WX       WY       WZ       AQX      AQY      AQZ 

                         PX       PY       PZ       AMX      AMY      AMZ 

                         mm       mm       mm        kN       kN       kN 

                       mrad     mrad     mrad       kNm      kNm      kNm 

 

  Dead load            0.00     0.00     0.00     0.092    0.014   ‐0.458 

                      ‐0.06     0.62    ‐0.00     0.000    0.000    0.000 

 

  Operation1           0.00     0.00     0.00    ‐0.646   ‐0.215   ‐0.056 

                       1.46    ‐0.51    ‐0.46     0.000    0.000    0.000 

 

  Operation2           0.00     0.00     0.00    ‐0.238   ‐0.011   ‐0.345 

                       0.07     0.36    ‐0.04     0.000    0.000    0.000 

 

  Earthquake_X         0.00     0.00     0.00     0.670    0.028   ‐0.029 

                       0.11     0.03    ‐0.08     0.000    0.000    0.000 

 

  Earthquake_Y         0.00     0.00     0.00     0.306    0.310    0.166 

                      ‐1.47    ‐0.17     0.98     0.000    0.000    0.000 

 

  Earthquake_Z         0.00     0.00     0.00    ‐0.011   ‐0.002    0.055 

                       0.01    ‐0.07     0.00     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

  Extreme value        0.00     0.00     0.00    ‐1.382   ‐0.526   ‐0.635 

                       2.93     0.81    ‐1.44     0.000    0.000    0.000 

 

  Pressure test        0.00     0.00     0.00     0.100    0.016   ‐0.473 

                      ‐0.07     0.61     0.00     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

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  L i n e      13     P o i n t   161    AR         EXISTING SUPPORT‐1 

  Support in Absolute Coordinate System 

 

  Axial stop + guide support Ya, vertical pipe 

 

  LoadCase               WX       WY       WZ       AQX      AQY      AQZ 

                         PX       PY       PZ       AMX      AMY      AMZ 

                         mm       mm       mm        kN       kN       kN 

                       mrad     mrad     mrad       kNm      kNm      kNm 

 

  Dead load            0.39    ‐0.00    ‐0.00     0.000   ‐0.021   ‐0.852 

                       0.01    ‐0.66     0.00     0.000    0.000    0.000 

 

  Operation1           4.46     0.00    ‐0.03     0.287    0.110   ‐0.847 

                       1.06    ‐0.19    ‐0.31     0.000    0.000    0.000 

 

  Operation2           0.36    ‐0.00    ‐0.03     0.280   ‐0.007   ‐0.927 

                       0.09     0.19    ‐0.02     0.000    0.000    0.000 

 

  Earthquake_X         0.03    ‐0.00    ‐0.00     0.000   ‐0.046   ‐0.010 

                       0.28    ‐0.05    ‐0.06     0.000    0.000    0.000 

 

  Earthquake_Y        ‐0.05     0.00     0.00     0.000    0.219    0.032 

                      ‐2.24     0.09     0.54     0.000    0.000    0.000 

 

  Earthquake_Z        ‐0.05     0.00     0.00     0.000    0.002    0.102 

                      ‐0.00     0.08    ‐0.00     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

  Extreme value        4.54     0.00    ‐0.03     0.287    0.334   ‐1.035 

                       3.32    ‐0.78    ‐0.86     0.000    0.000    0.000 

 

  Pressure test        0.38    ‐0.00    ‐0.00     0.000   ‐0.023   ‐0.879 

                       0.00    ‐0.64     0.01     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

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  L i n e      23     P o i n t   173    AR         POS009‐P150‐037‐30 

  Support in Absolute Coordinate System 

 

  Guide support 

 

  LoadCase               WX       WY       WZ       AQX      AQY      AQZ 

                         PX       PY       PZ       AMX      AMY      AMZ 

                         mm       mm       mm        kN       kN       kN 

                       mrad     mrad     mrad       kNm      kNm      kNm 

 

  Dead load           ‐0.00    ‐0.55    ‐0.00    ‐0.017    0.000   ‐0.773 

                       0.15    ‐0.33     0.26     0.000    0.000    0.000 

 

  Operation1          ‐0.02     5.11     1.33    ‐0.535    0.155    0.041 

                       3.43     3.48    ‐3.85     0.000    0.000    0.000 

 

  Operation2          ‐0.00     0.00    ‐0.02    ‐0.073    0.022   ‐0.653 

                       0.57    ‐0.01    ‐0.14     0.000    0.000    0.000 

 

  Earthquake_X         0.00     0.06    ‐0.00     0.342    0.000   ‐0.076 

                      ‐0.23    ‐1.45     1.40     0.000    0.000    0.000 

 

  Earthquake_Y        ‐0.00     2.95     0.00    ‐0.021    0.000    0.176 

                      ‐0.75    ‐0.66     0.71     0.000    0.000    0.000 

 

  Earthquake_Z         0.00     0.07     0.00     0.002    0.000    0.093 

                      ‐0.02     0.04    ‐0.03     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

  Extreme value       ‐0.02     8.06     1.33    ‐0.877    0.155   ‐0.986 

                       4.21     5.07    ‐5.42     0.000    0.000    0.000 

 

  Pressure test       ‐0.00    ‐0.57    ‐0.00    ‐0.018    0.000   ‐0.840 

                       0.16    ‐0.33     0.27     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

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THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

25/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

 R E S U L T S       ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page      7 

 Commiss.   THTF058                             Date  06/12/20  11:29:14 

 

 

 

  L i n e      23     P o i n t   175    AR         POS010‐P150‐037‐30 

  Support in Absolute Coordinate System 

 

  Guide support 

 

  LoadCase               WX       WY       WZ       AQX      AQY      AQZ 

                         PX       PY       PZ       AMX      AMY      AMZ 

                         mm       mm       mm        kN       kN       kN 

                       mrad     mrad     mrad       kNm      kNm      kNm 

 

  Dead load           ‐0.17     0.00    ‐0.00     0.000    0.030   ‐0.603 

                      ‐0.48    ‐0.74    ‐0.01     0.000    0.000    0.000 

 

  Operation1         ‐19.73    ‐0.01    ‐0.02    ‐0.304   ‐0.460   ‐0.553 

                      ‐4.85    ‐0.58    ‐0.82     0.000    0.000    0.000 

 

  Operation2          ‐2.11    ‐0.00    ‐0.02    ‐0.191   ‐0.035   ‐0.602 

                      ‐1.04    ‐0.70    ‐0.08     0.000    0.000    0.000 

 

  Earthquake_X         5.73    ‐0.00    ‐0.00     0.000   ‐0.024   ‐0.039 

                       0.27    ‐0.26     0.26     0.000    0.000    0.000 

 

  Earthquake_Y         0.04     0.00    ‐0.00     0.000    0.455   ‐0.095 

                       2.80    ‐0.21    ‐0.51     0.000    0.000    0.000 

 

  Earthquake_Z         0.02    ‐0.00     0.00     0.000   ‐0.004    0.073 

                       0.06     0.09     0.00     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

  Extreme value      ‐25.46    ‐0.01    ‐0.02    ‐0.304   ‐0.915   ‐0.728 

                      ‐7.66    ‐1.09    ‐1.38     0.000    0.000    0.000 

 

  Pressure test       ‐0.18     0.00    ‐0.00     0.000    0.033   ‐0.655 

                      ‐0.50    ‐0.76    ‐0.02     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

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THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

26/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

 R E S U L T S       ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page      8 

 Commiss.   THTF058                             Date  06/12/20  11:29:14 

 

 

 

  L i n e      23     P o i n t   177    AR         POS011‐P150‐037‐30 

  Support in Absolute Coordinate System 

 

  Guide support 

 

  LoadCase               WX       WY       WZ       AQX      AQY      AQZ 

                         PX       PY       PZ       AMX      AMY      AMZ 

                         mm       mm       mm        kN       kN       kN 

                       mrad     mrad     mrad       kNm      kNm      kNm 

 

  Dead load           ‐0.17    ‐0.00    ‐0.00     0.000   ‐0.003   ‐0.691 

                      ‐0.34     1.07     0.00     0.000    0.000    0.000 

 

  Operation1         ‐13.15     0.00    ‐0.02    ‐0.222    0.095   ‐0.646 

                      ‐4.07     0.83     0.81     0.000    0.000    0.000 

 

  Operation2          ‐1.37     0.00    ‐0.02    ‐0.208    0.011   ‐0.682 

                      ‐0.82     0.99     0.09     0.000    0.000    0.000 

 

  Earthquake_X         5.73     0.00     0.00     0.000    0.044    0.077 

                       0.21    ‐0.04    ‐0.05     0.000    0.000    0.000 

 

  Earthquake_Y         0.04     0.00     0.00     0.000    0.210    0.029 

                       2.31     0.06     0.43     0.000    0.000    0.000 

 

  Earthquake_Z         0.02     0.00     0.00     0.000    0.000    0.083 

                       0.04    ‐0.13    ‐0.00     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

  Extreme value      ‐18.88     0.00    ‐0.02    ‐0.222    0.309   ‐0.808 

                      ‐6.39     1.21     1.25     0.000    0.000    0.000 

 

  Pressure test       ‐0.18    ‐0.00    ‐0.00     0.000   ‐0.004   ‐0.751 

                      ‐0.35     1.09     0.00     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

Page 27: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

27/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

 R E S U L T S       ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page      9 

 Commiss.   THTF058                             Date  06/12/20  11:29:14 

 

 

 

  L i n e      23     P o i n t   179    AR         POS012‐P150‐037‐30 

  Support in Absolute Coordinate System 

 

  Guide support 

 

  LoadCase               WX       WY       WZ       AQX      AQY      AQZ 

                         PX       PY       PZ       AMX      AMY      AMZ 

                         mm       mm       mm        kN       kN       kN 

                       mrad     mrad     mrad       kNm      kNm      kNm 

 

  Dead load           ‐0.17     0.00    ‐0.00     0.000    0.004   ‐0.774 

                      ‐0.06    ‐0.88     0.03     0.000    0.000    0.000 

 

  Operation1          ‐0.01    ‐0.01    ‐0.04    ‐0.309   ‐0.426   ‐1.174 

                      ‐2.52     0.21    ‐3.23     0.000    0.000    0.000 

 

  Operation2           0.09    ‐0.00    ‐0.03     0.265   ‐0.051   ‐0.835 

                      ‐0.36    ‐0.69    ‐0.35     0.000    0.000    0.000 

 

  Earthquake_X         5.72    ‐0.00    ‐0.00     0.000   ‐0.085   ‐0.310 

                       0.09     0.75    ‐0.23     0.000    0.000    0.000 

 

  Earthquake_Y         0.04     0.00    ‐0.00     0.000    0.309   ‐0.016 

                       1.33     0.07    ‐0.13     0.000    0.000    0.000 

 

  Earthquake_Z         0.02    ‐0.00     0.00     0.000   ‐0.000    0.093 

                       0.01     0.11    ‐0.00     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

  Extreme value       ‐5.90    ‐0.01    ‐0.04    ‐0.309   ‐0.747   ‐1.498 

                      ‐3.85    ‐1.65    ‐3.50     0.000    0.000    0.000 

 

  Pressure test       ‐0.18     0.00    ‐0.00     0.000    0.004   ‐0.841 

                      ‐0.06    ‐0.91     0.03     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

Page 28: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

28/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

 R E S U L T S       ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     10 

 Commiss.   THTF058                             Date  06/12/20  11:29:14 

 

 

 

  L i n e      21     P o i n t   181    AR         POS004‐P150‐037‐30 

  Support in Absolute Coordinate System 

 

  Guide support 

 

  LoadCase               WX       WY       WZ       AQX      AQY      AQZ 

                         PX       PY       PZ       AMX      AMY      AMZ 

                         mm       mm       mm        kN       kN       kN 

                       mrad     mrad     mrad       kNm      kNm      kNm 

 

  Dead load            0.00     0.00    ‐0.00     0.000    0.005   ‐0.364 

                       0.03    ‐1.75    ‐0.00     0.000    0.000    0.000 

 

  Operation1          10.91     0.10    ‐0.02     1.124    3.092   ‐0.653 

                      ‐0.31    ‐4.76     2.14     0.000    0.000    0.000 

 

  Operation2           1.22     0.01    ‐0.01     0.226    0.357   ‐0.396 

                       0.00    ‐2.01     0.25     0.000    0.000    0.000 

 

  Earthquake_X         0.00    ‐0.00    ‐0.00     0.000   ‐0.006   ‐0.006 

                       0.00    ‐0.05     0.00     0.000    0.000    0.000 

 

  Earthquake_Y         0.00    ‐0.00     0.00     0.000   ‐0.023    0.074 

                       0.17    ‐0.18    ‐0.06     0.000    0.000    0.000 

 

  Earthquake_Z        ‐0.00    ‐0.00     0.00     0.000   ‐0.001    0.044 

                      ‐0.00     0.21     0.00     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

  Extreme value       10.92     0.10    ‐0.02     1.124    3.116   ‐0.739 

                      ‐0.48    ‐5.04     2.20     0.000    0.000    0.000 

 

  Pressure test        0.00     0.00    ‐0.00     0.000    0.006   ‐0.395 

                       0.04    ‐1.80    ‐0.00     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

Page 29: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

29/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

 R E S U L T S       ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     11 

 Commiss.   THTF058                             Date  06/12/20  11:29:14 

 

 

 

  L i n e      21     P o i n t   183    AR         POS003‐P150‐037‐30 

  Support in Absolute Coordinate System 

 

  Guide support 

 

  LoadCase               WX       WY       WZ       AQX      AQY      AQZ 

                         PX       PY       PZ       AMX      AMY      AMZ 

                         mm       mm       mm        kN       kN       kN 

                       mrad     mrad     mrad       kNm      kNm      kNm 

 

  Dead load           ‐0.00    ‐0.00    ‐0.00     0.000   ‐0.004   ‐0.385 

                      ‐0.01    ‐1.74    ‐0.00     0.000    0.000    0.000 

 

  Operation1          10.91    ‐0.10    ‐0.01     1.065   ‐3.094   ‐0.456 

                      ‐0.01    ‐4.95    ‐2.14     0.000    0.000    0.000 

 

  Operation2           1.22    ‐0.01    ‐0.01     0.227   ‐0.359   ‐0.396 

                      ‐0.01    ‐2.01    ‐0.23     0.000    0.000    0.000 

 

  Earthquake_X         0.00     0.00     0.00     0.000    0.005    0.001 

                       0.01    ‐0.03     0.00     0.000    0.000    0.000 

 

  Earthquake_Y        ‐0.00     0.00    ‐0.00     0.000    0.253   ‐0.085 

                       0.07    ‐0.02    ‐0.09     0.000    0.000    0.000 

 

  Earthquake_Z         0.00     0.00     0.00     0.000    0.001    0.046 

                       0.00     0.21     0.00     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

  Extreme value       10.91    ‐0.10    ‐0.01     1.065   ‐3.347   ‐0.553 

                      ‐0.08    ‐5.16    ‐2.23     0.000    0.000    0.000 

 

  Pressure test       ‐0.00    ‐0.00    ‐0.00     0.000   ‐0.005   ‐0.419 

                      ‐0.01    ‐1.79    ‐0.00     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

Page 30: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

30/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

 R E S U L T S       ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     12 

 Commiss.   THTF058                             Date  06/12/20  11:29:14 

 

 

 

  L i n e      23     P o i n t   185    ST         POS014‐P150‐037‐30 

  Support in Absolute Coordinate System 

 

  Guide support + axial stop 

 

  LoadCase               WX       WY       WZ       AQX      AQY      AQZ 

                         PX       PY       PZ       AMX      AMY      AMZ 

                         mm       mm       mm        kN       kN       kN 

                       mrad     mrad     mrad       kNm      kNm      kNm 

 

  Dead load            0.00     0.00     0.00    ‐0.007    0.002   ‐0.602 

                      ‐0.15     0.14     0.02     0.000    0.000    0.000 

 

  Operation1           0.00     0.00     0.00    ‐0.062    0.371    2.219 

                       8.08    ‐3.41    ‐0.01     0.000    0.000    0.000 

 

  Operation2           0.00     0.00     0.00    ‐0.017    0.195   ‐0.271 

                       0.79    ‐0.37    ‐0.01     0.000    0.000    0.000 

 

  Earthquake_X         0.00     0.00     0.00     0.222    0.062   ‐0.024 

                       0.14    ‐3.29    ‐1.03     0.000    0.000    0.000 

 

  Earthquake_Y         0.00     0.00     0.00    ‐0.013    0.589   ‐0.327 

                      ‐0.50     0.01    ‐0.00     0.000    0.000    0.000 

 

  Earthquake_Z         0.00     0.00     0.00     0.001   ‐0.000    0.072 

                       0.02    ‐0.02    ‐0.00     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

  Extreme value        0.00     0.00     0.00    ‐0.284    0.963    2.555 

                       8.59    ‐6.69     1.05     0.000    0.000    0.000 

 

  Pressure test        0.00     0.00     0.00    ‐0.007    0.001   ‐0.650 

                      ‐0.14     0.14     0.02     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

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THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

31/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

 R E S U L T S       ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     13 

 Commiss.   THTF058                             Date  06/12/20  11:29:14 

 

 

 

  L i n e      23     P o i n t   207    AR         POS008‐P150‐037‐30 

  Support in Absolute Coordinate System 

 

  Guide support 

 

  LoadCase               WX       WY       WZ       AQX      AQY      AQZ 

                         PX       PY       PZ       AMX      AMY      AMZ 

                         mm       mm       mm        kN       kN       kN 

                       mrad     mrad     mrad       kNm      kNm      kNm 

 

  Dead load            0.19    ‐0.00    ‐0.00     0.000   ‐0.047   ‐0.453 

                       0.17    ‐0.12     0.18     0.000    0.000    0.000 

 

  Operation1          ‐4.96     0.00    ‐0.03    ‐0.295    0.131   ‐0.854 

                      ‐0.70    ‐3.26    ‐3.06     0.000    0.000    0.000 

 

  Operation2          ‐0.00    ‐0.00    ‐0.02    ‐0.137   ‐0.050   ‐0.529 

                       0.01    ‐0.55    ‐0.08     0.000    0.000    0.000 

 

  Earthquake_X         2.65    ‐0.00     0.00     0.000   ‐0.080    0.075 

                      ‐0.09    ‐0.23     0.26     0.000    0.000    0.000 

 

  Earthquake_Y         1.42     0.00    ‐0.00     0.000    0.513   ‐0.059 

                      ‐1.68    ‐1.06     2.86     0.000    0.000    0.000 

 

  Earthquake_Z        ‐0.02     0.00     0.00     0.000    0.006    0.054 

                      ‐0.02     0.01    ‐0.02     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

  Extreme value       ‐7.96     0.00    ‐0.03    ‐0.295    0.650   ‐0.964 

                      ‐2.38    ‐4.35    ‐5.93     0.000    0.000    0.000 

 

  Pressure test        0.19    ‐0.00    ‐0.00     0.000   ‐0.052   ‐0.491 

                       0.17    ‐0.12     0.19     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

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THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

32/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

 R E S U L T S       ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     14 

 Commiss.   THTF058                             Date  06/12/20  11:29:14 

 

 

 

  L i n e      15     P o i n t   197    AR         POS007‐P150‐037‐30 

  Support in Absolute Coordinate System 

 

  Axial stop + guide support Ya, vertical pipe 

 

  LoadCase               WX       WY       WZ       AQX      AQY      AQZ 

                         PX       PY       PZ       AMX      AMY      AMZ 

                         mm       mm       mm        kN       kN       kN 

                       mrad     mrad     mrad       kNm      kNm      kNm 

 

  Dead load            0.04     0.00    ‐0.00     0.000    0.009   ‐1.465 

                      ‐0.11     0.02     0.02     0.000    0.000    0.000 

 

  Operation1          ‐1.22     0.00    ‐0.08    ‐0.816    0.042   ‐2.683 

                       0.41    ‐1.35    ‐0.07     0.000    0.000    0.000 

 

  Operation2          ‐0.00     0.00    ‐0.05    ‐0.115    0.002   ‐1.463 

                      ‐0.11    ‐0.11     0.08     0.000    0.000    0.000 

 

  Earthquake_X         0.95    ‐0.00     0.00     0.000   ‐0.012    1.009 

                      ‐0.12     0.78     0.09     0.000    0.000    0.000 

 

  Earthquake_Y        ‐0.04     0.00    ‐0.00     0.000    0.193   ‐0.231 

                      ‐2.09    ‐0.05     0.83     0.000    0.000    0.000 

 

  Earthquake_Z        ‐0.00    ‐0.00     0.00     0.000   ‐0.001    0.176 

                       0.01    ‐0.00    ‐0.00     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

  Extreme value       ‐2.17     0.00    ‐0.08    ‐0.816    0.235   ‐3.734 

                       2.50    ‐2.13     0.91     0.000    0.000    0.000 

 

  Pressure test        0.04     0.00    ‐0.00     0.000    0.010   ‐1.496 

                      ‐0.11     0.03     0.02     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

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THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

33/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

 R E S U L T S       ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     15 

 Commiss.   THTF058                             Date  06/12/20  11:29:14 

 

 

 

  L i n e      14     P o i n t   189    ST         POS006‐P150‐037‐30 

  Support in Absolute Coordinate System 

 

  Axial stop + guide support Xa+Ya, vertical pipe 

 

  LoadCase               WX       WY       WZ       AQX      AQY      AQZ 

                         PX       PY       PZ       AMX      AMY      AMZ 

                         mm       mm       mm        kN       kN       kN 

                       mrad     mrad     mrad       kNm      kNm      kNm 

 

  Dead load           ‐0.00     0.00    ‐0.00     0.027    0.015   ‐1.981 

                      ‐0.13     0.08     0.01     0.000    0.000    0.000 

 

  Operation1          ‐0.00     0.00    ‐0.00     0.828   ‐0.016   ‐2.716 

                       0.58     1.07    ‐0.12     0.000    0.000    0.000 

 

  Operation2          ‐0.00    ‐0.00    ‐0.00     0.229    0.034   ‐2.217 

                      ‐0.18     0.38     0.02     0.000    0.000    0.000 

 

  Earthquake_X         0.00     0.00    ‐0.00     1.219    0.039   ‐1.154 

                      ‐0.22     2.55     0.03     0.000   ‐0.000    0.000 

 

  Earthquake_Y         0.00    ‐0.00    ‐0.00    ‐0.037    0.540    0.087 

                      ‐3.03    ‐0.12     0.40    ‐0.000    0.000    0.000 

 

  Earthquake_Z        ‐0.00     0.00     0.00    ‐0.003   ‐0.002    0.238 

                       0.02    ‐0.01    ‐0.00     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

  Extreme value       ‐0.00     0.00    ‐0.00     2.047    0.575   ‐3.898 

                       3.62     3.62    ‐0.53     0.000    0.000    0.000 

 

  Pressure test       ‐0.00     0.00     0.00     0.029    0.017   ‐2.030 

                      ‐0.13     0.08     0.01     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

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THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

34/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

 R E S U L T S       ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     16 

 Commiss.   THTF058                             Date  06/12/20  11:29:14 

 

 

 

  L i n e      18     P o i n t   215    ST 

  Support in Absolute Coordinate System 

 

  Axial stop + guide support Xa+Ya, vertical pipe 

   POS001‐P150‐039‐03 (EXISTING) 

 

  LoadCase               WX       WY       WZ       AQX      AQY      AQZ 

                         PX       PY       PZ       AMX      AMY      AMZ 

                         mm       mm       mm        kN       kN       kN 

                       mrad     mrad     mrad       kNm      kNm      kNm 

 

  Dead load            0.00     0.00    ‐0.00    ‐0.246   ‐0.312   ‐0.757 

                      ‐0.70    ‐0.36    ‐0.45     0.000   ‐0.000   ‐0.000 

 

  Operation1          ‐0.00    ‐0.00     0.00    ‐2.191   ‐1.100   ‐2.513 

                       2.20    ‐1.84     1.75    ‐0.000   ‐0.000    0.000 

 

  Operation2           0.00     0.00     0.00    ‐0.341   ‐0.415   ‐0.858 

                      ‐0.26    ‐0.32    ‐0.12     0.000    0.000   ‐0.000 

 

  Earthquake_X        ‐0.00    ‐0.00     0.00     0.692    0.391    0.576 

                      ‐0.65     1.06    ‐0.52    ‐0.000    0.000    0.000 

 

  Earthquake_Y        ‐0.00    ‐0.00     0.00    ‐0.090   ‐0.048   ‐0.123 

                      ‐0.48    ‐0.14    ‐0.34    ‐0.000   ‐0.000   ‐0.000 

 

  Earthquake_Z        ‐0.00    ‐0.00     0.00     0.030    0.038    0.091 

                       0.08     0.04     0.05     0.000    0.000   ‐0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

  Extreme value       ‐0.00     0.00     0.00    ‐2.889   ‐1.495   ‐3.108 

                       3.01    ‐2.91     2.37    ‐0.000   ‐0.000   ‐0.000 

 

  Pressure test        0.00    ‐0.00    ‐0.00    ‐0.253   ‐0.322   ‐0.801 

                      ‐0.67    ‐0.34    ‐0.44     0.000   ‐0.000   ‐0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

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THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

35/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

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 Commiss.   THTF058                             Date  06/12/20  11:29:14 

 

 

 

  L i n e      7      P o i n t   81     AR         EXISTING SUPPORT‐2 

  Support in Absolute Coordinate System 

 

  Guide support 

 

  LoadCase               WX       WY       WZ       AQX      AQY      AQZ 

                         PX       PY       PZ       AMX      AMY      AMZ 

                         mm       mm       mm        kN       kN       kN 

                       mrad     mrad     mrad       kNm      kNm      kNm 

 

  Dead load           ‐0.19     0.00    ‐0.00     0.000    0.347   ‐0.116 

                      ‐1.16    ‐0.00    ‐0.48     0.000    0.000    0.000 

 

  Operation1           0.47     0.01     0.02     0.989    1.069    2.239 

                       0.59     1.63     1.67     0.000    0.000    0.000 

 

  Operation2          ‐0.00     0.00     0.00    ‐0.040    0.435    0.057 

                      ‐0.84     0.16    ‐0.15     0.000    0.000    0.000 

 

  Earthquake_X         0.55    ‐0.00    ‐0.00     0.000   ‐0.293   ‐0.309 

                      ‐0.08    ‐0.04    ‐0.49     0.000    0.000    0.000 

 

  Earthquake_Y        ‐0.07     0.00     0.00     0.000    0.526    0.209 

                      ‐0.56     0.00    ‐0.34     0.000    0.000    0.000 

 

  Earthquake_Z         0.02    ‐0.00     0.00     0.000   ‐0.042    0.014 

                       0.14     0.00     0.06     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

  Extreme value        1.03     0.01     0.02     0.989    1.673    2.613 

                      ‐1.74     1.67     2.27     0.000    0.000    0.000 

 

  Pressure test       ‐0.18     0.00    ‐0.00     0.000    0.357   ‐0.132 

                      ‐1.11    ‐0.00    ‐0.46     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

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THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

36/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

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 Commiss.   THTF058                             Date  06/12/20  11:29:14 

 

 

 

  L i n e      23     P o i n t   217    AR         POS013‐P150‐037‐30 

  Support in Absolute Coordinate System 

 

  Guide support 

 

  LoadCase               WX       WY       WZ       AQX      AQY      AQZ 

                         PX       PY       PZ       AMX      AMY      AMZ 

                         mm       mm       mm        kN       kN       kN 

                       mrad     mrad     mrad       kNm      kNm      kNm 

 

  Dead load            0.00    ‐0.00    ‐0.00     0.004    0.000   ‐0.520 

                      ‐0.01     0.17     0.00     0.000    0.000    0.000 

 

  Operation1           0.03    ‐7.80    ‐0.02     1.061   ‐0.514   ‐0.651 

                      ‐3.83    ‐6.08     0.53     0.000    0.000    0.000 

 

  Operation2           0.01    ‐0.88    ‐0.02     0.167   ‐0.206   ‐0.521 

                      ‐0.45    ‐0.74     0.12     0.000    0.000    0.000 

 

  Earthquake_X         0.00     0.00     0.00     0.947    0.000    0.312 

                      ‐0.41    ‐4.94     1.46     0.000    0.000    0.000 

 

  Earthquake_Y         0.00     0.00     0.00     0.024    0.000    0.017 

                       0.43     0.04     0.11     0.000    0.000    0.000 

 

  Earthquake_Z        ‐0.00     0.00     0.00    ‐0.000    0.000    0.063 

                       0.00    ‐0.02    ‐0.00     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

  Extreme value        0.03    ‐7.80    ‐0.02     2.008   ‐0.514   ‐0.970 

                      ‐4.42   ‐11.02     1.99     0.000    0.000    0.000 

 

  Pressure test        0.00    ‐0.00    ‐0.00     0.004    0.000   ‐0.565 

                      ‐0.01     0.17     0.00     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

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THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

37/65

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

 R E S U L T S       ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     19 

 Commiss.   THTF058                             Date  06/12/20  11:29:14 

 

 

 

  L i n e      17     P o i n t   211    ST         POS015‐P150‐037‐30 

  Support in Absolute Coordinate System 

 

  Axial stop + guide support Xa+Ya, vertical pipe 

 

  LoadCase               WX       WY       WZ       AQX      AQY      AQZ 

                         PX       PY       PZ       AMX      AMY      AMZ 

                         mm       mm       mm        kN       kN       kN 

                       mrad     mrad     mrad       kNm      kNm      kNm 

 

  Dead load            0.00     0.00    ‐0.00     0.250   ‐0.039   ‐1.801 

                      ‐0.43     0.02     0.05    ‐0.000    0.000    0.000 

 

  Operation1           0.00     0.00     0.00     1.207    0.504   ‐4.724 

                      ‐6.75     2.56     2.41     0.000    0.000    0.000 

 

  Operation2           0.00    ‐0.00     0.00     0.386    0.033   ‐2.147 

                      ‐1.12     0.40     0.32     0.000    0.000    0.000 

 

  Earthquake_X         0.00    ‐0.00    ‐0.00     0.213   ‐0.085   ‐0.273 

                       0.33     1.58    ‐0.23    ‐0.000    0.000    0.000 

 

  Earthquake_Y         0.00     0.00     0.00     0.091    0.283    0.234 

                      ‐1.50     0.00     0.55     0.000    0.000    0.000 

 

  Earthquake_Z         0.00    ‐0.00    ‐0.00    ‐0.030    0.005    0.217 

                       0.05    ‐0.00    ‐0.01     0.000   ‐0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

  Extreme value        0.00     0.00     0.00     1.441    0.799   ‐5.143 

                      ‐8.29     4.14     3.00     0.000    0.000    0.000 

 

  Pressure test       ‐0.00     0.00     0.00     0.257   ‐0.039   ‐1.884 

                      ‐0.43     0.02     0.06     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

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  L i n e      21     P o i n t   225    ST         POS005‐P150‐037‐30 

  Support in Absolute Coordinate System 

 

  Guide support + axial stop 

 

  LoadCase               WX       WY       WZ       AQX      AQY      AQZ 

                         PX       PY       PZ       AMX      AMY      AMZ 

                         mm       mm       mm        kN       kN       kN 

                       mrad     mrad     mrad       kNm      kNm      kNm 

 

  Dead load            0.00     0.00     0.00    ‐0.011   ‐0.005   ‐0.883 

                       0.20     0.58     0.01     0.000    0.000    0.000 

 

  Operation1           0.00     0.00     0.00    ‐0.479    0.093    0.771 

                      ‐2.30     6.58    ‐1.11     0.000    0.000    0.000 

 

  Operation2           0.00     0.00     0.00    ‐0.155    0.022   ‐0.676 

                      ‐0.03     1.24    ‐0.16     0.000    0.000    0.000 

 

  Earthquake_X         0.00     0.00     0.00     0.617    0.044    0.141 

                      ‐0.02     0.13    ‐0.02     0.000    0.000    0.000 

 

  Earthquake_Y         0.00     0.00     0.00     0.107    0.590    0.111 

                       1.26     0.40    ‐1.06     0.000    0.000    0.000 

 

  Earthquake_Z         0.00     0.00     0.00     0.001    0.001    0.106 

                      ‐0.02    ‐0.07    ‐0.00     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

  Extreme value        0.00     0.00     0.00    ‐1.105    0.685   ‐1.091 

                      ‐3.56     7.01    ‐2.16     0.000    0.000    0.000 

 

  Pressure test        0.00     0.00     0.00    ‐0.012   ‐0.006   ‐0.951 

                       0.21     0.60     0.02     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

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  L i n e      21     P o i n t   223    ST         POS002‐P150‐037‐30 

  Support in Absolute Coordinate System 

 

  Guide support + axial stop 

 

  LoadCase               WX       WY       WZ       AQX      AQY      AQZ 

                         PX       PY       PZ       AMX      AMY      AMZ 

                         mm       mm       mm        kN       kN       kN 

                       mrad     mrad     mrad       kNm      kNm      kNm 

 

  Dead load            0.00     0.00     0.00    ‐0.004    0.002   ‐0.808 

                       0.00     0.58    ‐0.01     0.000    0.000    0.000 

 

  Operation1           0.00     0.00     0.00    ‐0.694    0.049    0.846 

                       0.12     7.04     1.07     0.000    0.000    0.000 

 

  Operation2           0.00     0.00     0.00    ‐0.184    0.008   ‐0.616 

                       0.02     1.27     0.11     0.000    0.000    0.000 

 

  Earthquake_X         0.00     0.00     0.00     0.456    0.001    0.035 

                       0.00     0.04    ‐0.01     0.000    0.000    0.000 

 

  Earthquake_Y         0.00     0.00     0.00    ‐0.075    0.348   ‐0.017 

                       0.50    ‐0.01    ‐0.33     0.000    0.000    0.000 

 

  Earthquake_Z         0.00     0.00     0.00     0.001   ‐0.000    0.097 

                      ‐0.00    ‐0.07     0.00     0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

  Extreme value        0.00     0.00     0.00    ‐1.156    0.398    0.951 

                       0.62     7.12     1.40     0.000    0.000    0.000 

 

  Pressure test        0.00     0.00     0.00    ‐0.005    0.002   ‐0.878 

                       0.01     0.59    ‐0.01     0.000    0.000    0.000 

 

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  L i n e      16     P o i n t   205    ST         POS001‐P150‐037‐30 

  Support in Absolute Coordinate System 

 

  Axial stop + guide support Xa+Ya, vertical pipe 

 

  LoadCase               WX       WY       WZ       AQX      AQY      AQZ 

                         PX       PY       PZ       AMX      AMY      AMZ 

                         mm       mm       mm        kN       kN       kN 

                       mrad     mrad     mrad       kNm      kNm      kNm 

 

  Dead load            0.00    ‐0.00    ‐0.00    ‐0.088    0.005   ‐0.601 

                      ‐0.03     0.03    ‐0.01    ‐0.000   ‐0.000   ‐0.000 

 

  Operation1           0.00    ‐0.00     0.00    ‐0.008    0.116   ‐2.474 

                       0.41    ‐1.34     0.87    ‐0.000   ‐0.000    0.000 

 

  Operation2          ‐0.00     0.00    ‐0.00    ‐0.080    0.017   ‐0.810 

                       0.01    ‐0.15     0.09     0.000   ‐0.000   ‐0.000 

 

  Earthquake_X         0.00    ‐0.00    ‐0.00    ‐0.007    0.017    0.005 

                      ‐0.03     0.11    ‐0.06    ‐0.000   ‐0.000    0.000 

 

  Earthquake_Y        ‐0.00     0.00     0.00    ‐0.291    0.104   ‐0.182 

                      ‐1.05    ‐0.39    ‐0.03    ‐0.000    0.000   ‐0.000 

 

  Earthquake_Z        ‐0.00     0.00     0.00     0.011   ‐0.001    0.072 

                       0.00    ‐0.00     0.00    ‐0.000    0.000    0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

  Extreme value        0.00    ‐0.00    ‐0.00    ‐0.380    0.221   ‐2.671 

                       1.46    ‐1.75     0.93    ‐0.000   ‐0.000   ‐0.000 

 

  Pressure test        0.00    ‐0.00    ‐0.00    ‐0.095    0.005   ‐0.644 

                      ‐0.03     0.03    ‐0.01    ‐0.000    0.000   ‐0.000 

 

  ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

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 I N D E X 

 ========= 

 

 LINE PT   NAVO  PAGE 

 13   161  AR       5 

 12   167  ST       4 

 23   173  AR       6 

 23   175  AR       7 

 23   177  AR       8 

 23   179  AR       9 

 21   181  AR      10 

 21   183  AR      11 

 23   185  ST      12 

 14   189  ST      15 

 15   197  AR      14 

 16   205  ST      22 

 23   207  AR      13 

 17   211  ST      19 

 18   215  ST      16 

 23   217  AR      18 

 21   223  ST      21 

 21   225  ST      20 

 7    81   AR      17 

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10 Graphical Outputs

10.1 Graphics / Plots

System overview

Line names

Dimensions

Materials

Operation data

Displacements

Stress utilization

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11 Appendices

11.1 Appendix A-Detail Stress Report for HCU Heavy Naphta to Diesel for Flash Point Optimization

11.2 Appendix B- Internal Pressure Analysis

11.3 Appendix C- Straight Pipe Required Minimum Wall Thickness Calculation

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Index

STRESS ANALYSIS .............................................................................................................................. 2 

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Stress analysis  I N P U T S         ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page      1 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

   CCC   ************************************************************   CCC 

   CCC       Stress analysis                                            CCC 

   CCC   ************************************************************   CCC 

 

   Results at internal nodes are only documented if the 

   stress utilisation is >90% 

 

 

 

 WWWWW For the material   SA106B 

 WWWWW lower temperatures have been used than those available in the material 

 WWWWW file. The material data from the next higher available temperature 

 WWWWW will be used. 

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   Stress analysis acc. to  PRESSURE  PIPING   ASME  B31.3    edit. 2016 

 

 

 

   Automatic determination of allowable stresses using the following rules: 

   ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

 

   The allowable stresses Sh and Sa are determined by the program 

   according to ASME B31.3 Art. 302.3 

   with strength values from the material file or taken directly 

   from the material file, if it is an ASME/ASTM‐material. 

   Values for Sh or Sa entered directly in the ET‐record (RR‐task) 

   overwrite the calculated values. 

 

      Sc = min (Rm\RT\min/3.0 , Rp0.2\RT\min/1.5) 

      For ferritic materials: 

      Sh = min (Sc , Rm\T\min/3.0 , Rp0.2\T\min/1.5 , 

                   , Rm\100000\mitt/1.5, 0.8*Rm\100000\min  ) 

      For austenitic materials: 

      Sh = min (Sc , Rp1.0\T\min/1.5 , 

                   , Rm\100000\mitt/1.5, 0.8*Rm\100000\min  ) 

      SA = f * (1.25*Sc + 0.25*Sh) = f * Sa 

      In Equation SA: Sc,Sh limited to 138 N/mm² (302.3.6 (d)) 

 

   The allowable operating stress SoA for the code ASME B31.3 

   Appendix P is calculated from Sc and Sh 

 

      SoA = 1.25 * f * (Sc + Sh) 

 

   The allowable stress for the load case pressure test is calculated as in 

   ASME B31.3 Art.345.2 as equal to the elastic limit. 

 

      Sh_test = 1.00*Rp\T\min 

 

     Rm\RT\min      =min. tensile strength at 20 deg. C       in N/mm^2 

     Rm\T\min       =min. tensile strength at calulat. temp   in N/mm^2 

     Rp02\RT\min    =min. 0.2% yield strength at 20 deg. C    in N/mm^2 

     Rp02\T\min     =min. 0.2% yield strength at calulat.Temp in N/mm^2 

     Rp1.0\T\min    =min. 1.0% yield strength at calcul. temp in N/mm^2 

     Rm\100000\mitt =rupture stength 100000h average value   in N/mm^2 

     Rm\100000\min  =rupture stength 100000h min value        in N/mm^2 

 

   Comments: 

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   Austenitic steels with a yield/tensile strength relationship 

   at 20 deg C <= 0.5 are calculated with the 1% yield strength value. 

   This value, used in german rules to determine the 

   allowable stresses for austenitic steel (/1.5), replaces the value 

   "90% of the yield strength at temperature" in ASME B31.3(302.3.2 d(3)) 

   If Rm\T\min is not present, the following approx. formula is used: 

   For ferritic materials: 

   Rm\T\min = Rm\RT\min * (Rp02\RT\min + Rp02\T\min) / (2 * Rp02\RT\min) 

 

   The factor f (stress reduction factor depending on load cycle ratio) 

   may be specified using R2WIN or the SPI record. 

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   +‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐+ 

   | ASME B31.3 Edit.2016           Material: SA106B               Ferrite | 

   |‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐| 

   | Material: SA106B                                                      | 

   | Material properties                   Spec.                   Rev.    | 

   | ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ | 

   | Young's modulus                       ASME II/D, Table Y1     01/2013 | 

   | Expansion coefficient                 ASME II/D, Table Y1     01/2013 | 

   | Tensile strength                      ASME II/D, Table Y1     01/2013 | 

   | 0.2% Yield strength                   ASME II/D, Table Y1     07/2015 | 

   |‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐| 

   | Temperature  T  °C  |  190.00 |   20.00 |  190.00 |   20.00 |         | 

   | Y‐mod\cold kN/mm^2  |  203.56 |  203.56 |  203.56 |  203.56 |         | 

   | Y‐mod\hot  kN/mm^2  |  192.06 |  203.46 |  192.06 |  203.46 |         | 

   |‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐| 

   | wall thickness  mm  |  6 ‐   7|  6 ‐   7|  0 ‐   6|  0 ‐   6|         | 

   |‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐| 

   | Rm\RT\min           |   ‐.‐   |         |   ‐.‐   |         |         | 

   | Rm\T\min            |   ‐.‐   |         |   ‐.‐   |         |         | 

   | Rp0.2\RT\min        |   ‐.‐   |         |   ‐.‐   |         |         | 

   | Rp0.2\T\min         |  208.12 |  241.32 |  208.12 |  241.32 |         | 

   | Rm\100000\mit       |   ‐.‐   |         |   ‐.‐   |         |         | 

   | Rm\100000\min       |   ‐.‐   |         |   ‐.‐   |         |         | 

   |‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐| 

   | Rm\RT\min/3.0       |   ‐.‐   |         |   ‐.‐   |         |         | 

   | Rp0.2\RT\min/1.5    |   ‐.‐   |         |   ‐.‐   |         |         | 

   | Sc                  |  137.90 |         |  137.90 |         |         | 

   |‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐| 

   | Rm\T\min/3.0        |   ‐.‐   |         |   ‐.‐   |         |         | 

   | Rp0.2\T\min /1.5    |  138.75 |         |  138.75 |         |         | 

   | Rm\100000\mitt/1.5  |   ‐.‐   |         |   ‐.‐   |         |         | 

   | 0.8*Rm\100000\min   |   ‐.‐   |         |   ‐.‐   |         |         | 

   | Sh                  |  137.38 |         |  137.38 |         |         | 

   | Sh_test             |         |  241.32 |         |  241.32 |         | 

   |‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐+‐‐‐‐‐‐‐‐‐| 

   | Sa                  |  206.71 |         |  206.71 |         |         | 

   | SoA                 |  344.09 |         |  344.09 |         |         | 

   +‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐+ 

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   The stress analysis takes the following load cases into account: 

 

 

   Lc‐File       Lc‐Array Lc‐Name          calculated at: 

 

   deadl1.erg    G1       Dead load          06/12/20  11:29:06 

   htest1.erg    P1       Pressure test      06/12/20  11:29:12 

   temp1.erg     T1       Operation1         06/12/20  11:29:07 

   temp3.erg     T3       Operation2         06/12/20  11:29:09 

   earthq1.erg   EB00     Earthquake_X       06/12/20  11:29:10 

   earthq1.erg   EB01     Earthquake_Y       06/12/20  11:29:10 

   earthq1.erg   EB02     Earthquake_Z       06/12/20  11:29:10 

 

 

 

 

   Cross section data printed are net values. 

   Internal ROHR2Win points not printed, if utilisation <  90.0 % 

 

   Tolerance inputs are taken into account for: 

                         Pressure stress components      S(P) 

                           Moment stress components in   SL, SOL 

 

 

 

                S U P E R P O S I T I O N  S P E C I F I C A T I O N 

 

   Lc‐array TMP      Loadc. Temp.0           = ARITHMET by : 

                        Lc‐array T1       Loadc. Operation1       *   1.00 

                      + Lc‐array G1       Loadc. Dead load        *  ‐1.00 

   Lc‐array TMP1     Loadc. Temp.4           = ARITHMET by : 

                        Lc‐array T3       Loadc. Operation2       *   1.00 

                      + Lc‐array G1       Loadc. Dead load        *  ‐1.00 

   Lc‐array EQRMS    Loadc. Earthquake‐XYZ   = SRSS     by : 

                        Lc‐array EB00     Loadc. Earthquake_X     *   1.00 

                      + Lc‐array EB01     Loadc. Earthquake_Y     *   1.00 

                      + Lc‐array EB02     Loadc. Earthquake_Z     *   1.00 

   LC Group GRP_T        Temp. loads     : 

                        Lc‐array TMP      Loadc. Temp.0 

                        Lc‐array TMP1     Loadc. Temp.4 

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   Required equations: 

   ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ 

 

 ANSI B31.3  Analysis 01  SL = SQRT(|ia*Fa/Ap|+SQRT( 

                          (.75ii*MiL)²+(.75io*MoL)²)/Z)²+(it*MtL/Z)²)  < Sh 

       P=Pc (calculation pressure) 

       Fa,MiL,MoL,MtL         from load case  Dead load 

       Sh calculated using MATDAT or the ET‐record factor = 1.00 

 

 ANSI B31.3  Analysis 02  SE = SQRT(|ia*Fa/Ap|+SQRT( 

                          (ii*MiE)²+(io*MoE)²)/Z)²+(it*MtE/Z)² <f*(Sa+Sh‐SL) 

       Fa,MiL,MoL,MtL         from load case  Dead load 

       Fa,MiE,MoE,MtE = RANGE from load case    Temp.0 

                                         +    Temp.4 

       Sh calculated using MATDAT or the ET‐record factor = 1.00 

       SA calculated using MATDAT or the ET‐record 

       Fatigue factor      f = 1.00 

       P,Ma for determination of SL in equation SE 

       ME = ME * Y‐MODcold / Y‐MODhot 

 

 ANSI B31.3  Analysis 03  SOL= SL + SQRT(|ia*Fa/Ap|+SQRT( 

                          (.75ii*MiO)²+(.75io*MoO)²)/Z)²+(it*MtO/Z)²)< k*Sh 

       P=Pc (calculation pressure) 

       Fa,MiL,MoL,MtL         from load case  Dead load 

       Fa,MiO,MoO,MtO  from load case Earthquake‐XYZ 

       Sh calculated using MATDAT or the ET‐record factor = 1.33 

 

 ANSI B31.3  Analysis 04  SLP= SQRT(|ia*Fa/Ap|+SQRT( 

                          (.75ii*MiL)²+(.75io*MoL)²)/Z)²+(MtL/Z)²) < Sh_test 

       Fa,MiL,MoL,MtL         from load case  Pressure test 

       Sh calculated using MATDAT or the ET‐record factor = 1.00 

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 Pt  81     Line 7    n Da=  168.3 mm s=  5.6 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL n  20.5   13.8    0.000    0.000    0.000    0.0   13.8  137.4   10 

 02 SERn   SL=   13.8    1.089    0.000    0.000    0.0    0.3  330.2    0 

 03 SOLn   SL=   13.8    0.000    0.000    0.000    0.0   13.8  182.7    8 

 04 SLPn  76.0   51.3    0.000    0.000    0.000    0.0   51.3  241.3   21 

 

 Pt  79     Line 7    v Da=  168.3 mm s=  5.6 mm (TTU ) Unreinf. fabr. tee 

            Line 7    n Da=  168.3 mm s=  5.6 mm  ii= 3.7  io= 4.5  it= 1.0 

            Line 19   n Da=   88.9 mm s=  4.0 mm 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   13.8    0.000   ‐0.099    0.016    2.5   16.3  137.4   12 

 01 SL n  20.5   13.8   ‐0.246    0.123    0.065    3.8   17.5  137.4   13 

 01 SL n  20.5    9.9    0.034   ‐0.222    0.151   25.1   35.1  137.4   26 

 02 SERv   SL=   16.3   ‐1.048   ‐0.218   ‐0.711   23.9   24.2  327.8    7 

 02 SERn   SL=   17.5   ‐2.061    0.329   ‐0.266   12.6   13.1  326.6    4 

 02 SERn   SL=   35.1   ‐0.070   ‐0.547    0.405   70.8   70.9  309.0   23 

 03 SOLv   SL=   16.3    0.042    0.167    0.106    5.2   21.5  182.7   12 

 03 SOLn   SL=   17.5    0.565    0.166    0.120    5.7   23.3  182.7   13 

 03 SOLn   SL=   35.1    0.317    0.314    0.191   34.0   69.4  182.7   38 

 04 SLPv  76.0   51.3    0.000   ‐0.102    0.019    2.5   53.9  241.3   22 

 04 SLPn  76.0   51.3   ‐0.253    0.127    0.069    4.0   55.1  241.3   23 

 04 SLPn  76.0   36.8    0.036   ‐0.229    0.156   25.9   62.7  241.3   26 

 

 Pt  83     Line 7    v Da=  168.3 mm s=  5.6 mm (BGL ) pipe bend 

            Line 7    m Da=  168.3 mm s=  5.6 mm   R=  228.6 mm 

            Line 7    n Da=  168.3 mm s=  5.6 mm  ii= 2.2  io= 1.8  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   13.8   ‐0.246   ‐0.004   ‐0.071    1.6   14.8  137.4   11 

 01 SL m  20.5   13.9    0.196   ‐0.099    0.107    2.3   15.9  137.4   12 

 01 SL n  20.5   14.1    0.597   ‐0.176    0.223    3.7   17.8  137.4   13 

 02 SERv   SL=   14.8   ‐2.061   ‐0.574   ‐0.191    9.9   10.4  329.3    3 

 02 SERm   SL=   15.9   ‐0.141   ‐1.013    0.286   16.7   16.7  328.2    5 

 02 SERn   SL=   17.8    1.861   ‐1.471    0.596   24.6   25.1  326.3    8 

 03 SOLv   SL=   14.8    0.589    0.215    0.095    3.8   18.7  182.7   10 

 03 SOLm   SL=   15.9    0.040    0.350    0.135    5.6   21.5  182.7   12 

Page 74: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

9/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 03 SOLn   SL=   17.8    0.593    0.491    0.283    8.0   26.0  182.7   14 

 04 SLPv  76.0   51.3   ‐0.253   ‐0.002   ‐0.074    1.6   52.3  241.3   22 

 04 SLPm  76.0   51.4    0.210   ‐0.101    0.110    2.4   53.4  241.3   22 

 04 SLPn  76.0   51.6    0.632   ‐0.181    0.230    3.9   55.4  241.3   23 

 

 Pt  213    Line 7    v Da=  168.3 mm s=  5.6 mm (KUH ) Fillet weld conc. 

            Line 7    n Da=  168.3 mm s=  5.6 mm  ii= 1.3  io= 1.3  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   14.1    0.597   ‐0.223   ‐0.176    2.5   16.6  137.4   12 

 01 SL n  20.5   13.8   ‐0.081   ‐0.000   ‐0.000    0.0   13.8  137.4   10 

 02 SERv   SL=   16.6    1.861   ‐0.597   ‐1.474   14.8   15.4  327.5    5 

 02 SERn   SL=   13.8    0.000   ‐0.000    0.000    0.0    0.0  330.2    0 

Page 75: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

10/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page      7 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 03 SOLv   SL=   16.6    0.593    0.284    0.492    5.0   21.8  182.7   12 

 03 SOLn   SL=   13.8    0.010    0.003    0.003    0.0   13.9  182.7    8 

 04 SLPv  76.0   51.6    0.632   ‐0.230   ‐0.181    2.6   54.2  241.3   22 

 04 SLPn  76.0   51.3   ‐0.091   ‐0.000    0.000    0.0   51.3  241.3   21 

 

 Pt  85     Line 7    v Da=  168.3 mm s=  5.6 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   13.8    0.000   ‐0.000   ‐0.000    0.0   13.8  137.4   10 

 02 SERv   SL=   13.8   ‐0.000   ‐0.000    0.000    0.0    0.0  330.2    0 

 03 SOLv   SL=   13.8    0.000    0.000    0.000    0.0   13.8  182.7    8 

 04 SLPv  76.0   51.3    0.000   ‐0.000    0.000    0.0   51.3  241.3   21 

 

 Pt  45     Line 21   n Da=   88.9 mm s=  4.0 mm (TFS ) Butt welding tee 

            Line 22   n Da=   88.9 mm s=  4.0 mm  ii= 1.5  io= 1.6  it= 1.0 

            Line 8    n Da=   88.9 mm s=  4.0 mm 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL n  20.5    9.9   ‐0.296   ‐0.014   ‐0.018    1.3   11.2  137.4    8 

 01 SL n  20.5    9.9   ‐0.933   ‐0.074    0.020    4.0   13.9  137.4   10 

 01 SL n  20.5    9.9   ‐0.100    0.089    0.002    4.4   14.3  137.4   10 

 02 SERn   SL=   11.2   ‐1.570    0.793    0.042   41.6   42.7  332.9   13 

 02 SERn   SL=   13.9    0.837   ‐0.123   ‐0.037    6.8    7.4  330.2    2 

 02 SERn   SL=   14.3   ‐0.314   ‐0.671   ‐0.068   33.3   33.5  329.8   10 

 03 SOLn   SL=   11.2    0.172    0.227    0.494   30.8   42.2  182.7   23 

 03 SOLn   SL=   13.9    0.675    0.449    0.465   35.0   49.6  182.7   27 

 03 SOLn   SL=   14.3    0.029    0.245    0.141   14.3   28.6  182.7   16 

 04 SLPn  76.0   36.8   ‐0.317   ‐0.015   ‐0.020    1.4   38.2  241.3   16 

 04 SLPn  76.0   36.8   ‐0.964   ‐0.077    0.022    4.1   40.9  241.3   17 

 04 SLPn  76.0   36.8   ‐0.102    0.091    0.002    4.5   41.3  241.3   17 

 

 Pt  91     Line 8    v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 8    n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.100    0.003    0.034    1.6   11.5  137.4    8 

 01 SL n  20.5    9.9   ‐0.100    0.003    0.034    1.6   11.5  137.4    8 

Page 76: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

11/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 02 SERv   SL=   11.5   ‐0.314   ‐0.056   ‐0.608   21.6   21.8  332.6    7 

 02 SERn   SL=   11.5   ‐0.314   ‐0.056   ‐0.608   21.6   21.8  332.6    7 

 03 SOLv   SL=   11.5    0.031    0.157    0.198   11.8   23.3  182.7   13 

 03 SOLn   SL=   11.5    0.049    0.157    0.198   11.8   23.4  182.7   13 

 04 SLPv  76.0   36.8   ‐0.102    0.003    0.036    1.7   38.4  241.3   16 

 04 SLPn  76.0   36.8   ‐0.102    0.003    0.036    1.7   38.4  241.3   16 

 

 Pt  101    Line 8    v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.100    0.003   ‐0.009    0.5   10.4  137.4    8 

 02 SERv   SL=   10.4   ‐0.314   ‐0.045   ‐0.551   19.6   19.8  333.7    6 

 03 SOLv   SL=   10.4    0.052    0.171    0.156   10.8   21.2  182.7   12 

Page 77: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

12/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page      8 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 04 SLPv  76.0   36.8   ‐0.102    0.003   ‐0.008    0.4   37.2  241.3   15 

 

 Pt  103    Line 8    n Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL n  20.5    9.9   ‐0.100    0.005   ‐0.086    4.0   13.9  137.4   10 

 02 SERn   SL=   13.9   ‐0.314   ‐0.002   ‐0.318   11.2   11.5  330.2    3 

 03 SOLn   SL=   13.9    0.270    0.191    0.030    9.1   23.2  182.7   13 

 04 SLPn  76.0   36.8   ‐0.102    0.006   ‐0.087    4.0   40.8  241.3   17 

 

 Pt  97     Line 8    v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 8    n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.100    0.010    0.014    0.8   10.7  137.4    8 

 01 SL n  20.5    9.9   ‐0.100    0.010    0.014    0.8   10.7  137.4    8 

 02 SERv   SL=   10.7    0.247    0.036    0.157    5.7    5.9  333.4    2 

 02 SERn   SL=   10.7    0.247    0.036    0.157    5.7    5.9  333.4    2 

 03 SOLv   SL=   10.7    0.325    0.151    0.344   17.5   28.5  182.7   16 

 03 SOLn   SL=   10.7    0.325    0.151    0.344   17.5   28.5  182.7   16 

 04 SLPv  76.0   36.8   ‐0.102    0.011    0.013    0.8   37.5  241.3   16 

 04 SLPn  76.0   36.8   ‐0.102    0.011    0.013    0.8   37.5  241.3   16 

 

 Pt  155    Line 10   n Da=  114.3 mm s=  4.5 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL n  20.5   11.5    0.078   ‐0.006   ‐0.242    5.9   17.4  137.4   13 

 02 SERn   SL=   17.4   ‐0.303    0.039    0.184    4.0    4.1  326.7    1 

 03 SOLn   SL=   17.4    0.079    0.041    0.032    3.6   21.0  182.7   11 

 04 SLPn  76.0   42.5    0.080   ‐0.006   ‐0.248    6.0   48.5  241.3   20 

 

 Pt  157    Line 10   v Da=  114.3 mm s=  4.5 mm (RKR ) Reducer r < 0.1D 

            Line 10   n Da=   88.9 mm s=  4.0 mm   A=   60.0 deg 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

Page 78: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

13/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   11.5    0.077   ‐0.007   ‐0.274    6.7   18.1  137.4   13 

 01 SL n  20.5   10.0    0.077   ‐0.007   ‐0.274   12.7   22.7  137.4   17 

 02 SERv   SL=   18.1   ‐0.303    0.046    0.183    4.0    4.1  325.9    1 

 02 SERn   SL=   22.7   ‐0.303    0.046    0.183    7.4    7.6  321.4    2 

 03 SOLv   SL=   18.1    0.083    0.049    0.036    3.7   21.8  182.7   12 

 03 SOLn   SL=   22.7    0.083    0.049    0.036    7.0   29.7  182.7   16 

 04 SLPv  76.0   42.5    0.079   ‐0.008   ‐0.281    6.8   49.3  241.3   20 

 04 SLPn  76.0   36.8    0.079   ‐0.008   ‐0.281   13.0   49.8  241.3   21 

Page 79: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

14/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page      9 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Pt  153    Line 10   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 10   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   10.0    0.076   ‐0.008   ‐0.305   14.2   24.1  137.4   18 

 01 SL n  20.5    9.9    0.000   ‐0.010   ‐0.305   14.2   24.1  137.4   18 

 02 SERv   SL=   24.1   ‐0.303    0.053    0.181    7.4    7.6  320.0    2 

 02 SERn   SL=   24.1   ‐0.304    0.064    0.181    7.4    7.6  320.0    2 

 03 SOLv   SL=   24.1    0.086    0.056    0.040    7.1   31.3  182.7   17 

 03 SOLn   SL=   24.1    0.109    0.073    0.040    7.1   31.3  182.7   17 

 04 SLPv  76.0   36.8    0.078   ‐0.009   ‐0.313   14.5   51.3  241.3   21 

 04 SLPn  76.0   36.8    0.000   ‐0.010   ‐0.313   14.5   51.3  241.3   21 

 

 Pt  151    Line 10   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9    0.000   ‐0.011   ‐0.348   16.1   26.0  137.4   19 

 02 SERv   SL=   26.0   ‐0.304    0.074    0.181    7.5    7.7  318.1    2 

 03 SOLv   SL=   26.0    0.113    0.082    0.046    7.4   33.5  182.7   18 

 04 SLPv  76.0   36.8    0.000   ‐0.012   ‐0.357   16.5   53.3  241.3   22 

 

 Pt  149    Line 10   n Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL n  20.5    9.9    0.000   ‐0.017   ‐0.411   19.0   28.9  137.4   21 

 02 SERn   SL=   28.9   ‐0.304    0.112    0.183    8.1    8.3  315.1    3 

 03 SOLn   SL=   28.9    0.336    0.085    0.057    7.7   36.8  182.7   20 

 04 SLPn  76.0   36.8    0.000   ‐0.018   ‐0.422   19.6   56.3  241.3   23 

 

 Pt  145    Line 10   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 10   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9    0.000   ‐0.018   ‐0.404   18.7   28.6  137.4   21 

 01 SL n  20.5    9.9    0.019   ‐0.020   ‐0.404   18.7   28.7  137.4   21 

 02 SERv   SL=   28.6   ‐0.304    0.123    0.183    8.3    8.5  315.4    3 

 02 SERn   SL=   28.7   ‐0.301    0.132    0.183    8.3    8.5  315.4    3 

Page 80: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

15/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 03 SOLv   SL=   28.6    0.340    0.079    0.057    7.5   36.4  182.7   20 

 03 SOLn   SL=   28.7    0.360    0.093    0.057    7.5   36.4  182.7   20 

 04 SLPv  76.0   36.8    0.000   ‐0.020   ‐0.416   19.3   56.1  241.3   23 

 04 SLPn  76.0   36.8    0.018   ‐0.022   ‐0.416   19.3   56.1  241.3   23 

 

 Pt  147    Line 10   v Da=   88.9 mm s=  4.0 mm (RKR ) Reducer r < 0.1D 

            Line 10   n Da=  114.3 mm s=  4.5 mm   A=   60.0 deg 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9    0.020   ‐0.021   ‐0.396   18.4   28.3  137.4   21 

 01 SL n  20.5   11.5    0.020   ‐0.021   ‐0.396    9.6   21.1  137.4   15 

 02 SERv   SL=   28.3   ‐0.301    0.139    0.185    8.5    8.7  315.8    3 

 02 SERn   SL=   21.1   ‐0.301    0.139    0.185    4.6    4.7  323.0    1 

Page 81: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

16/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     10 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 03 SOLv   SL=   28.3    0.362    0.088    0.058    7.4   35.9  182.7   20 

 03 SOLn   SL=   21.1    0.362    0.088    0.058    3.9   25.1  182.7   14 

 04 SLPv  76.0   36.8    0.019   ‐0.023   ‐0.408   18.9   55.7  241.3   23 

 04 SLPn  76.0   42.4    0.019   ‐0.023   ‐0.408    9.9   52.4  241.3   22 

 

 Pt  139    Line 10   v Da=  114.3 mm s=  4.5 mm (VUU ) GirtButtWeldAsWeld 

            Line 10   n Da=  114.3 mm s=  4.5 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   11.5    0.022   ‐0.022   ‐0.387    9.4   20.9  137.4   15 

 01 SL n  20.5   11.4    0.000   ‐0.021   ‐0.387    9.4   20.9  137.4   15 

 02 SERv   SL=   20.9   ‐0.301    0.146    0.187    4.7    4.8  323.2    1 

 02 SERn   SL=   20.9   ‐0.304    0.137    0.187    4.7    4.8  323.2    1 

 03 SOLv   SL=   20.9    0.366    0.083    0.059    3.8   24.9  182.7   14 

 03 SOLn   SL=   20.9    0.370    0.069    0.059    3.8   24.8  182.7   14 

 04 SLPv  76.0   42.4    0.021   ‐0.024   ‐0.400    9.7   52.2  241.3   22 

 04 SLPn  76.0   42.4    0.000   ‐0.022   ‐0.400    9.7   52.2  241.3   22 

 

 Pt  5      Line 10   v Da=  114.3 mm s=  4.5 mm (TTU ) Unreinf. fabr. tee 

            Line 10   n Da=  114.3 mm s=  4.5 mm  ii= 3.2  io= 3.9  it= 1.0 

            Line 20   n Da=   88.9 mm s=  4.0 mm 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   11.4    0.000    0.023    0.362   25.7   37.2  137.4   27 

 01 SL n  20.5   11.5    0.092   ‐0.012    0.320   22.7   34.2  137.4   25 

 01 SL n  20.5    9.9   ‐0.007    0.036    0.012    4.0   13.6  137.4   10 

 02 SERv   SL=   37.2   ‐0.304   ‐0.155   ‐0.188   16.8   17.0  306.9    6 

 02 SERn   SL=   34.2   ‐0.782    0.211   ‐0.370   30.1   30.5  309.9   10 

 02 SERn   SL=   13.6   ‐0.105   ‐0.366   ‐0.083   37.0   37.1  330.5   11 

 03 SOLv   SL=   37.2    0.381    0.060    0.059    6.3   43.7  182.7   24 

 03 SOLn   SL=   34.2    0.672    0.242    0.151   17.6   52.2  182.7   29 

 03 SOLn   SL=   13.6    0.079    0.222    0.131   25.8   39.5  182.7   22 

 04 SLPv  76.0   42.4    0.000    0.025    0.376   26.7   69.1  241.3   29 

 04 SLPn  76.0   42.5    0.100   ‐0.014    0.330   23.4   65.9  241.3   27 

 04 SLPn  76.0   36.8   ‐0.007    0.039    0.014    4.3   40.7  241.3   17 

 

 Pt  163    Line 10   v Da=  114.3 mm s=  4.5 mm (KUH ) Fillet weld conc. 

            Line 10   n Da=  114.3 mm s=  4.5 mm  ii= 1.3  io= 1.3  it= 1.0 

 

Page 82: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

17/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   11.5    0.092    0.010   ‐0.274    6.7   18.2  137.4   13 

 01 SL n  20.5   11.4   ‐0.000    0.000    0.008    0.2   11.6  137.4    8 

 02 SERv   SL=   18.2   ‐0.782   ‐0.170    0.299    8.5    8.9  325.9    3 

 02 SERn   SL=   11.6    0.000   ‐0.000    0.000    0.0    0.0  332.5    0 

 03 SOLv   SL=   18.2    0.683    0.201    0.123    5.7   24.3  182.7   13 

 03 SOLn   SL=   11.6    0.025    0.003    0.003    0.1   11.8  182.7    6 

 04 SLPv  76.0   42.5    0.100    0.011   ‐0.283    6.9   49.4  241.3   20 

 04 SLPn  76.0   42.4   ‐0.000    0.000    0.009    0.2   42.6  241.3   18 

Page 83: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

18/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     11 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Pt  3      Line 10   v Da=  114.3 mm s=  4.5 mm (BGL ) pipe bend 

            Line 10   m Da=  114.3 mm s=  4.5 mm   R=  152.4 mm 

            Line 10   n Da=  114.3 mm s=  4.5 mm  ii= 1.9  io= 1.6  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   11.4   ‐0.000   ‐0.008    0.000    0.3   11.7  137.4    9 

 01 SL m  20.5   11.4   ‐0.032   ‐0.002   ‐0.000    0.1   11.5  137.4    8 

 01 SL n  20.5   11.4   ‐0.019   ‐0.000   ‐0.000    0.0   11.4  137.4    8 

 02 SERv   SL=   11.7    0.000    0.000   ‐0.000    0.0    0.0  332.4    0 

 02 SERm   SL=   11.5    0.000    0.000    0.000    0.0    0.0  332.6    0 

 02 SERn   SL=   11.4    0.000   ‐0.000    0.000    0.0    0.0  332.7    0 

 03 SOLv   SL=   11.7    0.025    0.003    0.003    0.1   11.9  182.7    6 

 03 SOLm   SL=   11.5    0.012    0.002    0.001    0.1   11.6  182.7    6 

 03 SOLn   SL=   11.4    0.002    0.000    0.000    0.0   11.5  182.7    6 

 04 SLPv  76.0   42.4   ‐0.000   ‐0.009    0.000    0.3   42.7  241.3   18 

 04 SLPm  76.0   42.4   ‐0.035   ‐0.002   ‐0.000    0.1   42.5  241.3   18 

 04 SLPn  76.0   42.4   ‐0.021   ‐0.000   ‐0.000    0.0   42.4  241.3   18 

 

 Pt  1      Line 10   v Da=  114.3 mm s=  4.5 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   11.4    0.000    0.000   ‐0.000    0.0   11.4  137.4    8 

 02 SERv   SL=   11.4   ‐0.000   ‐0.000   ‐0.000    0.0    0.0  332.7    0 

 03 SOLv   SL=   11.4    0.000    0.000    0.000    0.0   11.4  182.7    6 

 04 SLPv  76.0   42.4    0.000    0.000   ‐0.000    0.0   42.4  241.3   18 

 

 Pt  155    Line 11   n Da=  114.3 mm s=  4.5 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL n  20.5   11.4    0.000    0.007   ‐0.242    5.9   17.3  137.4   13 

 02 SERn   SL=   17.3   ‐0.304   ‐0.050    0.184    4.0    4.1  326.8    1 

 03 SOLn   SL=   17.3    0.078    0.058    0.032    3.6   20.9  182.7   11 

 04 SLPn  76.0   42.4    0.000    0.008   ‐0.248    6.0   48.5  241.3   20 

 

 Pt  7      Line 11   v Da=  114.3 mm s=  4.5 mm (BGL ) pipe bend 

            Line 11   m Da=  114.3 mm s=  4.5 mm   R=  152.4 mm 

            Line 11   n Da=  114.3 mm s=  4.5 mm  ii= 1.9  io= 1.6  it= 1.0 

 

Page 84: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

19/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   11.4    0.000    0.106    0.003    3.7   15.2  137.4   11 

 01 SL m  20.5   11.8    0.499    0.032   ‐0.009    1.2   12.9  137.4    9 

 01 SL n  20.5   11.9    0.731    0.000   ‐0.016    0.5   12.4  137.4    9 

 02 SERv   SL=   15.2   ‐0.304   ‐0.183   ‐0.021    6.9    7.0  328.9    2 

 02 SERm   SL=   12.9   ‐0.219   ‐0.196    0.059    7.5    7.6  331.2    2 

 02 SERn   SL=   12.4   ‐0.005   ‐0.229    0.104    8.9    8.9  331.7    3 

 03 SOLv   SL=   15.2    0.062    0.014    0.026    3.3   18.5  182.7   10 

 03 SOLm   SL=   12.9    0.078    0.007    0.093    3.7   16.7  182.7    9 

 03 SOLn   SL=   12.4    0.094    0.010    0.159    4.6   17.1  182.7    9 

 04 SLPv  76.0   42.4    0.000    0.110    0.003    3.9   46.3  241.3   19 

 04 SLPm  76.0   42.8    0.514    0.033   ‐0.010    1.2   43.9  241.3   18 

 04 SLPn  76.0   42.9    0.755    0.000   ‐0.017    0.5   43.4  241.3   18 

Page 85: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

20/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     12 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Pt  159    Line 11   v Da=  114.3 mm s=  4.5 mm (KUH ) Fillet weld conc. 

            Line 11   n Da=  114.3 mm s=  4.5 mm  ii= 1.3  io= 1.3  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   11.9    0.732   ‐0.016   ‐0.000    0.4   12.3  137.4    9 

 01 SL n  20.5   11.4   ‐0.038   ‐0.000   ‐0.000    0.0   11.4  137.4    8 

 02 SERv   SL=   12.3   ‐0.005    0.104    0.229    6.2    6.2  331.8    2 

 02 SERn   SL=   11.4    0.000    0.000   ‐0.000    0.0    0.0  332.7    0 

 03 SOLv   SL=   12.3    0.094    0.159    0.010    3.9   16.2  182.7    9 

 03 SOLn   SL=   11.4    0.005    0.001    0.001    0.0   11.5  182.7    6 

 04 SLPv  76.0   42.9    0.755   ‐0.017   ‐0.000    0.4   43.3  241.3   18 

 04 SLPn  76.0   42.4   ‐0.042    0.000   ‐0.000    0.0   42.4  241.3   18 

 

 Pt  137    Line 11   v Da=  114.3 mm s=  4.5 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   11.4    0.000   ‐0.000   ‐0.000    0.0   11.4  137.4    8 

 02 SERv   SL=   11.4    0.000    0.000   ‐0.000    0.0    0.0  332.7    0 

 03 SOLv   SL=   11.4    0.000    0.000    0.000    0.0   11.4  182.7    6 

 04 SLPv  76.0   42.4   ‐0.000    0.000   ‐0.000    0.0   42.4  241.3   18 

 

 Pt  163    Line 12   n Da=   88.9 mm s=  4.0 mm (KUH ) Fillet weld conc. 

                                                 ii=  1.3 io=  1.3 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL n  20.5   10.0    0.092    0.010   ‐0.281   13.0   23.0  137.4   17 

 02 SERn   SL=   23.0   ‐0.782   ‐0.170    0.299   15.8   16.4  321.1    5 

 03 SOLn   SL=   23.0    0.706    0.204    0.122   11.0   34.7  182.7   19 

 04 SLPn   0.0    0.1    0.100    0.011   ‐0.292   13.5   13.6  241.3    6 

 

 Pt  167    Line 12   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 12   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   10.0    0.092    0.000    0.001    0.1   10.1  137.4    7 

 01 SL n  20.5    9.9   ‐0.000    0.000    0.001    0.1   10.0  137.4    7 

 02 SERv   SL=   10.1   ‐0.782   ‐0.000    0.000    0.0    0.5  334.0    0 

 02 SERn   SL=   10.0    0.000   ‐0.000    0.000    0.0    0.0  334.1    0 

Page 86: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

21/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 03 SOLv   SL=   10.1    0.731    0.000    0.000    0.0   10.8  182.7    6 

 03 SOLn   SL=   10.0    0.006    0.000    0.000    0.0   10.0  182.7    5 

 04 SLPv   0.0    0.1    0.100    0.000    0.001    0.1    0.2  241.3    0 

 04 SLPn   0.0    0.0    0.000    0.000    0.001    0.1    0.1  241.3    0 

 

 Pt  165    Line 12   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.000    0.000   ‐0.000    0.0    9.9  137.4    7 

 02 SERv   SL=    9.9    0.000   ‐0.000   ‐0.000    0.0    0.0  334.2    0 

 03 SOLv   SL=    9.9    0.000    0.000    0.000    0.0    9.9  182.7    5 

 04 SLPv   0.0    0.0    0.000    0.000   ‐0.000    0.0    0.0  241.3    0 

Page 87: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

22/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     13 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Pt  159    Line 13   n Da=   88.9 mm s=  4.0 mm (KUH ) Fillet weld conc. 

                                                 ii=  1.3 io=  1.3 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL n  20.5    9.9   ‐0.769    0.016   ‐0.000    0.7   10.6  137.4    8 

 02 SERn   SL=   10.6    0.005   ‐0.104    0.229   11.6   11.6  333.5    3 

 03 SOLn   SL=   10.6    0.098    0.158    0.011    7.3   18.0  182.7   10 

 04 SLPn   0.0    0.7   ‐0.797    0.017    0.000    0.8    1.5  241.3    1 

 

 Pt  161    Line 13   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.852    0.000   ‐0.000    0.0    9.9  137.4    7 

 02 SERv   SL=    9.9    0.080    0.000    0.000    0.0    0.1  334.2    0 

 03 SOLv   SL=    9.9    0.108    0.000    0.000    0.0   10.0  182.7    5 

 04 SLPv   0.0    0.8   ‐0.879    0.000    0.000    0.0    0.8  241.3    0 

 

 Pt  187    Line 14   n Da=   88.9 mm s=  4.0 mm (KUH ) Fillet weld conc. 

                                                 ii=  1.3 io=  1.3 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL n  20.5    9.9   ‐1.902   ‐0.011    0.019    1.0   10.9  137.4    8 

 02 SERn   SL=   10.9   ‐0.780    0.024    0.606   27.9   28.4  333.2    9 

 03 SOLn   SL=   10.9    1.179    0.377    0.861   43.5   55.5  182.7   30 

 04 SLPn   0.0    1.8   ‐1.952   ‐0.012    0.021    1.1    3.0  241.3    1 

 

 Pt  189    Line 14   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐1.981    0.000    0.000    0.0    9.9  137.4    7 

 02 SERv   SL=    9.9   ‐0.780    0.000    0.000    0.0    0.5  334.2    0 

 03 SOLv   SL=    9.9    1.181    0.000    0.000    0.0   11.0  182.7    6 

 04 SLPv   0.0    1.9   ‐2.030    0.000    0.000    0.0    1.9  241.3    1 

 

 Pt  195    Line 15   n Da=   88.9 mm s=  4.0 mm (KUH ) Fillet weld conc. 

                                                 ii=  1.3 io=  1.3 it=  1.0 

 

Page 88: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

23/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL n  20.5    9.9   ‐1.387   ‐0.006    0.000    0.3   10.2  137.4    7 

 02 SERn   SL=   10.2   ‐1.292   ‐0.025   ‐0.618   28.5   29.4  333.9    9 

 03 SOLn   SL=   10.2    1.049    0.128    0.010    6.0   17.2  182.7    9 

 04 SLPn   0.0    1.3   ‐1.417   ‐0.007    0.000    0.3    1.7  241.3    1 

 

 Pt  197    Line 15   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐1.465    0.000    0.000    0.0    9.9  137.4    7 

 02 SERv   SL=    9.9    1.294    0.000    0.000    0.0    0.9  334.2    0 

 03 SOLv   SL=    9.9    1.050    0.000    0.000    0.0   10.9  182.7    6 

Page 89: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

24/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     14 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 04 SLPv   0.0    1.4   ‐1.496    0.000    0.000    0.0    1.4  241.3    1 

 

 Pt  203    Line 16   n Da=   88.9 mm s=  4.0 mm (KUH ) Fillet weld conc. 

                                                 ii=  1.3 io=  1.3 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL n  20.5    9.9   ‐0.523   ‐0.004   ‐0.063    2.9   12.8  137.4    9 

 02 SERn   SL=   12.8   ‐1.985   ‐0.084    0.061    4.8    6.1  331.3    2 

 03 SOLn   SL=   12.8    0.193    0.066    0.209   10.1   23.2  182.7   13 

 04 SLPn   0.0    0.5   ‐0.566   ‐0.004   ‐0.068    3.1    3.7  241.3    2 

 

 Pt  205    Line 16   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.601    0.000    0.000    0.0    9.9  137.4    7 

 02 SERv   SL=    9.9   ‐1.985    0.000    0.000    0.0    1.4  334.2    0 

 03 SOLv   SL=    9.9    0.196    0.000    0.000    0.0   10.1  182.7    6 

 04 SLPv   0.0    0.6   ‐0.644    0.000   ‐0.000    0.0    0.6  241.3    0 

 

 Pt  209    Line 17   n Da=   88.9 mm s=  4.0 mm (KUH ) Fillet weld conc. 

                                                 ii=  1.3 io=  1.3 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL n  20.5    9.9   ‐1.723    0.028    0.179    8.4   18.3  137.4   13 

 02 SERn   SL=   18.3   ‐3.098   ‐0.411    0.725   38.4   40.5  325.8   12 

 03 SOLn   SL=   18.3    0.415    0.201    0.158   11.8   30.5  182.7   17 

 04 SLPn   0.0    1.7   ‐1.806    0.028    0.184    8.6   10.3  241.3    4 

 

 Pt  211    Line 17   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐1.801    0.000   ‐0.000    0.0    9.9  137.4    7 

 02 SERv   SL=    9.9   ‐3.098   ‐0.000   ‐0.000    0.0    2.2  334.2    1 

 03 SOLv   SL=    9.9    0.420    0.000    0.000    0.0   10.3  182.7    6 

 04 SLPv   0.0    1.8   ‐1.884    0.000   ‐0.000    0.0    1.8  241.3    1 

Page 90: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

25/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 

 Pt  213    Line 18   n Da=   88.9 mm s=  4.0 mm (KUH ) Fillet weld conc. 

                                                 ii=  1.3 io=  1.3 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL n  20.5    9.9   ‐0.678    0.223   ‐0.176   13.2   23.1  137.4   17 

 02 SERn   SL=   23.1   ‐1.861    0.597   ‐1.474   73.2   74.5  321.0   23 

 03 SOLn   SL=   23.1    0.594    0.284    0.489   26.2   49.8  182.7   27 

 04 SLPn   0.0    0.7   ‐0.723    0.230   ‐0.181   13.5   14.2  241.3    6 

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THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

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54TH58-SS-115-001

SH/OF

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STAR DOCUMENT No.

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REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     15 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Pt  215    Line 18   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.757   ‐0.000    0.000    0.0    9.9  137.4    7 

 02 SERv   SL=    9.9   ‐1.861    0.000    0.000    0.0    1.3  334.2    0 

 03 SOLv   SL=    9.9    0.596    0.000    0.000    0.0   10.5  182.7    6 

 04 SLPv   0.0    0.8   ‐0.801   ‐0.000    0.000    0.0    0.8  241.3    0 

 

 Pt  77     Line 19   v Da=   88.9 mm s=  4.0 mm (BGL ) pipe bend 

            Line 19   m Da=   88.9 mm s=  4.0 mm   R=  114.3 mm 

            Line 19   n Da=   88.9 mm s=  4.0 mm  ii= 1.8  io= 1.5  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9    0.034   ‐0.078    0.053    5.9   15.6  137.4   11 

 01 SL m  20.5    9.9   ‐0.150   ‐0.057    0.096    6.0   15.9  137.4   12 

 01 SL n  20.5    9.9   ‐0.246   ‐0.046    0.082    6.5   15.5  137.4   11 

 02 SERv   SL=   15.6   ‐0.070    0.043   ‐0.775   43.3   43.3  328.5   13 

 02 SERm   SL=   15.9   ‐0.765    0.123   ‐0.284   35.4   35.7  328.2   11 

 02 SERn   SL=   15.5   ‐1.013    0.151    0.372   36.9   37.3  328.6   11 

 03 SOLv   SL=   15.6    0.292    0.162    0.072   11.1   26.9  182.7   15 

 03 SOLm   SL=   15.9    0.431    0.164    0.028   11.0   27.3  182.7   15 

 03 SOLn   SL=   15.5    0.489    0.150    0.055   10.1   26.1  182.7   14 

 04 SLPv  76.0   36.8    0.036   ‐0.081    0.054    6.1   42.5  241.3   18 

 04 SLPm  76.0   36.8   ‐0.154   ‐0.059    0.098    6.2   42.9  241.3   18 

 04 SLPn  76.0   36.8   ‐0.253   ‐0.048    0.084    6.6   42.1  241.3   17 

 

 Pt  233    Line 19   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.246    0.028   ‐0.208   10.5   20.0  137.4   15 

 02 SERv   SL=   20.0   ‐1.013   ‐0.114   ‐0.033   30.3   30.4  324.1    9 

 03 SOLv   SL=   20.0    0.438    0.053    0.144    7.9   28.3  182.7   15 

 04 SLPv  76.0   36.8   ‐0.253    0.029   ‐0.210   10.6   46.7  241.3   19 

 

 Pt  229    Line 19   n Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

Page 92: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

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STAR DOCUMENT No.

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REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL n  20.5    9.9   ‐0.246    0.007   ‐0.000    4.1   11.0  137.4    8 

 02 SERn   SL=   11.0   ‐1.013   ‐0.072    0.348   32.5   32.8  333.1   10 

 03 SOLn   SL=   11.0    0.116    0.046    0.304   14.7   25.8  182.7   14 

 04 SLPn  76.0   36.8   ‐0.253    0.007    0.002    4.1   37.3  241.3   15 

 

 Pt  75     Line 19   v Da=   88.9 mm s=  4.0 mm (BGL ) pipe bend 

            Line 19   m Da=   88.9 mm s=  4.0 mm   R=  114.3 mm 

            Line 19   n Da=   88.9 mm s=  4.0 mm  ii= 1.8  io= 1.5  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.246   ‐0.067    0.005    5.8   14.6  137.4   11 

 01 SL m  20.5   10.4    0.499   ‐0.152   ‐0.061   10.2   20.4  137.4   15 

 01 SL n  20.5   10.8    0.965   ‐0.204   ‐0.091   13.3   24.1  137.4   18 

Page 93: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

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STAR DOCUMENT No.

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REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     16 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 02 SERv   SL=   14.6   ‐1.013   ‐0.397   ‐0.066   39.0   39.5  329.5   12 

 02 SERm   SL=   20.4   ‐0.267   ‐0.482    0.558   47.5   47.7  323.7   15 

 02 SERn   SL=   24.1    0.635   ‐0.585    0.855   57.5   57.9  320.0   18 

 03 SOLv   SL=   14.6    0.102    0.326    0.038   20.3   35.0  182.7   19 

 03 SOLm   SL=   20.4    0.220    0.348    0.049   21.7   42.2  182.7   23 

 03 SOLn   SL=   24.1    0.303    0.357    0.096   22.4   46.7  182.7   26 

 04 SLPv  76.0   36.8   ‐0.253   ‐0.070    0.005    5.9   41.3  241.3   17 

 04 SLPm  76.0   37.2    0.503   ‐0.156   ‐0.062   10.5   47.4  241.3   20 

 04 SLPn  76.0   37.7    0.979   ‐0.209   ‐0.093   13.6   51.3  241.3   21 

 

 Pt  209    Line 19   v Da=   88.9 mm s=  4.0 mm (KUH ) Fillet weld conc. 

                                                 ii=  1.3 io=  1.3 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   10.8    0.965   ‐0.091    0.204   10.3   21.2  137.4   15 

 02 SERv   SL=   21.2    0.635    0.855    0.586   47.8   48.2  322.9   15 

 03 SOLv   SL=   21.2    0.303    0.096    0.357   17.2   38.6  182.7   21 

 04 SLPv  76.0   37.7    0.979   ‐0.093    0.209   10.6   48.3  241.3   20 

 

 Pt  9      Line 20   v Da=   88.9 mm s=  4.0 mm (BGL ) pipe bend 

            Line 20   m Da=   88.9 mm s=  4.0 mm   R=  114.3 mm 

            Line 20   n Da=   88.9 mm s=  4.0 mm  ii= 1.8  io= 1.5  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.007   ‐0.003   ‐0.001    2.0   10.3  137.4    7 

 01 SL m  20.5    9.9   ‐0.069    0.005   ‐0.031    2.1   11.6  137.4    8 

 01 SL n  20.5    9.9   ‐0.092    0.007   ‐0.042    2.2   12.1  137.4    9 

 02 SERv   SL=   10.3   ‐0.105    0.194    0.073   14.2   14.3  333.8    4 

 02 SERm   SL=   11.6    0.263    0.152   ‐0.042   11.9   12.0  332.5    4 

 02 SERn   SL=   12.1    0.477    0.127   ‐0.133   11.4   11.7  332.0    4 

 03 SOLv   SL=   10.3    0.063    0.099    0.058    8.4   18.7  182.7   10 

 03 SOLm   SL=   11.6    0.233    0.074    0.101    7.1   19.0  182.7   10 

 03 SOLn   SL=   12.1    0.361    0.061    0.085    6.0   18.4  182.7   10 

 04 SLPv  76.0   36.8   ‐0.007   ‐0.003   ‐0.002    2.1   37.0  241.3   15 

 04 SLPm  76.0   36.8   ‐0.075    0.005   ‐0.034    2.2   38.5  241.3   16 

 04 SLPn  76.0   36.8   ‐0.100    0.008   ‐0.045    2.3   39.1  241.3   16 

 

 Pt  33     Line 20   v Da=   88.9 mm s=  4.0 mm (BGL ) pipe bend 

            Line 20   m Da=   88.9 mm s=  4.0 mm   R=  114.3 mm 

Page 94: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

29/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

            Line 20   n Da=   88.9 mm s=  4.0 mm  ii= 1.8  io= 1.5  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.092   ‐0.045    0.001    2.8   12.7  137.4    9 

 01 SL m  20.5   10.0    0.057   ‐0.062    0.001    3.8   13.7  137.4   10 

 01 SL n  20.5   10.1    0.185   ‐0.075    0.001    4.6   14.7  137.4   11 

 02 SERv   SL=   12.7    0.477   ‐0.305    0.021   19.5   19.8  331.4    6 

 02 SERm   SL=   13.7    0.643   ‐0.323   ‐0.079   20.8   21.3  330.4    6 

 02 SERn   SL=   14.7    0.431   ‐0.299   ‐0.134   19.9   20.2  329.4    6 

 03 SOLv   SL=   12.7    0.336    0.120    0.032    7.7   20.7  182.7   11 

 03 SOLm   SL=   13.7    0.145    0.145    0.005    9.1   23.0  182.7   13 

 03 SOLn   SL=   14.7    0.203    0.174    0.035   10.9   25.8  182.7   14 

Page 95: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

30/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     17 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 04 SLPv  76.0   36.8   ‐0.100   ‐0.048    0.001    2.9   39.7  241.3   16 

 04 SLPm  76.0   36.8    0.060   ‐0.066    0.002    4.0   40.8  241.3   17 

 04 SLPn  76.0   37.0    0.199   ‐0.080    0.002    4.9   41.9  241.3   17 

 

 Pt  203    Line 20   v Da=   88.9 mm s=  4.0 mm (KUH ) Fillet weld conc. 

                                                 ii=  1.3 io=  1.3 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   10.1    0.185   ‐0.001   ‐0.075    3.5   13.6  137.4   10 

 02 SERv   SL=   13.6    0.431    0.134   ‐0.299   15.1   15.4  330.5    5 

 03 SOLv   SL=   13.6    0.203    0.035    0.175    8.4   22.1  182.7   12 

 04 SLPv  76.0   37.0    0.199   ‐0.002   ‐0.080    3.7   40.7  241.3   17 

 

 Pt  87     Line 21   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 21   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.278   ‐0.019    0.013    1.1   11.0  137.4    8 

 01 SL n  20.5    9.9   ‐0.278   ‐0.019    0.013    1.1   11.0  137.4    8 

 02 SERv   SL=   11.0   ‐1.570    0.056   ‐0.733   26.1   27.2  333.1    8 

 02 SERn   SL=   11.0   ‐1.570    0.056   ‐0.733   26.1   27.2  333.1    8 

 03 SOLv   SL=   11.0    0.171    0.483    0.221   25.1   36.2  182.7   20 

 03 SOLn   SL=   11.0    0.171    0.483    0.221   25.1   36.2  182.7   20 

 04 SLPv  76.0   36.8   ‐0.298   ‐0.021    0.014    1.2   37.9  241.3   16 

 04 SLPn  76.0   36.8   ‐0.298   ‐0.021    0.014    1.2   37.9  241.3   16 

 

 Pt  43     Line 21   v Da=   88.9 mm s=  4.0 mm (BGL ) pipe bend 

            Line 21   m Da=   88.9 mm s=  4.0 mm   R=  114.3 mm 

            Line 21   n Da=   88.9 mm s=  4.0 mm  ii= 1.8  io= 1.5  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   10.0    0.055   ‐0.029   ‐0.014    1.9   11.9  137.4    9 

 01 SL m  20.5   10.0    0.058   ‐0.029   ‐0.013    1.9   11.8  137.4    9 

 01 SL n  20.5   10.0    0.051   ‐0.027   ‐0.010    1.8   11.7  137.4    9 

 02 SERv   SL=   11.9   ‐1.570    0.436    0.888   53.5   54.6  332.2   16 

 02 SERm   SL=   11.8   ‐1.513    0.429    0.828   52.5   53.6  332.2   16 

 02 SERn   SL=   11.7   ‐1.226    0.396    0.642   48.2   48.9  332.4   15 

 03 SOLv   SL=   11.9    0.168    0.048    0.093    7.6   19.6  182.7   11 

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 03 SOLm   SL=   11.8    0.236    0.042    0.116    7.8   19.9  182.7   11 

 03 SOLn   SL=   11.7    0.281    0.036    0.130    8.0   20.0  182.7   11 

 04 SLPv  76.0   36.8    0.064   ‐0.033   ‐0.015    2.1   39.0  241.3   16 

 04 SLPm  76.0   36.8    0.067   ‐0.032   ‐0.014    2.1   38.9  241.3   16 

 04 SLPn  76.0   36.8    0.058   ‐0.031   ‐0.011    2.0   38.8  241.3   16 

 

 Pt  41     Line 21   v Da=   88.9 mm s=  4.0 mm (BGL ) pipe bend 

            Line 21   m Da=   88.9 mm s=  4.0 mm   R=  114.3 mm 

            Line 21   n Da=   88.9 mm s=  4.0 mm  ii= 1.8  io= 1.5  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   10.0    0.088   ‐0.014    0.004    1.0   10.9  137.4    8 

 01 SL m  20.5   10.0    0.077   ‐0.012    0.003    0.8   10.7  137.4    8 

 01 SL n  20.5    9.9    0.012   ‐0.004    0.000    0.4   10.2  137.4    7 

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APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     18 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 02 SERv   SL=   10.9   ‐1.226    0.901   ‐0.029   61.2   62.0  333.2   19 

 02 SERm   SL=   10.7   ‐1.362    0.916   ‐0.430   63.8   64.7  333.4   19 

 02 SERn   SL=   10.2   ‐0.700    0.841   ‐0.580   60.5   60.9  333.9   18 

 03 SOLv   SL=   10.9    0.293    0.186    0.027   12.1   23.3  182.7   13 

 03 SOLm   SL=   10.7    0.328    0.192    0.054   12.5   23.5  182.7   13 

 03 SOLn   SL=   10.2    0.224    0.177    0.074   11.6   21.9  182.7   12 

 04 SLPv  76.0   36.9    0.099   ‐0.015    0.004    1.1   37.8  241.3   16 

 04 SLPm  76.0   36.8    0.086   ‐0.013    0.004    0.9   37.7  241.3   16 

 04 SLPn  76.0   36.8    0.012   ‐0.004   ‐0.000    0.4   37.0  241.3   15 

 

 Pt  169    Line 21   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 21   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9    0.012    0.002    0.026    1.2   11.1  137.4    8 

 01 SL n  20.5    9.9    0.012    0.002    0.026    1.2   11.1  137.4    8 

 02 SERv   SL=   11.1   ‐0.700   ‐0.155    0.721   26.3   26.8  333.0    8 

 02 SERn   SL=   11.1   ‐0.700   ‐0.155    0.721   26.3   26.8  333.0    8 

 03 SOLv   SL=   11.1    0.233    0.060    0.129    6.8   18.2  182.7   10 

 03 SOLn   SL=   11.1    0.233    0.060    0.129    6.8   18.2  182.7   10 

 04 SLPv  76.0   36.8    0.012    0.002    0.029    1.4   38.1  241.3   16 

 04 SLPn  76.0   36.8    0.012    0.002    0.029    1.4   38.1  241.3   16 

 

 Pt  99     Line 21   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 21   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9    0.012   ‐0.000    0.137    6.3   16.3  137.4   12 

 01 SL n  20.5    9.9    0.012   ‐0.000    0.137    6.3   16.3  137.4   12 

 02 SERv   SL=   16.3   ‐0.700   ‐0.072   ‐0.072    4.7    5.1  327.8    2 

 02 SERn   SL=   16.3   ‐0.700   ‐0.072   ‐0.072    4.7    5.1  327.8    2 

 03 SOLv   SL=   16.3    0.282    0.115    0.056    6.2   22.7  182.7   12 

 03 SOLn   SL=   16.3    0.282    0.115    0.056    6.2   22.7  182.7   12 

 04 SLPv  76.0   36.8    0.012   ‐0.001    0.151    7.0   43.8  241.3   18 

 04 SLPn  76.0   36.8    0.012   ‐0.001    0.151    7.0   43.8  241.3   18 

 

 Pt  225    Line 21   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 21   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

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THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

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SH/OF

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STAR DOCUMENT No.

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APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9    0.012   ‐0.003    0.356   16.5   26.4  137.4   19 

 01 SL n  20.5    9.9    0.001   ‐0.003    0.356   16.5   26.4  137.4   19 

 02 SERv   SL=   26.4   ‐0.700    0.016   ‐0.916   32.6   33.1  317.7   10 

 02 SERn   SL=   26.4   ‐1.197    0.016   ‐0.916   32.6   33.4  317.7   11 

 03 SOLv   SL=   26.4    0.334    0.317    0.077   15.2   41.9  182.7   23 

 03 SOLn   SL=   26.4    0.293    0.317    0.077   15.2   41.9  182.7   23 

 04 SLPv  76.0   36.8    0.012   ‐0.003    0.386   17.9   54.6  241.3   23 

 04 SLPn  76.0   36.8    0.001   ‐0.003    0.386   17.9   54.6  241.3   23 

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APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     19 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Pt  227    Line 21   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 21   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9    0.001   ‐0.001   ‐0.262   12.1   22.1  137.4   16 

 01 SL n  20.5    9.9    0.001   ‐0.001   ‐0.262   12.1   22.1  137.4   16 

 02 SERv   SL=   22.1   ‐1.197    0.167   ‐0.460   17.6   18.4  322.0    6 

 02 SERn   SL=   22.1   ‐1.197    0.167   ‐0.460   17.6   18.4  322.0    6 

 03 SOLv   SL=   22.1    0.168    0.006    0.043    2.8   24.9  182.7   14 

 03 SOLn   SL=   22.1    0.168    0.006    0.043    2.8   24.9  182.7   14 

 04 SLPv  76.0   36.8    0.001   ‐0.001   ‐0.285   13.2   50.0  241.3   21 

 04 SLPn  76.0   36.8    0.001   ‐0.001   ‐0.285   13.2   50.0  241.3   21 

 

 Pt  181    Line 21   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 21   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9    0.001    0.001    0.018    0.9   10.7  137.4    8 

 01 SL n  20.5    9.9    0.001    0.001    0.018    0.9   10.7  137.4    8 

 02 SERv   SL=   10.7   ‐1.197    0.317   ‐0.004   11.6   12.4  333.4    4 

 02 SERn   SL=   10.7   ‐0.006    0.317   ‐0.004   11.6   11.6  333.4    3 

 03 SOLv   SL=   10.7    0.066    0.006    0.006    1.9   12.7  182.7    7 

 03 SOLn   SL=   10.7    0.066    0.006    0.006    1.9   12.7  182.7    7 

 04 SLPv  76.0   36.8    0.001    0.001    0.019    0.9   37.7  241.3   16 

 04 SLPn  76.0   36.8    0.001    0.001    0.019    0.9   37.7  241.3   16 

 

 Pt  39     Line 21   v Da=   88.9 mm s=  4.0 mm (BGL ) pipe bend 

            Line 21   m Da=   88.9 mm s=  4.0 mm   R=  114.3 mm 

            Line 21   n Da=   88.9 mm s=  4.0 mm  ii= 1.8  io= 1.5  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9    0.001   ‐0.000   ‐0.007    0.4   10.3  137.4    7 

 01 SL m  20.5    9.9   ‐0.002   ‐0.000    0.003    0.4   10.1  137.4    7 

 01 SL n  20.5    9.9   ‐0.004    0.000    0.010    0.5   10.4  137.4    8 

 02 SERv   SL=   10.3   ‐0.006    0.279    0.027   17.7   17.7  333.8    5 

 02 SERm   SL=   10.1   ‐2.276    0.538   ‐0.031   33.7   35.3  334.0   11 

 02 SERn   SL=   10.4   ‐3.212    0.646   ‐0.071   40.4   42.6  333.7   13 

 03 SOLv   SL=   10.3    0.063    0.012    0.021    2.3   12.6  182.7    7 

 03 SOLm   SL=   10.1    0.116    0.018    0.008    2.4   12.6  182.7    7 

 03 SOLn   SL=   10.4    0.107    0.017    0.031    2.3   12.8  182.7    7 

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HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

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THTF-2018-058

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 04 SLPv  76.0   36.8    0.001   ‐0.001   ‐0.007    0.5   37.1  241.3   15 

 04 SLPm  76.0   36.8   ‐0.003   ‐0.000    0.003    0.4   36.9  241.3   15 

 04 SLPn  76.0   36.8   ‐0.005   ‐0.000    0.011    0.6   37.3  241.3   15 

 

 Pt  37     Line 21   v Da=   88.9 mm s=  4.0 mm (BGL ) pipe bend 

            Line 21   m Da=   88.9 mm s=  4.0 mm   R=  114.3 mm 

            Line 21   n Da=   88.9 mm s=  4.0 mm  ii= 1.8  io= 1.5  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.004    0.000    0.005    0.3   10.2  137.4    7 

 01 SL m  20.5    9.9   ‐0.003    0.000    0.002    0.1   10.0  137.4    7 

 01 SL n  20.5    9.9   ‐0.001   ‐0.000   ‐0.004    0.2   10.1  137.4    7 

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HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

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THTF-2018-058

UNIT Nº

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54TH58-SS-115-001

SH/OF

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REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     20 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 02 SERv   SL=   10.2   ‐3.212    0.643   ‐0.019   40.1   42.3  333.9   13 

 02 SERm   SL=   10.0   ‐2.267    0.535   ‐0.032   33.4   34.9  334.1   10 

 02 SERn   SL=   10.1    0.006    0.275   ‐0.027   17.2   17.2  334.0    5 

 03 SOLv   SL=   10.2    0.129    0.009    0.006    1.5   11.8  182.7    6 

 03 SOLm   SL=   10.0    0.054    0.018    0.010    1.8   11.8  182.7    6 

 03 SOLn   SL=   10.1    0.065    0.031    0.021    2.3   12.5  182.7    7 

 04 SLPv  76.0   36.8   ‐0.005    0.000    0.006    0.3   37.1  241.3   15 

 04 SLPm  76.0   36.8   ‐0.004    0.000    0.002    0.1   36.9  241.3   15 

 04 SLPn  76.0   36.8   ‐0.001   ‐0.000   ‐0.004    0.2   37.0  241.3   15 

 

 Pt  183    Line 21   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 21   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.001    0.001    0.019    0.9   10.8  137.4    8 

 01 SL n  20.5    9.9   ‐0.001    0.001    0.019    0.9   10.8  137.4    8 

 02 SERv   SL=   10.8    0.006    0.321    0.004   11.4   11.4  333.3    3 

 02 SERn   SL=   10.8   ‐1.123    0.321    0.004   11.4   12.2  333.3    4 

 03 SOLv   SL=   10.8    0.069    0.058    0.006    2.8   13.6  182.7    7 

 03 SOLn   SL=   10.8    0.069    0.058    0.006    2.8   13.6  182.7    7 

 04 SLPv  76.0   36.8   ‐0.001    0.001    0.020    0.9   37.7  241.3   16 

 04 SLPn  76.0   36.8   ‐0.001    0.001    0.020    0.9   37.7  241.3   16 

 

 Pt  223    Line 21   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 21   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.001   ‐0.002    0.356   16.5   26.4  137.4   19 

 01 SL n  20.5    9.9    0.004   ‐0.002    0.356   16.5   26.4  137.4   19 

 02 SERv   SL=   26.4   ‐1.123    0.007   ‐0.992   35.1   35.9  317.7   11 

 02 SERn   SL=   26.4   ‐0.393    0.007   ‐0.992   35.1   35.4  317.7   11 

 03 SOLv   SL=   26.4    0.298    0.181    0.043    8.6   35.3  182.7   19 

 03 SOLn   SL=   26.4    0.165    0.181    0.043    8.6   35.2  182.7   19 

 04 SLPv  76.0   36.8   ‐0.001   ‐0.002    0.387   17.9   54.7  241.3   23 

 04 SLPn  76.0   36.8    0.005   ‐0.002    0.387   17.9   54.7  241.3   23 

 

 Pt  171    Line 21   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 21   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

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HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

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APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9    0.004   ‐0.000    0.035    1.6   11.5  137.4    8 

 01 SL n  20.5    9.9    0.004   ‐0.000    0.035    1.6   11.5  137.4    8 

 02 SERv   SL=   11.5   ‐0.393   ‐0.006    0.638   22.6   22.8  332.5    7 

 02 SERn   SL=   11.5   ‐0.393   ‐0.006    0.638   22.6   22.8  332.5    7 

 03 SOLv   SL=   11.5    0.111    0.006    0.035    1.8   13.4  182.7    7 

 03 SOLn   SL=   11.5    0.111    0.006    0.035    1.8   13.4  182.7    7 

 04 SLPv  76.0   36.8    0.005   ‐0.000    0.038    1.7   38.5  241.3   16 

 04 SLPn  76.0   36.8    0.005   ‐0.000    0.038    1.7   38.5  241.3   16 

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APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     21 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Pt  35     Line 21   v Da=   88.9 mm s=  4.0 mm (BGL ) pipe bend 

            Line 21   m Da=   88.9 mm s=  4.0 mm   R=  114.3 mm 

            Line 21   n Da=   88.9 mm s=  4.0 mm  ii= 1.8  io= 1.5  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9    0.004   ‐0.004   ‐0.000    0.3   10.2  137.4    7 

 01 SL m  20.5   10.0    0.138   ‐0.020    0.000    1.2   11.3  137.4    8 

 01 SL n  20.5   10.1    0.179   ‐0.026    0.000    1.6   11.7  137.4    8 

 02 SERv   SL=   10.2   ‐0.393    0.918    0.008   57.2   57.5  333.9   17 

 02 SERm   SL=   11.3   ‐1.376    1.031    0.010   64.2   65.1  332.8   20 

 02 SERn   SL=   11.7   ‐1.554    1.051    0.006   65.4   66.5  332.4   20 

 03 SOLv   SL=   10.2    0.101    0.041    0.018    2.8   13.1  182.7    7 

 03 SOLm   SL=   11.3    0.096    0.041    0.012    2.9   14.3  182.7    8 

 03 SOLn   SL=   11.7    0.043    0.035    0.002    2.6   14.3  182.7    8 

 04 SLPv  76.0   36.8    0.005   ‐0.005   ‐0.000    0.3   37.1  241.3   15 

 04 SLPm  76.0   36.9    0.151   ‐0.022    0.000    1.4   38.3  241.3   16 

 04 SLPn  76.0   36.9    0.194   ‐0.029    0.000    1.8   38.7  241.3   16 

 

 Pt  203    Line 21   v Da=   88.9 mm s=  4.0 mm (KUH ) Fillet weld conc. 

                                                 ii=  1.3 io=  1.3 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.338   ‐0.004    0.012    0.6   10.5  137.4    8 

 02 SERv   SL=   10.5   ‐1.554    0.050    0.360   16.7   17.8  333.6    5 

 03 SOLv   SL=   10.5    0.055    0.098    0.053    5.4   15.9  182.7    9 

 04 SLPv  76.0   36.8   ‐0.367   ‐0.005    0.012    0.6   37.4  241.3   15 

 

 Pt  89     Line 22   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 22   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.951   ‐0.019    0.065    3.1   13.0  137.4    9 

 01 SL n  20.5    9.9   ‐0.951   ‐0.019    0.065    3.1   13.0  137.4    9 

 02 SERv   SL=   13.0   ‐0.837    0.035    0.156    5.7    6.2  331.0    2 

 02 SERn   SL=   13.0   ‐0.837    0.035    0.156    5.7    6.2  331.0    2 

 03 SOLv   SL=   13.0    0.675    0.457    0.455   29.9   43.5  182.7   24 

 03 SOLn   SL=   13.0    0.675    0.457    0.455   29.9   43.5  182.7   24 

 04 SLPv  76.0   36.8   ‐0.983   ‐0.021    0.067    3.2   40.0  241.3   17 

 04 SLPn  76.0   36.8   ‐0.983   ‐0.021    0.067    3.2   40.0  241.3   17 

 

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HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

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THTF-2018-058

UNIT Nº

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APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 Pt  193    Line 22   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐1.077   ‐0.014    0.018    1.1   11.0  137.4    8 

 02 SERv   SL=   11.0   ‐0.837    0.024    0.317   11.3   11.8  333.1    4 

 03 SOLv   SL=   11.0    0.678    0.413    0.476   29.2   40.8  182.7   22 

 04 SLPv  76.0   36.8   ‐1.114   ‐0.016    0.019    1.1   37.9  241.3   16 

 

 Pt  191    Line 22   n Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL n  20.5    9.9   ‐1.578   ‐0.011   ‐0.013    0.8   10.7  137.4    8 

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HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

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APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     22 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 02 SERn   SL=   10.7   ‐0.837    0.016    0.426   15.1   15.7  333.4    5 

 03 SOLn   SL=   10.7    0.692    0.350    0.456   26.6   38.0  182.7   21 

 04 SLPn  76.0   36.8   ‐1.618   ‐0.012   ‐0.013    0.8   37.6  241.3   16 

 

 Pt  187    Line 22   v Da=   88.9 mm s=  4.0 mm (KUH ) Fillet weld conc. 

            Line 22   n Da=   88.9 mm s=  4.0 mm  ii= 1.3  io= 1.3  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐1.659   ‐0.010   ‐0.024    1.2   11.1  137.4    8 

 01 SL n  20.5   10.1    0.244    0.001   ‐0.043    2.0   12.2  137.4    9 

 02 SERv   SL=   11.1   ‐0.837    0.013    0.464   21.4   22.0  333.0    7 

 02 SERn   SL=   12.2   ‐0.057   ‐0.011   ‐0.142    6.5    6.6  331.9    2 

 03 SOLv   SL=   11.1    0.695    0.317    0.439   25.1   36.9  182.7   20 

 03 SOLn   SL=   12.2    0.493    0.059    0.422   19.7   32.4  182.7   18 

 04 SLPv  76.0   36.8   ‐1.700   ‐0.011   ‐0.024    1.2   38.0  241.3   16 

 04 SLPn  76.0   37.0    0.252    0.001   ‐0.045    2.1   39.1  241.3   16 

 

 Pt  47     Line 22   v Da=   88.9 mm s=  4.0 mm (BGL ) pipe bend 

            Line 22   m Da=   88.9 mm s=  4.0 mm   R=  114.3 mm 

            Line 22   n Da=   88.9 mm s=  4.0 mm  ii= 1.8  io= 1.5  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   10.1    0.244   ‐0.044   ‐0.001    2.7   12.8  137.4    9 

 01 SL m  20.5   10.1    0.223   ‐0.042   ‐0.001    2.6   12.7  137.4    9 

 01 SL n  20.5   10.0    0.084   ‐0.027   ‐0.000    1.7   11.7  137.4    8 

 02 SERv   SL=   12.8   ‐0.057   ‐0.141    0.011    8.8    8.8  331.3    3 

 02 SERm   SL=   12.7   ‐0.913   ‐0.043    0.012    2.7    3.4  331.4    1 

 02 SERn   SL=   11.7    1.011    0.021    0.006    1.4    2.1  332.4    1 

 03 SOLv   SL=   12.8    0.493    0.421    0.059   25.9   39.2  182.7   21 

 03 SOLm   SL=   12.7    0.360    0.324    0.048   19.9   33.0  182.7   18 

 03 SOLn   SL=   11.7    0.993    0.251    0.010   15.4   28.0  182.7   15 

 04 SLPv  76.0   37.0    0.252   ‐0.045   ‐0.001    2.8   39.8  241.3   16 

 04 SLPm  76.0   37.0    0.228   ‐0.044   ‐0.001    2.7   39.7  241.3   16 

 04 SLPn  76.0   36.8    0.085   ‐0.028   ‐0.000    1.7   38.6  241.3   16 

 

 Pt  109    Line 22   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 22   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

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HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

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54TH58-SS-115-001

SH/OF

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STAR DOCUMENT No.

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REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   10.0    0.084    0.000   ‐0.014    0.6   10.6  137.4    8 

 01 SL n  20.5   10.0    0.113    0.000   ‐0.014    0.6   10.7  137.4    8 

 02 SERv   SL=   10.6   ‐1.235    0.006    0.018    0.7    1.6  333.5    0 

 02 SERn   SL=   10.7   ‐1.228    0.007    0.018    0.7    1.6  333.4    0 

 03 SOLv   SL=   10.6    0.983    0.021    0.152    7.3   18.9  182.7   10 

 03 SOLn   SL=   10.7    0.892    0.015    0.152    7.3   18.8  182.7   10 

 04 SLPv  76.0   36.8    0.085    0.000   ‐0.013    0.6   37.5  241.3   16 

 04 SLPn  76.0   36.9    0.114    0.000   ‐0.013    0.6   37.5  241.3   16 

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HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

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APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     23 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Pt  115    Line 22   v Da=   88.9 mm s=  4.0 mm (RKR ) Reducer r < 0.1D 

            Line 22   n Da=   60.3 mm s=  2.4 mm   A=   60.0 deg 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   10.0    0.112    0.000   ‐0.021    1.0   11.0  137.4    8 

 01 SL n  20.5   11.6    0.112    0.000   ‐0.021    3.5   15.0  137.4   11 

 02 SERv   SL=   11.0   ‐1.228    0.007    0.011    0.6    1.4  333.1    0 

 02 SERn   SL=   15.0   ‐1.228    0.007    0.011    1.7    3.4  329.1    1 

 03 SOLv   SL=   11.0    0.890    0.021    0.123    6.1   17.9  182.7   10 

 03 SOLn   SL=   15.0    0.890    0.021    0.123   21.7   38.6  182.7   21 

 04 SLPv  76.0   36.9    0.113    0.000   ‐0.021    1.0   37.8  241.3   16 

 04 SLPn  76.0   42.2    0.113    0.000   ‐0.021    3.4   45.6  241.3   19 

 

 Pt  113    Line 22   v Da=   60.3 mm s=  2.4 mm (VUU ) GirtButtWeldAsWeld 

            Line 22   n Da=   60.3 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   11.6    0.112    0.001   ‐0.029    4.7   16.3  137.4   12 

 01 SL n  20.5    6.3    0.084    0.001   ‐0.029    3.1    9.3  137.4    7 

 02 SERv   SL=   16.3   ‐1.228    0.007    0.005    1.3    2.9  327.8    1 

 02 SERn   SL=    9.3   ‐1.235    0.005    0.005    1.0    2.1  334.8    1 

 03 SOLv   SL=   16.3    0.889    0.028    0.094   17.6   35.7  182.7   20 

 03 SOLn   SL=    9.3    0.979    0.034    0.094   11.4   22.0  182.7   12 

 04 SLPv  76.0   42.2    0.112    0.001   ‐0.029    4.7   46.8  241.3   19 

 04 SLPn  76.0   22.9    0.085    0.001   ‐0.029    3.0   26.0  241.3   11 

 

 Pt  117    Line 22   v Da=   60.3 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    6.3    0.084    0.001   ‐0.050    5.3   11.6  137.4    8 

 02 SERv   SL=   11.6   ‐1.235    0.004    0.012    1.4    2.5  332.5    1 

 03 SOLv   SL=   11.6    0.975    0.052    0.034    7.7   20.6  182.7   11 

 04 SLPv  76.0   22.9    0.085    0.001   ‐0.050    5.3   28.3  241.3   12 

 

 Pt  119    Line 22   n Da=   60.3 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

Page 108: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

43/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL n  20.5    6.3    0.084    0.002   ‐0.048    5.1   11.4  137.4    8 

 02 SERn   SL=   11.4    1.011    0.003    0.034    3.0    4.0  332.7    1 

 03 SOLn   SL=   11.4    0.847    0.073    0.098   13.6   26.1  182.7   14 

 04 SLPn  76.0   22.9    0.085    0.002   ‐0.048    5.1   28.1  241.3   12 

 

 Pt  121    Line 22   v Da=   60.3 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 22   n Da=   60.3 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    6.3    0.084    0.002   ‐0.035    3.7   10.0  137.4    7 

 01 SL n  20.5    6.3    0.120    0.002   ‐0.035    3.7   10.0  137.4    7 

 02 SERv   SL=   10.0    1.011    0.004    0.040    3.5    4.6  334.1    1 

 02 SERn   SL=   10.0    0.982    0.006    0.040    3.5    4.5  334.1    1 

Page 109: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

44/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     24 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 03 SOLv   SL=   10.0    0.844    0.074    0.131   16.5   27.6  182.7   15 

 03 SOLn   SL=   10.0    0.897    0.079    0.131   16.5   27.8  182.7   15 

 04 SLPv  76.0   22.9    0.085    0.003   ‐0.035    3.7   26.7  241.3   11 

 04 SLPn  76.0   23.0    0.121    0.003   ‐0.035    3.7   26.7  241.3   11 

 

 Pt  125    Line 22   v Da=   60.3 mm s=  4.0 mm (RKR ) Reducer r < 0.1D 

            Line 22   n Da=   88.9 mm s=  6.1 mm   A=   60.0 deg 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    6.3    0.121    0.002   ‐0.025    2.7    9.0  137.4    7 

 01 SL n  20.5    6.0    0.121    0.002   ‐0.025    0.8    6.8  137.4    5 

 02 SERv   SL=    9.0    0.982    0.007    0.052    4.5    5.5  335.1    2 

 02 SERn   SL=    6.8    0.982    0.007    0.052    1.5    2.0  337.3    1 

 03 SOLv   SL=    9.0    0.896    0.079    0.147   17.9   28.2  182.7   15 

 03 SOLn   SL=    6.8    0.896    0.079    0.147    5.5   12.9  182.7    7 

 04 SLPv  76.0   23.0    0.121    0.003   ‐0.025    2.7   25.7  241.3   11 

 04 SLPn  76.0   22.1    0.121    0.003   ‐0.025    0.8   22.9  241.3   10 

 

 Pt  123    Line 22   v Da=   88.9 mm s=  6.1 mm (VUU ) GirtButtWeldAsWeld 

            Line 22   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    6.0    0.122    0.003   ‐0.015    0.5    6.5  137.4    5 

 01 SL n  20.5   10.0    0.084    0.003   ‐0.015    0.7   10.7  137.4    8 

 02 SERv   SL=    6.5    0.982    0.007    0.064    1.8    2.3  337.6    1 

 02 SERn   SL=   10.7    1.011    0.006    0.064    2.3    3.0  333.4    1 

 03 SOLv   SL=    6.5    0.893    0.078    0.163    5.9   13.0  182.7    7 

 03 SOLn   SL=   10.7    0.826    0.073    0.163    8.5   19.9  182.7   11 

 04 SLPv  76.0   22.1    0.123    0.003   ‐0.015    0.5   22.6  241.3    9 

 04 SLPn  76.0   36.8    0.085    0.003   ‐0.015    0.7   37.6  241.3   16 

 

 Pt  111    Line 22   v Da=   88.9 mm s=  4.0 mm (BGL ) pipe bend 

            Line 22   m Da=   88.9 mm s=  4.0 mm   R=  114.3 mm 

            Line 22   n Da=   88.9 mm s=  4.0 mm  ii= 1.8  io= 1.5  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   10.0    0.084   ‐0.008    0.003    0.5   10.5  137.4    8 

Page 110: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

45/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 01 SL m  20.5   10.2    0.252   ‐0.027    0.003    1.6   11.8  137.4    9 

 01 SL n  20.5   10.2    0.285   ‐0.029    0.001    1.8   12.0  137.4    9 

 02 SERv   SL=   10.5    1.011    0.073    0.007    4.6    5.3  333.6    2 

 02 SERm   SL=   11.8    0.644    0.115    0.014    7.2    7.6  332.3    2 

 02 SERn   SL=   12.0    0.057   ‐0.207   ‐0.011   12.9   12.9  332.1    4 

 03 SOLv   SL=   10.5    0.821    0.208    0.073   13.4   24.6  182.7   13 

 03 SOLm   SL=   11.8    0.925    0.221    0.077   14.1   26.7  182.7   15 

 03 SOLn   SL=   12.0    0.493    0.171    0.036   11.1   23.5  182.7   13 

 04 SLPv  76.0   36.8    0.085   ‐0.008    0.003    0.5   37.4  241.3   15 

 04 SLPm  76.0   37.0    0.254   ‐0.027    0.003    1.6   38.7  241.3   16 

 04 SLPn  76.0   37.0    0.289   ‐0.029    0.001    1.8   38.8  241.3   16 

Page 111: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

46/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     25 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Pt  195    Line 22   v Da=   88.9 mm s=  4.0 mm (KUH ) Fillet weld conc. 

                                                 ii=  1.3 io=  1.3 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   10.2    0.285   ‐0.001   ‐0.029    1.4   11.5  137.4    8 

 02 SERv   SL=   11.5    0.057    0.011   ‐0.208    9.6    9.6  332.6    3 

 03 SOLv   SL=   11.5    0.493    0.036    0.171    8.7   20.7  182.7   11 

 04 SLPv  76.0   37.0    0.289   ‐0.001   ‐0.029    1.4   38.4  241.3   16 

 

 Pt  209    Line 23   n Da=   88.9 mm s=  4.0 mm (KUH ) Fillet weld conc. 

                                                 ii=  1.3 io=  1.3 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL n  20.5    9.9   ‐0.758   ‐0.063    0.025    3.2   13.1  137.4   10 

 02 SERn   SL=   13.1   ‐2.463    0.444   ‐0.139   21.5   23.2  331.0    7 

 03 SOLn   SL=   13.1    0.333    0.109    0.206   10.9   24.3  182.7   13 

 04 SLPn  76.0   36.8   ‐0.827   ‐0.064    0.026    3.2   40.0  241.3   17 

 

 Pt  235    Line 23   v Da=   88.9 mm s=  4.0 mm (BGL ) pipe bend 

            Line 23   m Da=   88.9 mm s=  4.0 mm   R=  114.3 mm 

            Line 23   n Da=   88.9 mm s=  4.0 mm  ii= 1.8  io= 1.5  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.221    0.046   ‐0.011    2.9   12.8  137.4    9 

 01 SL m  20.5    9.9   ‐0.197    0.044   ‐0.010    2.8   12.7  137.4    9 

 01 SL n  20.5    9.9   ‐0.144    0.039   ‐0.008    2.4   12.3  137.4    9 

 02 SERv   SL=   12.8   ‐2.463    1.446    0.145   90.4   92.1  331.3   28 

 02 SERm   SL=   12.7   ‐2.469    1.447    0.156   90.4   92.2  331.4   28 

 02 SERn   SL=   12.3   ‐2.099    1.404    0.144   87.8   89.2  331.8   27 

 03 SOLv   SL=   12.8    0.322    0.007    0.232   11.9   25.0  182.7   14 

 03 SOLm   SL=   12.7    0.346    0.009    0.226   11.9   24.9  182.7   14 

 03 SOLn   SL=   12.3    0.319    0.006    0.186   11.6   24.2  182.7   13 

 04 SLPv  76.0   36.8   ‐0.243    0.051   ‐0.011    3.2   39.9  241.3   17 

 04 SLPm  76.0   36.8   ‐0.217    0.049   ‐0.010    3.0   39.8  241.3   16 

 04 SLPn  76.0   36.8   ‐0.159    0.043   ‐0.008    2.7   39.4  241.3   16 

 

 Pt  71     Line 23   v Da=   88.9 mm s=  4.0 mm (BGL ) pipe bend 

            Line 23   m Da=   88.9 mm s=  4.0 mm   R=  114.3 mm 

            Line 23   n Da=   88.9 mm s=  4.0 mm  ii= 1.8  io= 1.5  it= 1.0 

 

Page 112: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

47/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.040    0.062    0.004    3.8   13.7  137.4   10 

 01 SL m  20.5    9.9   ‐0.049    0.063    0.006    3.9   13.8  137.4   10 

 01 SL n  20.5    9.9   ‐0.049    0.064    0.007    3.9   13.8  137.4   10 

 02 SERv   SL=   13.7   ‐2.099    0.009   ‐0.145    7.9    9.3  330.4    3 

 02 SERm   SL=   13.8   ‐2.469    0.051   ‐0.158    8.8   10.5  330.3    3 

 02 SERn   SL=   13.8   ‐2.463    0.050   ‐0.146    8.5   10.1  330.3    3 

 03 SOLv   SL=   13.7    0.356    0.116    0.175   13.2   27.2  182.7   15 

 03 SOLm   SL=   13.8    0.367    0.117    0.215   13.4   27.6  182.7   15 

 03 SOLn   SL=   13.8    0.321    0.112    0.222   13.3   27.4  182.7   15 

 04 SLPv  76.0   36.8   ‐0.047    0.068    0.004    4.1   40.9  241.3   17 

 04 SLPm  76.0   36.8   ‐0.057    0.069    0.006    4.3   41.0  241.3   17 

 04 SLPn  76.0   36.8   ‐0.056    0.070    0.008    4.3   41.1  241.3   17 

Page 113: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

48/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     26 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Pt  69     Line 23   v Da=   88.9 mm s=  4.0 mm (BGL ) pipe bend 

            Line 23   m Da=   88.9 mm s=  4.0 mm   R=  114.3 mm 

            Line 23   n Da=   88.9 mm s=  4.0 mm  ii= 1.8  io= 1.5  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   10.1    0.168   ‐0.071   ‐0.002    4.3   14.4  137.4   10 

 01 SL m  20.5   10.0    0.131   ‐0.065    0.001    4.0   14.0  137.4   10 

 01 SL n  20.5    9.9    0.005   ‐0.050    0.003    3.1   13.0  137.4    9 

 02 SERv   SL=   14.4   ‐2.463    0.713    0.149   45.1   46.8  329.7   14 

 02 SERm   SL=   14.0   ‐2.099    0.672    0.147   42.6   44.0  330.1   13 

 02 SERn   SL=   13.0   ‐0.506    0.490    0.060   31.1   31.4  331.1    9 

 03 SOLv   SL=   14.4    0.321    0.231    0.100   15.0   29.7  182.7   16 

 03 SOLm   SL=   14.0    0.418    0.241    0.075   15.4   29.9  182.7   16 

 03 SOLn   SL=   13.0    0.274    0.225    0.015   14.3   27.5  182.7   15 

 04 SLPv  76.0   36.9    0.180   ‐0.075   ‐0.002    4.6   41.5  241.3   17 

 04 SLPm  76.0   36.9    0.140   ‐0.069    0.001    4.2   41.1  241.3   17 

 04 SLPn  76.0   36.8    0.004   ‐0.053    0.003    3.3   40.0  241.3   17 

 

 Pt  185    Line 23   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 23   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9    0.005   ‐0.006    0.193    8.9   18.8  137.4   14 

 01 SL n  20.5    9.9    0.003   ‐0.006    0.193    8.9   18.8  137.4   14 

 02 SERv   SL=   18.8   ‐0.506   ‐0.061   ‐1.803   64.1   64.4  325.2   20 

 02 SERn   SL=   18.8   ‐0.896   ‐0.061   ‐1.803   64.1   64.7  325.3   20 

 03 SOLv   SL=   18.8    0.323    0.138    0.081    8.4   27.5  182.7   15 

 03 SOLn   SL=   18.8    0.276    0.138    0.081    8.4   27.5  182.7   15 

 04 SLPv  76.0   36.8    0.004   ‐0.007    0.208    9.6   46.4  241.3   19 

 04 SLPn  76.0   36.8    0.003   ‐0.007    0.208    9.6   46.4  241.3   19 

 

 Pt  217    Line 23   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 23   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9    0.003    0.003    0.131    6.1   16.0  137.4   12 

 01 SL n  20.5    9.9    0.003    0.003    0.131    6.1   16.0  137.4   12 

 02 SERv   SL=   16.0   ‐0.896    0.142    0.078    7.8    8.3  328.1    3 

 02 SERn   SL=   16.0   ‐0.352    0.142    0.078    7.8    8.0  328.1    2 

 03 SOLv   SL=   16.0    0.110    0.310    0.105   15.7   31.8  182.7   17 

Page 114: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

49/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 03 SOLn   SL=   16.0    0.110    0.310    0.105   15.7   31.8  182.7   17 

 04 SLPv  76.0   36.8    0.003    0.004    0.143    6.6   43.4  241.3   18 

 04 SLPn  76.0   36.8    0.003    0.004    0.143    6.6   43.4  241.3   18 

 

 Pt  67     Line 23   v Da=   88.9 mm s=  4.0 mm (BGL ) pipe bend 

            Line 23   m Da=   88.9 mm s=  4.0 mm   R=  114.3 mm 

            Line 23   n Da=   88.9 mm s=  4.0 mm  ii= 1.8  io= 1.5  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9    0.003    0.012   ‐0.003    0.7   10.7  137.4    8 

 01 SL m  20.5   10.1    0.142   ‐0.005   ‐0.001    0.3   10.3  137.4    8 

 01 SL n  20.5   10.1    0.185   ‐0.011    0.001    0.7   10.8  137.4    8 

Page 115: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

50/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     27 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 02 SERv   SL=   10.7   ‐0.352    0.266    0.375   26.1   26.3  333.4    8 

 02 SERm   SL=   10.3   ‐0.523    0.286    0.246   26.2   26.5  333.8    8 

 02 SERn   SL=   10.8   ‐0.387    0.270   ‐0.027   24.4   24.5  333.3    7 

 03 SOLv   SL=   10.7    0.093    0.072    0.080    7.2   17.9  182.7   10 

 03 SOLm   SL=   10.3    0.255    0.086    0.058    8.9   19.4  182.7   11 

 03 SOLn   SL=   10.8    0.282    0.086    0.004    9.4   20.3  182.7   11 

 04 SLPv  76.0   36.8    0.003    0.013   ‐0.003    0.8   37.6  241.3   16 

 04 SLPm  76.0   36.9    0.154   ‐0.005   ‐0.001    0.3   37.2  241.3   15 

 04 SLPn  76.0   37.0    0.201   ‐0.012    0.002    0.7   37.7  241.3   16 

 

 Pt  65     Line 23   v Da=   88.9 mm s=  4.0 mm (BGL ) pipe bend 

            Line 23   m Da=   88.9 mm s=  4.0 mm   R=  114.3 mm 

            Line 23   n Da=   88.9 mm s=  4.0 mm  ii= 1.8  io= 1.5  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   10.0    0.074    0.002    0.009    0.5   10.5  137.4    8 

 01 SL m  20.5   10.0    0.043    0.005    0.008    0.5   10.5  137.4    8 

 01 SL n  20.5    9.9   ‐0.001    0.009    0.002    0.7   10.5  137.4    8 

 02 SERv   SL=   10.5   ‐0.387    0.793    0.001   52.4   52.7  333.6   16 

 02 SERm   SL=   10.5   ‐1.026    0.866   ‐0.321   57.9   58.6  333.6   18 

 02 SERn   SL=   10.5   ‐1.063    0.870   ‐0.456   59.1   59.9  333.6   18 

 03 SOLv   SL=   10.5    0.282    0.583    0.033   36.5   47.2  182.7   26 

 03 SOLm   SL=   10.5    0.713    0.632    0.120   39.5   50.6  182.7   28 

 03 SOLn   SL=   10.5    0.723    0.634    0.159   39.6   50.7  182.7   28 

 04 SLPv  76.0   36.8    0.081    0.003    0.010    0.5   37.4  241.3   15 

 04 SLPm  76.0   36.8    0.046    0.005    0.009    0.6   37.4  241.3   15 

 04 SLPn  76.0   36.8   ‐0.001    0.010    0.003    0.8   37.4  241.3   15 

 

 Pt  179    Line 23   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 23   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.001   ‐0.004    0.375   17.4   27.3  137.4   20 

 01 SL n  20.5    9.9   ‐0.001   ‐0.004    0.375   17.4   27.3  137.4   20 

 02 SERv   SL=   27.3   ‐1.063    0.485    0.165   18.2   18.9  316.8    6 

 02 SERn   SL=   27.3   ‐0.736    0.485    0.165   18.2   18.7  316.8    6 

 03 SOLv   SL=   27.3    0.584    0.174    0.127   10.1   37.9  182.7   21 

 03 SOLn   SL=   27.3    0.584    0.174    0.127   10.1   37.9  182.7   21 

 04 SLPv  76.0   36.8   ‐0.001   ‐0.005    0.407   18.8   55.6  241.3   23 

Page 116: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

51/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 04 SLPn  76.0   36.8   ‐0.001   ‐0.005    0.407   18.8   55.6  241.3   23 

 

 Pt  177    Line 23   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 23   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.001    0.002    0.331   15.3   25.2  137.4   18 

 01 SL n  20.5    9.9   ‐0.001    0.002    0.331   15.3   25.2  137.4   18 

 02 SERv   SL=   25.2   ‐0.736   ‐0.138   ‐0.052    5.4    5.9  318.9    2 

 02 SERn   SL=   25.2   ‐0.501   ‐0.138   ‐0.052    5.4    5.8  318.9    2 

 03 SOLv   SL=   25.2    0.273    0.100    0.069    5.8   31.3  182.7   17 

 03 SOLn   SL=   25.2    0.273    0.100    0.069    5.8   31.3  182.7   17 

 04 SLPv  76.0   36.8   ‐0.001    0.002    0.359   16.6   53.4  241.3   22 

 04 SLPn  76.0   36.8   ‐0.001    0.002    0.359   16.6   53.4  241.3   22 

Page 117: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

THTF058

HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

PROJECT

CONTRACT Nº

THTF-2018-058

UNIT Nº

150

CONTRACTOR DOC No:

54TH58-SS-115-001

SH/OF

52/64

STAR DOCUMENT No.

150-L-ZE-0097001-015

REV 0

APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     28 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Pt  175    Line 23   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 23   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.001   ‐0.005    0.176    8.1   18.1  137.4   13 

 01 SL n  20.5    9.9   ‐0.001   ‐0.005    0.176    8.1   18.1  137.4   13 

 02 SERv   SL=   18.1   ‐0.501   ‐0.137   ‐0.016    5.1    5.4  326.0    2 

 02 SERn   SL=   18.1   ‐0.179   ‐0.137   ‐0.016    5.1    5.2  326.0    2 

 03 SOLv   SL=   18.1    0.118    0.151    0.109    8.7   26.9  182.7   15 

 03 SOLn   SL=   18.1    0.118    0.151    0.109    8.7   26.9  182.7   15 

 04 SLPv  76.0   36.8   ‐0.001   ‐0.005    0.191    8.8   45.6  241.3   19 

 04 SLPn  76.0   36.8   ‐0.001   ‐0.005    0.191    8.8   45.6  241.3   19 

 

 Pt  63     Line 23   v Da=   88.9 mm s=  4.0 mm (BGL ) pipe bend 

            Line 23   m Da=   88.9 mm s=  4.0 mm   R=  114.3 mm 

            Line 23   n Da=   88.9 mm s=  4.0 mm  ii= 1.8  io= 1.5  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.001    0.024   ‐0.005    1.5   11.4  137.4    8 

 01 SL m  20.5   10.2    0.263   ‐0.007   ‐0.012    0.8   10.9  137.4    8 

 01 SL n  20.5   10.3    0.360   ‐0.019   ‐0.012    1.4   11.6  137.4    8 

 02 SERv   SL=   11.4   ‐0.179    0.007    0.328   17.1   17.2  332.7    5 

 02 SERm   SL=   10.9   ‐0.172    0.006    0.244   16.1   16.2  333.2    5 

 02 SERn   SL=   11.6   ‐0.064   ‐0.006    0.018   13.7   13.8  332.5    4 

 03 SOLv   SL=   11.4    0.099    0.099    0.078    7.4   18.9  182.7   10 

 03 SOLm   SL=   10.9    0.090    0.095    0.054    7.1   18.1  182.7   10 

 03 SOLn   SL=   11.6    0.084    0.087    0.009    6.7   18.3  182.7   10 

 04 SLPv  76.0   36.8   ‐0.001    0.026   ‐0.006    1.7   38.4  241.3   16 

 04 SLPm  76.0   37.0    0.286   ‐0.007   ‐0.013    0.8   37.9  241.3   16 

 04 SLPn  76.0   37.1    0.391   ‐0.021   ‐0.013    1.5   38.6  241.3   16 

 

 Pt  61     Line 23   v Da=   88.9 mm s=  4.0 mm (BGL ) pipe bend 

            Line 23   m Da=   88.9 mm s=  4.0 mm   R=  114.3 mm 

            Line 23   n Da=   88.9 mm s=  4.0 mm  ii= 1.8  io= 1.5  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5   10.2    0.249   ‐0.033    0.020    2.3   12.4  137.4    9 

 01 SL m  20.5   10.1    0.187   ‐0.027    0.020    2.0   12.1  137.4    9 

 01 SL n  20.5    9.9    0.028   ‐0.010    0.009    1.2   10.7  137.4    8 

 02 SERv   SL=   12.4   ‐0.064    0.418    0.144   30.3   30.4  331.7    9 

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 02 SERm   SL=   12.1   ‐0.412    0.457   ‐0.158   32.6   32.8  332.0   10 

 02 SERn   SL=   10.7   ‐0.519    0.470   ‐0.367   35.4   35.7  333.4   11 

 03 SOLv   SL=   12.4    0.078    0.253    0.034   16.1   28.6  182.7   16 

 03 SOLm   SL=   12.1    0.258    0.275    0.042   17.4   29.6  182.7   16 

 03 SOLn   SL=   10.7    0.288    0.279    0.093   17.7   28.7  182.7   16 

 04 SLPv  76.0   37.0    0.271   ‐0.036    0.022    2.5   39.5  241.3   16 

 04 SLPm  76.0   37.0    0.203   ‐0.030    0.022    2.2   39.1  241.3   16 

 04 SLPn  76.0   36.8    0.030   ‐0.011    0.010    1.3   37.6  241.3   16 

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APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     29 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Pt  173    Line 23   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 23   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9    0.028    0.013    0.285   13.2   23.1  137.4   17 

 01 SL n  20.5    9.9    0.028    0.013    0.285   13.2   23.1  137.4   17 

 02 SERv   SL=   23.1   ‐0.519    0.357   ‐0.209   15.8   16.1  321.0    5 

 02 SERn   SL=   23.1   ‐0.354    0.357   ‐0.209   15.8   16.0  321.0    5 

 03 SOLv   SL=   23.1    0.078    0.201    0.056    9.7   33.0  182.7   18 

 03 SOLn   SL=   23.1    0.078    0.201    0.056    9.7   33.0  182.7   18 

 04 SLPv  76.0   36.8    0.030    0.014    0.309   14.4   51.1  241.3   21 

 04 SLPn  76.0   36.8    0.030    0.014    0.309   14.4   51.1  241.3   21 

 

 Pt  59     Line 23   v Da=   88.9 mm s=  4.0 mm (BGL ) pipe bend 

            Line 23   m Da=   88.9 mm s=  4.0 mm   R=  114.3 mm 

            Line 23   n Da=   88.9 mm s=  4.0 mm  ii= 1.8  io= 1.5  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9    0.028   ‐0.038    0.002    2.5   12.3  137.4    9 

 01 SL m  20.5   10.1    0.209   ‐0.059   ‐0.012    3.8   13.8  137.4   10 

 01 SL n  20.5   10.2    0.255   ‐0.066   ‐0.018    4.1   14.3  137.4   10 

 02 SERv   SL=   12.3   ‐0.354    0.652   ‐0.013   41.0   41.3  331.8   12 

 02 SERm   SL=   13.8   ‐0.906    0.715   ‐0.095   45.0   45.6  330.3   14 

 02 SERn   SL=   14.3   ‐0.927    0.717   ‐0.122   45.1   45.8  329.8   14 

 03 SOLv   SL=   12.3    0.031    0.091    0.089    7.3   19.6  182.7   11 

 03 SOLm   SL=   13.8    0.082    0.101    0.061    7.5   21.4  182.7   12 

 03 SOLn   SL=   14.3    0.128    0.107    0.018    7.6   22.0  182.7   12 

 04 SLPv  76.0   36.8    0.030   ‐0.042    0.002    2.8   39.4  241.3   16 

 04 SLPm  76.0   37.0    0.227   ‐0.065   ‐0.013    4.1   41.0  241.3   17 

 04 SLPn  76.0   37.0    0.277   ‐0.072   ‐0.020    4.5   41.6  241.3   17 

 

 Pt  57     Line 23   v Da=   88.9 mm s=  4.0 mm (BGL ) pipe bend 

            Line 23   m Da=   88.9 mm s=  4.0 mm   R=  114.3 mm 

            Line 23   n Da=   88.9 mm s=  4.0 mm  ii= 1.8  io= 1.5  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.131    0.023   ‐0.008    1.5   11.4  137.4    8 

 01 SL m  20.5    9.9   ‐0.113    0.020   ‐0.010    1.3   11.2  137.4    8 

 01 SL n  20.5    9.9   ‐0.016    0.008   ‐0.006    0.8   10.5  137.4    8 

 02 SERv   SL=   11.4   ‐0.927    0.874    0.233   55.7   56.4  332.7   17 

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APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 02 SERm   SL=   11.2   ‐0.917    0.873    0.173   55.5   56.1  332.9   17 

 02 SERn   SL=   10.5   ‐0.371    0.810    0.011   51.4   51.6  333.6   15 

 03 SOLv   SL=   11.4    0.126    0.113    0.030    8.0   19.5  182.7   11 

 03 SOLm   SL=   11.2    0.086    0.108    0.088    8.1   19.4  182.7   11 

 03 SOLn   SL=   10.5    0.036    0.099    0.095    8.0   18.6  182.7   10 

 04 SLPv  76.0   36.8   ‐0.142    0.026   ‐0.009    1.6   38.4  241.3   16 

 04 SLPm  76.0   36.8   ‐0.122    0.022   ‐0.011    1.5   38.2  241.3   16 

 04 SLPn  76.0   36.8   ‐0.017    0.009   ‐0.007    0.9   37.4  241.3   16 

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APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     30 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Pt  207    Line 23   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 23   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.016   ‐0.025    0.130    6.2   16.1  137.4   12 

 01 SL n  20.5    9.9   ‐0.016   ‐0.025    0.130    6.2   16.1  137.4   12 

 02 SERv   SL=   16.1   ‐0.371    0.250   ‐0.185   14.7   14.9  328.0    5 

 02 SERn   SL=   16.1   ‐0.684    0.250   ‐0.185   14.7   15.0  328.0    5 

 03 SOLv   SL=   16.1    0.070    0.192    0.068    9.7   25.8  182.7   14 

 03 SOLn   SL=   16.1    0.070    0.192    0.068    9.7   25.8  182.7   14 

 04 SLPv  76.0   36.8   ‐0.017   ‐0.027    0.141    6.7   43.4  241.3   18 

 04 SLPn  76.0   36.8   ‐0.017   ‐0.027    0.141    6.7   43.4  241.3   18 

 

 Pt  55     Line 23   v Da=   88.9 mm s=  4.0 mm (BGL ) pipe bend 

            Line 23   m Da=   88.9 mm s=  4.0 mm   R=  114.3 mm 

            Line 23   n Da=   88.9 mm s=  4.0 mm  ii= 1.8  io= 1.5  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.016   ‐0.004   ‐0.001    0.6   10.2  137.4    7 

 01 SL m  20.5    9.9   ‐0.025   ‐0.003    0.005    0.5   10.2  137.4    7 

 01 SL n  20.5    9.9   ‐0.020   ‐0.003    0.008    0.5   10.4  137.4    8 

 02 SERv   SL=   10.2   ‐0.684    0.429    0.360   34.0   34.5  333.9   10 

 02 SERm   SL=   10.2   ‐0.600    0.420    0.101   31.3   31.7  333.9    9 

 02 SERn   SL=   10.4   ‐0.165    0.370   ‐0.217   29.6   29.7  333.7    9 

 03 SOLv   SL=   10.2    0.126    0.165    0.110   11.7   22.0  182.7   12 

 03 SOLm   SL=   10.2    0.243    0.189    0.058   12.9   23.3  182.7   13 

 03 SOLn   SL=   10.4    0.293    0.197    0.039   13.3   24.0  182.7   13 

 04 SLPv  76.0   36.8   ‐0.017   ‐0.004   ‐0.001    0.6   37.0  241.3   15 

 04 SLPm  76.0   36.8   ‐0.027   ‐0.003    0.005    0.6   37.1  241.3   15 

 04 SLPn  76.0   36.8   ‐0.022   ‐0.003    0.009    0.6   37.3  241.3   15 

 

 Pt  53     Line 23   v Da=   88.9 mm s=  4.0 mm (BGL ) pipe bend 

            Line 23   m Da=   88.9 mm s=  4.0 mm   R=  114.3 mm 

            Line 23   n Da=   88.9 mm s=  4.0 mm  ii= 1.8  io= 1.5  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.020    0.021    0.012    1.4   11.3  137.4    8 

 01 SL m  20.5    9.9   ‐0.068    0.026    0.013    1.7   11.6  137.4    8 

 01 SL n  20.5    9.9   ‐0.089    0.027    0.006    1.8   11.6  137.4    8 

 02 SERv   SL=   11.3   ‐0.165    0.065    0.013   15.3   15.4  332.7    5 

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HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

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APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 02 SERm   SL=   11.6   ‐0.472    0.100   ‐0.231   17.8   18.0  332.4    5 

 02 SERn   SL=   11.6   ‐0.502    0.103   ‐0.339   19.0   19.3  332.5    6 

 03 SOLv   SL=   11.3    0.265    0.015    0.207   11.9   23.4  182.7   13 

 03 SOLm   SL=   11.6    0.155    0.006    0.073   11.2   22.9  182.7   13 

 03 SOLn   SL=   11.6    0.048    0.021    0.106   11.3   23.0  182.7   13 

 04 SLPv  76.0   36.8   ‐0.022    0.023    0.013    1.6   38.3  241.3   16 

 04 SLPm  76.0   36.8   ‐0.074    0.029    0.014    1.9   38.7  241.3   16 

 04 SLPn  76.0   36.8   ‐0.097    0.030    0.007    2.0   38.6  241.3   16 

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APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     31 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Pt  95     Line 23   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 23   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.129   ‐0.022   ‐0.010    1.3   11.1  137.4    8 

 01 SL n  20.5    9.9   ‐0.129   ‐0.022   ‐0.010    1.3   11.1  137.4    8 

 02 SERv   SL=   11.1   ‐0.502   ‐0.058    0.153    6.6    6.9  333.0    2 

 02 SERn   SL=   11.1   ‐0.502   ‐0.058    0.153    6.6    6.9  333.0    2 

 03 SOLv   SL=   11.1    0.049    0.088    0.096   11.6   22.7  182.7   12 

 03 SOLn   SL=   11.1    0.049    0.088    0.096   11.6   22.7  182.7   12 

 04 SLPv  76.0   36.8   ‐0.140   ‐0.024   ‐0.012    1.4   38.0  241.3   16 

 04 SLPn  76.0   36.8   ‐0.140   ‐0.024   ‐0.012    1.4   38.0  241.3   16 

 

 Pt  51     Line 23   v Da=   88.9 mm s=  4.0 mm (TFS ) Butt welding tee 

            Line 23   n Da=   88.9 mm s=  4.0 mm  ii= 1.5  io= 1.6  it= 1.0 

            Line 8    v Da=   88.9 mm s=  4.0 mm 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.146   ‐0.012    0.020    1.4   11.2  137.4    8 

 01 SL n  20.5    9.9   ‐0.376   ‐0.045    0.019    2.6   12.5  137.4    9 

 01 SL v  20.5    9.9   ‐0.100   ‐0.034   ‐0.010    1.7   11.7  137.4    8 

 02 SERv   SL=   11.2    0.453    0.117    0.051    6.9    7.2  332.9    2 

 02 SERn   SL=   12.5    1.193    0.104    0.041    5.9    6.8  331.6    2 

 02 SERv   SL=   11.7    0.247    0.220    0.044   11.1   11.3  332.4    3 

 03 SOLv   SL=   11.2    0.050    0.098    0.108   12.7   24.0  182.7   13 

 03 SOLn   SL=   12.5    0.558    0.355    0.133   20.0   33.0  182.7   18 

 03 SOLv   SL=   11.7    0.328    0.391    0.145   20.8   32.8  182.7   18 

 04 SLPv  76.0   36.8   ‐0.159   ‐0.013    0.022    1.6   38.2  241.3   16 

 04 SLPn  76.0   36.8   ‐0.392   ‐0.046    0.020    2.6   39.4  241.3   16 

 04 SLPv  76.0   36.8   ‐0.102   ‐0.033   ‐0.011    1.7   38.5  241.3   16 

 

 Pt  93     Line 23   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

            Line 23   n Da=   88.9 mm s=  4.0 mm  ii= 1.0  io= 1.0  it= 1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.394   ‐0.018   ‐0.038    1.9   11.9  137.4    9 

 01 SL n  20.5    9.9   ‐0.394   ‐0.018   ‐0.038    1.9   11.9  137.4    9 

 02 SERv   SL=   11.9    1.193    0.039    0.126    4.7    5.5  332.2    2 

 02 SERn   SL=   11.9    1.193    0.039    0.126    4.7    5.5  332.2    2 

 03 SOLv   SL=   11.9    0.558    0.143    0.310   16.1   28.5  182.7   16 

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 03 SOLn   SL=   11.9    0.558    0.143    0.310   16.1   28.5  182.7   16 

 04 SLPv  76.0   36.8   ‐0.411   ‐0.019   ‐0.038    2.0   38.8  241.3   16 

 04 SLPn  76.0   36.8   ‐0.411   ‐0.019   ‐0.038    2.0   38.8  241.3   16 

 

 Pt  201    Line 23   v Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐0.521   ‐0.012   ‐0.003    0.6   10.5  137.4    8 

 02 SERv   SL=   10.5   ‐1.235   ‐0.025   ‐0.269    9.6   10.4  333.6    3 

 03 SOLv   SL=   10.5    0.559    0.183    0.084    9.9   20.9  182.7   11 

 04 SLPv  76.0   36.8   ‐0.543   ‐0.013   ‐0.003    0.7   37.4  241.3   16 

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APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     32 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

 Pt  199    Line 23   n Da=   88.9 mm s=  4.0 mm (VUU ) GirtButtWeldAsWeld 

                                                 ii=  1.0 io=  1.0 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL n  20.5    9.9   ‐1.021   ‐0.009    0.021    1.1   11.0  137.4    8 

 02 SERn   SL=   11.0   ‐1.235   ‐0.017   ‐0.373   13.2   14.1  333.1    4 

 03 SOLn   SL=   11.0    0.569    0.176    0.105   10.0   21.5  182.7   12 

 04 SLPn  76.0   36.8   ‐1.046   ‐0.010    0.021    1.1   37.8  241.3   16 

 

 Pt  195    Line 23   v Da=   88.9 mm s=  4.0 mm (KUH ) Fillet weld conc. 

                                                 ii=  1.3 io=  1.3 it=  1.0 

 

 Na  Gl      P     Sa    Qx,Mt       Mi       Mo   S(M)  S‐sum S‐allw Util 

         (bar)(N/mm2) (kN,kNm)    (kNm)    (kNm)(N/mm2)(N/mm2)(N/mm2)  (%) 

 01 SL v  20.5    9.9   ‐1.102   ‐0.008    0.029    1.4   11.3  137.4    8 

 02 SERv   SL=   11.3   ‐1.235   ‐0.014   ‐0.410   18.9   19.7  332.8    6 

 03 SOLv   SL=   11.3    0.571    0.164    0.181   11.8   23.6  182.7   13 

 04 SLPv  76.0   36.8   ‐1.129   ‐0.008    0.029    1.4   38.2  241.3   16 

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APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     33 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

   EXTRACT OF STRESS ANALYSIS ACC. TO ASME   B31.3: 

 

    Analysis 01  Stresses due to sustained loads    (SL) 

                   Fa,MiL,MoL,MtL         from load case  Dead load 

 

               Components with maximum stress percentages 

 

                                         Sum of   Allowable 

         Pt                             stresses  stresses 

                        ii    io         (N/mm2)   (N/mm2)       (%) 

 

       5    (TTU )    3.17  3.89            37.2     137.4      27.1 

       79   (TTU )    3.66  4.54            35.1     137.4      25.5 

       149  (VUU )    1.00  1.00            28.9     137.4      21.1 

       145  (VUU )    1.00  1.00            28.7     137.4      20.9 

       147  (RKR )    1.00  1.00            28.3     137.4      20.6 

       179  (VUU )    1.00  1.00            27.3     137.4      19.8 

       225  (VUU )    1.00  1.00            26.4     137.4      19.2 

       223  (VUU )    1.00  1.00            26.4     137.4      19.2 

       151  (VUU )    1.00  1.00            26.0     137.4      19.0 

       177  (VUU )    1.00  1.00            25.2     137.4      18.4 

       153  (VUU )    1.00  1.00            24.1     137.4      17.6 

       75   (BGL )    1.76  1.47            24.1     137.4      17.5 

       173  (VUU )    1.00  1.00            23.1     137.4      16.8 

       213  (KUH )    1.30  1.30            23.1     137.4      16.8 

       163  (KUH )    1.30  1.30            23.0     137.4      16.8 

       157  (RKR )    1.00  1.00            22.7     137.4      16.5 

       227  (VUU )    1.00  1.00            22.1     137.4      16.1 

       209  (KUH )    1.30  1.30            21.2     137.4      15.4 

       139  (VUU )    1.00  1.00            20.9     137.4      15.2 

       233  (VUU )    1.00  1.00            20.0     137.4      14.6 

       185  (VUU )    1.00  1.00            18.8     137.4      13.7 

       175  (VUU )    1.00  1.00            18.1     137.4      13.1 

       83   (BGL )    2.20  1.84            17.8     137.4      13.0 

       155  (VUU )    1.00  1.00            17.4     137.4      12.6 

       113  (VUU )    1.00  1.00            16.3     137.4      11.8 

       99   (VUU )    1.00  1.00            16.3     137.4      11.8 

       207  (VUU )    1.00  1.00            16.1     137.4      11.7 

       217  (VUU )    1.00  1.00            16.0     137.4      11.6 

       77   (BGL )    1.76  1.47            15.9     137.4      11.6 

       7    (BGL )    1.92  1.60            15.2     137.4      11.0 

 

               0 Sections with stress(es) exceeded                      (*) 

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 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     34 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

   EXTRACT OF STRESS ANALYSIS ACC. TO ASME   B31.3: 

 

    Analysis 02  Stresses due to sust. and expansion loads 

                   Fa,MiL,MoL,MtL         from load case  Dead load 

                   Fa,MiE,MoE,MtE = RANGE from load case    Temp. loads 

 

               Components with maximum stress percentages 

 

                                         Sum of   Allowable 

         Pt                             stresses  stresses 

                        ii    io         (N/mm2)   (N/mm2)       (%) 

 

       235  (BGL )    1.76  1.47            92.2     331.4      27.8 

       213  (KUH )    1.30  1.30            74.5     321.0      23.2 

       79   (TTU )    3.66  4.54            70.9     309.0      22.9 

       35   (BGL )    1.76  1.47            66.5     332.4      20.0 

       185  (VUU )    1.00  1.00            64.7     325.3      19.9 

       41   (BGL )    1.76  1.47            64.7     333.4      19.4 

       75   (BGL )    1.76  1.47            57.9     320.0      18.1 

       65   (BGL )    1.76  1.47            59.9     333.6      18.0 

       57   (BGL )    1.76  1.47            56.4     332.7      16.9 

       43   (BGL )    1.76  1.47            54.6     332.2      16.4 

       209  (KUH )    1.30  1.30            48.2     322.9      14.9 

       69   (BGL )    1.76  1.47            46.8     329.7      14.2 

       59   (BGL )    1.76  1.47            45.8     329.8      13.9 

       77   (BGL )    1.76  1.47            43.3     328.5      13.2 

       45   (TFS )    1.48  1.64            42.7     332.9      12.8 

       39   (BGL )    1.76  1.47            42.6     333.7      12.8 

       37   (BGL )    1.76  1.47            42.3     333.9      12.7 

       223  (VUU )    1.00  1.00            35.9     317.7      11.3 

       5    (TTU )    3.17  3.89            37.1     330.5      11.2 

       61   (BGL )    1.76  1.47            35.7     333.4      10.7 

       225  (VUU )    1.00  1.00            33.4     317.7      10.5 

       55   (BGL )    1.76  1.47            34.5     333.9      10.3 

       229  (VUU )    1.00  1.00            32.8     333.1       9.8 

       233  (VUU )    1.00  1.00            30.4     324.1       9.4 

       195  (KUH )    1.30  1.30            29.4     333.9       8.8 

       187  (KUH )    1.30  1.30            28.4     333.2       8.5 

       87   (VUU )    1.00  1.00            27.2     333.1       8.2 

       169  (VUU )    1.00  1.00            26.8     333.0       8.0 

       67   (BGL )    1.76  1.47            26.5     333.8       7.9 

       83   (BGL )    2.20  1.84            25.1     326.3       7.7 

               0 Sections with stress(es) exceeded                      (*) 

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APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     35 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

   EXTRACT OF STRESS ANALYSIS ACC. TO ASME   B31.3: 

 

    Analysis 03  Stresses due to sustained + occasional loads (SOL) 

                   Fa,MiL,MoL,MtL         from load case  Dead load 

                   Fa,MiO,MoO,MtO  from load case Earthquake‐XYZ 

 

               Components with maximum stress percentages 

 

                                         Sum of   Allowable 

         Pt                             stresses  stresses 

                        ii    io         (N/mm2)   (N/mm2)       (%) 

 

       79   (TTU )    3.66  4.54            69.4     182.7      38.0 

       187  (KUH )    1.30  1.30            55.5     182.7      30.4 

       5    (TTU )    3.17  3.89            52.2     182.7      28.6 

       65   (BGL )    1.76  1.47            50.7     182.7      27.8 

       213  (KUH )    1.30  1.30            49.8     182.7      27.3 

       45   (TFS )    1.48  1.64            49.6     182.7      27.1 

       75   (BGL )    1.76  1.47            46.7     182.7      25.6 

       89   (VUU )    1.00  1.00            43.5     182.7      23.8 

       225  (VUU )    1.00  1.00            41.9     182.7      22.9 

       193  (VUU )    1.00  1.00            40.8     182.7      22.3 

       47   (BGL )    1.76  1.47            39.2     182.7      21.4 

       115  (RKR )    1.00  1.00            38.6     182.7      21.1 

       209  (KUH )    1.30  1.30            38.6     182.7      21.1 

       191  (VUU )    1.00  1.00            38.0     182.7      20.8 

       179  (VUU )    1.00  1.00            37.9     182.7      20.7 

       149  (VUU )    1.00  1.00            36.8     182.7      20.1 

       145  (VUU )    1.00  1.00            36.4     182.7      19.9 

       87   (VUU )    1.00  1.00            36.2     182.7      19.8 

       147  (RKR )    1.00  1.00            35.9     182.7      19.7 

       113  (VUU )    1.00  1.00            35.7     182.7      19.5 

       223  (VUU )    1.00  1.00            35.3     182.7      19.3 

       163  (KUH )    1.30  1.30            34.7     182.7      19.0 

       151  (VUU )    1.00  1.00            33.5     182.7      18.3 

       173  (VUU )    1.00  1.00            33.0     182.7      18.0 

       51   (TFS )    1.48  1.64            33.0     182.7      18.0 

       217  (VUU )    1.00  1.00            31.8     182.7      17.4 

       153  (VUU )    1.00  1.00            31.3     182.7      17.1 

       177  (VUU )    1.00  1.00            31.3     182.7      17.1 

       69   (BGL )    1.76  1.47            29.9     182.7      16.3 

       157  (RKR )    1.00  1.00            29.7     182.7      16.2 

               0 Sections with stress(es) exceeded                      (*) 

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HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

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CONTRACT Nº

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UNIT Nº

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CONTRACTOR DOC No:

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STAR DOCUMENT No.

150-L-ZE-0097001-015

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APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION

 S T R E S S E S     ‐‐   Program  ROHR2       CIMT/32.1   ‐‐   Page     36 

 Commiss.   THTF058                             Date  06/12/20  11:29:15 

 

 

   EXTRACT OF STRESS ANALYSIS ACC. TO ASME   B31.3: 

 

    Analysis 04  Primary  stresses, pressure testing (SLP) 

                   Fa,MiL,MoL,MtL         from load case  Pressure test 

 

               Components with maximum stress percentages 

 

                                         Sum of   Allowable 

         Pt                             stresses  stresses 

                        ii    io         (N/mm2)   (N/mm2)       (%) 

 

       5    (TTU )    3.17  3.89            69.1     241.3      28.6 

       79   (TTU )    3.66  4.54            62.7     241.3      26.0 

       149  (VUU )    1.00  1.00            56.3     241.3      23.3 

       145  (VUU )    1.00  1.00            56.1     241.3      23.2 

       147  (RKR )    1.00  1.00            55.7     241.3      23.1 

       179  (VUU )    1.00  1.00            55.6     241.3      23.0 

       83   (BGL )    2.20  1.84            55.4     241.3      23.0 

       223  (VUU )    1.00  1.00            54.7     241.3      22.7 

       225  (VUU )    1.00  1.00            54.6     241.3      22.6 

       213  (KUH )    1.30  1.30            54.2     241.3      22.4 

       177  (VUU )    1.00  1.00            53.4     241.3      22.1 

       151  (VUU )    1.00  1.00            53.3     241.3      22.1 

       139  (VUU )    1.00  1.00            52.2     241.3      21.6 

       153  (VUU )    1.00  1.00            51.3     241.3      21.3 

       85   (VUU )    1.00  1.00            51.3     241.3      21.3 

       81   (VUU )    1.00  1.00            51.3     241.3      21.3 

       75   (BGL )    1.76  1.47            51.3     241.3      21.3 

       173  (VUU )    1.00  1.00            51.1     241.3      21.2 

       227  (VUU )    1.00  1.00            50.0     241.3      20.7 

       157  (RKR )    1.00  1.00            49.8     241.3      20.7 

       163  (KUH )    1.30  1.30            49.4     241.3      20.5 

       155  (VUU )    1.00  1.00            48.5     241.3      20.1 

       209  (KUH )    1.30  1.30            48.3     241.3      20.0 

       113  (VUU )    1.00  1.00            46.8     241.3      19.4 

       233  (VUU )    1.00  1.00            46.7     241.3      19.4 

       185  (VUU )    1.00  1.00            46.4     241.3      19.2 

       7    (BGL )    1.92  1.60            46.3     241.3      19.2 

       175  (VUU )    1.00  1.00            45.6     241.3      18.9 

       115  (RKR )    1.00  1.00            45.6     241.3      18.9 

       99   (VUU )    1.00  1.00            43.8     241.3      18.1 

 

               0 Sections with stress(es) exceeded                      (*)

Page 130: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

APPENDIX B

APPENDIX B of Doc. 150-L-ZE-0097001-015

1 of 19

Page 131: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

Dimensions - THTF058

Overview Pipes and Elbows/BendsInternal pressure analysis acc. to ASME B31.3-2016

Analysis for Pipes and Bends/Elbows Design Test

Nominaldiameter

Material Out. dia. Wall-thk. C1 C2 V P T Util. P T Util.

mm mm mm mm bar (g) °C % bar (g) °C %

NPS2.0 P SA106B 60.33 5.54 12.50% 1.50 1.00 20.50 190.00 12.86 76.00 20.00 27.14

NPS2.0 B SA106B 60.33 5.54 12.50% 1.50 1.00 20.50 190.00 17.07 76.00 20.00 36.03

NPS3.0 P SA106B 88.90 5.49 12.50% 1.50 1.00 20.50 190.00 19.50 76.00 20.00 41.15

NPS3.0 B SA106B 88.90 5.49 12.50% 1.50 1.00 20.50 190.00 25.70 76.00 20.00 54.25

NPS4.0 P SA106B 114.30 6.02 12.50% 1.50 1.00 20.50 190.00 22.04 76.00 20.00 46.52

NPS4.0 B SA106B 114.30 6.02 12.50% 1.50 1.00 20.50 190.00 28.65 76.00 20.00 60.47

NPS6.0 P SA106B 168.28 7.11 12.50% 1.50 1.00 20.50 190.00 25.99 76.00 20.00 54.84

NPS6.0 B SA106B 168.28 7.11 12.50% 1.50 1.00 20.50 190.00 33.55 76.00 20.00 70.82

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APPENDIX B of Doc. 150-L-ZE-0097001-015

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Page 132: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

Dimensions - THTF058

Internal pressure analysis acc. to ASME B31.3-2016

Input dataNom. diameter: NPS2.0

Pipe ASME B36.10M:2004 60.33 x 5.54

NPS2.0

Material: SA106B

Design pressure/temperature: 20.50 bar (g) / 190.00 °C

Test pressure/temperature: 76.00 bar (g) / 20.00 °C

Analysis straight pipeDimensions

Outer diameter: 60.33 mm

Wall thickness: 5.54 mm

Add. thickness c1: 12.50% (Rel. minus tolerance (%))

Add. thickness c2: 1.50 mm

Welding factors E x W: 1.00

Coefficient Y: 0.40

Range of validity

t < D / 6 10.054 met

P / S*E <= 0.385 0.015 met

Allowable stresses Design cond. Test cond.

Allowable stresses: 137.38 N/mm² 241.32 N/mm²

Results Design cond. Test cond.

Required wall thickness: 0.45 mm 0.94 mm

Calculated stress: 17.67 N/mm² 65.49 N/mm²

Stress utilization: 12.86 % 27.14 %

Analysis Elbow/BendDimensions

Outer diameter: 60.33 mm

Thickness of connection: 5.54 mm

Add. thickness c1: 12.50% (Rel. minus tolerance (%))

Inner wall thickn.: 5.54 mm

Add. thickness c1: 12.50% (Rel. minus tolerance (%))

Outer wall thickn.: 5.54 mm

Add. thickness c1: 12.50% (Rel. minus tolerance (%))

Add. thickness c2: 1.50 mm

Bend radius 76.20 mm

Welding factors E x W: 1.00

Coefficient Y: 0.40

Allowable stresses bend Design cond. Test cond.

Allowable stresses: 137.38 N/mm² 241.32 N/mm²

Results Design cond. Test cond.

Required wall thickness: inside 0.59 mm 1.24 mm

Calculated stress inside: 23.45 N/mm² 86.94 N/mm²

Required wall thickness: outside 0.38 mm 0.81 mm

Calculated stress outside: 15.16 N/mm² 56.20 N/mm²

Max. stress util.: 17.07 % 36.03 %

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APPENDIX B of Doc. 150-L-ZE-0097001-015

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Page 133: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

Dimensions - THTF058

Internal pressure analysis acc. to ASME B31.3-2016 NPS2.0 Pipe ASME B36.10M:2004 60.33 x 5.54

NPS2.0

Results Pipe

Description Temperature Pressure Allowable stresses Calculated stress: Utilization:

Design 190.00 °C 20.50 bar (g) 137.38 N/mm² 17.67 N/mm² 12.86 %

Pressure test 20.00 °C 76.00 bar (g) 241.32 N/mm² 65.49 N/mm² 27.14 %

Results Elbow/Bend

Design 190.00 °C 20.50 bar (g) 137.38 N/mm² 23.45 N/mm² 17.07 %

Pressure test 20.00 °C 76.00 bar (g) 241.32 N/mm² 86.94 N/mm² 36.03 %

3

APPENDIX B of Doc. 150-L-ZE-0097001-015

4 of 19

Page 134: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

Dimensions - THTF058

Internal pressure analysis acc. to ASME B31.3-2016

Input dataNom. diameter: NPS3.0

Pipe ASME B36.10M:2004 88.90 x 5.49

NPS3.0

Material: SA106B

Design pressure/temperature: 20.50 bar (g) / 190.00 °C

Test pressure/temperature: 76.00 bar (g) / 20.00 °C

Analysis straight pipeDimensions

Outer diameter: 88.90 mm

Wall thickness: 5.49 mm

Add. thickness c1: 12.50% (Rel. minus tolerance (%))

Add. thickness c2: 1.50 mm

Welding factors E x W: 1.00

Coefficient Y: 0.40

Range of validity

t < D / 6 14.817 met

P / S*E <= 0.385 0.015 met

Allowable stresses Design cond. Test cond.

Allowable stresses: 137.38 N/mm² 241.32 N/mm²

Results Design cond. Test cond.

Required wall thickness: 0.66 mm 1.38 mm

Calculated stress: 26.79 N/mm² 99.31 N/mm²

Stress utilization: 19.50 % 41.15 %

Analysis Elbow/BendDimensions

Outer diameter: 88.90 mm

Thickness of connection: 5.49 mm

Add. thickness c1: 12.50% (Rel. minus tolerance (%))

Inner wall thickn.: 5.49 mm

Add. thickness c1: 12.50% (Rel. minus tolerance (%))

Outer wall thickn.: 5.49 mm

Add. thickness c1: 12.50% (Rel. minus tolerance (%))

Add. thickness c2: 1.50 mm

Bend radius 114.30 mm

Welding factors E x W: 1.00

Coefficient Y: 0.40

Allowable stresses bend Design cond. Test cond.

Allowable stresses: 137.38 N/mm² 241.32 N/mm²

Results Design cond. Test cond.

Required wall thickness: inside 0.87 mm 1.82 mm

Calculated stress inside: 35.31 N/mm² 130.91 N/mm²

Required wall thickness: outside 0.57 mm 1.19 mm

Calculated stress outside: 23.04 N/mm² 85.41 N/mm²

Max. stress util.: 25.70 % 54.25 %

4

APPENDIX B of Doc. 150-L-ZE-0097001-015

5 of 19

Page 135: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

Dimensions - THTF058

Internal pressure analysis acc. to ASME B31.3-2016 NPS3.0 Pipe ASME B36.10M:2004 88.90 x 5.49

NPS3.0

Results Pipe

Description Temperature Pressure Allowable stresses Calculated stress: Utilization:

Design 190.00 °C 20.50 bar (g) 137.38 N/mm² 26.79 N/mm² 19.50 %

Pressure test 20.00 °C 76.00 bar (g) 241.32 N/mm² 99.31 N/mm² 41.15 %

Results Elbow/Bend

Design 190.00 °C 20.50 bar (g) 137.38 N/mm² 35.31 N/mm² 25.70 %

Pressure test 20.00 °C 76.00 bar (g) 241.32 N/mm² 130.91 N/mm² 54.25 %

5

APPENDIX B of Doc. 150-L-ZE-0097001-015

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Page 136: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

Dimensions - THTF058

Internal pressure analysis acc. to ASME B31.3-2016

Input dataNom. diameter: NPS4.0

Pipe ASME B36.10M:2004 114.30 x 6.02

NPS4.0

Material: SA106B

Design pressure/temperature: 20.50 bar (g) / 190.00 °C

Test pressure/temperature: 76.00 bar (g) / 20.00 °C

Analysis straight pipeDimensions

Outer diameter: 114.30 mm

Wall thickness: 6.02 mm

Add. thickness c1: 12.50% (Rel. minus tolerance (%))

Add. thickness c2: 1.50 mm

Welding factors E x W: 1.00

Coefficient Y: 0.40

Range of validity

t < D / 6 19.050 met

P / S*E <= 0.385 0.015 met

Allowable stresses Design cond. Test cond.

Allowable stresses: 137.38 N/mm² 241.32 N/mm²

Results Design cond. Test cond.

Required wall thickness: 0.85 mm 1.78 mm

Calculated stress: 30.28 N/mm² 112.25 N/mm²

Stress utilization: 22.04 % 46.52 %

Analysis Elbow/BendDimensions

Outer diameter: 114.30 mm

Thickness of connection: 6.02 mm

Add. thickness c1: 12.50% (Rel. minus tolerance (%))

Inner wall thickn.: 6.02 mm

Add. thickness c1: 12.50% (Rel. minus tolerance (%))

Outer wall thickn.: 6.02 mm

Add. thickness c1: 12.50% (Rel. minus tolerance (%))

Add. thickness c2: 1.50 mm

Bend radius 152.40 mm

Welding factors E x W: 1.00

Coefficient Y: 0.40

Allowable stresses bend Design cond. Test cond.

Allowable stresses: 137.38 N/mm² 241.32 N/mm²

Results Design cond. Test cond.

Required wall thickness: inside 1.10 mm 2.30 mm

Calculated stress inside: 39.36 N/mm² 145.93 N/mm²

Required wall thickness: outside 0.73 mm 1.54 mm

Calculated stress outside: 26.15 N/mm² 96.94 N/mm²

Max. stress util.: 28.65 % 60.47 %

6

APPENDIX B of Doc. 150-L-ZE-0097001-015

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Page 137: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

Dimensions - THTF058

Internal pressure analysis acc. to ASME B31.3-2016 NPS4.0 Pipe ASME B36.10M:2004 114.30 x 6.02

NPS4.0

Results Pipe

Description Temperature Pressure Allowable stresses Calculated stress: Utilization:

Design 190.00 °C 20.50 bar (g) 137.38 N/mm² 30.28 N/mm² 22.04 %

Pressure test 20.00 °C 76.00 bar (g) 241.32 N/mm² 112.25 N/mm² 46.52 %

Results Elbow/Bend

Design 190.00 °C 20.50 bar (g) 137.38 N/mm² 39.36 N/mm² 28.65 %

Pressure test 20.00 °C 76.00 bar (g) 241.32 N/mm² 145.93 N/mm² 60.47 %

7

APPENDIX B of Doc. 150-L-ZE-0097001-015

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Page 138: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

Dimensions - THTF058

Internal pressure analysis acc. to ASME B31.3-2016

Input dataNom. diameter: NPS6.0

Pipe ASME B36.10M:2004 168.28 x 7.11

NPS6.0

Material: SA106B

Design pressure/temperature: 20.50 bar (g) / 190.00 °C

Test pressure/temperature: 76.00 bar (g) / 20.00 °C

Analysis straight pipeDimensions

Outer diameter: 168.28 mm

Wall thickness: 7.11 mm

Add. thickness c1: 12.50% (Rel. minus tolerance (%))

Add. thickness c2: 1.50 mm

Welding factors E x W: 1.00

Coefficient Y: 0.40

Range of validity

t < D / 6 28.046 met

P / S*E <= 0.385 0.015 met

Allowable stresses Design cond. Test cond.

Allowable stresses: 137.38 N/mm² 241.32 N/mm²

Results Design cond. Test cond.

Required wall thickness: 1.25 mm 2.62 mm

Calculated stress: 35.70 N/mm² 132.35 N/mm²

Stress utilization: 25.99 % 54.84 %

Analysis Elbow/BendDimensions

Outer diameter: 168.28 mm

Thickness of connection: 7.11 mm

Add. thickness c1: 12.50% (Rel. minus tolerance (%))

Inner wall thickn.: 7.11 mm

Add. thickness c1: 12.50% (Rel. minus tolerance (%))

Outer wall thickn.: 7.11 mm

Add. thickness c1: 12.50% (Rel. minus tolerance (%))

Add. thickness c2: 1.50 mm

Bend radius 228.60 mm

Welding factors E x W: 1.00

Coefficient Y: 0.40

Allowable stresses bend Design cond. Test cond.

Allowable stresses: 137.38 N/mm² 241.32 N/mm²

Results Design cond. Test cond.

Required wall thickness: inside 1.61 mm 3.37 mm

Calculated stress inside: 46.10 N/mm² 170.89 N/mm²

Required wall thickness: outside 1.08 mm 2.27 mm

Calculated stress outside: 30.90 N/mm² 114.55 N/mm²

Max. stress util.: 33.55 % 70.82 %

8

APPENDIX B of Doc. 150-L-ZE-0097001-015

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Page 139: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

Dimensions - THTF058

Internal pressure analysis acc. to ASME B31.3-2016 NPS6.0 Pipe ASME B36.10M:2004 168.28 x 7.11

NPS6.0

Results Pipe

Description Temperature Pressure Allowable stresses Calculated stress: Utilization:

Design 190.00 °C 20.50 bar (g) 137.38 N/mm² 35.70 N/mm² 25.99 %

Pressure test 20.00 °C 76.00 bar (g) 241.32 N/mm² 132.35 N/mm² 54.84 %

Results Elbow/Bend

Design 190.00 °C 20.50 bar (g) 137.38 N/mm² 46.10 N/mm² 33.55 %

Pressure test 20.00 °C 76.00 bar (g) 241.32 N/mm² 170.89 N/mm² 70.82 %

9

APPENDIX B of Doc. 150-L-ZE-0097001-015

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Page 140: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

Dimensions - THTF058

Overview ReducersInternal pressure analysis acc. to ASME B31.3-2016

Analysis for reducers Design Test

Description Nominal diameter Wall-thk. C1 C2 P T Util. P T Util.

mm mm mm bar (g) °C % bar (g) °C %

NPS3.0/NPS2.0

NW1 88.90 mm 5.49 12.50% 1.50 20.50 190.00 22.81 76.00 20.00 48.15

NW2 60.33 mm 3.91 12.50% 1.50

NPS3.0/NPS2.0_1

NW1 88.90 mm 7.62 12.50% 1.50 20.50 190.00 12.86 76.00 20.00 27.14

NW2 60.33 mm 5.54 12.50% 1.50

NPS4.0/NPS3.0

NW1 114.30 mm 6.02 12.50% 1.50 20.50 190.00 22.04 76.00 20.00 46.52

NW2 88.90 mm 5.49 12.50% 1.50

10

APPENDIX B of Doc. 150-L-ZE-0097001-015

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Page 141: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

Dimensions - THTF058

Internal pressure analysis of Reducer acc. to ASME B31.3According to ASME B31.3 the dimensions of the the Reducer are sufficient if the utilization of a matching

straight pipe is <= 100% due to the same loads.

NPS3.0/NPS2.0

Component with full utilization factor.

Input data Nom. diameter 1 Nom. diameter 2Nom. diameter: NPS3.0 NPS2.0

Material: SA106B SA106B

Design pressure / temperature: 20.50 bar (g) / 190.00 °C

Test pressure/temperature: 76.00 bar (g) / 20.00 °C

Dimensions Nom. diameter 1 Nom. diameter 2

Outer diameter Da / da: 88.90 mm 60.33 mm

Wall thickn. e_ord_s / e_ord_b: 5.49 mm 3.91 mm

Add. thickness c1: 12.50% 12.50%

Add.thickness c0: 1.50 mm 1.50 mm

Welding factors E x W: 1.00 1.00

Angle alpha: 75.00°

Allowable streses Diameter 1 Design cond. Test cond.

Allowable stresses: 137.38 N/mm² 241.32 N/mm²

Allowable streses Diameter 2 Design cond. Test cond.

Allowable stresses: 137.38 N/mm² 241.32 N/mm²

Stress analysis design conditionsNom. diameter 1 Nom. diameter 2

Calculated stress: 26.79 N/mm² 31.34 N/mm²

Allowable stresses: 137.38 N/mm² 137.38 N/mm²

Utilization: 19.50 % 22.81 %

Stress analysis test conditionsNom. diameter 1 Nom. diameter 2

Calculated stress: 99.31 N/mm² 116.19 N/mm²

Allowable stresses: 241.32 N/mm² 241.32 N/mm²

Utilization: 41.15 % 48.15 %

Results

Description Temperature Pressure Allowed Calculated Utilization:

Design 190.00 °C 20.50 bar (g) 137.38 N/mm² 31.34 N/mm² 22.81 %

Pressure test 20.00 °C 76.00 bar (g) 241.32 N/mm² 116.19 N/mm² 48.15 %

11

APPENDIX B of Doc. 150-L-ZE-0097001-015

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Page 142: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

Dimensions - THTF058

Internal pressure analysis of Reducer acc. to ASME B31.3According to ASME B31.3 the dimensions of the the Reducer are sufficient if the utilization of a matching

straight pipe is <= 100% due to the same loads.

NPS3.0/NPS2.0_1

Component with full utilization factor.

Input data Nom. diameter 1 Nom. diameter 2Nom. diameter: NPS3.0 NPS2.0

Material: SA106B SA106B

Design pressure / temperature: 20.50 bar (g) / 190.00 °C

Test pressure/temperature: 76.00 bar (g) / 20.00 °C

Dimensions Nom. diameter 1 Nom. diameter 2

Outer diameter Da / da: 88.90 mm 60.33 mm

Wall thickn. e_ord_s / e_ord_b: 7.62 mm 5.54 mm

Add. thickness c1: 12.50% 12.50%

Add.thickness c0: 1.50 mm 1.50 mm

Welding factors E x W: 1.00 1.00

Angle alpha: 75.00°

Allowable streses Diameter 1 Design cond. Test cond.

Allowable stresses: 137.38 N/mm² 241.32 N/mm²

Allowable streses Diameter 2 Design cond. Test cond.

Allowable stresses: 137.38 N/mm² 241.32 N/mm²

Stress analysis design conditionsNom. diameter 1 Nom. diameter 2

Calculated stress: 16.81 N/mm² 17.67 N/mm²

Allowable stresses: 137.38 N/mm² 137.38 N/mm²

Utilization: 12.24 % 12.86 %

Stress analysis test conditionsNom. diameter 1 Nom. diameter 2

Calculated stress: 62.33 N/mm² 65.49 N/mm²

Allowable stresses: 241.32 N/mm² 241.32 N/mm²

Utilization: 25.83 % 27.14 %

Results

Description Temperature Pressure Allowed Calculated Utilization:

Design 190.00 °C 20.50 bar (g) 137.38 N/mm² 17.67 N/mm² 12.86 %

Pressure test 20.00 °C 76.00 bar (g) 241.32 N/mm² 65.49 N/mm² 27.14 %

12

APPENDIX B of Doc. 150-L-ZE-0097001-015

13 of 19

Page 143: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

Dimensions - THTF058

Internal pressure analysis of Reducer acc. to ASME B31.3According to ASME B31.3 the dimensions of the the Reducer are sufficient if the utilization of a matching

straight pipe is <= 100% due to the same loads.

NPS4.0/NPS3.0

Component with full utilization factor.

Input data Nom. diameter 1 Nom. diameter 2Nom. diameter: NPS4.0 NPS3.0

Material: SA106B SA106B

Design pressure / temperature: 20.50 bar (g) / 190.00 °C

Test pressure/temperature: 76.00 bar (g) / 20.00 °C

Dimensions Nom. diameter 1 Nom. diameter 2

Outer diameter Da / da: 114.30 mm 88.90 mm

Wall thickn. e_ord_s / e_ord_b: 6.02 mm 5.49 mm

Add. thickness c1: 12.50% 12.50%

Add.thickness c0: 1.50 mm 1.50 mm

Welding factors E x W: 1.00 1.00

Angle alpha: 75.00°

Allowable streses Diameter 1 Design cond. Test cond.

Allowable stresses: 137.38 N/mm² 241.32 N/mm²

Allowable streses Diameter 2 Design cond. Test cond.

Allowable stresses: 137.38 N/mm² 241.32 N/mm²

Stress analysis design conditionsNom. diameter 1 Nom. diameter 2

Calculated stress: 30.28 N/mm² 26.79 N/mm²

Allowable stresses: 137.38 N/mm² 137.38 N/mm²

Utilization: 22.04 % 19.50 %

Stress analysis test conditionsNom. diameter 1 Nom. diameter 2

Calculated stress: 112.25 N/mm² 99.31 N/mm²

Allowable stresses: 241.32 N/mm² 241.32 N/mm²

Utilization: 46.52 % 41.15 %

Results

Description Temperature Pressure Allowed Calculated Utilization:

Design 190.00 °C 20.50 bar (g) 137.38 N/mm² 30.28 N/mm² 22.04 %

Pressure test 20.00 °C 76.00 bar (g) 241.32 N/mm² 112.25 N/mm² 46.52 %

13

APPENDIX B of Doc. 150-L-ZE-0097001-015

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Page 144: PIPE STRESS ANALYSIS REPORT - portal.cimtas.com

Dimensions - THTF058

Overview Branches/TeesInternal pressure analysis acc. to ASME B31.3-2016

Analysis for tees Design Test

Description Nominal diameter Wall-thk. C1 C2 P T Util. P T Util.

mm mm mm bar (g) °C % bar (g) °C %

NPS4.0/NPS3.0

R 4 6.02 12.50% 1.50 20.50 190.00 22.26 76.00 20.00 65.04

B 3 5.49 12.50% 1.50

NPS3.0/NPS3.0

R 3 5.49 12.50% 1.50 20.50 190.00 19.50 76.00 20.00 41.15

B 3 5.49 12.50% 1.50

NPS6.0/NPS3.0

R 6 7.11 12.50% 1.50 20.50 190.00 28.60 76.00 20.00 91.84

B 3 5.49 12.50% 1.50

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Dimensions - THTF058

Internal pressure analysis Branch/Tee acc. to ASME B31.3-2016NPS4.0/NPS3.0

Areas of welds according to 328.5.4

Input data Run BranchNom. diameter: NPS4.0 NPS3.0

Material: SA106B SA106B

Design pressure / temperature: 20.50 bar (g) / 190.00 °C

Test pressure/temperature: 76.00 bar (g) / 20.00 °C

Dimensions Run Branch

Outer diameter Da / da: 114.30 mm 88.90 mm

Wall thickn. e_ord_s / e_ord_b: 6.02 mm 5.49 mm

Add. thickness c1: 12.50% 12.50%

Add.thickness c0: 1.50 mm 1.50 mm

Welding factors E x W: 1.00 1.00

Coefficient Y: 0.40 0.40

Length: 164.60 mm 65.40 mm

Effective width ls / length lb: 82.30 mm 8.25 mm

Allowable stresses run Design cond. Test cond.

Allowable stresses: 137.38 N/mm² 241.32 N/mm²

Allowable stresses branch Design cond. Test cond.

Allowable stresses: 137.38 N/mm² 241.32 N/mm²

Range of validity

Db/Dh <= 1.000 0.778 met

Dh/Th <= 100.000 18.987 met

phi <= 45.000 0.000 met

Results Design cond. Test cond.Analysis straight pipe - RunCalculated stress: 30.28 N/mm² 112.25 N/mm²

Stress utilization: 22.04 % 46.52 %

Analysis straight pipe - BranchCalculated stress: 26.79 N/mm² 99.31 N/mm²

Stress utilization: 19.50 % 41.15 %

Area for design conditionsAnalysis equation (6a)

Required Area: 69.77 mm²

Reinforcement area: 313.37 mm²

Utilization: 22.26 %

Area for test conditionsAnalysis equation (6a)

Required Area: 146.28 mm²

Reinforcement area: 224.93 mm²

Utilization: 65.04 %

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Dimensions - THTF058

Internal pressure analysis Branch/Tee acc. to ASME B31.3-2016According to ASME B31.3 the dimensions of the tee are sufficient if the utilization of a matching straight pipe is <= 100% due to the

same loads.

NPS3.0/NPS3.0

Tee ASME B16.9 88.90 x 5.49 88.90 x 5.49

Component with full utilization factor.

Input data Run BranchNom. diameter: 3 3

Material: SA106B SA106B

Design pressure / temperature: 20.50 bar (g) / 190.00 °C

Test pressure/temperature: 76.00 bar (g) / 20.00 °C

Dimensions Run Branch

Outer diameter Da / da: 88.90 mm 88.90 mm

Wall thickn. e_ord_s / e_ord_b: 5.49 mm 5.49 mm

Add. thickness c1: 12.50% 12.50%

Add.thickness c0: 1.50 mm 1.50 mm

Welding factors E x W: 1.00 1.00

Coefficient Y: 0.40 0.40

Allowable stresses run Design cond. Test cond.

Allowable stresses: 137.38 N/mm² 241.32 N/mm²

Allowable stresses branch Design cond. Test cond.

Allowable stresses: 137.38 N/mm² 241.32 N/mm²

Range of validity

Db/Dh <= 1.000 1.000 met

Dh/Th <= 100.000 16.204 met

phi <= 45.000 0.000 met

Results Design cond. Test cond.Analysis straight pipe - RunCalculated stress: 26.79 N/mm² 99.31 N/mm²

Stress utilization: 19.50 % 41.15 %

Analysis straight pipe - BranchCalculated stress: 26.79 N/mm² 99.31 N/mm²

Stress utilization: 19.50 % 41.15 %

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Dimensions - THTF058

Internal pressure analysis Branch/Tee acc. to ASME B31.3-2016NPS6.0/NPS3.0

Areas of welds according to 328.5.4

Input data Run BranchNom. diameter: NPS6.0 NPS3.0

Material: SA106B SA106B

Design pressure / temperature: 20.50 bar (g) / 190.00 °C

Test pressure/temperature: 76.00 bar (g) / 20.00 °C

Dimensions Run Branch

Outer diameter Da / da: 168.28 mm 88.90 mm

Wall thickn. e_ord_s / e_ord_b: 7.11 mm 5.49 mm

Add. thickness c1: 12.50% 12.50%

Add.thickness c0: 1.50 mm 1.50 mm

Welding factors E x W: 1.00 1.00

Coefficient Y: 0.40 0.40

Length: 164.60 mm 92.39 mm

Effective width ls / length lb: 82.30 mm 8.25 mm

Allowable stresses run Design cond. Test cond.

Allowable stresses: 137.38 N/mm² 241.32 N/mm²

Allowable stresses branch Design cond. Test cond.

Allowable stresses: 137.38 N/mm² 241.32 N/mm²

Range of validity

Db/Dh <= 1.000 0.528 met

Dh/Th <= 100.000 23.661 met

phi <= 45.000 0.000 met

Results Design cond. Test cond.Analysis straight pipe - RunCalculated stress: 35.70 N/mm² 132.35 N/mm²

Stress utilization: 25.99 % 54.84 %

Analysis straight pipe - BranchCalculated stress: 26.79 N/mm² 99.31 N/mm²

Stress utilization: 19.50 % 41.15 %

Area for design conditionsAnalysis equation (6a)

Required Area: 102.71 mm²

Reinforcement area: 359.08 mm²

Utilization: 28.60 %

Area for test conditionsAnalysis equation (6a)

Required Area: 215.36 mm²

Reinforcement area: 234.50 mm²

Utilization: 91.84 %

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Calculation of allowable stresses +-----------------------------------------------------------------------+

| ASME B31.3 Edit.2016 Material: SA106B Ferrite |

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

| Material: SA106B |

| Material properties Spec. Rev. |

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

| Young's modulus ASME II/D, Table Y1 01/2013 |

| Expansion coefficient ASME II/D, Table Y1 01/2013 |

| Tensile strength ASME II/D, Table Y1 01/2013 |

| 0.2% Yield strength ASME II/D, Table Y1 07/2015 |

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

| Temperature T °C | 190.00 | 190.00 | 20.00 | 20.00 | |

| Y-mod\cold kN/mm^2 | 203.46 | 203.46 | 203.46 | 203.46 | |

| Y-mod\hot kN/mm^2 | 192.06 | 192.06 | 203.46 | 203.46 | |

|---------------------+---------+---------+---------+---------+---------|

| wall thickness mm | 6 - 7| 0 - 6| 6 - 7| 0 - 6| |

|---------------------+---------+---------+---------+---------+---------|

| Rm\RT\min | -.- | -.- | -.- | | |

| Rm\T\min | -.- | -.- | -.- | | |

| Rp0.2\RT\min | -.- | -.- | -.- | | |

| Rp0.2\T\min | 208.12 | 208.12 | 241.32 | 241.32 | |

| Rm\100000\mit | -.- | -.- | -.- | | |

| Rm\100000\min | -.- | -.- | -.- | | |

|---------------------+---------+---------+---------+---------+---------|

| Rm\RT\min/3.0 | -.- | -.- | -.- | | |

| Rp0.2\RT\min/1.5 | -.- | -.- | -.- | | |

| Sc | 137.90 | 137.90 | 137.90 | | |

|---------------------+---------+---------+---------+---------+---------|

| Rm\T\min/3.0 | -.- | -.- | -.- | | |

| Rp0.2\T\min /1.5 | 138.75 | 138.75 | 160.88 | | |

| Rm\100000\mitt/1.5 | -.- | -.- | -.- | | |

| 0.8*Rm\100000\min | -.- | -.- | -.- | | |

| Sh | 137.38 | 137.38 | 137.90 | | |

| Sh_test | | | | 241.32 | |

|---------------------+---------+---------+---------+---------+---------|

| Sa | 206.71 | 206.71 | 206.84 | | |

| SoA | 344.09 | 344.09 | 344.74 | | |

+-----------------------------------------------------------------------+

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APPENDIX C

APPENDIX C of Doc. 150-L-ZE-0097001-015

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Cylinder #1

ASME Section VIII Division 1, 2017 Edition Metric

Component Cylinder

Material SA-106 B Smls Pipe (II-D Metric p. 14, ln. 10)

Pipe NPS andSchedule NPS 3 Sch 40 (Std) DN 80

ImpactTested Normalized Fine Grain

Practice PWHT Maximize MDMT/No MAWP

No No No No No

DesignPressure (bar)

DesignTemperature (°C)

DesignMDMT (°C)

Internal 20.5 190 -10External 1.03 190

Static Liquid Head

Condition Ps (bar) Hs (mm) SG

Test horizontal 0.01 77.92 1

Dimensions

Outer Diameter 88.9 mm

Length 12,300 mm

Pipe NominalThickness 5.49 mm

Pipe MinimumThickness1 4.8 mm

Corrosion Inner 1.5 mm

Outer 0 mm

Weight and Capacity

Weight (kg) Capacity (liters)

New 138.6 58.65

Corroded 102.52 63.26

Radiography

Longitudinal seam Seamless No RT

Left Circumferentialseam Full UW-11(a) Type 1

Right Circumferentialseam Full UW-11(a) Type 1

1Pipe minimum thickness = nominal thickness times pipe tolerance factor of 0.875.

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Results Summary

Governing condition UG-16

Minimum thickness per UG-16 1.5 mm + 1.5 mm = 3 mm

Design thickness due to internal pressure (t) 2.27 mm

Design thickness due to external pressure (te) 2.3 mm

Maximum allowable working pressure (MAWP) 90.36 bar

Maximum allowable pressure (MAP) 133.29 bar

Maximum allowable external pressure (MAEP) 43.5 bar

Rated MDMT -105 °C

UCS-66 Material Toughness Requirements

Governing thickness, tg = 4.8 mm

Impact test exempt per UCS-66(d) (NPS 4 or smaller pipe) = -105°C

Material is exempt from impact testing at the Design MDMT of -10°C.

Design thickness, (at 190 °C) Appendix 1-1

t = P*Ro / (S*E + 0.40*P) + Corrosion= 20.5*44.45 / (1,180*1.00 + 0.40*20.5) + 1.5= 2.27 mm

Maximum allowable working pressure, (at 190 °C) Appendix 1-1

P = S*E*t / (Ro - 0.40*t) - Ps= 1,180*1.00*(5.49*0.875 - 1.5) / (44.45 - 0.40*(5.49*0.875 - 1.5)) - 0= 90.36 bar

Maximum allowable pressure, (at -10 °C) Appendix 1-1

P = S*E*t / (Ro - 0.40*t)= 1,180*1.00*(5.49*0.875) / (44.45 - 0.40*(5.49*0.875))= 133.29 bar

External Pressure, (Corroded & at 190 °C) UG-28(c)

L / Do = 12,300 / 88.9 = 50.0000Do / t = 88.9 / 0.79 = 111.9522

From table G: A = 0.000091From table CS-2 Metric: B = 88.5451 kg/cm2 (86.83 bar)

Pa = 4*B / (3*(Do / t))= 4*86.83 / (3*(88.9 / 0.79))= 1.03 bar

Design thickness for external pressure Pa = 1.03 bar

ta = t + Corrosion = 0.79 + 1.5 = 2.3 mm

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Maximum Allowable External Pressure, (Corroded & at 190 °C) UG-28(c)

L / Do = 12,300 / 88.9 = 50.0000Do / t = 88.9 / (5.49*0.875 - 1.5) = 26.9181

From table G: A = 0.001553From table CS-2 Metric: B = 895.4649 kg/cm2 (878.1495 bar)

Pa = 4*B / (3*(Do / t))= 4*878.15 / (3*(88.9 / (5.49*0.875 - 1.5)))= 43.5 bar

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