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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
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REVISION INDEX
Rev. Date Rev. Description
11.06.2020 0 Issued for Review
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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
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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:
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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
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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
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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.
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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.
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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)]
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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
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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)
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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
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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)
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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”.
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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
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
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19/65
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R E S U L T S ‐‐ Program ROHR2 CIMT/32.1 ‐‐ Page 2
Commiss. THTF058 Date 06/12/20 11:29:14
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
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
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21/65
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R E S U L T S ‐‐ Program ROHR2 CIMT/32.1 ‐‐ Page 3
Commiss. THTF058 Date 06/12/20 11:29:14
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
‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐
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
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22/65
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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
‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐
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
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23/65
STAR DOCUMENT No.
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R E S U L T S ‐‐ Program ROHR2 CIMT/32.1 ‐‐ Page 5
Commiss. THTF058 Date 06/12/20 11:29:14
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
‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐
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
24/65
STAR DOCUMENT No.
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R E S U L T S ‐‐ Program ROHR2 CIMT/32.1 ‐‐ Page 6
Commiss. THTF058 Date 06/12/20 11:29:14
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
‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐
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
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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
‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐
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
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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
‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐
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
‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐
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
‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐
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
‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐
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
‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐
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
‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐
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
‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐
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
‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐
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
‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐
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
R E S U L T S ‐‐ Program ROHR2 CIMT/32.1 ‐‐ Page 17
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
‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐
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
R E S U L T S ‐‐ Program ROHR2 CIMT/32.1 ‐‐ Page 18
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
‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐
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
‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐
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
38/65
STAR DOCUMENT No.
150-L-ZE-0097001-015
REV 0
R E S U L T S ‐‐ Program ROHR2 CIMT/32.1 ‐‐ Page 20
Commiss. THTF058 Date 06/12/20 11:29:14
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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APPENDIX A-11.1 DETAIL STRESS REPORT FOR HCU HEAVY NAPHTA TO DIESEL FOR FLASH POINT OPTIMIZATION
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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S T R E S S E S ‐‐ Program ROHR2 CIMT/32.1 ‐‐ Page 2
Commiss. THTF058 Date 06/12/20 11:29:15
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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S T R E S S E S ‐‐ Program ROHR2 CIMT/32.1 ‐‐ Page 3
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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 | | |
+‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐+
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
6/64
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 4
Commiss. THTF058 Date 06/12/20 11:29:15
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
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
7/64
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 5
Commiss. THTF058 Date 06/12/20 11:29:15
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
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
8/64
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 6
Commiss. THTF058 Date 06/12/20 11:29:15
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
26/64
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 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
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
27/64
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 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
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
28/64
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 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
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
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
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
31/64
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 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
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
32/64
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 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
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
33/64
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 0.012 ‐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
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
34/64
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 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
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
35/64
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 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
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
36/64
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 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
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
37/64
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 0.004 ‐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
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
38/64
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 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
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
39/64
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 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
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
40/64
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 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
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
41/64
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 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
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
42/64
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 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
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
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
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
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
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
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
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
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
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
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
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
53/64
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 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
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
54/64
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 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
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
55/64
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 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
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
56/64
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 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
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
57/64
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 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
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
58/64
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 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
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
59/64
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= 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
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
60/64
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 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
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
61/64
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 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 (*)
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
62/64
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 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 (*)
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
63/64
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 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 (*)
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
64/64
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 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 (*)
APPENDIX B
APPENDIX B of Doc. 150-L-ZE-0097001-015
1 of 19
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
1
APPENDIX B of Doc. 150-L-ZE-0097001-015
2 of 19
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 %
2
APPENDIX B of Doc. 150-L-ZE-0097001-015
3 of 19
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
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
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
6 of 19
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 %
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APPENDIX B of Doc. 150-L-ZE-0097001-015
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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 %
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APPENDIX B of Doc. 150-L-ZE-0097001-015
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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 %
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APPENDIX B of Doc. 150-L-ZE-0097001-015
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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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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
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APPENDIX B of Doc. 150-L-ZE-0097001-015
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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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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
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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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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
14
APPENDIX B of Doc. 150-L-ZE-0097001-015
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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 %
15
APPENDIX B of Doc. 150-L-ZE-0097001-015
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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 %
16
APPENDIX B of Doc. 150-L-ZE-0097001-015
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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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APPENDIX B of Doc. 150-L-ZE-0097001-015
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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 B of Doc. 150-L-ZE-0097001-015
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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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APPENDIX C of Doc. 150-L-ZE-0097001-015
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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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APPENDIX C of Doc. 150-L-ZE-0097001-015
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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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APPENDIX C of Doc. 150-L-ZE-0097001-015
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