FFS-579 Out

PV Elite® 2019
Project Data Page:

PV Elite® 2019
Table of Contents
Cover Page 1
Title Page 2
Warnings and Errors: 3
Input Echo: 4
XY Coordinate Calculations: 14
Internal Pressure Calculations: 15
External Pressure Calculations: 22
Element and Detail Weights: 28
Nozzle Flange MAWP: 30
Wind Load Calculation: 31
Earthquake Load Calculation: 33
Center of Gravity Calculation: 34
Horizontal Vessel Analysis (Ope.) 35
Nozzle Summary: 46
Nozzle Calcs.: N1 48
Nozzle Calcs.: MH1 72
Nozzle Calcs.: MH2 117
Nozzle Schedule: 122
MDMT Summary: 124
API-579 Calcs: Thinning 126
Vessel Design Summary: 131
Cover Page PV Elite® 2019
DESIGN CALCULATION
In Accordance with ASME Section VIII Division 1
ASME Code Version : 2017
Analysis Performed by : SPLM Licensed User
Job File : E:\PV\FFS-579.Pvdb
Date of Analysis : Aug 29,2023 10:40am
PV Elite 2019 SP1, March 2019

Title Page PV Elite® 2019
Note:
PV Elite performs all calculations internally in Imperial Units
to remain compliant with the ASME Code and any built in assumptions
in the ASME Code formulas. The finalized results are reflected to show
the user's set of selected units.
® SPLM Licensed User
PV Elite 2019
PV Elite 2019 SP1 Licensee:
FileName : FFS-579 Page 3 of 132
Warnings and Errors: Step: 0 10:40am Aug 29,2023
Class From To : Basic Element Checks.

==========================================================================
Class From To: Check of Additional Element Data

==========================================================================
There were no geometry errors or warnings.
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2019

PV Elite 2019
Input Echo: Step: 1 10:40am Aug 29,2023
PV Elite Vessel Analysis Program: Input Data
Design Internal Pressure (for Hydrotest) 15 kgf/cm²

Design Internal Temperature 60.0 °C
Type of Hydrotest not Specified
Hydrotest Position Horizontal
Projection of Nozzle from Vessel Top 0 mm
Projection of Nozzle from Vessel Bottom 0 mm
Minimum Design Metal Temperature -8.0 °C
Type of Construction Welded
Special Service None
Degree of Radiography RT-1
Use Higher Longitudinal Stresses (Flag) Y
Select t for Internal Pressure (Flag) N
Select t for External Pressure (Flag) N
Select t for Axial Stress (Flag) N
Select Location for Stiff. Rings (Flag) N
Consider Vortex Shedding N
Perform a Corroded Hydrotest N
Load Case 1 NP+EW+WI+FW+BW

Load Case 2 NP+EW+EE+FS+BS
Load Case 3 NP+OW+WI+FW+BW
Load Case 4 NP+OW+EQ+FS+BS
Load Case 5 NP+HW+HI
Load Case 6 NP+HW+HE
Load Case 7 IP+OW+WI+FW+BW
Load Case 8 IP+OW+EQ+FS+BS
Load Case 9 EP+OW+WI+FW+BW
Load Case 10 EP+OW+EQ+FS+BS
Load Case 11 HP+HW+HI
Load Case 12 HP+HW+HE
Load Case 13 IP+WE+EW
Load Case 14 IP+WF+CW
Load Case 15 IP+VO+OW
Load Case 16 IP+VE+EW
Load Case 17 NP+VO+OW
Load Case 18 FS+BS+IP+OW
Load Case 19 FS+BS+EP+OW
Wind Design Code ASCE-7 93

Basic Wind Speed [V] 112.65 km/hr
Surface Roughness Category C: Open Terrain
Importance Factor 1.0
Type of Surface Moderately Smooth
Base Elevation 0 cm
Percent Wind for Hydrotest 33.0
Using User defined Wind Press. Vs Elev. N
Damping Factor (Beta) for Wind (Ope) 0.0100
Damping Factor (Beta) for Wind (Empty) 0.0000
Damping Factor (Beta) for Wind (Filled) 0.0000
Seismic Design Code UBC 94

UBC Seismic Zone (1=1,2=2a,3=2b,4=3,5=4) 0.000
UBC Importance Factor 1.000
UBC Soil Type S1
UBC Horizontal Force Factor 3.000
UBC Percent Seismic for Hydrotest 0.000
Design Pressure + Static Head Y

Consider MAP New and Cold in Noz. Design N
Consider External Loads for Nozzle Des. Y
Use ASME VIII-1 Appendix 1-9 N
PV Elite 2019
Material Database Year Current w/Addenda or Code Year
Configuration Directives:
Do not use Nozzle MDMT Interpretation VIII-1 01-37 No

Use Table G instead of exact equation for "A" Yes
Shell Head Joints are Tapered Yes
Compute "K" in corroded condition Yes
Use Code Case 2286 No
Use the MAWP to compute the MDMT Yes
For thickness ratios <= 0.35, MDMT will be -155F (-104C) Yes
For PWHT & P1 Materials the MDMT can be < -55F (-48C) No
Using Metric Material Databases, ASME II D No

Calculate B31.3 type stress for Nozzles with Loads Yes
Reduce the MDMT due to lower membrane stress Yes
Consider Longitudinal Stress in MDMT calcs. (Div. 1) No
Complete Listing of Vessel Elements and Details:
Element From Node 10

Element To Node 20
Element Type Elliptical
Description HEAD 1
Distance "FROM" to "TO" 20 cm
Inside Diameter 3658 mm
Element Thickness 26.69 mm
Internal Corrosion Allowance 0 mm
Nominal Thickness 0 mm
External Corrosion Allowance 0 mm
Design Internal Pressure 15 kgf/cm²
Design Temperature Internal Pressure 60 °C
Design External Pressure 1.0299 kgf/cm²
Design Temperature External Pressure 33 °C
Effective Diameter Multiplier 1.2
Material Name SA-516 70 [Impact Tested]
Allowable Stress, Ambient 1406.1 kgf/cm²
Allowable Stress, Operating 1406.1 kgf/cm²
Allowable Stress, Hydrotest 1828 kgf/cm²
Material Density 0.00775 kg/cm³
P Number Thickness 29.997 mm
Yield Stress, Operating 2542.3 kgf/cm²
UCS-66 Chart Curve Designation Impact Tested
External Pressure Chart Name CS-2
UNS Number K02700
Product Form Plate
Efficiency, Longitudinal Seam 1.0
Efficiency, Circumferential Seam 1.0
Elliptical Head Factor 1.5
Weld is pre-Heated No

Element To Node 30
Element Type Cylinder
Description SHELL 1
Distance "FROM" to "TO" 186.3 cm
PV Elite 2019


Detail Type Saddle
Detail ID Lft Sdl
Dist. from "FROM" Node / Offset dist 86.3 cm
Width of Saddle 300 mm
Height of Saddle at Bottom 2429 mm
Saddle Contact Angle 135.0
Height of Composite Ring Stiffener 0 mm
Width of Wear Plate 500 mm
Thickness of Wear Plate 24 mm
Contact Angle, Wear Plate (degrees) 162.0
Friction coefficient 0.0
Moment Factor 3.0
Dimension E at base (optional) 2000 mm
Circumferential Eff. over Saddle 1.0
Circumferential Eff. at Midspan 1.0
Tangent to Tangent dist. (optional) 0 cm

Detail Type Nozzle
Detail ID N1
Dist. from "FROM" Node / Offset dist 30 cm
Nozzle Diameter 4 in.
Nozzle Schedule 40
Nozzle Class 150
Layout Angle 90.0
Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 0 kgf
Grade of Attached Flange GR 1.1
Nozzle Matl SA-106 B

Detail Type Nozzle
Detail ID N2
Nozzle Schedule 40
Nozzle Class 150
Layout Angle 90.0

Detail Type Nozzle
Detail ID N18
Nozzle Schedule 40
Nozzle Class 150
Layout Angle 270.0
PV Elite 2019

Element To Node 40
Description SHELL 2

Detail Type Nozzle
Detail ID N3
Nozzle Schedule 40
Nozzle Class 150
Layout Angle 90.0

Element To Node 50
Description SHELL 3

Detail Type Saddle
Detail ID Lft Sdl
Dist. from "FROM" Node / Offset dist 176.3 cm
PV Elite 2019

Moment Factor 3.0

Element To Node 60
Description SHELL 4

Detail Type Nozzle
Detail ID MH1
Nozzle Schedule 40
Nozzle Class 150
Layout Angle 90.0
Blind Flange (Y/N) Y

Detail Type Nozzle
Detail ID N6
Nozzle Schedule 40
Nozzle Class 150
Layout Angle 90.0

Element To Node 70
Description SHELL 5
PV Elite 2019


Detail Type Nozzle
Detail ID N5
Nozzle Schedule 40
Nozzle Class 150
Layout Angle 90.0

Detail Type Nozzle
Detail ID N4
Nozzle Schedule 40
Nozzle Class 150
Layout Angle 90.0

Detail Type Nozzle
Detail ID N11
Nozzle Schedule 40
Nozzle Class 150
Layout Angle 270.0

Detail Type Nozzle
Detail ID N12
Nozzle Schedule 40
Nozzle Class 150
Layout Angle 270.0
PV Elite 2019


Detail Type Nozzle
Detail ID N13
Nozzle Schedule 40
Nozzle Class 150
Layout Angle 270.0

Detail Type For./Mom.
Detail ID F/M:[1 of 1]
Force in X Direction 0 kgf
Force in Y Direction 0 kgf
Force in Z Direction 0 kgf
Moment about X Axis 0 kgf-m.
Moment about Y Axis 0 kgf-m.
Moment about Z Axis 0 kgf-m.
Force/Moment Combination Method SRSS

Element To Node 80
Description SHELL 6

Element To Node 90
Description SHELL 7
PV Elite 2019


Detail Type Saddle
Detail ID Lft Sdl
Moment Factor 3.0

Detail Type Nozzle
Detail ID N8
Nozzle Schedule 40
Nozzle Class 150
Layout Angle 270.0

Detail Type Nozzle
Detail ID N9
Nozzle Schedule 40
Nozzle Class 150
Layout Angle 270.0

Detail Type Nozzle
Detail ID N10
Nozzle Schedule 40
Nozzle Class 150
Layout Angle 270.0
PV Elite 2019

Element To Node 100
Description SHELL 8

Element To Node 110
Description SHELL 9

Detail Type Saddle
Detail ID Lft Sdl
Moment Factor 3.0

Detail Type Nozzle
Detail ID N7
PV Elite 2019

Nozzle Schedule 40
Nozzle Class 150
Layout Angle 270.0

Element To Node 120
Element Type Elliptical
Description HEAD 2
Distance "FROM" to "TO" 20 cm
Elliptical Head Factor 1.5

Detail Type Nozzle
Detail ID MH2
Dist. from "FROM" Node / Offset dist 0 mm
Nozzle Schedule 40
Nozzle Class 150
Layout Angle 0.0
Blind Flange (Y/N) Y

PV Elite 2019
XY Coordinate Calculations: Step: 2 10:40am Aug 29,2023
XY Coordinate Calculations:
From To X (Horiz.) Y (Vert.) DX (Horiz.) DY (Vert.)

cm cm cm cm
HEAD 1 20 ... 20 ...

SHELL 1 206.3 ... 186.3 ...
SHELL 2 392.6 ... 186.3 ...
SHELL 3 578.9 ... 186.3 ...
SHELL 4 765.2 ... 186.3 ...
SHELL 5 951.5 ... 186.3 ...
SHELL 6 1137.8 ... 186.3 ...
SHELL 7 1324.1 ... 186.3 ...
SHELL 8 1510.4 ... 186.3 ...
SHELL 9 1696.7 ... 186.3 ...
HEAD 2 1716.7 ... 20 ...

PV Elite 2019
Internal Pressure Calculations: Step: 3 10:40am Aug 29,2023
Element Thickness, Pressure, Diameter and Allowable Stress :
Int. Press Nominal Total Corr Element Allowable

From To + Liq. Hd Thickness Allowance Diameter Stress(SE)
kgf/cm² mm mm mm kgf/cm²
HEAD 1 15 ... ... 3658 1406.1

SHELL 1 15 ... ... 3658 1406.1
SHELL 2 15 ... ... 3658 1406.1
SHELL 3 15 ... ... 3658 1406.1
SHELL 4 15 ... ... 3658 1406.1
SHELL 5 15 ... ... 3658 1406.1
SHELL 6 15 ... ... 3658 1406.1
SHELL 7 15 ... ... 3658 1406.1
SHELL 8 15 ... ... 3658 1406.1
SHELL 9 15 ... ... 3658 1406.1
HEAD 2 15 ... ... 3658 1406.1
Element Required Thickness and MAWP :
Design M.A.W.P. M.A.P. Minimum Required

From To Pressure Corroded New & Cold Thickness Thickness
kgf/cm² kgf/cm² kgf/cm² mm mm
HEAD 1 15 20.3412 28.9089 26.69 13.835

SHELL 1 15 18.7611 18.7611 24.6 19.6365
SHELL 2 15 18.8973 18.8973 24.78 19.6365
SHELL 3 15 18.8973 18.8973 24.78 19.6365
SHELL 4 15 21.4815 21.4815 28.2 19.6365
SHELL 5 15 18.8897 18.8897 24.77 19.6365
SHELL 6 15 18.9124 18.9124 24.8 19.6365
SHELL 7 15 18.8973 18.8973 24.78 19.6365
SHELL 8 15 18.8897 18.8897 24.77 19.6365
SHELL 9 15 18.8973 18.8973 24.78 19.6365
HEAD 2 15 20.4017 28.9954 26.77 13.835
Minimum 18.761 18.761
MAWP: 15.218 kgf/cm², limited by: Nozzle Reinforcement.
Internal Pressure Calculation Results :
ASME Code, Section VIII Division 1, 2017
Elliptical Head From 10 To 20 SA-516 70 at 60 °C
HEAD 1
Material UNS Number: K02700
Required Thickness due to Internal Pressure [tr]:

= (P*D*Kcor)/(2*S*E-0.2*P) Appendix 1-4(c)
= (15.0*3658.0*0.708)/(2*1406.14*1.0-0.2*15.0)
= 13.8350 + 0.0000 = 13.8350 mm
Max. Allowable Working Pressure at given Thickness, corroded [MAWP]:

= (2*S*E*t)/(Kcor*D+0.2*t) per Appendix 1-4 (c)
= (2*1406.14*1.0*26.69)/(0.708*3658.0+0.2*26.69)
= 28.909 kgf/cm²
Maximum Allowable Pressure, New and Cold [MAPNC]:

= (2*S*E*t)/(K*D+0.2*t) per Appendix 1-4 (c)
PV Elite 2019
= (2*1406.14*1.0*26.69)/(0.708*3658.0+0.2*26.69)
= 28.909 kgf/cm²
Actual stress at given pressure and thickness, corroded [Sact]:

= (P*(Kcor*D+0.2*t))/(2*E*t)
= (15.0*(0.708*3658.0+0.2*26.69))/(2*1.0*26.69)
= 729.605 kgf/cm²
Straight Flange Required Thickness:

= (P*R)/(S*E-0.6*P) + c per UG-27 (c)(1)
= (15.0*1829.0)/(1406.14*1.0-0.6*15.0)+0.0
= 19.637 mm
Straight Flange Maximum Allowable Working Pressure:

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)
= (1406.14 * 1.0 * 26.69)/(1829.0 + 0.6 * 26.69 )
= 20.341 kgf/cm²
Percent Elong. per UCS-79, VIII-1-01-57 (75*tnom/Rf)*(1-Rf/Ro) 3.151 %
MDMT Calculations in the Knuckle Portion:
Note: This Element/Detail was specified as being Impact Tested.
MDMT Calculations in the Head Straight Flange:
Cylindrical Shell From 20 To 30 SA-516 70 at 60 °C
SHELL 1

= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406.14*1.0-0.6*15.0)
= 19.6365 + 0.0000 = 19.6365 mm

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)
= (1406.14*1.0*24.6)/(1829.0+0.6*24.6)
= 18.761 kgf/cm²

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)
= (1406.14*1.0*24.6)/(1829.0+0.6*24.6)
= 18.761 kgf/cm²

= (P*(R+0.6*t))/(E*t)
= (15.0*(1829.0+0.6*24.6))/(1.0*24.6)
= 1124.244 kgf/cm²
% Elongation per Table UG-79-1 (50*tnom/Rf*(1-Rf/Ro)) 0.668 %
Minimum Design Metal Temperature Results:

PV Elite 2019
SHELL 2

= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406.14*1.0-0.6*15.0)
= 19.6365 + 0.0000 = 19.6365 mm

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)
= (1406.14*1.0*24.78)/(1829.0+0.6*24.78)
= 18.897 kgf/cm²

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)
= (1406.14*1.0*24.78)/(1829.0+0.6*24.78)
= 18.897 kgf/cm²

= (P*(R+0.6*t))/(E*t)
= (15.0*(1829.0+0.6*24.78))/(1.0*24.78)
= 1116.143 kgf/cm²
SHELL 3

= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406.14*1.0-0.6*15.0)
= 19.6365 + 0.0000 = 19.6365 mm

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)
= (1406.14*1.0*24.78)/(1829.0+0.6*24.78)
= 18.897 kgf/cm²

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)
= (1406.14*1.0*24.78)/(1829.0+0.6*24.78)
= 18.897 kgf/cm²

= (P*(R+0.6*t))/(E*t)
= (15.0*(1829.0+0.6*24.78))/(1.0*24.78)
= 1116.143 kgf/cm²

PV Elite 2019
SHELL 4

= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406.14*1.0-0.6*15.0)
= 19.6365 + 0.0000 = 19.6365 mm

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)
= (1406.14*1.0*28.2)/(1829.0+0.6*28.2)
= 21.482 kgf/cm²

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)
= (1406.14*1.0*28.2)/(1829.0+0.6*28.2)
= 21.482 kgf/cm²

= (P*(R+0.6*t))/(E*t)
= (15.0*(1829.0+0.6*28.2))/(1.0*28.2)
= 981.872 kgf/cm²
SHELL 5

= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406.14*1.0-0.6*15.0)
= 19.6365 + 0.0000 = 19.6365 mm

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)
= (1406.14*1.0*24.77)/(1829.0+0.6*24.77)
= 18.890 kgf/cm²

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)
= (1406.14*1.0*24.77)/(1829.0+0.6*24.77)
= 18.890 kgf/cm²

= (P*(R+0.6*t))/(E*t)
= (15.0*(1829.0+0.6*24.77))/(1.0*24.77)
= 1116.590 kgf/cm²

PV Elite 2019
SHELL 6

= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406.14*1.0-0.6*15.0)
= 19.6365 + 0.0000 = 19.6365 mm

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)
= (1406.14*1.0*24.8)/(1829.0+0.6*24.8)
= 18.912 kgf/cm²

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)
= (1406.14*1.0*24.8)/(1829.0+0.6*24.8)
= 18.912 kgf/cm²

= (P*(R+0.6*t))/(E*t)
= (15.0*(1829.0+0.6*24.8))/(1.0*24.8)
= 1115.250 kgf/cm²
SHELL 7

= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406.14*1.0-0.6*15.0)
= 19.6365 + 0.0000 = 19.6365 mm

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)
= (1406.14*1.0*24.78)/(1829.0+0.6*24.78)
= 18.897 kgf/cm²

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)
= (1406.14*1.0*24.78)/(1829.0+0.6*24.78)
= 18.897 kgf/cm²

= (P*(R+0.6*t))/(E*t)
= (15.0*(1829.0+0.6*24.78))/(1.0*24.78)
= 1116.143 kgf/cm²
PV Elite 2019
SHELL 8

= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406.14*1.0-0.6*15.0)
= 19.6365 + 0.0000 = 19.6365 mm

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)
= (1406.14*1.0*24.77)/(1829.0+0.6*24.77)
= 18.890 kgf/cm²

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)
= (1406.14*1.0*24.77)/(1829.0+0.6*24.77)
= 18.890 kgf/cm²

= (P*(R+0.6*t))/(E*t)
= (15.0*(1829.0+0.6*24.77))/(1.0*24.77)
= 1116.590 kgf/cm²
SHELL 9

= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406.14*1.0-0.6*15.0)
= 19.6365 + 0.0000 = 19.6365 mm

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)
= (1406.14*1.0*24.78)/(1829.0+0.6*24.78)
= 18.897 kgf/cm²

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)
= (1406.14*1.0*24.78)/(1829.0+0.6*24.78)
= 18.897 kgf/cm²

PV Elite 2019
= (P*(R+0.6*t))/(E*t)
= (15.0*(1829.0+0.6*24.78))/(1.0*24.78)
= 1116.143 kgf/cm²
Elliptical Head From 110 To 120 SA-516 70 at 60 °C
HEAD 2

= (15.0*3658.0*0.708)/(2*1406.14*1.0-0.2*15.0)
= 13.8350 + 0.0000 = 13.8350 mm

= (2*S*E*t)/(Kcor*D+0.2*t) per Appendix 1-4 (c)
= (2*1406.14*1.0*26.77)/(0.708*3658.0+0.2*26.77)
= 28.995 kgf/cm²

= (2*S*E*t)/(K*D+0.2*t) per Appendix 1-4 (c)
= (2*1406.14*1.0*26.77)/(0.708*3658.0+0.2*26.77)
= 28.995 kgf/cm²

= (P*(Kcor*D+0.2*t))/(2*E*t)
= (15.0*(0.708*3658.0+0.2*26.77))/(2*1.0*26.77)
= 727.429 kgf/cm²
Straight Flange Required Thickness:

= (P*R)/(S*E-0.6*P) + c per UG-27 (c)(1)
= (15.0*1829.0)/(1406.14*1.0-0.6*15.0)+0.0
= 19.637 mm
Straight Flange Maximum Allowable Working Pressure:

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)
= (1406.14 * 1.0 * 26.77)/(1829.0 + 0.6 * 26.77 )
= 20.402 kgf/cm²
Percent Elong. per UCS-79, VIII-1-01-57 (75*tnom/Rf)*(1-Rf/Ro) 3.161 %
MDMT Calculations in the Knuckle Portion:
MDMT Calculations in the Head Straight Flange:
Elements Suitable for Internal Pressure.

PV Elite 2019
External Pressure Calculations: Step: 4 10:40am Aug 29,2023
External Pressure Calculation Results :
External Pressure Calculations:
Section Outside Corroded Factor Factor

From To Length Diameter Thickness A B
cm mm mm kgf/cm²
10 20 No Calc 3711.38 26.69 0.0012981 947.453

20 30 1797.99 3707.2 24.6 0.00013539 138.028
30 40 1797.99 3707.56 24.78 0.00013677 139.432
40 50 1797.99 3707.56 24.78 0.00013677 139.432
50 60 1797.99 3714.4 28.2 0.0001662 169.438
60 70 1797.99 3707.54 24.77 0.00013668 139.34
70 80 1797.99 3707.6 24.8 0.00013695 139.617
80 90 1797.99 3707.56 24.78 0.00013677 139.432
90 100 1797.99 3707.54 24.77 0.00013668 139.34
100 110 1797.99 3707.56 24.78 0.00013677 139.432
110 120 No Calc 3711.54 26.77 0.0013019 948.284
External External External External

From To Actual T. Required T. Design Pressure M.A.W.P.
mm mm kgf/cm² kgf/cm²
10 20 26.69 7.30681 1.02988 9.83901

20 30 24.6 22.8389 1.02988 1.22122
30 40 24.78 22.8401 1.02988 1.24255
40 50 24.78 22.8401 1.02988 1.24255
50 60 28.2 22.8626 1.02988 1.71518
60 70 24.77 22.84 1.02988 1.24123
70 80 24.8 22.8403 1.02988 1.24519
80 90 24.78 22.8401 1.02988 1.24255
90 100 24.77 22.84 1.02988 1.24123
100 110 24.78 22.8401 1.02988 1.24255
110 120 26.77 7.30712 1.02988 9.87673
Minimum 1.221
Actual Length Allowable Length Ring Inertia Ring Inertia

From To Bet. Stiffeners Bet. Stiffeners Required Available
cm cm cm**4 cm**4
10 20 No Calc No Calc No Calc No Calc

20 30 1797.99 2101.06 No Calc No Calc
30 40 1797.99 2134.49 No Calc No Calc
40 50 1797.99 2134.49 No Calc No Calc
50 60 1797.99 2860.83 No Calc No Calc
60 70 1797.99 2132.43 No Calc No Calc
70 80 1797.99 2138.62 No Calc No Calc
80 90 1797.99 2134.49 No Calc No Calc
90 100 1797.99 2132.43 No Calc No Calc
100 110 1797.99 2134.49 No Calc No Calc
110 120 No Calc No Calc No Calc No Calc
Elements Suitable for External Pressure.

PV Elite 2019
Elliptical Head From 10 to 20 Ext. Chart: CS-2 at 33 °C
HEAD 1
Elastic Modulus from Chart: CS-2 at 33 °C : 0.204E+07 kgf/cm²
Results for Maximum Allowable External Pressure (MAEP):

Tca OD D/t Factor A B
26.690 3711.38 139.06 0.0012981 947.45
EMAP = B/(K0*D/t) = 947.4533/( 0.6925 *139.0551 ) = 9.839 kgf/cm²
Results for Required Thickness (Tca):

7.307 3711.38 507.93 0.0003554 362.28
EMAP = B/(K0*D/t) = 362.2838/( 0.6925 *507.9347 ) = 1.03 kgf/cm²
Check the requirements of UG-33(a)(1) using P = 1.67 * External Design

pressure for this head.

= (1.72*3658.0*0.708)/(2*1406.14*1.0-0.2*1.72)
= 1.5848 + 0.0000 = 1.5848 mm

= ((2*S*E*t)/(Kcor*D+0.2*t))/1.67 per Appendix 1-4 (c)
= ((2*1406.14*1.0*26.69)/(0.708*3658.0+0.2*26.69))/1.67
= 17.311 kgf/cm²
Maximum Allowable External Pressure [MAEP]:

= min( MAEP, MAWP )
= min( 9.84, 17.3107 )
= 9.839 kgf/cm²
Thickness requirements per UG-33(a)(1) do not govern the required

thickness of this head.
Cylindrical Shell From 20 to 30 Ext. Chart: CS-2 at 33 °C
SHELL 1

Tca OD SLEN D/t L/D Factor A B
24.600 3707.20 17979.89 150.70 4.8500 0.0001354 138.03
EMAP = (4*B)/(3*(D/t)) = (4*138.0277)/(3*150.6992) = 1.2212 kgf/cm²

22.839 3707.20 17979.89 162.32 4.8500 0.0001230 125.39
EMAP = (4*B)/(3*(D/t)) = (4*125.3851)/(3*162.3197) = 1.0299 kgf/cm²
Results for Maximum Stiffened Length (Slen):

24.600 3707.20 21010.63 150.70 5.6675 0.0001143 116.48
EMAP = (4*B)/(3*(D/t)) = (4*116.4817)/(3*150.6992) = 1.0306 kgf/cm²
SHELL 2
PV Elite 2019

24.780 3707.56 17979.89 149.62 4.8495 0.0001368 139.43
EMAP = (4*B)/(3*(D/t)) = (4*139.4322)/(3*149.619) = 1.2426 kgf/cm²

22.840 3707.56 17979.89 162.33 4.8495 0.0001230 125.39
EMAP = (4*B)/(3*(D/t)) = (4*125.3912)/(3*162.3267) = 1.0299 kgf/cm²

24.780 3707.56 21344.91 149.62 5.7571 0.0001134 115.65
EMAP = (4*B)/(3*(D/t)) = (4*115.6547)/(3*149.619) = 1.0307 kgf/cm²
SHELL 3

24.780 3707.56 17979.89 149.62 4.8495 0.0001368 139.43
EMAP = (4*B)/(3*(D/t)) = (4*139.4322)/(3*149.619) = 1.2426 kgf/cm²

22.840 3707.56 17979.89 162.33 4.8495 0.0001230 125.39
EMAP = (4*B)/(3*(D/t)) = (4*125.3912)/(3*162.3267) = 1.0299 kgf/cm²

24.780 3707.56 21344.91 149.62 5.7571 0.0001134 115.65
EMAP = (4*B)/(3*(D/t)) = (4*115.6547)/(3*149.619) = 1.0307 kgf/cm²
SHELL 4

28.200 3714.40 17979.89 131.72 4.8406 0.0001662 169.44
EMAP = (4*B)/(3*(D/t)) = (4*169.4377)/(3*131.7163) = 1.7152 kgf/cm²

22.863 3714.40 17979.89 162.47 4.8406 0.0001231 125.50
EMAP = (4*B)/(3*(D/t)) = (4*125.4983)/(3*162.466) = 1.0299 kgf/cm²

28.200 3714.40 28608.34 131.72 7.7020 0.0000999 101.83
EMAP = (4*B)/(3*(D/t)) = (4*101.8284)/(3*131.7163) = 1.0308 kgf/cm²
SHELL 5

PV Elite 2019

24.770 3707.54 17979.89 149.68 4.8495 0.0001367 139.34
EMAP = (4*B)/(3*(D/t)) = (4*139.3396)/(3*149.6786) = 1.2412 kgf/cm²

22.840 3707.54 17979.89 162.33 4.8495 0.0001230 125.39
EMAP = (4*B)/(3*(D/t)) = (4*125.3908)/(3*162.3263) = 1.0299 kgf/cm²

24.770 3707.54 21324.25 149.68 5.7516 0.0001135 115.70
EMAP = (4*B)/(3*(D/t)) = (4*115.7004)/(3*149.6786) = 1.0307 kgf/cm²
SHELL 6

24.800 3707.60 17979.89 149.50 4.8495 0.0001370 139.62
EMAP = (4*B)/(3*(D/t)) = (4*139.6172)/(3*149.5) = 1.2452 kgf/cm²

22.840 3707.60 17979.89 162.33 4.8495 0.0001230 125.39
EMAP = (4*B)/(3*(D/t)) = (4*125.3919)/(3*162.3275) = 1.0299 kgf/cm²

24.800 3707.60 21386.21 149.50 5.7682 0.0001134 115.56
EMAP = (4*B)/(3*(D/t)) = (4*115.5637)/(3*149.5) = 1.0307 kgf/cm²
SHELL 7

24.780 3707.56 17979.89 149.62 4.8495 0.0001368 139.43
EMAP = (4*B)/(3*(D/t)) = (4*139.4322)/(3*149.619) = 1.2426 kgf/cm²

22.840 3707.56 17979.89 162.33 4.8495 0.0001230 125.39
EMAP = (4*B)/(3*(D/t)) = (4*125.3912)/(3*162.3267) = 1.0299 kgf/cm²

24.780 3707.56 21344.91 149.62 5.7571 0.0001134 115.65
EMAP = (4*B)/(3*(D/t)) = (4*115.6547)/(3*149.619) = 1.0307 kgf/cm²
SHELL 8

PV Elite 2019
24.770 3707.54 17979.89 149.68 4.8495 0.0001367 139.34

EMAP = (4*B)/(3*(D/t)) = (4*139.3396)/(3*149.6786) = 1.2412 kgf/cm²

22.840 3707.54 17979.89 162.33 4.8495 0.0001230 125.39
EMAP = (4*B)/(3*(D/t)) = (4*125.3908)/(3*162.3263) = 1.0299 kgf/cm²

24.770 3707.54 21324.25 149.68 5.7516 0.0001135 115.70
EMAP = (4*B)/(3*(D/t)) = (4*115.7004)/(3*149.6786) = 1.0307 kgf/cm²
SHELL 9

24.780 3707.56 17979.89 149.62 4.8495 0.0001368 139.43
EMAP = (4*B)/(3*(D/t)) = (4*139.4322)/(3*149.619) = 1.2426 kgf/cm²

22.840 3707.56 17979.89 162.33 4.8495 0.0001230 125.39
EMAP = (4*B)/(3*(D/t)) = (4*125.3912)/(3*162.3267) = 1.0299 kgf/cm²

24.780 3707.56 21344.91 149.62 5.7571 0.0001134 115.65
EMAP = (4*B)/(3*(D/t)) = (4*115.6547)/(3*149.619) = 1.0307 kgf/cm²
Elliptical Head From 110 to 120 Ext. Chart: CS-2 at 33 °C
HEAD 2

26.770 3711.54 138.65 0.0013019 948.28
EMAP = B/(K0*D/t) = 948.2844/( 0.6925 *138.6455 ) = 9.8767 kgf/cm²

7.307 3711.54 507.93 0.0003554 362.28
EMAP = B/(K0*D/t) = 362.2839/( 0.6925 *507.9345 ) = 1.03 kgf/cm²
Check the requirements of UG-33(a)(1) using P = 1.67 * External Design

pressure for this head.

= (1.72*3658.0*0.708)/(2*1406.14*1.0-0.2*1.72)
= 1.5848 + 0.0000 = 1.5848 mm

= ((2*S*E*t)/(Kcor*D+0.2*t))/1.67 per Appendix 1-4 (c)
= ((2*1406.14*1.0*26.77)/(0.708*3658.0+0.2*26.77))/1.67
= 17.363 kgf/cm²
PV Elite 2019
Maximum Allowable External Pressure [MAEP]:

= min( MAEP, MAWP )
= min( 9.88, 17.3625 )
= 9.877 kgf/cm²
Thickness requirements per UG-33(a)(1) do not govern the required

thickness of this head.

PV Elite 2019
Element and Detail Weights: Step: 5 10:40am Aug 29,2023
Element and Detail Weights:
Element Element Corroded Corroded Extra due

From To Metal Wgt. ID Volume Metal Wgt. ID Volume Misc %
kg cm³ kg cm³ kg
10 20 4772.44 10644839 4772.44 10644839 ...

20 30 4109.37 19578984 4109.37 19578984 ...
30 40 4139.64 19578984 4139.64 19578984 ...
40 50 4139.64 19578984 4139.64 19578984 ...
50 60 4715.34 19578984 4715.34 19578984 ...
60 70 4137.96 19578984 4137.96 19578984 ...
70 80 4143.01 19578984 4143.01 19578984 ...
80 90 4139.64 19578984 4139.64 19578984 ...
90 100 4137.96 19578984 4137.96 19578984 ...
100 110 4139.64 19578984 4139.64 19578984 ...
110 120 4786.94 10644839 4786.94 10644839 ...
Total 47361 0.198E+09 47361 0.198E+09 0
Weight of Details:
Weight of X Offset, Y Offset,

From Type Detail Dtl. Cent. Dtl. Cent. Description
kg cm cm
20 Sadl 1719.76 86.3 210.47 Lft Sdl

20 Nozl 15.5957 30 187.98 N1
20 Nozl 20.1386 100 190.52 N2
20 Nozl 20.1785 20 190.52 N18
30 Nozl 21.8286 20 190.52 N3
40 Sadl 1719.76 176.3 210.461 Lft Sdl
50 Nozl 303.319 100 208.3 MH1
50 Nozl 11.8412 40 186.71 N6
60 Nozl 4.35718 40 185.44 N5
60 Nozl 15.8135 80 187.98 N4
60 Nozl 4.49351 40 185.44 N11
60 Nozl 23.4224 80 190.52 N12
60 Nozl 4.35054 120 185.44 N13
60 Forc ... ... ... F/M:[1 of 1]
80 Sadl 1719.76 10 210.461 Lft Sdl
80 Nozl 4.43731 50 185.44 N8
80 Nozl 4.52292 80 185.44 N9
80 Nozl 4.54562 110 185.44 N10
100 Sadl 1809.62 100 215.461 Lft Sdl
100 Nozl 14.8045 160 185.44 N7
110 Nozl 249.884 141.933 ... MH2
Total Weight of Each Detail Type:
Saddles 6968.9
Nozzles 723.5
Sum of the Detail Weights 7692.4 kg
Weight Summation Results: (kg)
Fabricated Shop Test Shipping Erected Empty Operating
Main Elements 47361.6 47361.6 47361.6 47361.6 47361.6 47361.6

Saddles 6968.9 6968.9 6968.9 6968.9 6968.9 6968.9
Nozzles 723.5 723.5 723.5 723.5 723.5 723.5
Test Liquid ... 197411.9 ... ... ... ...
PV Elite 2019
Element and Detail Weights: Step: 5 10:40am Aug 29,2023
Totals 55054.0 252465.9 55054.0 55054.0 55054.0 55054.0
Weight Summary:
Fabricated Wt. - Bare Weight without Removable Internals 55054.0 kg

Shop Test Wt. - Fabricated Weight + Water ( Full ) 252465.9 kg
Shipping Wt. - Fab. Weight + removable Intls.+ Shipping App. 55054.0 kg
Erected Wt. - Fab. Wt + or - loose items (trays,platforms etc.) 55054.0 kg
Ope. Wt. no Liq - Fab. Weight + Internals. + Details + Weights 55054.0 kg
Operating Wt. - Empty Weight + Operating Liq. Uncorroded 55054.0 kg
Oper. Wt. + CA - Corr Wt. + Operating Liquid 55054.0 kg
Field Test Wt. - Empty Weight + Water (Full) 252465.9 kg
Note:
The Corroded Weight and thickness are used in the Horizontal
Vessel Analysis (Ope Case) and Earthquake Load Calculations.
Outside Surface Areas of Elements:
Surface
From To Area
cm²
10 20 193587
20 30 216975
30 40 216996
40 50 216996
50 60 217396
60 70 216994
70 80 216998
80 90 216996
90 100 216994
100 110 216996
110 120 193603
Total 2340529.000 cm²

PV Elite 2019
Nozzle Flange MAWP: Step: 6 10:40am Aug 29,2023
Nozzle Flange MAWP Results:
Nozzle Flange Rating Design Grade/ Equiv. - - - - - - Max Pressure

Description Ope. Ambient Temp Class Group Press PVP 50% DNV
kgf/cm² kgf/cm² °C kgf/cm²
N1 19.27 19.99 60 150 GR 1.1 ... ... ... ...

N2 19.27 19.99 60 150 GR 1.1 ... ... ... ...
N18 19.27 19.99 60 150 GR 1.1 ... ... ... ...
N3 19.27 19.99 60 150 GR 1.1 ... ... ... ...
MH1 19.27 19.99 60 150 GR 1.1 ... ... ... ...
N6 19.27 19.99 60 150 GR 1.1 ... ... ... ...
N5 19.27 19.99 60 150 GR 1.1 ... ... ... ...
N4 19.27 19.99 60 150 GR 1.1 ... ... ... ...
N11 19.27 19.99 60 150 GR 1.1 ... ... ... ...
N12 19.27 19.99 60 150 GR 1.1 ... ... ... ...
N13 19.27 19.99 60 150 GR 1.1 ... ... ... ...
N8 19.27 19.99 60 150 GR 1.1 ... ... ... ...
N9 19.27 19.99 60 150 GR 1.1 ... ... ... ...
N10 19.27 19.99 60 150 GR 1.1 ... ... ... ...
N7 19.27 19.99 60 150 GR 1.1 ... ... ... ...
MH2 19.27 19.99 60 150 GR 1.1 ... ... ... ...
Min Rating 19.273 19.987 kgf/cm² [for Core Elements] 0.000 0.000 0.000
Selected Method for Derating ANSI B16.5 Flange MAWP: None Selected
ANSI Ratings are per ANSI/ASME B16.5 2013 Metric Edition

PV Elite 2019
Wind Load Calculation: Step: 7 10:40am Aug 29,2023
Wind Analysis Results
User Entered Importance Factor is 1.000

Gust Factor (Gh, Gbar) Static Dynamic 1.197
Shape Factor (Cf) for the Vessel is 0.567
User Entered Basic Wind Speed 112.7 km/hr
Exposure Category C
Table Lookup Value Alpha from Table C6 7.0000
Table Lookup Value Zg from Table C6 900.0000
Table Lookup Value Do from Table C6 0.0050
Wind Load Results per ASCE-7 93:
Sample Calculation for the First Element:
Rougness Factor = 1.0
Values [cf1] and [cf2]

Because RoughFact = 1 and DQZ > 2.5 and H/D < 7.0
Interpolating to find the final cf:
Because H / D < 7.0
CF = CF1 + (CF2-CF1)*( H/D - 1) / (7 - 1)
= 0.5 + ( 0.6- 0.5)*( 5.038 - 1)/(7 - 1)
= 0.567
Value of Alpha, Zg is taken from Table C6-2 [Alpha, Zg]

For Exposure Category C:
Alpha = 7.0, Zg = 27432.0 cm
Height of Interest for First Element [z]

= Centroid Hgt + Base Height
= 252.9 + 0.0 = 252.9 cm
but: z = Max(457.2, 252.9) = 457.2 cm
Note: Because z < 15 feet, use 15 feet to compute kz.
Velocity Pressure Coefficient [kZ]:

= 2.58( z/zg )^(2/Alpha) : z is Elevation of First Element
= 2.58( 457.2/900 )^(2/7.0)
= 0.801
Determine if Static or Dynamic Gust Factor Applies
Height to Diameter ratio :

= Maximum Height(length)^2 / Sum of Area of the Elements
= 1841.311(^2)/672938
= 5.038
Vibration Frequency = 33.0 Hz

Because H/D > 5 Or Freqency < 1.0: Dynamic Analysis Implemented
Element O/Dia =3 cm
Vibration Damping Factor (Operating) Beta = 0.01
For Terrain Category C
S = 1.0, Gamma = 0.23, Drag Coeff. = 0.005, Alpha = 7.0
Compute [fbar]
= 10.5 * Frequency(Hz) * Vessel Height(ft) / (S * Vr(mph))
= 10.5 * 33.0(Hz) * 60.41(ft)/S * 1.0(mph)
= 299.032
Because FBAR > 40: FBAR = 40.0

Wind Pressure - (performed in Imperial Units) [qz]
Importance Factor: I = 1.0
PV Elite 2019
Wind Load Calculation: Step: 7 10:40am Aug 29,2023
Wind Speed = 112.651 km/hr Converts to 70.0 mph

qz = 0.00256 * kZ * (I * Vr)²
= 0.00256 * 0.801*(1.0 * 70.0)² = 10.046 psf
Converts to: 49.051 kgf/m²
Force on the First Element [Fz]

= qz * Gh * CF * Wind Area
= 49.051 * 1.197 * 0.567 * 45227.789
= 150.63 kgf
Element z GH Area qz Force

cm cm² kgf/m² kgf
HEAD 1 252.9 1.197 45227.8 49.1 150.6

SHELL 1 252.9 1.197 82878.2 49.1 276.0
SHELL 2 252.9 1.197 82886.2 49.1 276.1
SHELL 3 252.9 1.197 82886.2 49.1 276.1
SHELL 4 252.9 1.197 83039.1 49.1 276.6
SHELL 5 252.9 1.197 82885.8 49.1 276.0
SHELL 6 252.9 1.197 82887.1 49.1 276.1
SHELL 7 252.9 1.197 82886.2 49.1 276.1
SHELL 8 252.9 1.197 82885.8 49.1 276.0
SHELL 9 252.9 1.197 82886.2 49.1 276.1
HEAD 2 252.9 1.197 45232.1 49.1 150.6
Wind Load Calculation:
Wind Wind Wind Wind Element

From To Height Diameter Area Pressure Wind Load
cm cm cm² kgf/m² kgf
10 20 252.9 445.366 45227.8 49.0511 150.63

20 30 252.9 444.864 82878.2 49.0511 276.024
30 40 252.9 444.907 82886.2 49.0511 276.051
40 50 252.9 444.907 82886.2 49.0511 276.051
50 60 252.9 445.728 83039.1 49.0511 276.56
60 70 252.9 444.905 82885.8 49.0511 276.05
70 80 252.9 444.912 82887.1 49.0511 276.054
80 90 252.9 444.907 82886.2 49.0511 276.051
90 100 252.9 444.905 82885.8 49.0511 276.05
100 110 252.9 444.907 82886.2 49.0511 276.051
110 120 252.9 445.385 45232.1 49.0511 150.645

PV Elite 2019
Earthquake Load Calculation: Step: 8 10:40am Aug 29,2023
Earthquake Analysis Results
The UBC Zone Factor for the Vessel is ............. 0.0000

The Importance Factor as Specified by the User is 1.000
The UBC Frequency and Soil Factor (C) is ......... 2.750
The UBC Force Factor as Specified by the User is .. 3.000
The UBC Total Weight (W) for the Vessel is ........ 55054.0 kgf
The UBC Total Shear (V) for the Vessel is ......... 0.0 kgf
The UBC Top Shear (Ft) for the Vessel is .......... 0.0 kgf
Earthquake Load Calculation:
Earthquake Earthquake Element

From To Height Weight Ope Load
cm kgf kgf
10 20 182.9 3670.27 ...

20 30 182.9 3670.27 ...
20 30 182.9 3670.27 ...
30 40 182.9 3670.27 ...
40 0 182.9 3670.27 ...
40 50 182.9 3670.27 ...
50 60 182.9 3670.27 ...
60 70 182.9 3670.27 ...
70 80 182.9 3670.27 ...
80 90 182.9 3670.27 ...
80 90 182.9 3670.27 ...
90 100 182.9 3670.27 ...
100 0 182.9 3670.27 ...
100 110 182.9 3670.27 ...
110 120 182.9 3670.27 ...

PV Elite 2019
Center of Gravity Calculation: Step: 9 10:40am Aug 29,2023
Shop/Field Installation Options :
Note : The CG is computed from the first Element From Node
Center of Gravity of Saddles 868.047 cm

Center of Gravity of Nozzles 1060.021 cm
Center of Gravity of Bare Shell New and Cold 856.831 cm

Center of Gravity of Bare Shell Corroded 856.831 cm
Vessel CG in the Operating Condition 860.921 cm

Vessel CG in the Fabricated (Shop/Empty) Condition 860.921 cm
Vessel CG in the Test Condition 858.911 cm

PV Elite 2019
Horizontal Vessel Analysis (Ope.): Step: 10 10:40am Aug 29,2023
ASME Horizontal Vessel Analysis: Stresses for the Left Saddle

(per ASME Sec. VIII Div. 2 based on the Zick method.)
Horizontal Vessel Stress Calculations : Operating Case
Note: There are more than two saddles present in this model. The load on
the saddle supports has been taken as the total weight divided by the
number of saddles. Insure that this is an appropriate assumption for
this vessel model.
Note:
Wear Pad Width (500.00) is less than 1.56*sqrt(rm*t)
and less than 2a. The wear plate will be ignored.
Minimum Wear Plate Width to be considered in analysis [b1]:

= min( b + 1.56*sqrt( Rm * t ), 2a )
= min( 300.0 + 1.56*sqrt( 1841.2999 * 24.6 ), 2 * 1000.0 )
= 632.0125 mm
Input and Calculated Values:
Vessel Mean Radius Rm 1841.30 mm

Stiffened Vessel Length per 4.15.6 L 1716.70 cm
Distance from Saddle to Vessel tangent a 1000.00 mm
Saddle Width b 300.00 mm

Saddle Bearing Angle theta 135.00 degrees
Inside Depth of Head h2 121.93 cm
Shell Allowable Stress used in Calculation 1406.14 kgf/cm²

Head Allowable Stress used in Calculation 1406.14 kgf/cm²
Circumferential Efficiency in Plane of Saddle 1.00
Circumferential Efficiency at Mid-Span 1.00
Saddle Force Q, Operating Case 16301.40 kgf
Horizontal Vessel Analysis Results: Actual Allowable

kgf/cm² kgf/cm²
Long. Stress at Top of Midspan 542.89 1406.14

Long. Stress at Bottom of Midspan 579.86 1406.14
Long. Stress at Top of Saddles 565.57 1406.14
Long. Stress at Bottom of Saddles 559.00 1406.14
Tangential Shear in Shell 27.84 1124.91

Circ. Stress at Horn of Saddle 78.71 1757.68
Circ. Compressive Stress in Shell 74.53 1406.14
Intermediate Results: Saddle Reaction Q due to Wind or Seismic
Saddle Reaction Force due to Wind Ft [Fwt]:

= Ftr * ( Ft/Num of Saddles + Z Force Load ) * B / E
= 3.0 * ( 2786.2/4 + 0 ) * 2429.0/2000.0
= 2537.9 kgf
Saddle Reaction Force due to Wind Fl or Friction [Fwl]:

= max( Fl, Friction Load, Sum of X Forces) * B / Ls
= max( 635.35, 0.0, 0 ) * 2429.0/15804.001
= 97.6 kgf
Load Combination Results for Q + Wind or Seismic [Q]:

= Saddle Load + Max( Fwl, Fwt, Fsl, Fst )
PV Elite 2019
= 13764 + Max( 98, 2538, 0, 0 )

= 16301.4 kgf
Summary of Loads at the base of this Saddle:

Vertical Load (including saddle weight) 18021.16 kgf
Transverse Shear Load Saddle Ft 696.55 kgf
Longitudinal Shear Load Saddle 635.35 kgf
Formulas and Substitutions for Horizontal Vessel Analysis:
Note: Wear Plate is not Welded to the Shell, k = 1.0
The Computed K values from Table 4.15.1:

K1 = 0.1320 K2 = 0.9584 K3 = 0.6538 K4 = 0.3439
K5 = 0.7108 K6 = 0.0413 K7 = 0.0130 K8 = 0.3234
K9 = 0.2463 K10 = 0.0471 K1* = 0.2339
Note: Dimension a is greater than or equal to Rm / 2.
Moment per Equation 4.15.3 [M1]:

= -Q*a [1 - (1- a/L + (R²-h2²)/(2a*L))/(1+(4h2)/3L)]
= -16301*100.0[1-(1-100.0/1716.7+(184.13²-121.933²)/
(2*100.0*1716.7))/(1+(4*121.93)/(3*1716.7))]
= -1452.1 kgf-m.

= Q*L/4(1+2(R²-h2²)/(L²))/(1+(4h2)/( 3L))-4a/L
= 16301*1717/4(1+2(184²-122²)/(1717²))/(1+(4*122)/
(3*1717))-4*100/1717
= 48433.4 kgf-m.
Longitudinal Stress at Top of Shell (4.15.6) [Sigma1]:

= P * Rm/(2t) - M2/(pi*Rm²t)
= 15.0 * 1841.3/(2*24.6) - 48433.4/(pi*1841.3²*24.6)
= 542.89 kgf/cm²
Longitudinal Stress at Bottom of Shell (4.15.7) [Sigma2]:

= P * Rm/(2t) + M2/(pi * Rm² * t)
= 15.0 * 1841.3/(2 * 24.6) + 48433.4/(pi * 1841.3² * 24.6 )
= 579.86 kgf/cm²
Longitudinal Stress at Top of Shell at Support (4.15.10) [Sigma*3]:

= P * Rm/(2t) - M1/(K1*pi*Rm²t)
= 15.0*1841.3/(2*24.6)--1452.1/(0.132*pi*1841.3²*24.6)
= 565.57 kgf/cm²
Longitudinal Stress at Bottom of Shell at Support (4.15.11) [Sigma*4]:

= P * Rm/(2t) + M1/(K1* * pi * Rm² * t)
= 15.0*1841.3/(2*24.6)+-1452.1/(0.2339*pi*1841.3²*24.6)
= 559.00 kgf/cm²
Maximum Shear Force in the Saddle (4.15.5) [T]:

= Q(L-2a)/(L+(4*h2/3))
= 16301( 1716.7 - 2 * 100.0)/(1716.7 + ( 4 * 121.93/3))
= 13156.3 kgf
Shear Stress in the shell no rings, not stiffened (4.15.14) [tau2]:

= K2 * T / ( Rm * t )
= 0.9584 * 13156.29/( 1841.2999 * 24.6 )
= 27.84 kgf/cm²
Decay Length (4.15.22) [x1,x2]:

= 0.78 * sqrt( Rm * t )
= 0.78 * sqrt( 1841.3 * 24.6 )
= 166.006 mm
PV Elite 2019
Circumferential Stress in shell, no rings (4.15.23) [sigma6]:

= -K5 * Q * k / ( t * ( b + X1 + X2 ) )
= - 0.7108 * 16301 * 1.0/( 24.6 * ( 300.0 + 166.01 + 166.01 ) )
= -74.53 kgf/cm²
Circ. Comp. Stress at Horn of Saddle, L>=8Rm (4.15.24) [sigma7]:

= -Q/(4*t*(b+X1+X2)) - 3*K7*Q/(2*t²)
= -16301/(4*24.6*(300.0+166.006+166.006)) -
3* 0.013*16301/(2*24.6²)
= -78.71 kgf/cm²
Effective reinforcing plate width (4.15.1) [B1]:

= min( b + 1.56 * sqrt( Rm * t ), 2a )
= min( 300.0 + 1.56 * sqrt( 1841.3 * 24.6 ), 2 * 100.0 )
= 632.01 mm
Results for Vessel Ribs, Web and Base:

Baseplate Length Bplen 2989.9900 mm
Baseplate Thickness Bpthk 22.0000 mm
Baseplate Width Bpwid 380.0000 mm
Number of Ribs ( inc. outside ribs ) Nribs 6
Rib Thickness Ribtk 22.0000 mm
Web Thickness Webtk 22.0000 mm
Web Location Webloc Center
Saddle Yield Stress Sy 2446.7 kgf
Height of Web at Center Hw,c 250.0 mm
Friction Coefficient mu 0.000
Note: In the tables below Io is I for the rectangle + Area * Centroid Distance^2
Moment of Inertia of Saddle - Transverse Direction (90 degrees to long axis)
B D Y A AY Io
Shell 830.9 24.6 12.3 204.4 251414.2 0.553E+05

Wearplate 500.0 24.0 36.6 120.0 439200.0 0.236E+05
Web 22.0 529.4 313.3 116.5 3648940.5 0.490E+05
BasePlate 380.0 22.0 589.0 83.6 4924038.0 0.142E+06
Totals ... ... ... 524.5 9263593.0 0.270E+06
Distance to Centroid [C1]:

= AY / A
= 3647.084/524.47
= 176.628 mm
Angle [beta]:
= 180 - Saddle Angle/2
= 180 - 135.0/2
= 112.5
Saddle Splitting Coefficient [K1]:

= ( 1 + cos(beta) - 0.5*sin(beta)² )/(pi - beta + sin(beta)cos(beta) )
= ( 1 + cos(112.5) - 0.5*sin(112.5)² )/(pi - 1.963 + sin(112.5)cos(112.5) )
= 0.2311
Saddle Splitting Force [Fh]:

= K1 * Q
= 0.231 * 16301.398
= 3767.0107 kgf
Tension Stress, St = ( Fh/As ) = 11.7694 kgf/cm²

Allowed Stress, Sa = 0.6 * Yield Str = 1468.0079 kgf/cm²
Saddle Splitting Dimension [d]:

PV Elite 2019
= B - R * sin( theta )/ theta

= 2429.0 - 1829.0 * sin( 1.1781 )/1.1781
= 994.674 mm
Bending Moment, M = Fh * d = 3746.9517 kgf-m.
Bending Stress, Sb = ( M * C1 / I ) = 24.5082 kgf/cm²

Allowed Stress, Sa = 2/3 * Yield Str = 1631.1200 kgf/cm²
Minimum Thickness of Baseplate per Moss:

= ( 3( Q + Saddle_Wt )BasePlateWidth / ( 4 * BasePlateLength * AllStress ))½
= ( 3(16301 + 1720)380.0/( 4 * 2989.99 * 1631.12 ))½
= 10.262 mm
Calculation of Axial Load, Intermediate Values and Compressive Stress:
Web Length Dimension [ Web Length ]:

= 2 * cos( 90 - Saddle Angle/2 )( Inside Radius + Shell Thk + Wear Plate Thk )
= 2 * cos( 90 - 135.0/2 )( 1829.0 + 24.6 + 24.0 )
= 3469.353 mm
Distance between Ribs [e]:

= Web Length / ( Nribs - 1 )
= 3469.3525/( 6 - 1 )
= 693.871 mm
Baseplate Pressure Area [Ap]:

= e * Bpwid / 2
= 693.8705 * 380.0/2
= 1318.354 cm²
Axial Load [P]:

= Ap * Bp
= 1318.4 * 1.43
= 1891.488 kgf
Area of the Rib and Web [Ar]:

= Rib Area + Web Area
= 61.16 + 76.326
= 137.486 cm²
Compressive Stress [Sc]:

= P/Ar
= 1891.5/137.4858
= 13.758 kgf/cm²
Check of Outside Ribs:
Inertia of Saddle, Outer Ribs - Longitudinal Direction
B D Y A AY Io
Rib+Web 22.0 300.0 ... 66.0 ... 0.495E+04
Rib dimension [D]:

= Saddle Width - Web Thickness
= 300.0 - 22.0
= 278.000 mm
Distance to Centroid from Datum [ytot]:

= AY / A
= 0.0/137.486
= 0.000 mm

PV Elite 2019
= Saddle Width / 2
= 300.0/2
= 150.000 mm
Radius of Gyration [r]:

= sqrt( Total Inertia / Total Area )
= sqrt( 4950.0/137.486 )
= 60.003 mm
Intermediate Term [Cc]:

= sqrt( 2 * pi² * Elastic Modulus / Yield Stress )
= sqrt( 2 * pi² * 2038900/2446.7 )
= 128.255
Slenderness ratio [KL/r]:

= KL/r
= 1 * 712.686/60.003
= 11.877
Bending Moment [Rm]:

= Fl /( 2 * Bplen ) * e * L / 2
= 635.3/( 2 * 2989.99 ) * 693.871 * 712.69/2
= 26.270 kgf-m.
Compressive Allowable, KL/r < Cc ( 11.8775 < 128.255 ) per AISC E2-1 [Sca]:
= ( 1-(Klr)²/(2*Cc²))Fy/(5/3+3*(Klr)/(8*Cc)-(Klr³)/(8*Cc³)
= ( 1-( 11.88 )²/(2 * 128.25² ))2447/
( 5/3+3*(11.88)/(8* 128.25)-( 11.88³)/(8*128.25³)
= 1432 kgf/cm²
AISC Unity Check of Outside Ribs ( must be <= 1 )

= Sc/Sca + ( Rm * C1 / I )/Sba
= 13.76/1431.96 + ( 26.27 * 150.0/49499996 )/1631.12
= 0.014
Check of Inside Ribs:
Inertia of Saddle, Inner Ribs - Axial Direction

B D Y A AY Io
Rib 22.0 278.0 0.0 61.2 0.0 0.495E+04

Web 693.9 22.0 0.0 152.7 0.0 61.6
Totals ... ... ... 213.8 ... 0.501E+04

= AY / A
= 0.0/213.812
= 0.000 mm

= Saddle Width / 2
= 300.0/2
= 150.000 mm
Length of Inner Rib [L]:

= Saddle Height - sqrt( (Ro + Wpdthk)^2 - (Pitch/2)^2 ) - Bpthk
= 2429.0 - sqrt( (1877.6 + 24.0)^2 - (693.871/2)^2 ) - 22.0
= 561.731 mm

= sqrt( 5009.6/213.812 )
= 48.405 mm

PV Elite 2019
= KL/r
= 1 * 561.731/48.405
= 11.605
Unit Force [Force,u]:

= Fl / ( 2 * Baseplate Length )
= 635.347/( 2 * 2989.99 )
= 0.106 kgf/mm
Moment at base of inner Rib [Mbase,c]:

= Unit Force * e * L
= 0.106 * 693.871 * 561.731
= 41.411 kgf-m.
Bending Stress due to Transverse Force and Weight Load [SigmaB,base,c]:

= Bending Moment / Section Modulus
= 41.411/333974.438
= 12.400 kgf/cm²
= ( 1-( 11.6 )²/(2 * 128.25² ))2447/
( 5/3+3*(11.6)/(8* 128.25)-( 11.6³)/(8*128.25³)
= 1433 kgf/cm²
AISC Unity Check of Inside Ribs ( must be <= 1 )

= Sc/Sca + ( Mbase,c * C1/I )/Sba
= 16.75/1432.91 + ( 41.41 * 150.0/5009.617 )/1631.12
= 0.019
ASME Horizontal Vessel Analysis: Stresses for the Right Saddle

(per ASME Sec. VIII Div. 2 based on the Zick method.)
Note:
Wear Pad Width (500.00) is less than 1.56*sqrt(rm*t)
and less than 2a. The wear plate will be ignored.
Minimum Wear Plate Width to be considered in analysis [b1]:

= min( b + 1.56*sqrt( Rm * t ), 2a )
= min( 300.0 + 1.56*sqrt( 1841.3899 * 24.78 ), 2 * 1000.0 )
= 633.2331 mm
Input and Calculated Values:
Vessel Mean Radius Rm 1841.39 mm

Stiffened Vessel Length per 4.15.6 L 1716.70 cm
Distance from Saddle to Vessel tangent a 1000.00 mm
Saddle Width b 300.00 mm

Saddle Bearing Angle theta 135.00 degrees
Inside Depth of Head h2 121.93 cm
Shell Allowable Stress used in Calculation 1406.14 kgf/cm²

Head Allowable Stress used in Calculation 1406.14 kgf/cm²
Circumferential Efficiency in Plane of Saddle 1.00
Circumferential Efficiency at Mid-Span 1.00
Saddle Force Q, Operating Case 16405.88 kgf
Horizontal Vessel Analysis Results: Actual Allowable

kgf/cm² kgf/cm²
Long. Stress at Top of Midspan 542.80 1406.14

Long. Stress at Bottom of Midspan 580.00 1406.14
PV Elite 2019
Long. Stress at Top of Saddles 561.52 1406.14

Long. Stress at Bottom of Saddles 554.95 1406.14
Tangential Shear in Shell 27.81 1124.91

Circ. Stress at Horn of Saddle 78.20 1757.68
Circ. Compressive Stress in Shell 74.32 1406.14
Intermediate Results: Saddle Reaction Q due to Wind or Seismic
Saddle Reaction Force due to Wind Ft [Fwt]:

= Ftr * ( Ft/Num of Saddles + Z Force Load ) * B / E
= 3.0 * ( 2786.2/4 + 0 ) * 2529.0/2000.0
= 2642.4 kgf
Saddle Reaction Force due to Wind Fl or Friction [Fwl]:

= max( Fl, Friction Load, Sum of X Forces) * B / Ls
= max( 635.47, 0.0, 0 ) * 2529.0/15804.001
= 101.7 kgf
Load Combination Results for Q + Wind or Seismic [Q]:

= Saddle Load + Max( Fwl, Fwt, Fsl, Fst )
= 13764 + Max( 102, 2642, 0, 0 )
= 16405.9 kgf
Summary of Loads at the base of this Saddle:

Vertical Load (including saddle weight) 18215.50 kgf
Transverse Shear Load Saddle Ft 696.55 kgf
Longitudinal Shear Load Saddle 635.47 kgf
Formulas and Substitutions for Horizontal Vessel Analysis:
Note: Wear Plate is not Welded to the Shell, k = 1.0
The Computed K values from Table 4.15.1:

K1 = 0.1320 K2 = 0.9584 K3 = 0.6538 K4 = 0.3439
K5 = 0.7108 K6 = 0.0413 K7 = 0.0130 K8 = 0.3234
K9 = 0.2463 K10 = 0.0471 K1* = 0.2339
Note: Dimension a is greater than or equal to Rm / 2.

= -Q*a [1 - (1- a/L + (R²-h2²)/(2a*L))/(1+(4h2)/3L)]
= -16406*100.0[1-(1-100.0/1716.7+(184.139²-121.933²)/
(2*100.0*1716.7))/(1+(4*121.93)/(3*1716.7))]
= -1461.2 kgf-m.

= Q*L/4(1+2(R²-h2²)/(L²))/(1+(4h2)/( 3L))-4a/L
= 16406*1717/4(1+2(184²-122²)/(1717²))/(1+(4*122)/
(3*1717))-4*100/1717
= 48744.0 kgf-m.
Longitudinal Stress at Top of Shell (4.15.6) [Sigma1]:

= P * Rm/(2t) - M2/(pi*Rm²t)
= 15.0 * 1841.39/(2*24.6) - 48744.0/(pi*1841.4²*24.6)
= 542.80 kgf/cm²
Longitudinal Stress at Bottom of Shell (4.15.7) [Sigma2]:

= P * Rm/(2t) + M2/(pi * Rm² * t)
= 15.0 * 1841.39/(2 * 24.6) + 48744.0/(pi * 1841.4² * 24.6 )
= 580.00 kgf/cm²
Longitudinal Stress at Top of Shell at Support (4.15.10) [Sigma*3]:

= P * Rm/(2t) - M1/(K1*pi*Rm²t)
PV Elite 2019
= 15.0*1841.39/(2*24.78)--1461.2/(0.132*pi*1841.4²*24.78)
= 561.52 kgf/cm²
Longitudinal Stress at Bottom of Shell at Support (4.15.11) [Sigma*4]:

= P * Rm/(2t) + M1/(K1* * pi * Rm² * t)
= 15.0*1841.39/(2*24.78)+-1461.2/(0.2339*pi*1841.4²*24.78)
= 554.95 kgf/cm²
Maximum Shear Force in the Saddle (4.15.5) [T]:

= Q(L-2a)/(L+(4*h2/3))
= 16406( 1716.7 - 2 * 100.0)/(1716.7 + ( 4 * 121.93/3))
= 13240.6 kgf
Shear Stress in the shell no rings, not stiffened (4.15.14) [tau2]:

= K2 * T / ( Rm * t )
= 0.9584 * 13240.62/( 1841.3899 * 24.78 )
= 27.81 kgf/cm²
Decay Length (4.15.22) [x1,x2]:

= 0.78 * sqrt( Rm * t )
= 0.78 * sqrt( 1841.39 * 24.78 )
= 166.617 mm
Circumferential Stress in shell, no rings (4.15.23) [sigma6]:

= -K5 * Q * k / ( t * ( b + X1 + X2 ) )
= - 0.7108 * 16406 * 1.0/( 24.78 * ( 300.0 + 166.62 + 166.62 ) )
= -74.32 kgf/cm²
Circ. Comp. Stress at Horn of Saddle, L>=8Rm (4.15.24) [sigma7]:

= -Q/(4*t*(b+X1+X2)) - 3*K7*Q/(2*t²)
= -16406/(4*24.78*(300.0+166.617+166.617)) -
3* 0.013*16406/(2*24.78²)
= -78.20 kgf/cm²
Effective reinforcing plate width (4.15.1) [B1]:

= min( b + 1.56 * sqrt( Rm * t ), 2a )
= min( 300.0 + 1.56 * sqrt( 1841.39 * 24.78 ), 2 * 100.0 )
= 633.23 mm
Results for Vessel Ribs, Web and Base:
Baseplate Length Bplen 2989.9900 mm

Baseplate Thickness Bpthk 22.0000 mm
Baseplate Width Bpwid 380.0000 mm
Number of Ribs ( inc. outside ribs ) Nribs 6
Rib Thickness Ribtk 22.0000 mm
Web Thickness Webtk 22.0000 mm
Web Location Webloc Center
Saddle Yield Stress Sy 2446.7 kgf
Height of Web at Center Hw,c 250.0 mm
Friction Coefficient mu 0.000
Note: In the tables below Io is I for the rectangle + Area * Centroid Distance^2
Moment of Inertia of Saddle - Transverse Direction (90 degrees to long axis)
B D Y A AY Io
Shell 832.1 24.8 12.4 206.2 255477.9 0.802E+05

Wearplate 500.0 24.0 36.8 120.0 441360.0 0.359E+05
Web 22.0 629.2 363.4 138.4 5030347.5 0.784E+05
BasePlate 380.0 22.0 689.0 83.6 5760039.0 0.192E+06
Totals ... ... ... 548.2 11487225.0 0.387E+06

PV Elite 2019
= AY / A
= 4522.53/548.225
= 209.535 mm
Angle [beta]:
= 180 - Saddle Angle/2
= 180 - 135.0/2
= 112.5
Saddle Splitting Coefficient [K1]:

= ( 1 + cos(beta) - 0.5*sin(beta)² )/(pi - beta + sin(beta)cos(beta) )
= ( 1 + cos(112.5) - 0.5*sin(112.5)² )/(pi - 1.963 + sin(112.5)cos(112.5) )
= 0.2311
Saddle Splitting Force [Fh]:

= K1 * Q
= 0.231 * 16405.883
= 3791.1555 kgf
Tension Stress, St = ( Fh/As ) = 11.0843 kgf/cm²

Allowed Stress, Sa = 0.6 * Yield Str = 1468.0079 kgf/cm²
Saddle Splitting Dimension [d]:

= B - R * sin( theta )/ theta
= 2529.0 - 1829.0 * sin( 1.1781 )/1.1781
= 1094.674 mm
Bending Moment, M = Fh * d = 4150.0845 kgf-m.
Bending Stress, Sb = ( M * C1 / I ) = 22.4830 kgf/cm²

Allowed Stress, Sa = 2/3 * Yield Str = 1631.1200 kgf/cm²
Minimum Thickness of Baseplate per Moss:

= ( 3( Q + Saddle_Wt )BasePlateWidth / ( 4 * BasePlateLength * AllStress ))½
= ( 3(16406 + 1810)380.0/( 4 * 2989.99 * 1631.12 ))½
= 10.317 mm
Calculation of Axial Load, Intermediate Values and Compressive Stress:
Web Length Dimension [ Web Length ]:

= 2 * cos( 90 - Saddle Angle/2 )( Inside Radius + Shell Thk + Wear Plate Thk )
= 2 * cos( 90 - 135.0/2 )( 1829.0 + 24.78 + 24.0 )
= 3469.685 mm
Distance between Ribs [e]:

= Web Length / ( Nribs - 1 )
= 3469.6851/( 6 - 1 )
= 693.937 mm
Baseplate Pressure Area [Ap]:

= e * Bpwid / 2
= 693.937 * 380.0/2
= 1318.480 cm²
Axial Load [P]:

= Ap * Bp
= 1318.5 * 1.44
= 1903.794 kgf
Area of the Rib and Web [Ar]:

= Rib Area + Web Area
= 61.16 + 76.333
= 137.493 cm²
Compressive Stress [Sc]:

PV Elite 2019
= P/Ar
= 1903.8/137.4931
= 13.846 kgf/cm²
Check of Outside Ribs:
Inertia of Saddle, Outer Ribs - Longitudinal Direction
B D Y A AY Io
Rib+Web 22.0 300.0 ... 66.0 ... 0.495E+04
Rib dimension [D]:

= Saddle Width - Web Thickness
= 300.0 - 22.0
= 278.000 mm

= AY / A
= 0.0/137.493
= 0.000 mm

= Saddle Width / 2
= 300.0/2
= 150.000 mm

= sqrt( 4950.0/137.493 )
= 60.002 mm
Intermediate Term [Cc]:

= sqrt( 2 * pi² * Elastic Modulus / Yield Stress )
= sqrt( 2 * pi² * 2038900/2446.7 )
= 128.255

= KL/r
= 1 * 621.207/60.002
= 10.353
Bending Moment [Rm]:

= Fl /( 2 * Bplen ) * e * L / 2
= 635.5/( 2 * 2989.99 ) * 693.937 * 621.21/2
= 22.905 kgf-m.
= ( 1-( 10.35 )²/(2 * 128.25² ))2447/
( 5/3+3*(10.35)/(8* 128.25)-( 10.35³)/(8*128.25³)
= 1437 kgf/cm²
AISC Unity Check of Outside Ribs ( must be <= 1 )

= Sc/Sca + ( Rm * C1 / I )/Sba
= 13.85/1437.18 + ( 22.9 * 150.0/49499996 )/1631.12
= 0.014
Check of Inside Ribs:
Inertia of Saddle, Inner Ribs - Axial Direction

B D Y A AY Io
Rib 22.0 278.0 0.0 61.2 0.0 0.495E+04

Web 693.9 22.0 0.0 152.7 0.0 61.6
PV Elite 2019
Totals ... ... ... 213.8 ... 0.501E+04

= AY / A
= 0.0/213.826
= 0.000 mm

= Saddle Width / 2
= 300.0/2
= 150.000 mm
Length of Inner Rib [L]:

= Saddle Height - sqrt( (Ro + Wpdthk)^2 - (Pitch/2)^2 ) - Bpthk
= 2529.0 - sqrt( (1877.78 + 24.0)^2 - (693.937/2)^2 ) - 22.0
= 661.554 mm

= sqrt( 5009.6/213.826 )
= 48.403 mm

= KL/r
= 1 * 661.554/48.403
= 13.668
Unit Force [Force,u]:

= Fl / ( 2 * Baseplate Length )
= 635.471/( 2 * 2989.99 )
= 0.106 kgf/mm
Moment at base of inner Rib [Mbase,c]:

= Unit Force * e * L
= 0.106 * 693.937 * 661.554
= 48.784 kgf-m.
Bending Stress due to Transverse Force and Weight Load [SigmaB,base,c]:

= Bending Moment / Section Modulus
= 48.784/333974.844
= 14.607 kgf/cm²
= ( 1-( 13.67 )²/(2 * 128.25² ))2447/
( 5/3+3*(13.67)/(8* 128.25)-( 13.67³)/(8*128.25³)
= 1426 kgf/cm²
AISC Unity Check of Inside Ribs ( must be <= 1 )

= Sc/Sca + ( Mbase,c * C1/I )/Sba
= 16.86/1425.62 + ( 48.78 * 150.0/5009.623 )/1631.12
= 0.021

PV Elite 2019
Nozzle Summary: Step: 28 10:40am Aug 29,2023
Nozzle Calculation Summary:
Description MAWP Ext MAPNC UG-45 [tr] Weld Areas or

kgf/cm² kgf/cm² mm Path Stresses
N1 18.76 OK ... OK 5.26 OK Passed

N2 15.22 OK ... OK 6.22 OK Passed
N18 15.23 OK ... OK 6.22 OK Passed
N3 16.82 OK ... OK 6.22 OK Passed
MH1 16.55 OK ... ... OK Passed
N6 20.63 OK ... OK 4.80 OK Passed
N5 18.89 ... ... OK 4.52 OK No Calc[*]
N4 18.89 OK ... OK 5.26 OK Passed
N11 18.89 ... ... OK 4.52 OK No Calc[*]
N12 18.13 OK ... OK 6.22 OK Passed
N13 18.89 ... ... OK 4.52 OK No Calc[*]
N8 18.90 ... ... OK 4.52 OK No Calc[*]
N9 18.90 ... ... OK 4.52 OK No Calc[*]
N10 18.90 ... ... OK 4.52 OK No Calc[*]
N7 18.90 ... ... OK 4.52 OK No Calc[*]
MH2 19.24 OK ... ... OK Passed
MAWP Summary:
Minimum MAWP Nozzles : 15.218 Nozzle : N2
Minimum MAWP Shells/Flanges : 18.761 Element : SHELL 1
Minimum MAPnc Shells/Flanges : 18.761 Element : SHELL 1
Computed Vessel M.A.W.P. : 15.218 kgf/cm²
[*] - This was a small opening and the areas were not computed.
Note: MAWPs (Internal Case) shown above are at the High Point.
Warning: A Nozzle Reinforcement is governing the MAWP of this Vessel.
Check the Spatial Relationship between the Nozzles
From Node Nozzle Description X Coordinate Layout Angle Dia. Limit

mm deg mm
20 N1 500.000 90.000 203.200

20 N2 1200.000 90.000 304.800
20 N18 400.000 270.000 304.800
30 N3 2263.000 90.000 304.800
50 MH1 6789.000 90.000 1016.000
50 N6 6189.000 90.000 152.400
60 N5 8052.000 90.000 110.120
60 N4 8452.000 90.000 203.200
60 N11 8052.000 270.000 111.340
60 N12 8452.000 270.000 304.800
60 N13 8852.001 270.000 110.060
80 N8 11878.000 270.000 110.860
80 N9 12178.001 270.000 111.620
80 N10 12478.001 270.000 111.820
100 N7 16704.000 270.000 110.100
110 MH2 0.000 0.000 1016.000
The nozzle spacing is computed by the following:

= Sqrt( ll² + lc² ) where
ll - Arc length along the inside vessel surface in the long. direction.
lc - Arc length along the inside vessel surface in the circ. direction
PV Elite 2019
Nozzle Summary: Step: 28 10:40am Aug 29,2023
If any interferences/violations are found, they will be noted below.

No interference violations have been detected !

PV Elite 2019
Nozzle Calcs.: N1 Nozl: 17 10:40am Aug 29,2023
Input, Nozzle Desc: N1 From: 20
Pressure for Reinforcement Calculations P 15.000 kgf/cm²

Temperature for Internal Pressure Temp 60 °C
Design External Pressure Pext 1.03 kgf/cm²
Temperature for External Pressure Tempex 33 °C
Shell Material [Impact Tested] SA-516 70

Shell Allowable Stress at Temperature Sv 1406.14 kgf/cm²
Shell Allowable Stress At Ambient Sva 1406.14 kgf/cm²
Inside Diameter of Cylindrical Shell D 3658.00 mm

Design Length of Section L 17979.8906 mm
Shell Finished (Minimum) Thickness t 24.6000 mm
Shell Internal Corrosion Allowance c 0.0000 mm
Shell External Corrosion Allowance co 0.0000 mm
Distance from Bottom/Left Tangent 50.00 cm
User Entered Minimum Design Metal Temperature -8.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-106 B
Material UNS Number K03006
Material Specification/Type Smls. pipe
Allowable Stress at Temperature Sn 1202.25 kgf/cm²
Allowable Stress At Ambient Sna 1202.25 kgf/cm²
Diameter Basis (for tr calc only) ID

Layout Angle 90.00 deg
Diameter 4.0000 in.
Size and Thickness Basis Actual

Actual Thickness tn 5.6200 mm
Flange Material SA-105

Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm

Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 150.0000 mm

Weld leg size between Nozzle and Pad/Shell Wo 10.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 24.6000 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
Pad Material SA-516 70

Pad Allowable Stress at Temperature Sp 1406.14 kgf/cm²
Pad Allowable Stress At Ambient Spa 1406.14 kgf/cm²
Diameter of Pad along vessel surface Dp 216.0000 mm
Thickness of Pad te 24.8300 mm
Weld leg size between Pad and Shell Wp 20.0000 mm
Groove weld depth between Pad and Nozzle Wgpn 24.8300 mm
Reinforcing Pad Width 51.5800 mm
Class of attached Flange 150

Grade of attached Flange GR 1.1
The Pressure Design option was Design Pressure + static head.
Nozzle Sketch (may not represent actual weld type/configuration)

PV Elite 2019
Insert/Set-in Nozzle With Pad, no Inside projection
Reinforcement CALCULATION, Description: N1
ASME Code, Section VIII, Div. 1, 2017, UG-37 to UG-45
Actual Inside Diameter Used in Calculation 4.000 in.

Actual Thickness Used in Calculation 0.221 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a) of Cylindrical Shell, Tr [Int. Press]

= (P*R)/(Sv*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406*1.0-0.6*15.0)
= 19.6365 mm
Reqd thk per UG-37(a) of Nozzle Wall, Trn [Int. Press]

= (P*R)/(Sn*E-0.6*P) per UG-27 (c)(1)
= (15.0*50.8)/(1202*1.0-0.6*15.0)
= 0.6386 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.4034 mm
UG-40, Limits of Reinforcement : [Internal Pressure]

Parallel to Vessel Wall (Diameter Limit) Dl 203.2000 mm
Parallel to Vessel Wall, opening length d 101.6000 mm
Normal to Vessel Wall (Thickness Limit), pad side Tlwp 38.8800 mm
Note: The Pad diameter is greater than the Diameter Limit. The excess will not be considered.
Weld Strength Reduction Factor [fr1]:

= min( 1, Sn/Sv )
= min( 1, 1202.2/1406.1 )
= 0.855

= min( 1, Sn/Sv )
= min( 1, 1202.2/1406.1 )
= 0.855

= min( 1, Sp/Sv )
= min( 1, 1406.1/1406.1 )
= 1.000

= min( fr2, fr4 )
= min( 0.855, 1.0 )
= 0.855
Results of Nozzle Reinforcement Area Calculations: (cm²)

PV Elite 2019
AREA AVAILABLE, A1 to A5 Design External Mapnc
Area Required Ar 20.271 11.788 NA

Area in Shell A1 4.962 1.761 NA
Area in Nozzle Wall A2 3.312 3.468 NA
Area in Inward Nozzle A3 0.000 0.000 NA
Area in Welds A41+A42+A43 0.855 0.855 NA
Area in Element A5 22.436 22.436 NA
TOTAL AREA AVAILABLE Atot 31.565 28.520 NA
The Internal Pressure Case Governs the Analysis.
Nozzle Angle Used in Area Calculations 90.00 Degs.
The area available without a pad is Insufficient.

The area available with the given pad is Sufficient.
SELECTION OF POSSIBLE REINFORCING PADS: Diameter Thickness

Based on given Pad Thickness: 157.7128 24.8300 mm
Based on given Pad Diameter: 216.0000 12.3306 mm
Based on the Estimated Diameter Limit: 201.6125 12.5511 mm
Area Required [A]:

= ( d * tr*F + 2 * tn * tr*F * (1-fr1) ) UG-37(c)
= (101.6*19.6365*1.0+2*5.62*19.6365*1.0*(1-0.86))
= 20.271 cm²
Reinforcement Areas per Figure UG-37.1
Area Available in Shell [A1]:

= d( E1*t - F*tr ) - 2 * tn( E1*t - F*tr ) * ( 1 - fr1 )
= 101.6( 1.0 * 24.6 - 1.0 * 19.637 ) - 2 * 5.62
( 1.0 * 24.6 - 1.0 * 19.6365 ) * ( 1 - 0.855 )
= 4.962 cm²
Area Available in Nozzle Wall Projecting Outward [A2]:

= ( 2 * Tlwp ) * ( tn - trn ) * fr2
= ( 2 * 38.88 ) * ( 5.62 - 0.64 ) * 0.855
= 3.312 cm²
Area Available in Welds [A41 + A42 + A43]:

= Wo² * fr3 + (Wi-can/0.707)² * fr2 + Wp² * fr4
= 10.0² * 0.86 + (0.0)² * 0.86 + 0.0² * 1.0
= 0.855 cm²
Area Available in Element [A5]:

= (min(Dp,DL)-(Nozzle OD))*(min(tp,Tlwp,te)) * fr4
= ( 203.2 - 112.84 ) * 24.83 * 1.0
= 22.436 cm²
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]

Wall Thickness for Internal/External pressures ta = 0.6386 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 19.6365 mm
Wall Thickness tb1 = max(trb1, tr16b) = 19.6365 mm
Wall Thickness, shell/head, external pressure trb2 = 1.3402 mm
Wall Thickness per table UG-45 tb3 = 5.2578 mm
Determine Nozzle Thickness candidate [tb]:

= min[ tb3, max( tb1,tb2) ]
= min[ 5.258, max( 19.6365, 1.5 ) ]
= 5.2578 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:

PV Elite 2019
= max( ta, tb )
= max( 0.6386, 5.2578 )
= 5.2578 mm
Available Nozzle Neck Thickness = 5.6200 mm --> OK
Nozzle Junction Minimum Design Metal Temperature (MDMT) Calculations:
Nozzle Neck to Flange Weld, Curve: B
Govrn. thk, tg = 5.62, tr = 0.639, c = 0.0 mm, E* = 1.0

Thickness Ratio = tr * (E*)/(tg - c) = 0.114, Temp. Reduction = 78 °C
Min Metal Temp. w/o impact per UCS-66, Curve B -29 °C

Min Metal Temp. at Required thickness (UCS 66.1) -104 °C
Nozzle Neck to Pad Weld for the Nozzle, Curve: B


Nozzle Neck to Pad Weld for Reinforcement pad, Curve: B


Shell to Pad Weld Junction at Pad OD, Curve: B


Nozzle-Shell/Head Weld (UCS-66(a)1(b)), Curve: B


Governing MDMT of the Nozzle : -104 °C

Governing MDMT of the Reinforcement Pad : -13 °C
Governing MDMT of all the sub-joints of this Junction : -13 °C
ANSI Flange MDMT including Temperature reduction per UCS-66.1:
Unadjusted MDMT of ANSI B16.5/47 flanges per UCS-66(c) -29 °C

Flange MDMT with Temp reduction per UCS-66(b)(1)(-b) -43 °C
Flange MDMT with Temp reduction per UCS-66(b)(1)(-c) -104 °C
Where the Stress Reduction Ratio per UCS-66(b)(1)(-b) is :

Design Pressure/Ambient Rating = 15.00/19.99 = 0.750
Note:
Using the min value from (b)(1)(-b) and (b)(1)(-c) above as the computed nozzle flange MDMT.
Weld Size Calculations, Description: N1

PV Elite 2019
Intermediate Calc. for nozzle/shell Welds Tmin 5.6200 mm

Intermediate Calc. for pad/shell Welds TminPad 19.0000 mm
Results Per UW-16.1:

Required Thickness Actual Thickness
Nozzle Weld 3.9340 = 0.7 * tmin. 7.0700 = 0.7 * Wo mm
Pad Weld 9.5000 = 0.5*TminPad 14.1400 = 0.7 * Wp mm
Weld Strength and Weld Loads per UG-41.1, Sketch (a) or (b)
Weld Load [W]:

= max( 0, (A-A1+2*tn*fr1*(E1*t-tr))Sv)
= max( 0, (20.2708 - 4.962 + 2 * 5.62 * 0.855 *
(1.0 * 24.6 - 19.6365 ) )1406)
= 22196.99 kgf
Note: F is always set to 1.0 throughout the calculation.
Weld Load [W1]:

= (A2+A5+A4-(Wi-Can/.707)²*fr2)*Sv
= ( 3.3119 + 22.4364 + 0.855 - 0.0 * 0.86 ) * 1406
= 37407.87 kgf
Weld Load [W2]:

= (A2 + A3 + A4 + (2 * tn * t * fr1)) * Sv
= ( 3.3119 + 0.0 + 0.855 + ( 2.3641 ) ) * 1406
= 9183.47 kgf
Weld Load [W3]:

= (A2+A3+A4+A5+(2*tn*t*fr1))*S
= ( 3.3119 + 0.0 + 0.855 + 22.4364 + ( 2.3641 ) ) * 1406
= 40732.14 kgf
Strength of Connection Elements for Failure Path Analysis
Shear, Outward Nozzle Weld [Sonw]:

= (pi/2) * Dlo * Wo * 0.49 * Snw
= ( 3.1416/2.0 ) * 112.84 * 10.0 * 0.49 * 1202
= 10442. kgf
Shear, Pad Element Weld [Spew]:

= (pi/2) * DP * WP * 0.49 * SEW
= ( 3.1416/2.0 ) * 216.0 * 20.0 * 0.49 * 1406
= 46755. kgf
Shear, Nozzle Wall [Snw]:

= (pi *( Dlr + Dlo )/4 ) * ( Thk - Can ) * 0.7 * Sn
= (3.1416 * 53.61) * ( 5.62 - 0.0 ) * 0.7 * 1202
= 7966. kgf
Tension, Pad Groove Weld [Tpgw]:

= ( pi/2) * Dlo * Wgpn * 0.74 * Seg
= (3.1416/2 ) * 112.84 * 24.83 * 0.74 * 1406
= 45795. kgf
Tension, Shell Groove Weld [Tngw]:

= (pi/2) * Dlo * (Wgnvi-Cas) * 0.74 * Sng
= ( 3.1416/2.0 ) * 112.84 * ( 24.6 - 0.0 ) * 0.74 * 1406
= 45371. kgf
Strength of Failure Paths:
PATH11 = ( SPEW + SNW ) = ( 46755 + 7966 ) = 54721 kgf

PATH22 = ( Sonw + Tpgw + Tngw + Sinw )
PV Elite 2019
= ( 10442 + 45795 + 45371 + 0 ) = 101608 kgf

PATH33 = ( Spew + Tngw + Sinw )
= ( 46755 + 45371 + 0 ) = 92126 kgf
Summary of Failure Path Calculations:

Path 1-1 = 54720 kgf, must exceed W = 22196 kgf or W1 = 37407 kgf
Maximum Allowable Pressure for this Nozzle at this Location:

Converged Max. Allow. Pressure in Operating case 18.761 kgf/cm²
Note: The MAWP of this junction was limited by the parent Shell/Head.
Nozzle is O.K. for the External Pressure 1.030 kgf/cm²
The Drop for this Nozzle is : 0.8705 mm

The Cut Length for this Nozzle is, Drop + Ho + H + T : 175.4705 mm

PV Elite 2019



Material SA-106 B

Diameter 6.0000 in.







PV Elite 2019


= (P*R)/(Sv*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406*1.0-0.6*15.0)
= 19.6365 mm

= (P*R)/(Sn*E-0.6*P) per UG-27 (c)(1)
= (15.0*76.2)/(1202*1.0-0.6*15.0)
= 0.9579 mm


= min( 1, Sn/Sv )
= min( 1, 1202.2/1406.1 )
= 0.855

= min( 1, Sn/Sv )
= min( 1, 1202.2/1406.1 )
= 0.855

= min( 1, Sp/Sv )
= min( 1, 1406.1/1406.1 )
= 1.000

= min( fr2, fr4 )
= min( 0.855, 1.0 )
= 0.855

PV Elite 2019



Area Required [A]:

= ( d * tr*F + 2 * tn * tr*F * (1-fr1) ) UG-37(c)
= (152.4*19.6365*1.0+2*7.7*19.6365*1.0*(1-0.86))
= 30.365 cm²

= 152.4( 1.0 * 24.6 - 1.0 * 19.637 ) - 2 * 7.7
( 1.0 * 24.6 - 1.0 * 19.6365 ) * ( 1 - 0.855 )
= 7.453 cm²

= ( 2 * Tlwp ) * ( tn - trn ) * fr2
= ( 2 * 47.25 ) * ( 7.7 - 0.96 ) * 0.855
= 5.447 cm²

= 10.0² * 0.86 + (0.0)² * 0.86 + 20.0² * 1.0
= 4.855 cm²

= ( 216.0 - 167.8 ) * 28.0 * 1.0
= 13.496 cm²


= min[ 6.22, max( 19.6365, 1.5 ) ]
= 6.2200 mm

= max( ta, tb )
= max( 0.9579, 6.22 )
PV Elite 2019
= 6.2200 mm













Note:

PV Elite 2019

Weld Load [W]:

= max( 0, (30.3646 - 7.4535 + 2 * 7.7 * 0.855 *
(1.0 * 24.6 - 19.6365 ) )1406)
= 33135.14 kgf
Weld Load [W1]:

= (A2+A5+A4-(Wi-Can/.707)²*fr2)*Sv
= ( 5.4475 + 13.496 + 4.855 - 0.0 * 0.86 ) * 1406
= 33463.91 kgf
Weld Load [W2]:

= (A2 + A3 + A4 + (2 * tn * t * fr1)) * Sv
= ( 5.4475 + 0.0 + 0.855 + ( 3.2391 ) ) * 1406
= 13416.72 kgf
Weld Load [W3]:

= (A2+A3+A4+A5+(2*tn*t*fr1))*S
= ( 5.4475 + 0.0 + 4.855 + 13.496 + ( 3.2391 ) ) * 1406
= 38018.51 kgf

= (pi/2) * Dlo * Wo * 0.49 * Snw
= ( 3.1416/2.0 ) * 167.8 * 10.0 * 0.49 * 1202
= 15528. kgf

= (pi/2) * DP * WP * 0.49 * SEW
= ( 3.1416/2.0 ) * 216.0 * 20.0 * 0.49 * 1406
= 46755. kgf

= (3.1416 * 80.05) * ( 7.7 - 0.0 ) * 0.7 * 1202
= 16296. kgf

= ( pi/2) * Dlo * Wgpn * 0.74 * Seg
= (3.1416/2 ) * 167.8 * 24.83 * 0.74 * 1406
= 68100. kgf

= ( 3.1416/2.0 ) * 167.8 * ( 24.6 - 0.0 ) * 0.74 * 1406
= 67469. kgf
PATH11 = ( SPEW + SNW ) = ( 46755 + 16296 ) = 63051 kgf

= ( 15528 + 68100 + 67469 + 0 ) = 151097 kgf
PV Elite 2019
= ( 46755 + 67469 + 0 ) = 114224 kgf




PV Elite 2019



Material SA-106 B

Diameter 6.0000 in.







PV Elite 2019


= (P*R)/(Sv*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406*1.0-0.6*15.0)
= 19.6365 mm

= (P*R)/(Sn*E-0.6*P) per UG-27 (c)(1)
= (15.0*76.2)/(1202*1.0-0.6*15.0)
= 0.9579 mm


= min( 1, Sn/Sv )
= min( 1, 1202.2/1406.1 )
= 0.855

= min( 1, Sn/Sv )
= min( 1, 1202.2/1406.1 )
= 0.855

= min( 1, Sp/Sv )
= min( 1, 1406.1/1406.1 )
= 1.000

= min( fr2, fr4 )
= min( 0.855, 1.0 )
= 0.855

PV Elite 2019



Area Required [A]:

= ( d * tr*F + 2 * tn * tr*F * (1-fr1) ) UG-37(c)
= (152.4*19.6365*1.0+2*7.78*19.6365*1.0*(1-0.86))
= 30.369 cm²

= 152.4( 1.0 * 24.6 - 1.0 * 19.637 ) - 2 * 7.78
( 1.0 * 24.6 - 1.0 * 19.6365 ) * ( 1 - 0.855 )
= 7.452 cm²

= ( 2 * Tlwp ) * ( tn - trn ) * fr2
= ( 2 * 47.45 ) * ( 7.78 - 0.96 ) * 0.855
= 5.535 cm²

= 10.0² * 0.86 + (0.0)² * 0.86 + 20.0² * 1.0
= 4.855 cm²

= ( 216.0 - 167.96 ) * 28.0 * 1.0
= 13.451 cm²


= min[ 6.22, max( 19.6365, 1.5 ) ]
= 6.2200 mm

= max( ta, tb )
= max( 0.9579, 6.22 )
PV Elite 2019
= 6.2200 mm













Note:

PV Elite 2019

Weld Load [W]:

= max( 0, (30.3691 - 7.4523 + 2 * 7.78 * 0.855 *
(1.0 * 24.6 - 19.6365 ) )1406)
= 33152.71 kgf
Weld Load [W1]:

= (A2+A5+A4-(Wi-Can/.707)²*fr2)*Sv
= ( 5.5354 + 13.4512 + 4.855 - 0.0 * 0.86 ) * 1406
= 33524.62 kgf
Weld Load [W2]:

= (A2 + A3 + A4 + (2 * tn * t * fr1)) * Sv
= ( 5.5354 + 0.0 + 0.855 + ( 3.2727 ) ) * 1406
= 13587.74 kgf
Weld Load [W3]:

= (A2+A3+A4+A5+(2*tn*t*fr1))*S
= ( 5.5354 + 0.0 + 4.855 + 13.4512 + ( 3.2727 ) ) * 1406
= 38126.54 kgf

= (pi/2) * Dlo * Wo * 0.49 * Snw
= ( 3.1416/2.0 ) * 167.96 * 10.0 * 0.49 * 1202
= 15542. kgf

= (pi/2) * DP * WP * 0.49 * SEW
= ( 3.1416/2.0 ) * 216.0 * 20.0 * 0.49 * 1406
= 46755. kgf

= (3.1416 * 80.09) * ( 7.78 - 0.0 ) * 0.7 * 1202
= 16474. kgf

= ( pi/2) * Dlo * Wgpn * 0.74 * Seg
= (3.1416/2 ) * 167.96 * 24.8 * 0.74 * 1406
= 68083. kgf

= ( 3.1416/2.0 ) * 167.96 * ( 24.6 - 0.0 ) * 0.74 * 1406
= 67534. kgf
PATH11 = ( SPEW + SNW ) = ( 46755 + 16474 ) = 63229 kgf

= ( 15542 + 68083 + 67534 + 0 ) = 151159 kgf
PV Elite 2019
= ( 46755 + 67534 + 0 ) = 114289 kgf




PV Elite 2019



Material SA-106 B

Diameter 6.0000 in.







PV Elite 2019


= (P*R)/(Sv*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406*1.0-0.6*15.0)
= 19.6365 mm

= (P*R)/(Sn*E-0.6*P) per UG-27 (c)(1)
= (15.0*76.2)/(1202*1.0-0.6*15.0)
= 0.9579 mm


= min( 1, Sn/Sv )
= min( 1, 1202.2/1406.1 )
= 0.855

= min( 1, Sn/Sv )
= min( 1, 1202.2/1406.1 )
= 0.855

= min( 1, Sp/Sv )
= min( 1, 1406.1/1406.1 )
= 1.000

= min( fr2, fr4 )
= min( 0.855, 1.0 )
= 0.855

PV Elite 2019



Area Required [A]:

= ( d * tr*F + 2 * tn * tr*F * (1-fr1) ) UG-37(c)
= (152.4*19.6365*1.0+2*7.03*19.6365*1.0*(1-0.86))
= 30.326 cm²

= 152.4( 1.0 * 24.78 - 1.0 * 19.637 ) - 2 * 7.03
( 1.0 * 24.78 - 1.0 * 19.6365 ) * ( 1 - 0.855 )
= 7.734 cm²

= ( 2 * Tlwp ) * ( tn - trn ) * fr2
= ( 2 * 42.38 ) * ( 7.03 - 0.96 ) * 0.855
= 4.400 cm²

= 10.0² * 0.86 + (0.0)² * 0.86 + 20.0² * 1.0
= 4.855 cm²

= ( 250.0 - 166.46 ) * 24.8 * 1.0
= 20.718 cm²


= min[ 6.22, max( 19.6365, 1.5 ) ]
= 6.2200 mm

= max( ta, tb )
= max( 0.9579, 6.22 )
PV Elite 2019
= 6.2200 mm













Note:

PV Elite 2019

Weld Load [W]:

= max( 0, (30.3264 - 7.7338 + 2 * 7.03 * 0.855 *
(1.0 * 24.78 - 19.6365 ) )1406)
= 32637.82 kgf
Weld Load [W1]:

= (A2+A5+A4-(Wi-Can/.707)²*fr2)*Sv
= ( 4.3999 + 20.7179 + 4.855 - 0.0 * 0.86 ) * 1406
= 42145.96 kgf
Weld Load [W2]:

= (A2 + A3 + A4 + (2 * tn * t * fr1)) * Sv
= ( 4.3999 + 0.0 + 0.855 + ( 2.9789 ) ) * 1406
= 11577.87 kgf
Weld Load [W3]:

= (A2+A3+A4+A5+(2*tn*t*fr1))*S
= ( 4.3999 + 0.0 + 4.855 + 20.7179 + ( 2.9789 ) ) * 1406
= 46334.68 kgf

= (pi/2) * Dlo * Wo * 0.49 * Snw
= ( 3.1416/2.0 ) * 166.46 * 10.0 * 0.49 * 1202
= 15404. kgf

= (pi/2) * DP * WP * 0.49 * SEW
= ( 3.1416/2.0 ) * 250.0 * 20.0 * 0.49 * 1406
= 54115. kgf

= (3.1416 * 79.715) * ( 7.03 - 0.0 ) * 0.7 * 1202
= 14816. kgf

= ( pi/2) * Dlo * Wgpn * 0.74 * Seg
= (3.1416/2 ) * 166.46 * 24.78 * 0.74 * 1406
= 67420. kgf

= ( 3.1416/2.0 ) * 166.46 * ( 24.78 - 0.0 ) * 0.74 * 1406
= 67420. kgf
PATH11 = ( SPEW + SNW ) = ( 54115 + 14816 ) = 68931 kgf

= ( 15404 + 67420 + 67420 + 0 ) = 150244 kgf
PV Elite 2019
= ( 54115 + 67420 + 0 ) = 121535 kgf




PV Elite 2019
Nozzle Calcs.: MH1 Nozl: 21 10:40am Aug 29,2023
Input, Nozzle Desc: MH1 From: 50



Material SA-106 B

Diameter 20.0000 in.





This is a Manway or Access Opening.


PV Elite 2019
Reinforcement CALCULATION, Description: MH1


= (P*R)/(Sv*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406*1.0-0.6*15.0)
= 19.6365 mm

= (P*R)/(Sn*E-0.6*P) per UG-27 (c)(1)
= (15.0*254.0)/(1202*1.0-0.6*15.0)
= 3.1930 mm


= min( 1, Sn/Sv )
= min( 1, 1202.2/1406.1 )
= 0.855

= min( 1, Sn/Sv )
= min( 1, 1202.2/1406.1 )
= 0.855

= min( 1, Sp/Sv )
= min( 1, 1406.1/1406.1 )
= 1.000

= min( fr2, fr4 )
= min( 0.855, 1.0 )
= 0.855

PV Elite 2019



Based on Shell or Nozzle Thickness: 670.1150 24.5000 mm
Area Required [A]:

= ( d * tr*F + 2 * tn * tr*F * (1-fr1) ) UG-37(c)
= (508.0*19.6365*1.0+2*24.5*19.6365*1.0*(1-0.86))
= 101.149 cm²

= 508.0( 1.0 * 28.2 - 1.0 * 19.637 ) - 2 * 24.5
( 1.0 * 28.2 - 1.0 * 19.6365 ) * ( 1 - 0.855 )
= 42.894 cm²

= ( 2 * Tlwp ) * ( tn - trn ) * fr2
= ( 2 * 70.5 ) * ( 24.5 - 3.19 ) * 0.855
= 25.687 cm²

= 10.0² * 0.86 + (0.0)² * 0.86 + 20.0² * 1.0
= 4.855 cm²

= ( 754.0 - 557.0 ) * 24.79 * 1.0
= 48.836 cm²




PV Elite 2019


Govrn. thk, tg = 24.79, c = 0.0 mm, E* = 1.0

Pad governing, Conservatively assuming Pad stress = Shell stress(Div. 1 L-9.3).






Note:
Weld Size Calculations, Description: MH1


Nozzle Weld 6.0000 = Min per Code 7.0700 = 0.7 * Wo mm
Weld Load [W]:

= max( 0, (101.1488 - 42.8939 + 2 * 24.5 * 0.855 *
(1.0 * 28.2 - 19.6365 ) )1406)
= 86959.15 kgf
Weld Load [W1]:

= (A2+A5+A4-(Wi-Can/.707)²*fr2)*Sv
PV Elite 2019
= ( 25.6867 + 48.8363 + 4.855 - 0.0 * 0.86 ) * 1406

= 111616.43 kgf
Weld Load [W2]:

= (A2 + A3 + A4 + (2 * tn * t * fr1)) * Sv
= ( 25.6867 + 0.0 + 0.855 + ( 11.8144 ) ) * 1406
= 53933.96 kgf
Weld Load [W3]:

= (A2+A3+A4+A5+(2*tn*t*fr1))*S
= ( 25.6867 + 0.0 + 4.855 + 48.8363 + ( 11.8144 ) ) * 1406
= 128229.09 kgf

= (pi/2) * Dlo * Wo * 0.49 * Snw
= ( 3.1416/2.0 ) * 557.0 * 10.0 * 0.49 * 1202
= 51542. kgf

= (pi/2) * DP * WP * 0.49 * SEW
= ( 3.1416/2.0 ) * 754.0 * 20.0 * 0.49 * 1406
= 163209. kgf

= (3.1416 * 266.25) * ( 24.5 - 0.0 ) * 0.7 * 1202
= 172464. kgf

= ( pi/2) * Dlo * Wgpn * 0.74 * Seg
= (3.1416/2 ) * 557.0 * 24.79 * 0.74 * 1406
= 225689. kgf

= ( 3.1416/2.0 ) * 557.0 * ( 24.79 - 0.0 ) * 0.74 * 1406
= 225689. kgf
PATH11 = ( SPEW + SNW ) = ( 163209 + 172464 ) = 335673 kgf

= ( 51542 + 225689 + 225689 + 0 ) = 502921 kgf
= ( 163209 + 225689 + 0 ) = 388899 kgf




PV Elite 2019



Material SA-106 B

Diameter 3.0000 in.







PV Elite 2019


= (P*R)/(Sv*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406*1.0-0.6*15.0)
= 19.6365 mm

= (P*R)/(Sn*E-0.6*P) per UG-27 (c)(1)
= (15.0*38.1)/(1202*1.0-0.6*15.0)
= 0.4789 mm


= min( 1, Sn/Sv )
= min( 1, 1202.2/1406.1 )
= 0.855

= min( 1, Sn/Sv )
= min( 1, 1202.2/1406.1 )
= 0.855

= min( 1, Sp/Sv )
= min( 1, 1406.1/1406.1 )
= 1.000

= min( fr2, fr4 )
= min( 0.855, 1.0 )
= 0.855

PV Elite 2019



Area Required [A]:

= ( d * tr*F + 2 * tn * tr*F * (1-fr1) ) UG-37(c)
= (76.2*19.6365*1.0+2*5.59*19.6365*1.0*(1-0.86))
= 15.281 cm²

= 76.2( 1.0 * 28.2 - 1.0 * 19.637 ) - 2 * 5.59
( 1.0 * 28.2 - 1.0 * 19.6365 ) * ( 1 - 0.855 )
= 6.387 cm²

= ( 2 * Tlwp ) * ( tn - trn ) * fr2
= ( 2 * 38.76 ) * ( 5.59 - 0.48 ) * 0.855
= 3.387 cm²

= 10.0² * 0.86 + (0.0)² * 0.86 + 0.0² * 1.0
= 0.855 cm²

= ( 152.4 - 87.38 ) * 24.78 * 1.0
= 16.112 cm²


= min[ 4.8, max( 19.6365, 1.5 ) ]
= 4.8000 mm

PV Elite 2019
= max( ta, tb )
= max( 0.4789, 4.8 )
= 4.8000 mm






Govrn. thk, tg = 24.78, c = 0.0 mm, E* = 1.0







Note:
PV Elite 2019


Weld Load [W]:

= max( 0, (15.2814 - 6.3865 + 2 * 5.59 * 0.855 *
(1.0 * 28.2 - 19.6365 ) )1406)
= 13658.40 kgf
Weld Load [W1]:

= (A2+A5+A4-(Wi-Can/.707)²*fr2)*Sv
= ( 3.3872 + 16.112 + 0.855 - 0.0 * 0.86 ) * 1406
= 28620.68 kgf
Weld Load [W2]:

= (A2 + A3 + A4 + (2 * tn * t * fr1)) * Sv
= ( 3.3872 + 0.0 + 0.855 + ( 2.6956 ) ) * 1406
= 9755.45 kgf
Weld Load [W3]:

= (A2+A3+A4+A5+(2*tn*t*fr1))*S
= ( 3.3872 + 0.0 + 0.855 + 16.112 + ( 2.6956 ) ) * 1406
= 32411.08 kgf

= (pi/2) * Dlo * Wo * 0.49 * Snw
= ( 3.1416/2.0 ) * 87.38 * 10.0 * 0.49 * 1202
= 8086. kgf

= (pi/2) * DP * WP * 0.49 * SEW
= ( 3.1416/2.0 ) * 190.0 * 20.0 * 0.49 * 1406
= 41127. kgf

= (3.1416 * 40.895) * ( 5.59 - 0.0 ) * 0.7 * 1202
= 6044. kgf

= ( pi/2) * Dlo * Wgpn * 0.74 * Seg
= (3.1416/2 ) * 87.38 * 24.78 * 0.74 * 1406
= 35391. kgf

= ( 3.1416/2.0 ) * 87.38 * ( 24.79 - 0.0 ) * 0.74 * 1406
= 35405. kgf
PATH11 = ( SPEW + SNW ) = ( 41127 + 6044 ) = 47171 kgf

PV Elite 2019

= ( 8086 + 35391 + 35405 + 0 ) = 78882 kgf
= ( 41127 + 35405 + 0 ) = 76532 kgf




PV Elite 2019



Material SA-106 B

Diameter 2.0000 in.






PV Elite 2019
Insert/Set-in Nozzle No Pad, no Inside projection


= (P*R)/(Sv*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406*1.0-0.6*15.0)
= 19.6365 mm

= (P*R)/(Sn*E-0.6*P) per UG-27 (c)(1)
= (15.0*25.4)/(1202*1.0-0.6*15.0)
= 0.3193 mm

Parallel to Vessel Wall Rn+tn+t 55.0600 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 12.2250 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: N5.

This calculation is valid for nozzles that meet all the requirements of
paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.


= min[ 4.52, max( 19.6365, 1.5 ) ]
= 4.5200 mm

PV Elite 2019
= max( ta, tb )
= max( 0.3193, 4.52 )
= 4.5200 mm






Note:

Skipping the nozzle attachment weld strength calculations.

Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.



PV Elite 2019



Material SA-106 B

Diameter 4.0000 in.







PV Elite 2019


= (P*R)/(Sv*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406*1.0-0.6*15.0)
= 19.6365 mm

= (P*R)/(Sn*E-0.6*P) per UG-27 (c)(1)
= (15.0*50.8)/(1202*1.0-0.6*15.0)
= 0.6386 mm


= min( 1, Sn/Sv )
= min( 1, 1202.2/1406.1 )
= 0.855

= min( 1, Sn/Sv )
= min( 1, 1202.2/1406.1 )
= 0.855

= min( 1, Sp/Sv )
= min( 1, 1406.1/1406.1 )
= 1.000

= min( fr2, fr4 )
= min( 0.855, 1.0 )
= 0.855

PV Elite 2019



Area Required [A]:

= ( d * tr*F + 2 * tn * tr*F * (1-fr1) ) UG-37(c)
= (101.6*19.6365*1.0+2*5.55*19.6365*1.0*(1-0.86))
= 20.267 cm²

= 101.6( 1.0 * 24.77 - 1.0 * 19.637 ) - 2 * 5.55
( 1.0 * 24.77 - 1.0 * 19.6365 ) * ( 1 - 0.855 )
= 5.133 cm²

= ( 2 * Tlwp ) * ( tn - trn ) * fr2
= ( 2 * 39.88 ) * ( 5.55 - 0.64 ) * 0.855
= 3.349 cm²

= 10.0² * 0.86 + (0.0)² * 0.86 + 0.0² * 1.0
= 0.855 cm²

= ( 203.2 - 112.7 ) * 26.0 * 1.0
= 23.530 cm²


= min[ 5.258, max( 19.6365, 1.5 ) ]
= 5.2578 mm

PV Elite 2019
= max( ta, tb )
= max( 0.6386, 5.2578 )
= 5.2578 mm













Note:

PV Elite 2019


Weld Load [W]:

= max( 0, (20.2668 - 5.133 + 2 * 5.55 * 0.855 *
(1.0 * 24.77 - 19.6365 ) )1406)
= 21965.29 kgf
Weld Load [W1]:

= (A2+A5+A4-(Wi-Can/.707)²*fr2)*Sv
= ( 3.3489 + 23.53 + 0.855 - 0.0 * 0.86 ) * 1406
= 38997.70 kgf
Weld Load [W2]:

= (A2 + A3 + A4 + (2 * tn * t * fr1)) * Sv
= ( 3.3489 + 0.0 + 0.855 + ( 2.3508 ) ) * 1406
= 9216.82 kgf
Weld Load [W3]:

= (A2+A3+A4+A5+(2*tn*t*fr1))*S
= ( 3.3489 + 0.0 + 0.855 + 23.53 + ( 2.3508 ) ) * 1406
= 42303.24 kgf

= (pi/2) * Dlo * Wo * 0.49 * Snw
= ( 3.1416/2.0 ) * 112.7 * 10.0 * 0.49 * 1202
= 10429. kgf

= (pi/2) * DP * WP * 0.49 * SEW
= ( 3.1416/2.0 ) * 216.0 * 20.0 * 0.49 * 1406
= 46755. kgf

= (3.1416 * 53.575) * ( 5.55 - 0.0 ) * 0.7 * 1202
= 7861. kgf

= ( pi/2) * Dlo * Wgpn * 0.74 * Seg
= (3.1416/2 ) * 112.7 * 26.0 * 0.74 * 1406
= 47894. kgf

= ( 3.1416/2.0 ) * 112.7 * ( 24.77 - 0.0 ) * 0.74 * 1406
= 45628. kgf
PATH11 = ( SPEW + SNW ) = ( 46755 + 7861 ) = 54616 kgf

PV Elite 2019
= ( 10429 + 47894 + 45628 + 0 ) = 103950 kgf

= ( 46755 + 45628 + 0 ) = 92383 kgf




PV Elite 2019



Material SA-106 B

Diameter 2.0000 in.






PV Elite 2019


= (P*R)/(Sv*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406*1.0-0.6*15.0)
= 19.6365 mm

= (P*R)/(Sn*E-0.6*P) per UG-27 (c)(1)
= (15.0*25.4)/(1202*1.0-0.6*15.0)
= 0.3193 mm

Note:



= min[ 4.52, max( 19.6365, 1.5 ) ]
= 4.5200 mm

PV Elite 2019
= max( ta, tb )
= max( 0.3193, 4.52 )
= 4.5200 mm






Note:





PV Elite 2019



Material SA-106 B

Diameter 6.0000 in.







PV Elite 2019


= (P*R)/(Sv*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406*1.0-0.6*15.0)
= 19.6365 mm

= (P*R)/(Sn*E-0.6*P) per UG-27 (c)(1)
= (15.0*76.2)/(1202*1.0-0.6*15.0)
= 0.9579 mm


= min( 1, Sn/Sv )
= min( 1, 1202.2/1406.1 )
= 0.855

= min( 1, Sn/Sv )
= min( 1, 1202.2/1406.1 )
= 0.855

= min( 1, Sp/Sv )
= min( 1, 1406.1/1406.1 )
= 1.000

= min( fr2, fr4 )
= min( 0.855, 1.0 )
= 0.855

PV Elite 2019



Area Required [A]:

= ( d * tr*F + 2 * tn * tr*F * (1-fr1) ) UG-37(c)
= (152.4*19.6365*1.0+2*6.81*19.6365*1.0*(1-0.86))
= 30.314 cm²

= 152.4( 1.0 * 24.77 - 1.0 * 19.637 ) - 2 * 6.81
( 1.0 * 24.77 - 1.0 * 19.6365 ) * ( 1 - 0.855 )
= 7.722 cm²

= ( 2 * Tlwp ) * ( tn - trn ) * fr2
= ( 2 * 42.32 ) * ( 6.81 - 0.96 ) * 0.855
= 4.235 cm²

= (Wo² - Ar Lost)*Fr3+((Wi-can/0.707)² - Ar Lost)*fr2 + Trapfr4
= ( 1. ) * 0.86 + (0.0 ) * 0.86 + 393.24² * 1.0
= 4.787 cm²

= ( 270.0 - 166.02 ) * 25.29 * 1.0
= 26.297 cm²


= min[ 6.22, max( 19.6365, 1.5 ) ]
= 6.2200 mm

= max( ta, tb )
= max( 0.9579, 6.22 )
PV Elite 2019
= 6.2200 mm













Note:

PV Elite 2019

Weld Load [W]:

= max( 0, (30.3139 - 7.722 + 2 * 6.81 * 0.855 *
(1.0 * 24.77 - 19.6365 ) )1406)
= 32607.90 kgf
Weld Load [W1]:

= (A2+A5+A4-(Wi-Can/.707)²*fr2)*Sv
= ( 4.2345 + 26.2965 + 4.7874 - 0.0 * 0.86 ) * 1406
= 49662.61 kgf
Weld Load [W2]:

= (A2 + A3 + A4 + (2 * tn * t * fr1)) * Sv
= ( 4.2345 + 0.0 + 0.855 + ( 2.8845 ) ) * 1406
= 11212.55 kgf
Weld Load [W3]:

= (A2+A3+A4+A5+(2*tn*t*fr1))*S
= ( 4.2345 + 0.0 + 4.7874 + 26.2965 + ( 2.8845 ) ) * 1406
= 53718.60 kgf

= (pi/2) * Dlo * Wo * 0.49 * Snw
= ( 3.1416/2.0 ) * 166.02 * 10.0 * 0.49 * 1202
= 15363. kgf

= (pi/2) * DP * WP * 0.49 * SEW
= ( 3.1416/2.0 ) * 270.0 * 20.0 * 0.49 * 1406
= 58444. kgf

= (3.1416 * 79.605) * ( 6.81 - 0.0 ) * 0.7 * 1202
= 14333. kgf

= ( pi/2) * Dlo * Wgpn * 0.74 * Seg
= (3.1416/2 ) * 166.02 * 25.29 * 0.74 * 1406
= 68626. kgf

= ( 3.1416/2.0 ) * 166.02 * ( 24.77 - 0.0 ) * 0.74 * 1406
= 67215. kgf
PATH11 = ( SPEW + SNW ) = ( 58444 + 14333 ) = 72776 kgf

= ( 15363 + 68626 + 67215 + 0 ) = 151204 kgf
PV Elite 2019
= ( 58444 + 67215 + 0 ) = 125659 kgf




PV Elite 2019



Material SA-106 B

Diameter 2.0000 in.






PV Elite 2019


= (P*R)/(Sv*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406*1.0-0.6*15.0)
= 19.6365 mm

= (P*R)/(Sn*E-0.6*P) per UG-27 (c)(1)
= (15.0*25.4)/(1202*1.0-0.6*15.0)
= 0.3193 mm

Note:



= min[ 4.52, max( 19.6365, 1.5 ) ]
= 4.5200 mm

PV Elite 2019
= max( ta, tb )
= max( 0.3193, 4.52 )
= 4.5200 mm






Note:





PV Elite 2019



Material SA-106 B

Diameter 2.0000 in.






PV Elite 2019


= (P*R)/(Sv*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406*1.0-0.6*15.0)
= 19.6365 mm

= (P*R)/(Sn*E-0.6*P) per UG-27 (c)(1)
= (15.0*25.4)/(1202*1.0-0.6*15.0)
= 0.3193 mm

Note:



= min[ 4.52, max( 19.6365, 1.5 ) ]
= 4.5200 mm

PV Elite 2019
= max( ta, tb )
= max( 0.3193, 4.52 )
= 4.5200 mm






Note:





PV Elite 2019



Material SA-106 B

Diameter 2.0000 in.






PV Elite 2019


= (P*R)/(Sv*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406*1.0-0.6*15.0)
= 19.6365 mm

= (P*R)/(Sn*E-0.6*P) per UG-27 (c)(1)
= (15.0*25.4)/(1202*1.0-0.6*15.0)
= 0.3193 mm

Note:



= min[ 4.52, max( 19.6365, 1.5 ) ]
= 4.5200 mm

PV Elite 2019
= max( ta, tb )
= max( 0.3193, 4.52 )
= 4.5200 mm






Note:





PV Elite 2019



Material SA-106 B

Diameter 2.0000 in.






PV Elite 2019


= (P*R)/(Sv*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406*1.0-0.6*15.0)
= 19.6365 mm

= (P*R)/(Sn*E-0.6*P) per UG-27 (c)(1)
= (15.0*25.4)/(1202*1.0-0.6*15.0)
= 0.3193 mm

Note:



= min[ 4.52, max( 19.6365, 1.5 ) ]
= 4.5200 mm

PV Elite 2019
= max( ta, tb )
= max( 0.3193, 4.52 )
= 4.5200 mm






Note:





PV Elite 2019



Material SA-106 B

Diameter 2.0000 in.







PV Elite 2019


= (P*R)/(Sv*E-0.6*P) per UG-27 (c)(1)
= (15.0*1829.0)/(1406*1.0-0.6*15.0)
= 19.6365 mm

= (P*R)/(Sn*E-0.6*P) per UG-27 (c)(1)
= (15.0*25.4)/(1202*1.0-0.6*15.0)
= 0.3193 mm

Note:



= min[ 4.52, max( 19.6365, 1.5 ) ]
PV Elite 2019
= 4.5200 mm

= max( ta, tb )
= max( 0.3193, 4.52 )
= 4.5200 mm













Note:
PV Elite 2019






PV Elite 2019
Input, Nozzle Desc: MH2 From: 110


Inside Diameter of Elliptical Head D 3658.00 mm

Aspect Ratio of Elliptical Head Ar 1.50
Head Finished (Minimum) Thickness t 26.7700 mm
Head Internal Corrosion Allowance c 0.0000 mm
Head External Corrosion Allowance co 0.0000 mm
Distance from Head Centerline L1 0.0000 mm
Material SA-106 B

Diameter 20.0000 in.





This is a Manway or Access Opening.


PV Elite 2019
Reinforcement CALCULATION, Description: MH2

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

= (P*K1*D))/(2*Sv*E-0.2*P) per UG-37(a)(3)
= (15.0*0.692*3658.0)/(2 *1406.14*1.0-0.2*15.0)
= 13.5257 mm

= (P*R)/(Sn*E-0.6*P) per UG-27 (c)(1)
= (15.0*254.0)/(1202*1.0-0.6*15.0)
= 3.1930 mm


= min( 1, Sn/Sv )
= min( 1, 1202.2/1406.1 )
= 0.855

= min( 1, Sn/Sv )
= min( 1, 1202.2/1406.1 )
= 0.855

= min( 1, Sp/Sv )
= min( 1, 1406.1/1406.1 )
= 1.000

= min( fr2, fr4 )
= min( 0.855, 1.0 )
= 0.855

PV Elite 2019

The area available without a pad is Sufficient.

Area Required [A]:

= ( d * tr*F + 2 * tn * tr*F * (1-fr1) ) UG-37(c)
= (508.0*13.5257*1.0+2*24.5*13.5257*1.0*(1-0.86))
= 69.672 cm²

= 508.0( 1.0 * 26.77 - 1.0 * 13.526 ) - 2 * 24.5
( 1.0 * 26.77 - 1.0 * 13.5257 ) * ( 1 - 0.855 )
= 66.340 cm²

= ( 2 * Tlwp ) * ( tn - trn ) * fr2
= ( 2 * 66.93 ) * ( 24.5 - 3.19 ) * 0.855
= 24.384 cm²

= 10.0² * 0.86 + (0.0)² * 0.86 + 22.0² * 1.0
= 5.695 cm²

= ( 608.0 - 557.0 ) * 25.89 * 1.0
= 13.204 cm²





PV Elite 2019

Govrn. thk, tg = 25.89, c = 0.0 mm, E* = 1.0

Min Metal Temp. w/o impact per UCS-66, Curve B 0 °C






Note:
Weld Size Calculations, Description: MH2


Nozzle Weld 6.0000 = Min per Code 7.0700 = 0.7 * Wo mm
Weld Load [W]:

= max( 0, (69.6716 - 66.34 + 2 * 24.5 * 0.855 *
(1.0 * 26.77 - 13.5257 ) )1406)
= 12486.79 kgf
Weld Load [W1]:

= (A2+A5+A4-(Wi-Can/.707)²*fr2)*Sv
= ( 24.3841 + 13.2039 + 5.695 - 0.0 * 0.86 ) * 1406
= 60861.93 kgf
Weld Load [W2]:

= (A2 + A3 + A4 + (2 * tn * t * fr1)) * Sv
PV Elite 2019
= ( 24.3841 + 0.0 + 0.855 + ( 11.2153 ) ) * 1406

= 51259.98 kgf
Weld Load [W3]:

= (A2+A3+A4+A5+(2*tn*t*fr1))*S
= ( 24.3841 + 0.0 + 5.695 + 13.2039 + ( 11.2153 ) ) * 1406
= 76632.18 kgf

= (pi/2) * Dlo * Wo * 0.49 * Snw
= ( 3.1416/2.0 ) * 557.0 * 10.0 * 0.49 * 1202
= 51542. kgf

= (pi/2) * DP * WP * 0.49 * SEW
= ( 3.1416/2.0 ) * 608.0 * 22.0 * 0.49 * 1406
= 144767. kgf

= (3.1416 * 266.25) * ( 24.5 - 0.0 ) * 0.7 * 1202
= 172464. kgf

= ( pi/2) * Dlo * Wgpn * 0.74 * Seg
= (3.1416/2 ) * 557.0 * 25.89 * 0.74 * 1406
= 235704. kgf

= ( 3.1416/2.0 ) * 557.0 * ( 26.77 - 0.0 ) * 0.74 * 1406
= 243716. kgf
PATH11 = ( SPEW + SNW ) = ( 144767 + 172464 ) = 317231 kgf

= ( 51542 + 235704 + 243716 + 0 ) = 530962 kgf
= ( 144767 + 243716 + 0 ) = 388483 kgf




PV Elite 2019
Nozzle Schedule: Step: 27 10:40am Aug 29,2023
Nozzle Schedule:
Nominal or Schd Flg Nozzle Wall Reinforcing Pad Cut Flg

Actual or FVC Type O/Dia Thk Diameter Thk Length Class
Description Size Type in mm mm mm mm
N5 2.000 in Actual WNF 2.385 4.890 ... ... 175.02 150

N11 2.000 in Actual WNF 2.433 5.500 ... ... 175.03 150
N13 2.000 in Actual WNF 2.383 4.860 ... ... 175.02 150
N8 2.000 in Actual WNF 2.413 5.250 ... ... 175.04 150
N9 2.000 in Actual WNF 2.443 5.630 ... ... 175.04 150
N10 2.000 in Actual WNF 2.451 5.730 ... ... 175.04 150
N7 2.000 in Actual WNF 2.383 4.870 270.00 24.80 175.03 150
N6 3.000 in Actual WNF 3.440 5.590 190.00 24.78 178.72 150
N1 4.000 in Actual WNF 4.443 5.620 216.00 24.83 175.47 150
N4 4.000 in Actual WNF 4.437 5.550 216.00 26.00 175.64 150
N2 6.000 in Actual WNF 6.606 7.700 216.00 28.00 176.53 150
N18 6.000 in Actual WNF 6.613 7.780 216.00 28.00 176.53 150
N3 6.000 in Actual WNF 6.554 7.030 250.00 24.80 176.67 150
N12 6.000 in Actual WNF 6.536 6.810 270.00 25.29 176.65 150
MH1 20.000 in Actual WNF 21.929 24.500 754.00 24.79 199.53 150
MH2 20.000 in Actual WNF 21.929 24.500 608.00 25.89 117.06 150
General Notes for the above table:
The Cut Length is the Outside Projection + Inside Projection + Drop +

In Plane Shell Thickness. This value does not include weld gaps,
nor does it account for shrinkage.
In the case of Oblique Nozzles, the Outside Diameter must

be increased. The Re-Pad WIDTH around the nozzle is calculated as follows:
Width of Pad = (Pad Outside Dia. (per above) - Nozzle Outside Dia.)/2
For hub nozzles, the thickness and diameter shown are those of the smaller
and thinner section.
Nozzle Material and Weld Fillet Leg Size Details (mm):
Shl Grve Noz Shl/Pad Pad OD Pad Grve Inside

Description Material Weld Weld Weld Weld Weld
N5 SA-106 B 24.770 10.000 ... ... ...

N11 SA-106 B 24.770 10.000 ... ... ...
N13 SA-106 B 24.770 10.000 ... ... ...
N8 SA-106 B 24.780 10.000 ... ... ...
N9 SA-106 B 24.780 10.000 ... ... ...
N10 SA-106 B 24.780 10.000 ... ... ...
N7 SA-106 B 24.780 10.000 20.000 24.800 ...
N6 SA-106 B 24.790 10.000 20.000 24.780 ...
N1 SA-106 B 24.600 10.000 20.000 24.830 ...
N4 SA-106 B 24.770 10.000 20.000 26.000 ...
N2 SA-106 B 24.600 10.000 20.000 24.830 ...
N18 SA-106 B 24.600 10.000 20.000 24.800 ...
N3 SA-106 B 24.780 10.000 20.000 24.780 ...
N12 SA-106 B 24.770 10.000 20.000 25.290 ...
MH1 SA-106 B 24.790 10.000 20.000 24.790 ...
MH2 SA-106 B 26.770 10.000 22.000 25.890 ...
Note: The Outside projections below do not include the flange thickness.
Nozzle Miscellaneous Data:
Elev/Distance Layout Proj Proj Installed in

Description From Datum Angle Outside Inside Component
PV Elite 2019
Nozzle Schedule: Step: 27 10:40am Aug 29,2023
cm deg mm mm
N5 785.200 90.0 150.00 0.00 SHELL 5

N11 785.200 270.0 150.00 0.00 SHELL 5
N13 865.200 270.0 150.00 0.00 SHELL 5
N8 1167.800 270.0 150.00 0.00 SHELL 7
N9 1197.800 270.0 150.00 0.00 SHELL 7
N10 1227.800 270.0 150.00 0.00 SHELL 7
N7 1650.400 270.0 150.00 0.00 SHELL 9
N6 598.900 90.0 150.00 0.00 SHELL 4
N1 30.000 90.0 150.00 0.00 SHELL 1
N4 825.200 90.0 150.00 0.00 SHELL 5
N2 100.000 90.0 150.00 0.00 SHELL 1
N18 20.000 270.0 150.00 0.00 SHELL 1
N3 206.300 90.0 150.00 0.00 SHELL 2
N12 825.200 270.0 150.00 0.00 SHELL 5
MH1 658.900 90.0 150.00 0.00 SHELL 4
MH2 ... 0.0 75.00 0.00 HEAD 2

PV Elite 2019
MDMT Summary: Step: 29 10:40am Aug 29,2023
Minimum Design Metal Temperature Results Summary :
Curve Basic Reduced UG-20(f) Thickness Gov E* PWHT

Description MDMT MDMT MDMT ratio Thk reqd
Notes °C °C °C mm
HEAD 1 [10] ! -8 -37 0.526 26.690 1.00 No

HEAD 1 [7] ! -8 -22 0.746 26.690 1.00 No
SHELL 1 [8] ! -8 -19 0.810 24.600 1.00 No
SHELL 2 [8] ! -8 -19 0.804 24.780 1.00 No
SHELL 3 [8] ! -8 -19 0.804 24.780 1.00 No
SHELL 4 [8] ! -8 -24 0.707 28.200 1.00 No
SHELL 5 [8] ! -8 -19 0.804 24.770 1.00 No
SHELL 6 [8] ! -8 -19 0.803 24.800 1.00 No
SHELL 7 [8] ! -8 -19 0.804 24.780 1.00 No
SHELL 8 [8] ! -8 -19 0.804 24.770 1.00 No
SHELL 9 [8] ! -8 -19 0.804 24.780 1.00 No
HEAD 2 [10] ! -8 -37 0.524 26.770 1.00 No
HEAD 2 [7] ! -8 -22 0.744 26.770 1.00 No
N1 [1] B -1 -13 0.798 24.600 1.00 No
Nozzle Flg [4] B -29 -104
N2 [1] B -1 -13 0.798 24.600 1.00 No
N18 [1] B -1 -13 0.798 24.600 1.00 No
N3 [1] B -1 -13 0.792 24.780 1.00 No
MH1 [1] B -1 -18 0.696 24.790 1.00 No
N6 [1] B -1 -18 0.696 24.780 1.00 No
N5 [1] B -29 -104 0.065 4.890 1.00 No
N4 [1] B -1 -13 0.793 24.770 1.00 No
N11 [1] B -29 -104 0.058 5.500 1.00 No
N12 [1] B -1 -13 0.793 24.770 1.00 No
N13 [1] B -29 -104 0.066 4.860 1.00 No
N8 [1] B -29 -104 0.061 5.250 1.00 No
N9 [1] B -29 -104 0.057 5.630 1.00 No
N10 [1] B -29 -104 0.056 5.730 1.00 No
N7 [1] B -1 -13 0.792 24.780 1.00 No
MH2 [1] B 0 -32 0.505 25.890 1.00 No
Warmest MDMT: 0 -13
Required Minimum Design Metal Temperature -8.0 °C

Warmest Computed Minimum Design Metal Temperature -13.0 °C
Notes:
[ ! ] - This was an impact tested material.
[ 1] - Governing Nozzle Weld.
[ 4] - ANSI Flange MDMT Calcs; Thickness ratio per UCS-66(b)(1)(-c).
[ 5] - ANSI Flange MDMT Calcs; Thickness ratio per UCS-66(b)(1)(-b).
[ 6] - MDMT Calculations at the Shell/Head Joint.
[ 7] - MDMT Calculations for the Straight Flange.
PV Elite 2019
MDMT Summary: Step: 29 10:40am Aug 29,2023
[ 8] - Cylinder/Cone/Flange Junction MDMT.

[ 9] - Calculations in the Spherical Portion of the Head.
[10] - Calculations in the Knuckle Portion of the Head.
[11] - Calculated (Body Flange) Flange MDMT.
[12] - Calculated Flat Head MDMT per UCS-66.3
[13] - Tubesheet MDMT, shell side, if applicable
[14] - Tubesheet MDMT, tube side, if applicable
[15] - Nozzle Material
[16] - Shell or Head Material
[17] - Impact Testing required
[18] - Impact Testing not required, see UCS-66(b)(3)
[19] - Select a valid hydrotest type to get the UG-20(f) exemption
[20] - Cylinder/Cone Junction MDMT based on Longitudinal Stress considerations
[21] - Bolting Material
UG-84(b)(2) was not considered.

UCS-66(g) was not considered.
UCS-66(i) was not considered.
Notes:
Impact test temps were not entered in and not considered in the analysis.
UCS-66(i) applies to impact tested materials not by specification and
UCS-66(g) applies to materials impact tested per UG-84.1 General Note (c).
The Basic MDMT includes the (30F) PWHT credit if applicable.

PV Elite 2019
API-579 Calcs: Thinning
INPUT VALUES, Damage Description: Thinning From : 50
Inside Diameter Di 3658.000 mm

Thickness tnom 28.200 mm
Internal Pressure P 15.000 kgf/cm²
Design Temperature T 60 °C
Allowable Stress, Design S 1406.140 kgf/cm²
Allowable Stress, Ambient Sa 1406.140 kgf/cm²
Longitudinal Joint Efficiency EL 1.00
Circumferential Joint Efficiency EC 1.00
Specific Gravity G 0.00
Flaw Type General Metal Loss (Part 4)
Assessment Level Level 1 and 2
Future Corrosion Allowance FCAml 0.487 mm
Allowable Remaining Strength Factor RSFa 0.90
Measurement Method Point Thickness Readings

Number of Rows 24
Layout Angle 0.00 deg.
Rlife Thickness Approach included? Yes

Rlife MAWP Approach included? Yes
Corrosion Rate Crate 0.1220 mm/year
Previous Average Measured Thickness tam_prev 24.800 mm
Using design MAWP? No
Using overriding values? No
Thickness Measurements (mm):
No. PTR No. PTR No. PTR No. PTR No. PTR No. PTR
1 24.8 2 24.9 3 24.9 4 24.8 5 24.9 6 24.8

7 24.8 8 24.8 9 24.8 10 24.8 11 24.9 12 24.9
13 24.8 14 24.9 15 24.9 16 24.9 17 24.8 18 24.9
19 24.9 20 24.8 21 24.8 22 24.8 23 24.9 24 24.8
API 579 / ASME FFS-1, 2016 Edition
Part 4, General Metal Loss

Level 1 Assessment
Point Thickness Readings
STEP 1 - Take point thickness reading data and determine

minimum measured thickness, average measured thickness and coefficient
of variation.
Minimum Measured Thickness, [tmm]:

= 24.790 mm
Average Measured Thickness, [tam]:

= Sum of points/N
= 596.24/24
= 24.843 mm
Sum of Squares, [S]:

= SUM(trd, i - tam)^(2)
= 0.000 cm²
Coefficient of Variation, [COV]:

= ( 1 / tam )( S / ( N - 1 ) )^(0.5)
= ( 1/24.843 )( 0./( 24 - 1 ) )^(0.5)
= 0.002
STEP 2 - Determine viability of the point thickness readings

PV Elite 2019
through the coefficient of variation criterion.
Coefficient of Variation < 0.1

0.002 < 0.1
PASSED
The coefficient of variation is within the recommended values.
STEP 3 - Level 1 Criteria
Minimum Measured Thickness Criterion
Minimum Required Thickness from Circumferential Stress, [tmin_C]:

= ( P * R )/( S * E - 0.6 * P )
= ( 15.0 * 1829.487 )/( 1406.14 * 1.0 - 0.6 * 15.0 )
= 19.642 mm
Minimum Required Thickness from Longitudinal Stress, [tmin_L]:

= ( P * R )/( 2 * S * E + 0.4 * P )
= ( 15.0 * 1829.487 )/
( 2 * 1406.14 * 1.0 + 0.4 * 15.0 )
= 9.737 mm
Minimum Required Thickness, [tmin]:

= max( tmin_C, tmin_L )
= max( 19.642, 9.737 )
Limiting Thickness [t_lim]:

= max( 0.2 * tnom, 2.5 mm )
= max( 0.2 * 28.2, 2.5)
= 5.640 mm
( tmm - FCAml ) >= max( 0.5 * tmin, t_lim )

( 24.79 - 0.487 ) >= max( 0.5 * 19.642, 5.64 )
24.303 >= 9.821
PASSED
The minimum measured thickness criterion passed.
Average Measured Thickness Criterion
(tam - FCAml) >= tmin_C

(24.843 - 0.487) >= 19.642
24.356 >= 19.642
PASSED
The average measured thickness criterion passed.
Maximum Allowable Working Pressure Criterion
Note: Level 1 calculations assume that all supplemental loads are negligible.
Rerated MAWP, Circumferential [MAWPrC]:

= ( S * E( tam - FCAml ) )/( R + 0.6( tam - FCAml ) ) - Pstatic
= ( 1406.14 * 1.0( 24.843 - 0.487 )/
( 1829.487 + 0.6( 24.843 - 0.487 ) ) - 0.0
= 18.572 kgf/cm²
Rerated MAWP, Longitudinal [MAWPrL]:

= ( 2 * S * E( tam - FCAml ) ) )/( R - 0.4( tam - FCAml ) )
= ( 2 * 1406.14 * 1.0( 24.843 - 0.487 ) )/
( 1829.487 - 0.4( 24.843 - 0.487 ) )
= 37.641 kgf/cm²
PV Elite 2019
Determine the minimum MAWP, where tmin is the wall thickness.
MAWP, Circumferential [MAWPC]:

= ( S * E * tmin )/( R + 0.6 * tmin ) - Pstatic
= ( 1406.14 * 1.0 * 19.642 )/( 1829.487 + 0.6 * 19.642 ) - 0.0
= 15.000 kgf/cm²
MAWP, Longitudinal [MAWPL]:

= ( 2 * S * E * tmin )/( R - 0.4 * tmin )
= ( 2 * 1406.14 * 1.0 * 19.642 )/
( 1829.487 - 0.4 * 19.642 )
= 30.323 kgf/cm²
Minimum MAWP, [MAWP]:

= min( MAWPC, MAWPL )
= min( 15.0, 30.323 )
= 15.000 kgf/cm²
MAWPrC >= MAWP

18.572 >= 15.0
PASSED
The maximum allowable working pressure criterion passed.
Summary of Level 1 Assessment: P/F
Minimum Measured Thickness Criterion: PASSED

Average Measured Thickness Criterion: PASSED
Maximum Allowable Working Pressure Criterion: PASSED
This analysis passed the API 579 Part 4, Level 1 Assessment.
Part 4, General Metal Loss

Level 2 Assessment
Average Measured Thickness Criterion
Determine tmin_C and tmin_L using P * RSFa.
Minimum Required Thickness from Circumferential Stress, [tmin_C]:

= ( ( P * RSFa ) * R )/( S * E - 0.6( P * RSFa ) )
= ( ( 15.0 * 0.9 ) * 1829.487 )/
( 1406.14 * 1.0 - 0.6( 15.0 * 0.9 ) )
= 17.666 mm
Minimum Required Thickness from Longitudinal Stress, [tmin_L]:

= ( ( P * RSFa ) * R )/( 2 * S * E + 0.4( P * RSFa ) ) + tsl
= ( ( 15.0 * 0.9 ) * 1829.487 )/
( 2 * 1406.14 * 1.0 + 0.4( 15.0 * 0.9 ) ) + 0.0
= 8.765 mm
( tam - FCAml ) >= max( tmin_C, tmin_L )

( 24.843 - 0.487 ) >= max( 17.666, 8.765 )
24.356 >= 17.666
PASSED
The average measured thickness criterion passed.
Maximum Allowable Working Pressure Criterion

PV Elite 2019
Summary of Level 2 Assessment: P/F
Minimum Measured Thickness Criterion: PASSED

Average Measured Thickness Criterion: PASSED
Maximum Allowable Working Pressure Criterion: PASSED
This analysis passed the API 579 Part 4, Level 2 Assessment.
Remaining Life Assessment

Thickness Approach
Remaining Life, [R_life]:

= ( tam_prev - tmin )/Crate
= ( 24.8 - 17.666 )/0.122
= 58.5 years
MAWP Approach
STEP 1- Determine the metal loss of the component.
Metal Loss, [t_loss]:

= tnom - tam_prev
= 28.2 - 24.8
= 3.400 mm
STEP 2 - Determine the MAWP based on the effective corrosion allowance,

for a series of increasing time increments, and the nominal thickness.
Effective Corrosion Allowance, [CAe]:

= t_loss + Crate * time
= 3.4 + 0.122 * time
time CAe MAWPr

year(s) mm kgf/cm²
1.0 3.51 18.82

2.0 3.63 18.73
3.0 3.75 18.64
4.0 3.88 18.55
5.0 4.00 18.46
6.0 4.12 18.36
7.0 4.24 18.27
8.0 4.36 18.18
9.0 4.49 18.09
10.0 4.61 17.99
11.0 4.73 17.90
12.0 4.85 17.81
13.0 4.97 17.72
14.0 5.10 17.62
15.0 5.22 17.53
16.0 5.34 17.44
17.0 5.46 17.35
18.0 5.58 17.25
19.0 5.71 17.16
20.0 5.83 17.07
21.0 5.95 16.98
22.0 6.07 16.89
23.0 6.19 16.79
24.0 6.32 16.70
25.0 6.44 16.61
26.0 6.56 16.52
27.0 6.68 16.42
PV Elite 2019
28.0 6.80 16.33

29.0 6.93 16.24
30.0 7.05 16.15
31.0 7.17 16.05
32.0 7.29 15.96
33.0 7.41 15.87
34.0 7.54 15.78
35.0 7.66 15.68
36.0 7.78 15.59
37.0 7.90 15.50
38.0 8.02 15.41
39.0 8.15 15.31
40.0 8.27 15.22
41.0 8.39 15.13
42.0 8.51 15.04
STEP 3 - Determine the remaining life from the time at which the
iterative MAWP intersects the design MAWP.
Final Values:
42.3 8.56 15.00

PV Elite 2019
Vessel Design Summary: Step: 31 10:40am Aug 29,2023
Diameter Spec : 3658.000 mm ID

Vessel Design Length, Tangent to Tangent 1716.70 cm
Specified Datum Line Distance 20.00 cm
Internal Design Temperature 60 °C

Internal Design Pressure 15.000 kgf/cm²
External Design Temperature 33 °C

External Design Pressure 1.030 kgf/cm²
Maximum Allowable Working Pressure 15.218 kgf/cm²

External Max. Allowable Working Pressure 1.221 kgf/cm²
Hydrostatic Test Pressure 0.000 kgf/cm²
Required Minimum Design Metal Temperature -8.0 °C

Warmest Computed Minimum Design Metal Temperature -13.0 °C
Wind Design Code ASCE-93

Earthquake Design Code UBC-94
Materials of Construction:
Component Normal Impact
Type Material Class Thickness UNS # ized Tested
Shell SA-516 70 ... ... K02700 No Yes

Head SA-516 70 ... ... K02700 No Yes
Nozzle SA-106 B ... ... K03006 No No
Re-Pad SA-516 70 ... ... K02700 No No
Nozzle Flg SA-105 ... ... K03504 No No
Hrz Bolting SA-193 B7 ... 2 1/2 < t <= 4 G41400 No No
Normalized is determined based on the UCS-66 material curve selection and Figure UCS-66.
Impact Tested is based on material selection and material data properties.
Element Pressures and MAWP (kgf/cm² & mm):
Design Str. In
Element Description Pressure Ext. Element Corrosion Flg. Creep
or Type + Stat. head Press. M.A.W.P Allowance Gov. Range
HEAD 1 15.000 1.03 20.341 0.0000 Yes No

SHELL 1 15.000 1.03 18.761 0.0000 N/A No
SHELL 2 15.000 1.03 18.897 0.0000 N/A No
SHELL 3 15.000 1.03 18.897 0.0000 N/A No
SHELL 4 15.000 1.03 21.482 0.0000 N/A No
SHELL 5 15.000 1.03 18.890 0.0000 N/A No
SHELL 6 15.000 1.03 18.912 0.0000 N/A No
SHELL 7 15.000 1.03 18.897 0.0000 N/A No
SHELL 8 15.000 1.03 18.890 0.0000 N/A No
SHELL 9 15.000 1.03 18.897 0.0000 N/A No
HEAD 2 15.000 1.03 20.402 0.0000 Yes No
Element Types and Properties:
Element "To" Elev Element Nominal Finished Reqd Thk Reqd Thk Long Circ
Length Thickness Thickness Internal External Eff Eff
Type cm cm mm mm mm mm
Ellipse 0.0 20.0 ... 26.7 13.8 7.3 1.00 1.00

Cylinder 186.3 186.3 ... 24.6 19.6 22.8 1.00 1.00
PV Elite 2019
Vessel Design Summary: Step: 31 10:40am Aug 29,2023
Cylinder 372.6 186.3 ... 24.8 19.6 22.8 1.00 1.00

Cylinder 558.9 186.3 ... 24.8 19.6 22.8 1.00 1.00
Cylinder 745.2 186.3 ... 28.2 19.6 22.9 1.00 1.00
Cylinder 931.5 186.3 ... 24.8 19.6 22.8 1.00 1.00
Cylinder 1117.8 186.3 ... 24.8 19.6 22.8 1.00 1.00
Cylinder 1304.1 186.3 ... 24.8 19.6 22.8 1.00 1.00
Cylinder 1490.4 186.3 ... 24.8 19.6 22.8 1.00 1.00
Cylinder 1676.7 186.3 ... 24.8 19.6 22.8 1.00 1.00
Ellipse 1696.7 20.0 ... 26.8 13.8 7.3 1.00 1.00
Saddle Parameters:
Saddle Width 300.000 mm
Saddle Bearing Angle 135.000 deg.
Centerline Dimension 2429.000 mm
Wear Pad Width 500.000 mm
Wear Pad Thickness 24.000 mm
Wear Pad Bearing Angle 162.000 deg.
Distance from Saddle to Tangent 1000.000 mm
Baseplate Length 2989.990 mm

Baseplate Thickness 22.000 mm
Baseplate Width 380.000 mm
Number of Ribs (including outside ribs) 6
Rib Thickness 22.000 mm
Web Thickness 22.000 mm
Height of Center Web 250.000 mm
Baseplate Sketch
|------------------- 2989.990 mm --------------------|

------------------------------------------------------ ---
| |
| | 380.000 mm
| |
------------------------------------------------------ ---
Baseplate Plan View
------------------------------------------------------ ---
| | 22.000 mm
------------------------------------------------------ ---
Baseplate Side View
Note: The Wind and Seismic loads were not load factored in this analysis.
Weights:
Fabricated - Bare W/O Removable Internals 55054.0 kg
Shop Test - Fabricated + Water ( Full ) 252465.9 kg
Shipping - Fab. + Rem. Intls.+ Shipping App. 55054.0 kg
Erected - Fab. + Rem. Intls.+ Insul. (etc) 55054.0 kg
Empty - Fab. + Intls. + Details + Wghts. 55054.0 kg
Operating - Empty + Operating Liquid (No CA) 55054.0 kg
Field Test - Empty Weight + Water (Full) 252465.9 kg

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PV Elite® 2019

Project Data Page:

In Accordance with ASME Section VIII Division 1

ASME Code Version : 2017

Analysis Performed by : SPLM Licensed User

Job File : E:\PV\FFS-579.Pvdb

Date of Analysis : Aug 29,2023 10:40am

PV Elite 2019 SP1, March 2019

Class From To : Basic Element Checks.

Class From To: Check of Additional Element Data

There were no geometry errors or warnings.

PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2019

PV Elite Vessel Analysis Program: Input Data

Design Internal Pressure (for Hydrotest) 15 kgf/cm²

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

Wind Design Code ASCE-7 93

Seismic Design Code UBC 94

Design Pressure + Static Head Y

Material Database Year Current w/Addenda or Code Year

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

Using Metric Material Databases, ASME II D No

Complete Listing of Vessel Elements and Details:

Element From Node 10

Element From Node 20

Design Temperature Internal Pressure 60 °C

Element From Node 20

Element From Node 20

Element From Node 20

Element From Node 20

Element From Node 30

Element From Node 30

Element From Node 40

Element From Node 40

Height of Composite Ring Stiffener 0 mm

Element From Node 50

Element From Node 50

Element From Node 50

Element From Node 60

Distance "FROM" to "TO" 186.3 cm

Element From Node 60

Element From Node 60

Element From Node 60

Element From Node 60

Grade of Attached Flange GR 1.1

Element From Node 60

Element From Node 60

Element From Node 70

Element From Node 80

Design Temperature External Pressure 33 °C

Element From Node 80

Element From Node 80

Element From Node 80

Element From Node 80

Element From Node 90

Element From Node 100

Element From Node 100

Element From Node 100

Nozzle Diameter 2 in.

Element From Node 110

Percent Elong. per UCS-79, VIII-1-01-57 (75tnom/Rf)(1-Rf/Ro) 3.151 %

% Elongation per Table UG-79-1 (50tnom/Rf(1-Rf/Ro)) 0.668 %

% Elongation per Table UG-79-1 (50tnom/Rf(1-Rf/Ro)) 0.673 %

% Elongation per Table UG-79-1 (50tnom/Rf(1-Rf/Ro)) 0.673 %

% Elongation per Table UG-79-1 (50tnom/Rf(1-Rf/Ro)) 0.765 %