Pressure Vessel Design

SINGLE CHAMBER UNFIRED PRESSURE VESSEL WORKBOOK -- VERSION 09082015eASME CODE SECTION VIII, DIVISION I, 2013 EDITION

sources such as the web, I removed any company references before adapting them to interface with the complete workbook. My advice is to use this workbook a master and then work in copies only. Making entries directly in sheet may overide formulas.

Information is distributed to the calculating page (tabs) and results show on both the "tab" page and "WORKSHEET". Remember to press F9. The pages are protected to keep the formulas safe, but you can remove the protection to make changes with "Tools". There is no password.

There are drop down selections for the type of head. If you choose "WELD CAP" for head A, the workbook will default to WELD CAP throughout the book. If needed you can change the Dish and Knuckle radius of the F&D heads. Nozzles are calculated as being in the center 80% of the heads. If you select "F" for forged shell, the elliptical heads will be treated as forged with no thin-out. Weld caps are caluclated as 2:1 ellipticals with 12.5% undertolerance applied. Note that the weld cap thickness and shell thickness must be the same and will have the same pressure rating.There are sheets to compute the thickness required for flat heads and bolt on flat heads based on UG-34 and cones based on Appendix 1-5.When a Cone is selected as a Head, Head A Nozzle 3 and Head B Nozzle 2 are reserved as a nozzle in the cone's small end or an elliptical head on the cone. If no nozzle is used in the small end of the cone, a head will be calculated to seal it off. NOTE: The cone long seam efficiency will default to that of the shell.If you are going to have a CONE, you should fill in the YELLOW areas of the CONE sheet first. Otherwise some flags will pop up.You may have a shell attached to the small end of the cone by entering the length of that shell in the Shell #2 sheet. You must choose the location of thenozzles in Shell #1, Shell #2, or the side of the Cone by selecting the location. Head A & B nozzles locations may be located in the head or cone by selectingthe location. If you need more nozzles you can copy a nozzle sheet. New sheets will not be supported by the WORKSHEET.Please note that only original shell, heads and nozzles are calculated in the "VESSEL COSTING" sheet since it gets information from the "WORKSHEET" only.NOTE: WHEN A CONE IS SELECTED ENTRIES MUST BE MADE IN THE "CONE", "HEAD on CONE", and "SHELL #2" SHEETS IF USED. You must

may be entered in Shell nozzles 2 thru 5, Head A nozzles 1 & 2, and Head B nozzle 1. You must enter the offset on the nozzle worksheet page.If a swing bolt closure is being used, you must complete all entries in the "Closure" sheet. The closure may be attached to a cone, shell, or nozzle"

Shell #2 and Head on cone may be used as a boot on a horizontal vessel by making direct inputs on their sheets.

There are warning flags to help keep you from making mistakes. Remember to tell the sheet when you are using pipe, so it can derate the 12 1/2%. Please note that 2.375" I.D. and smaller do not require reinforcement calculations, more information is provided at the bottom of the "WORKSHEET".. Also note that when tangent nozzles are used, if the larger developed opening is greater than 2x the smaller, extra calculations are required.

Lifting lugs, baseplate, and skirt calculations for vertical vessels are done in the "Tower" sheet. It requires extra entries (see the yellow sections).Buckling calculations are performed for towers on the Tower sheet. Note that large diameter thin wall horizontal vessels should be analized for buckling also.

To print your results just go to the tabs you need to print and print them. Each tab is formatted to print, page print areas are already set.

For your information, there is a "Material Database" tab. Pipe/flange information is on the bottom of the "WORKSHEET" and in the "Flanges & pipe" tab. When using an Android tablet you type in the material type like it is found in the material database, the stress value will auto fill (if it is in the database).

Shell external pressure may be calculated using the "SHELL EXTERNAL" tab. You can change the length of the shell to determine how many re-inforcement rings (if any) are needed. I did not include the ring calculations. You must use the included charts for values "A" and "B".

I have modified the nozzle sheets to zero out left over reinforcement inputs if you forget to delete them on the WORKSHEET when not needed. There is drop down menu for flanges and couplings in the Nozzle area. For size enter the nominal pipe size, the O.D. will be calculated. Long weld neck andcouplings O.D. and thickness is calculated for you. If you select "OTHER" for Nozzle thickness you will be prompted to enter the nozzle O.D. (in Blue) and enter the I.D. instead on NPS. Flange pressure ratings are calculated for SA-105N and 316/316L (dual grade) materials only. Note: Flange pressure rating are calculated

pressure rating calculations are by-passed. You may use rolled plate or a forging for a nozzle neck by selecting "OTHER" then in the Nozzle sheet change the efficiency.Welding time calculations are for comparison purposes only so you can see the impact of changes in your design. Head seams are included on shells and cones.

The "VESSEL COSTING" tab contains a costing worksheet. It takes information from the summary page and calculates most of the vessel cost. You will need to make some inputs there. Such as the heat treating, x-ray, painting, and inspection. Most of these are calculated for you, but you should review them. There is a vessel internal area that you can use…double check to see that the costing makes it to the top of the sheet. You must put prices in for the flanges. The spreadsheet does not calculate them, however it does calculate the repad (if any) and nozzle cost.

Disclaimer: I strongly suggest that you check the results given by this worksheet. I assembled this information to assist in estimating vessels. Final design of any vessel should be done with the appropriate software or by a qualified engineer.

All sheets in this workbook have been reviewed against ASME Code Section VIII Division 1 Edition 2013, ASME B16.5, ASME B31.3, and/or

This workbook is for Vertical or Horizontal single chamber vessels. Since I have made major changes and corrections to sheets that were from other

The Workbook allows either I.D. or O.D. shells and heads. You must enter either the I.D. or the O.D. on the cover page, but not both.PLEASE NOTE THAT YOU SHOULD PRESS THE "F9" KEY AFTER NOZZLE REINFORCEMENT ENTRIES, Excel has a problem with large workbooks.You make entries mainly on the "COVER PAGE" and "WORKSHEET" tabs below. Please re-set the reinforcement material to "INHERENT" when not used.

Make your changes (entries) in the "yellow" areas. There are comment flags to help you. You must enter types and thickness for Head A and Head B.

also enter the distance from the Large Outside Diameter of the cone for nozzles in the side of a cone on the sheet for that nozzle. Tangent or offset nozzles

Note: UG-36 (3)(-c) no two isolated unreinforced openings shall have their centers closer to each other than the sum of their diameters.

from -20F to 600F, above 600F is approximate only. Nozzles are calculated for Shell, Elliptical Head, F&D Head, Elliptical of Weld Cap, and on Cone. Nozzles in Cone are calculated for information only by this workbook and may not totally comply with ASME Code Section VIII Div, 1. If you select "OTHER", the flange

Megyesy's Pressure Vessel Handbook for accuracy. Please email me at [email protected] with any comments or complaints.

COMPANY NAMEADDRESS

CITY, STATE

ASME CODE SECTION VIII, DIVISION I2013 EDITION

PRESSURE VESSEL CALCULATIONSSPREADSHEET VERSION: 09082015e

Customer name:

VESSEL O.D. 0 INCHVESSEL I.D. 0 INCHSHELL S/S LENGTH 0 INCH

VESSEL ORIENTATION HORIZONTAL VERTICALHORIZONTAL

JOB NO. 0 Drawing no:

NAMEPLATE INFORMATION

Vessel MAWP: 0 PSIG ALERT -- Below Code requirementDesign Temperature: 0 F INCREASEMin. Temperature 0 FSerial Number:National Board No. NONE ###Year Built: 2015 ###Radiography: NONE ###Post Weld Heat Treat NONE ###Construction Type: W ###Special Type:Corrosion Allowance 0.00000

Signature(s):

_____________________________________________ Date: 4/22/2023

_____________________________________________ Date: _________

E16

Enter either outside diameter (O.D.) or inside (I.D.) below, but not both.

E17

Enter either inside diameter (I.D.) or outside (O.D.) above, but not both.

E18

Enter main shell section length only.

C23

For your reference only, appears on all sheets.

D27

Division 1 begins at 15 psig ends at 3500 psig, but higher or lower pressures may be built using Div.1 formulas. Howerver Division 2 or 3 may be more economical.

D28

I have limited the flange pressure calculations to 600F. Design temperatre must me greater than minimum design temperature.

D29

I did not include low temperature carbon steel in the material selection. Check the minimum allowable per UCS-66 if below -20F is used.

D36

Example: "L" for Lethal service

COMPANY NAME 4/22/2023 ENTRY AREA WELDING 0.00 (HOURS)RESULTS AREA

VESSEL PURPOSE JOB NO. 0CUSTOMER NAME 0 LIFTING LUG (4:1 SAFETY FACTOR) MANHOURS 0VESSEL DESIGN SUMMARY HOLE DIAMETER 1 INCH 0DESIGN TEMPERATURE (COVER Pg) F. 0 0 OUTSIDE RADIUS 2 INCH(See Material Database temperature and flange ratings.) #N/A MIN.SHELL THICKNESS MATERIAL SA-240 304LVESSEL SHELL O.D. (COVER Pg) 0 INCH LUG STRESS VALUE 14,613 PSIVESSEL SHELL I.D. (COVER Pg) 0 INCH VESSEL WEIGHT 0 LBSMAIN SHELL S/S LENGTH (COVER Pg) 0 INCH DESIGN THICKNESS (MIN) 0.375 INCHNUMBER OF MAIN SHELL CYLINDERS 1 (DETERMINES GIRTH SEAMS) REQUIRED WELD (CODE) 0.250 INCHNUMBER OF SHELL LONG SEAMS 0 (0) FOR PIPE SHELLS (F) FORGING REQUIRED WELD (LOAD) 0.262 INCHDESIGN PRESSURE (COVER Pg) 0.00 PSIG STATIC HEAD PRESSURE 0.00 PSIG HYDROTEST PRESSURE 0 PSIGVESSEL ORIENTATION HORIZONTAL HSHELL MATERIAL INHERENT PIPE #N/A CURVE 'A' MATERIALSHELL STRESS VALUE #N/A PSI Impact testing exempt per UG20(F)SHELL THICKNESS 0.0000 INCH #N/A #N/A PSIG MAX CURVE "B" CURVE "D"SHELL JOINT EFF. 65% UCS-66 MIN. TEMP - SHELL #N/A #N/AHEAD MATERIAL SA-36 FOR HEADS AND NOZZLES SEE MATERIAL SHEETHEAD STRESS VALUE 16,600 PSI #N/AHEAD A (TOP/END) TYPE/THICKNESS ELLIPTICAL 0.0000 INCH #DIV/0! PSIG MAX #DIV/0!HEAD B (BOT/END) TYPE/THICKNESS ELLIPTICAL 0.0000 INCH #DIV/0! PSIG MAX #DIV/0!HEAD JOINT EFF. 70% X-RAY Check Code requirementCORROSION ALLOWANCE (COVER Pg) 0.000 INCHSHELL VOLUME 0.00 CUFT 0.00 GAL SEPARATOR CAPACITY 40% FLOODEDHEAD VOLUME 0.00 CUFT 0.00 GAL RETENTION TIME 5 MINUTESTOTAL VOLUME 0.00 CUFT 0.00 GAL TWO PHASE 0 Bbl/DTOTAL DRY WEIGHT 0.00 LBS THREE PHASE 0 Bbl/DHYDROTEST WEIGHT 0.00 LBS

NOZZLES IN SHELLS OR CONE SIDE NOZZLES IN HEADS OR CONESUG-36 MAX. SHELL NOZZLE I.D. SIZE (INCH) 0.000 0 0 HEAD A (END) ELLIPTICALNOZZLE 1 -- NOT USED 0.0000 INCH/PSI OTHER HEAD A NOZZLE 1 -- NOT USED 0.0000 INCH/PSI OTHERDESCRIPTION/SIZE (IN) OTHER 0 INCH I.D. DESCRIPTION/SIZE (IN) OTHER 0 INCH I.D.NUMBER OF NOZZLES 0 NUMBER OF NOZZLES 0NOZZLE MATERIAL INHERENT NOZZLE MATERIAL INHERENTSTRESS VALUE 0 PSI STRESS VALUE 0 PSIPIPE (1) FORGING/PLATE (0) 0 TYPE ENTER O.D PIPE (1) FORGING (0) 0 TYPE ENTER O.DNOZZLE THICKNESS OTHER INCH 0.000 0 NOZZLE THICKNESS OTHER INCH 0.000EXTERNAL PROJECTION 0 INCH INCREASE EXTERNAL PROJECTION 0 INCH INCREASEINTERNAL PROJECTION 0 INCH INTERNAL PROJECTION 0 INCHCORROSION ALLOWANCE 0.0000 INCH CORROSION ALLOWANCE 0.0000 INCHOUTSIDE FILLET WELD 0 INCH OUTSIDE FILLET WELD 0 INCHINSIDE FILLET WELD 0 INCH INSIDE FILLET WELD 0 INCHREINFORCEMENT CALCULATIONS NOT REQUIRED LOCATION SHELL REINFORCEMENT CALCULATIONS NOT REQUIRED LOCATION N/AWITH REPAD (Not Required) WITH REPAD (Not Required)NUMBER OF NOZZLES 0 NUMBER OF NOZZLES 0REPAD MATERIAL INHERENT REPAD MATERIAL INHERENTSTRESS VALUE 0 PSI INCREASE STRESS VALUE 0 PSI INCREASETHICKNESS 0 INCH THICKNESS 0 INCHREPAD O.D. 0 INCH INCREASE REPAD O.D. 0 INCHREPAD OS FILLET WELD 0 INCH REPAD OS FILLET WELD 0 INCHUG-27 UG-27UG-45 Thickness (IN) 0.0000 UG-45 Thickness (IN) 0.0000MATERIAL REPLACEMENT NA MATERIAL REPLACEMENT NATangent nozzles allowed - Sheet "SHELL NOZZLE 2"NOZZLE 2 -- NOT USED 0.0000 INCH/PSI OTHER HEAD A NOZZLE 2 -- NOT USED 0.0000 INCH/PSI OTHERDESCRIPTION/SIZE (IN) OTHER 0 INCH I.D. DESCRIPTION/SIZE (IN) OTHER 0 INCH I.D.NUMBER OF NOZZLES 0 NUMBER OF NOZZLES 0NOZZLE MATERIAL INHERENT NOZZLE MATERIAL INHERENTSTRESS VALUE 0 PSI STRESS VALUE 0 PSIPIPE (1) FORGING (0) 0 TYPE ENTER O.D PIPE (1) FORGING (0) 0 TYPE ENTER O.DNOZZLE THICKNESS OTHER INCH 0.000 NOZZLE THICKNESS OTHER INCH 0.000EXTERNAL PROJECTION 0 INCH INCREASE EXTERNAL PROJECTION 0 INCH INCREASEINTERNAL PROJECTION 0 INCH INTERNAL PROJECTION 0 INCHCORROSION ALLOWANCE 0.0000 INCH CORROSION ALLOWANCE 0.0000 INCHOUTSIDE FILLET WELD 0 INCH OUTSIDE FILLET WELD 0 INCHINSIDE FILLET WELD 0 INCH INSIDE FILLET WELD 0 INCHREINFORCEMENT CALCULATIONS NOT REQUIRED LOCATION SHELL REINFORCEMENT CALCULATIONS NOT REQUIRED LOCATION N/AWITH REPAD (Not Required) WITH REPAD (Not Required)NUMBER OF NOZZLES 0 NUMBER OF NOZZLES 0REPAD MATERIAL INHERENT REPAD MATERIAL INHERENTSTRESS VALUE 0 PSI INCREASE STRESS VALUE 0 PSI INCREASETHICKNESS 0 INCH THICKNESS 0 INCHREPAD O.D. 0 INCH INCREASE REPAD O.D. 0 INCHREPAD OS FILLET WELD 0 INCH REPAD OS FILLET WELD 0 INCHUG-27 UG-27

J4

Pressure retaining components only. Does not include skirt, saddles, or internals.

C11

Enter number of main shells. Example: 240" s/s would require at least two 120" cylinders. This entry is used by the costing sheet only. Quantity is computed on "Shell" sheet.

C12

If pipe is used enter "0", this applies the undertolerance to the main shell. Shell #2 is determined by your entry on that sheet.

C14

If the vessel is to be operated flooded and the extra pressure from the weight of the liquid is not included in the MAWP, add it here.

C16

Enter material for main shell. Shell #2 is entered in Shell #2 sheet.

C18

Main shell thickness. Shell #2 thickness is entered in Shell #2 sheet.

C19

Defines joint efficiency for main shell and Shell #2. Shell #2 can be changed.

C22

If Head A is part of a swing bolt closure, choose ELLIPTICAL.

C24

Defines head joint efficiency. This can be changed in the head and cone sheets.

C34

Calculated outside diameter of nozzle

E34

Calculated maximum working pressure for flange or coupling

D35

Enter the nominal pipe size or the I.D. of a fabricated nozzle

C36

Number of nozzles this size in shell with the same characteristics

C39

Applies 12.5% undertolerance to nozzle

E40

If a fabricated or unlisted nozzle is used enter the O.D. for it here. Nozzle thickness will be calculated.

C44

Weld Leg 41

C45

Weld Leg 43

E46

Allows the nozzle to be located in main Shell or Shell #2 on cone.

J46

Allows nozzle to be installed in the cone side, small end of the cone, on a head located on the main shell, shell #2, or cone.

C53

Weld Leg 42

C55

Calculated Nozzle wall thickness.

E70


J70

Allows nozzle to be installed in the cone side, small end of the cone, on a head located on the main shell, shell #2, or cone.

UG-45 Thickness (IN) 0.0000 UG-45 Thickness (IN) 0.0000MATERIAL REPLACEMENT NA MATERIAL REPLACEMENT NATangent nozzles allowed - Sheet "SHELL NOZZLE 3"NOZZLE 3 -- NOT USED 0.0000 INCH/PSI OTHER HEAD A NOZZLE 3 -- NOT USED 0.0000 INCH/PSI OTHERDESCRIPTION/SIZE (IN) OTHER 0 INCH I.D. DESCRIPTION/SIZE (IN) OTHER 0 INCH I.D.NUMBER OF NOZZLES 0 NUMBER OF NOZZLES 0NOZZLE MATERIAL INHERENT NOZZLE MATERIAL INHERENTSTRESS VALUE 0 PSI STRESS VALUE 0 PSIPIPE (1) FORGING (0) 0 TYPE ENTER O.D PIPE (1) FORGING (0) 0 TYPE ENTER O.DNOZZLE THICKNESS OTHER INCH 0.000 NOZZLE THICKNESS OTHER INCH 0.000EXTERNAL PROJECTION 0 INCH INCREASE EXTERNAL PROJECTION 0 INCH INCREASEINTERNAL PROJECTION 0 INCH INTERNAL PROJECTION 0 INCHCORROSION ALLOWANCE 0.0000 INCH CORROSION ALLOWANCE 0.0000 INCHOUTSIDE FILLET WELD 0 INCH OUTSIDE FILLET WELD 0 INCHINSIDE FILLET WELD 0 INCH INSIDE FILLET WELD 0 INCHREINFORCEMENT CALCULATIONS NOT REQUIRED LOCATION SHELL REINFORCEMENT CALCULATIONS NOT REQUIRED LOCATION N/AWITH REPAD (Not Required) WITH REPAD (Not Required)NUMBER OF NOZZLES 0 NUMBER OF NOZZLES 0REPAD MATERIAL INHERENT REPAD MATERIAL INHERENTSTRESS VALUE 0 PSI INCREASE STRESS VALUE 0 PSI INCREASETHICKNESS 0 INCH THICKNESS 0 INCHREPAD O.D. 0 INCH INCREASE REPAD O.D. 0 INCHREPAD OS FILLET WELD 0 INCH REPAD OS FILLET WELD 0 INCHUG-27 UG-27UG-45 Thickness (IN) 0.0000 UG-45 Thickness (IN) 0.0000MATERIAL REPLACEMENT NA MATERIAL REPLACEMENT NATangent nozzles allowed - Sheet "SHELL NOZZLE 4" 1 HEAD B (END) ELLIPTICALNOZZLE 4 -- NOT USED 0.0000 INCH/PSI OTHER HEAD B NOZZLE 1 -- NOT USED 0.0000 INCH/PSI OTHERDESCRIPTION/SIZE (IN) OTHER 0 INCH I.D. DESCRIPTION/SIZE (IN) OTHER 0 INCH I.D.NUMBER OF NOZZLES 0 NUMBER OF NOZZLES 0NOZZLE MATERIAL INHERENT NOZZLE MATERIAL INHERENTSTRESS VALUE 0 PSI STRESS VALUE 0 PSIPIPE (1) FORGING (0) 0 TYPE ENTER O.D PIPE (1) FORGING (0) 0 TYPE ENTER O.DNOZZLE THICKNESS OTHER INCH 0.000 NOZZLE THICKNESS OTHER INCH 0.000EXTERNAL PROJECTION 0 INCH INCREASE EXTERNAL PROJECTION 0 INCH INCREASEINTERNAL PROJECTION 0 INCH INTERNAL PROJECTION 0 INCHCORROSION ALLOWANCE 0.0000 INCH CORROSION ALLOWANCE 0.0000 INCHOUTSIDE FILLET WELD 0 INCH OUTSIDE FILLET WELD 0 INCHINSIDE FILLET WELD 0 INCH INSIDE FILLET WELD 0 INCHREINFORCEMENT CALCULATIONS NOT REQUIRED LOCATION SHELL REINFORCEMENT CALCULATIONS NOT REQUIRED LOCATION N/AWITH REPAD (Not Required) WITH REPAD (Not Required)NUMBER OF NOZZLES 0 NUMBER OF NOZZLES 0REPAD MATERIAL INHERENT REPAD MATERIAL INHERENTSTRESS VALUE 0 PSI INCREASE STRESS VALUE 0 PSI INCREASETHICKNESS 0 INCH THICKNESS 0 INCHREPAD O.D. 0 INCH INCREASE REPAD O.D. 0 INCHREPAD OS FILLET WELD 0 INCH REPAD OS FILLET WELD 0 INCHUG-27 UG-27UG-45 Thickness (IN) 0.0000 UG-45 Thickness (IN) 0.0000MATERIAL REPLACEMENT NA MATERIAL REPLACEMENT NATangent nozzles allowed - Sheet "SHELL NOZZLE 5" 1NOZZLE 5 -- NOT USED 0.0000 INCH/PSI OTHER HEAD B NOZZLE 2 -- NOT USED 0.0000 INCH/PSI OTHERDESCRIPTION/SIZE (IN) OTHER 0 INCH I.D. DESCRIPTION/SIZE (IN) OTHER 0 INCH I.D.NUMBER OF NOZZLES 0 NUMBER OF NOZZLES 0NOZZLE MATERIAL INHERENT NOZZLE MATERIAL INHERENTSTRESS VALUE 0 PSI STRESS VALUE 0 PSIPIPE (1) FORGING (0) 0 INCH ENTER O.D PIPE (1) FORGING (0) 0 TYPE ENTER O.DNOZZLE THICKNESS OTHER INCH 0.000 NOZZLE THICKNESS OTHER INCH 0.000EXTERNAL PROJECTION 0 INCH INCREASE EXTERNAL PROJECTION 0 INCH INCREASEINTERNAL PROJECTION 0 INCH INTERNAL PROJECTION 0 INCHCORROSION ALLOWANCE 0.0000 INCH CORROSION ALLOWANCE 0.0000 INCHOUTSIDE FILLET WELD 0 INCH OUTSIDE FILLET WELD 0 INCHINSIDE FILLET WELD 0 INCH INSIDE FILLET WELD 0 INCHREINFORCEMENT CALCULATIONS NOT REQUIRED LOCATION SHELL REINFORCEMENT CALCULATIONS NOT REQUIRED LOCATION N/AWITH REPAD (Not Required) WITH REPAD (Not Required)NUMBER OF NOZZLES 0 NUMBER OF NOZZLES 0REPAD MATERIAL INHERENT REPAD MATERIAL INHERENTSTRESS VALUE 0 PSI INCREASE STRESS VALUE 0 PSI INCREASETHICKNESS 0 INCH THICKNESS 0 INCHREPAD O.D. 0 INCH INCREASE REPAD O.D. 0 INCHREPAD OS FILLET WELD 0 INCH REPAD OS FILLET WELD 0 INCHUG-27 UG-27UG-45 Thickness (IN) 0.0000 UG-45 Thickness (IN) 0.0000MATERIAL REPLACEMENT NA MATERIAL REPLACEMENT NA

E94


J94

Allows nozzle to be installed in the small end of the cone or on a head located on the main shell, shell #2, or cone.

E118

Allows the nozzle to be located in Shell #!, Shell #2, or side of Cone. If side of cone, "Ln" must have didtance in nozzle sheet"

J118


E142

Allows the nozzle to be located in Shell #!, Shell #2, or side of Cone. If side of cone, "Ln" must have didtance in nozzle sheet"

J142


COMPANY NAMEASME CODE SECTION VIII, DIVISION I, 2013 EDITION


Shell Page 1 of 1PIPE USED AS SHELL 4/22/2023JOB NO. 0

Dimensions: 0 CYLINDERS = 1

0.0000.0000.0000.0000.000 0.000

Material and Conditions:INHERENT Material

#N/A0.650.65 0.000

12.5%0.0

Calculated Properties:((Di/2)^2)*pi()*L/1728 ((0/2)^2)*PI()*0/1728 = 0.00(Di+t)*pi()*L*t*40.84/144 (0+0)*PI()*0*0*40.84/144 = 0.00

Variables: Pipe used for shellt*UTP 0*0.1 = 0.000t-Corr-UT 0-0-0 = 0.000Di/2+UT+Corr 0/2+0+0= 0.000(Di/2)+t 0/2+0= 0.000

#N/A #N/A#N/A #N/A#N/A #N/A

Treq <= nt #N/A #N/A

#N/A #N/ATreq <= nt #N/A #N/Ant >= 0.0625+Corr 0 >= 0.0625 = ERROR

(S*El*nt)/(Ri+0.6*nt) #N/A #N/A(2*S*Ec*nt)/(Ri-0.4*nt) #N/A #N/A

#N/A #N/APMax >= P #N/A #N/A

Stress Classification:NOTE: Both validity checks need to be "Acceptable" in order to use this sheet

Treq < 0.5*(Do/2) #N/A #N/AP< 0.385*S*El #N/A #N/A

Minimum design temperature check: Impact testing exempt per UG20(F)UCS-66 CURVE 'B' RATING [F]: #N/A / 'D' [F]: #N/A

Allowable stress for vertical vessel: N/A(Tall thin wall vessel without stiffeners) N/A

Treq provides a worst case required thickness for nozzle analysis for a nozzle located on the long seam or circ seamThis sheet calculates vessel walls per ASME Section VIII Division 1 only.

All UG-16(b) minimum thickness requirements have not been taken into consideration here.

Use "SHELL EXTERNAL" sheet to check for allowable exterior pressure loads.

Do [in] - outside diameter Di [in] - inside diameter t [in] - nominal wall thickness L [in] -length Corr [in] - corrosion allowance

S [psi] - allowable stress El - long seam efficiency (circ stress) Ec - circ seam efficiency (long stress) UTP [%] - undertolerance allowance P [psi] - interior pressure

Volume [cuft] = Weight [lb] =

UT [in] = nt [in] = Ri [in] =

Ro [in] =

Required Thickness: UG-27(c)(1,2)

ta [in] = P*Ri/(S*El-0.6*P) ~~ long seam

tb [in] = P*Ri/(2*S*Ec+0.4*P) ~~ circ seamTreq [in] = MAX(ta,tb) ~~ required minimum thickness

CheckTreq =Required Thickness: Appendix 1-1(a)(1), UG-16(b)

ta [in] = P*Ro/(S*El+0.4*P) ~~ long seam

CheckTreq =Check UG-16(b) =

Maximum Pressure: UG-27(c)(1,2)Pint1 [psi] = Pint2 [psi] = PMax [psi] = Min(Pint1,Pint2) ~~ maximum allowed design pressure

CheckP =

ckValidity1 =ckValidity2 =

t Do

Length

Long Seam

I9

Computed based on 20' pipe or 10' rolled shell. Overide only if you are working from a copy.

B18

Use Weld efficiency program to calculate value

B19


B20

Typical -12.5% for pipe -0.0% for rolled plates and machined elements

ASME CODE SECTION VIII, DIVISION I, 2013 EDITIONPRESSURE VESSEL CALCULATIONS

SPREADSHEET VERSION: 09082015e

Shell #2 (Boot on Shell) Page 1 of 14/22/2023

JOB NO. 0

Dimensions: 0.000

0.0000.000

0 t [in] - nominal wall thickness t= 0.0000.0000.000

Material and Conditions: #N/AINHERENT Material 0.000#N/A

0 0.650 0.65

0.0% 0.0%0.0 0 CYLINDERS = 1

Calculated Properties:((Di/2)^2)*pi()*L/1728 ((0/2)^2)*PI()*0/1728 = 0.00(Di+t)*pi()*L*t*40.84/144 (0+0)*PI()*0*0*40.84/144 = 0.00

Variables: Rolled Plate used for shellt*UTP 0*0 = 0.000t-Corr-UT 0-0-0 = 0.000Di/2+UT+Corr 0/2+0+0= 0.000(Di/2)+t 0/2+0= 0.000

#N/A #N/A#N/A #N/A#N/A #N/A

Treq <= nt #N/A #N/A

#N/A #N/ATreq <= nt #N/A #N/Ant >= 0.0625+Corr 0 >= 0.0625 = ERROR

(S*El*nt)/(Ri+0.6*nt) #N/A #N/A(2*S*Ec*nt)/(Ri-0.4*nt) #N/A #N/A

#N/A #N/APMax >= P #N/A #N/A

Stress Classification:NOTE: Both validity checks need to be "Acceptable" in order to use this sheet

Treq < 0.5*(Do/2) #N/A #N/AP< 0.385*S*El #N/A #N/A


This sheet calculates vessel walls per ASME Section VIII Division 1 only. All UG-16(b) minimum thickness requirements have not been taken into consideration here.Use "SHELL EXTERNAL" sheet to check for allowable exterior pressure loads.

Do [in] - outside diameter Di [in] - inside diameter

L [in] -length Corr [in] - corrosion allowance

S [psi] - allowable stress El - long seam efficiency (circ stress) Ec - circ seam efficiency (long stress) UTP [%] - undertolerance allowance P [psi] - interior pressure

Volume [cuft] = Weight [lb] =

UT [in] = nt [in] = Ri [in] =

Ro [in] =


ta [in] = P*Ri/(S*El-0.6*P) ~~ long seamtb [in] = P*Ri/(2*S*Ec+0.4*P) ~~ circ seam

Treq [in] = MAX(ta,tb) ~~ required minimum thicknessCheckTreq =

Required Thickness: Appendix 1-1(a)(1), UG-16(b)

ta [in] = P*Ro/(S*El+0.4*P) ~~ long seam


Maximum Pressure: UG-27(c)(1,2)Pint1 [psi] = Pint2 [psi] = PMax [psi] = Min(Pint1,Pint2) ~~ maximum allowed design pressure

CheckP =

ckValidity1 =ckValidity2 =

t

Do

Leng

th

Long

Sea

m

B10

Enter boot outside diameter only. Leave blank for use on CONE.

G18


G19


G20


J21

Computed based on 20' pipe or 10' rolled shell. Overide only if you are working from a copy.



Page 1 of 1HEAD A ELLIPTICAL 2:1 RATIO Page 4/22/2023(TOP OR END)JOB NO. 0Dimensions:

0.0000.0000.0000.0000.0000.000

Material and Conditions:SA-36 Material 16,600

0.0%0.70

0.0Calculated Properties:note 1: Suggested thickness after forming Approx. head weight based on steel, lbs = 0.00

-0.0625 in Approx. head volume including skirt, cuft = 0.00Variables:

0*0 = 0.0000-0+0 = 0.000

0+2*0-(0*2) = 0.0000/4 = 0.000

h+nt 0+0 = 0.000D/(2*h) 0/(2*0) = #DIV/0!Do/(2*ho) 0+(0*2)/(2*0) = #DIV/0!#DIV/0! Interpolated value from table 1-4.1 1 = #DIV/0!#DIV/0! Interpolated value from table UG-37 0.9 = #DIV/0!#DIV/0! Interpolated value from table UG-33.1 0.889 = #DIV/0!Kzero*Do #DIV/0! #DIV/0!

tf/(Kone*D) #DIV/0! #DIV/0!#DIV/0!

#DIV/0! #DIV/0!Treq<=tf #DIV/0! #DIV/0!

nt >= 0.0625+Corr 0 >= 0.0625 = ERROR

#DIV/0! #DIV/0!Pmax >= P #DIV/0! #DIV/0!


All UG-16(b) minimum thickness requirements have not been taken into consideration here.Nozzles may be subject to a smaller required thickness depending on location in the head.Heads may be subject to stress relief if large elongation occurs - UCS-79(d), UNF-79(d), UHA-44(d)This sheet cannot be used to check for allowable exterior pressure loads.

Do [in] - outside diameter of head Di [in] - inside diameter of head tb [in] - thickness before forming tf [in] - thickness after forming (note 1) Corr [in] - corrosion allowance Skirt [in] - straight skirt length

S [psi] - allowable stress UTP [%] - undertolerance allowance E - head/shell joint efficiency P [psi] - interior pressure

ut [in] = tf*UTP ~~ undertorlerance allowancent [in] = tf-(Corr+ut) ~~ thickness with corrosion allowance removedD [in] = Do-2*nt ~ ID with corrosion allowance removedh [in] = D/4 ~~ inside crown height

ho [in] =D/2h =

Do/2ho =K =

Kone =Kzero =

Ro [in]=Required Thickness: App. 1-4(c), UG-37(a)(1)

App1-4(f) =

Treq [in] = (P*D*K)/(2*S*E-0.2*P)+Corr ~~ required minimum thickness


Maximum Pressure: App. 1-4(c), UG-37(a)(1)Pmax [psi] = (2*S*E*nt)/(K*D+0.2*nt) ~~ maximum allowed design pressure

CheckPMax =

B14

If not specified use the suggested value below note 1

B20


B21

Efficiency of weld in head. Not efficiency of head to shell. Use Weld Efficiency program.



Page 1 of 1HEAD B ELLIPTICAL 2:1 RATIO Page 4/22/2023(BOTTOM OR END)JOB NO. 0Dimensions:

0.0000.0000.0000.0000.0000.000


0.0%0.70

0.0Calculated Properties:note 1: Suggested thickness after forming Approx. head weight based on steel, lbs = 0.00


0*0 = 0.0000-0+0 = 0.000

0+2*0-(0*2) = 0.0000/4 = 0.000




nt >= 0.0625+Corr 0 >= 0.0625 = ERROR



All UG-16(b) minimum thickness requirements have not been taken into consideration here.Nozzles may be subject to a smaller required thickness depending on location in the head.Heads may be subject to stress relief if large elongation occurs - UCS-79(d), UNF-79(d), UHA-44(d)This sheet cannot be used to check for allowable exterior pressure loads.

Do [in] - outside diameter of head Di [in] - inside diameter of head tb [in] - thickness before forming tf [in] - thickness after forming (note 1) Corr [in] - corrosion allowance Skirt [in] - straight skirt length



ho [in] =D/2h =

Do/2ho =K =

Kone =Kzero =


App1-4(f) =




CheckPMax =

B14


B20


B21




Page 1 of 1HEAD A NOT USED (TOP or END) 4/22/2023

JOB NO. 0

Dimensions:

0.0000.0000.0000.0000.0000.0000.0000.000


0.700.0

Calculated Properties:note 1:Suggested radius L per UG-32(j) 0.00 Approx. head weight based on steel, lbs = 0.00note 2:Suggested radius IKR per UG-32(j) 0.000 Approx. head volume including skirt, cuft = 0.00note 3:Suggested thickness after forming -0.0320

Variables:0-0 = 0.000

0+2*0 = 0.000L/IKR 0/0 = #DIV/0!0.25*(3+sqrt(L/IKR)) 0.25*(3+SQRT(0/0)) = #DIV/0!L+tb 0+0 = 0.000

tf/L 0/0 = #DIV/0!if(AND(0.0005=<App1-4(f),App1-4(f)<0.002),"Calculation Required","Calculation not required")

#DIV/0!




App. 1-4(f) calculation is not included on this sheetNozzles may be subject to a smaller required thickness depending on location in the head.Heads may be subject to stress relief if large elongation occurs - UCS-79(d), UNF-79(d), UG-37(a)(1)All UG-16(b) minimum thickness requirements have not been taken into consideration here.This sheet cannot be used to check for allowable exterior pressure loads.

Note 1: If you change the Dish Radius, the sheet will no longer give the default for F&D.Note 2: The default value for the Knuckle Radius is 0.06 times the head O.D.

Di [in] - inside diameter of head Do [in] - outside diameter of head L [in] - inside crown radius (note 1) IKR [in] - inside knuckle radius (note 2) tb [in] - thickness before forming tf [in] - thickness after forming Corr [in] - corrosion allowance Skirt [in] - straight skirt length

S [psi] - allowable stress

E - head longitudinal efficiency P [psi] - interior pressure

nt [in] = tf-Corr ~~ thickness with corrosion allowance removedD [in] = Di+2*Corr ~~ ID with corrosion allowance removedL/r =M =

Ro [in] =

Required Thickness: App. 1-4(a), App. 1-4(d)App1-4(f) =

App1-4(f)Calc =

Treq [in] = (P*L*M)/(2*S*E-0.2*P)+Corr ~~ required minimum thickness

CheckTreq =

Maximum Pressure: App. 1-4(a), App. 1-4(d)Pmax [psi] = (2*S*E*nt)/(L*M+0.2*nt) ~~ maximum allowed design pressure

CheckPMax =

B16

If not specified use value indicated by note 3

B23




Page 1 of 1

HEAD B NOT USED (BOTTOM or END) Page 4/22/2023

JOB NO. 0

Dimensions:

0.0000.0000.0000.0000.0000.0000.0000.000


0.700.0

Calculated Properties:note 1:Suggested radius L per UG-32(j) 0.00 Approx. head weight based on steel, lbs = 0.00note 2:Suggested radius IKR per UG-32(j) 0.000 Approx. head volume including skirt, cuft = 0.00note 3:Suggested thickness after forming -0.0320

Variables:0-0 = 0.000

0+2*0 = 0.000L/IKR 0/0 = #DIV/0!0.25*(3+sqrt(L/IKR)) 0.25*(3+SQRT(0/0)) = #DIV/0!L+tb 0+0 = 0.000

tf/L 0/0 = #DIV/0!if(AND(0.0005=<App1-4(f),App1-4(f)<0.002),"Calculation Required","Calculation not required")

#DIV/0!




App. 1-4(f) calculation is not included on this sheetNozzles may be subject to a smaller required thickness depending on location in the head.Heads may be subject to stress relief if large elongation occurs - UCS-79(d), UNF-79(d), UG-37(a)(1)All UG-16(b) minimum thickness requirements have not been taken into consideration here.This sheet cannot be used to check for allowable exterior pressure loads.

Note 1: If you change the Dish Radius, the sheet will no longer give the default for F&D.Note 2: The default value for the Knuckle Radius is 0.06 times the head O.D.

Di [in] - inside diameter of head Do [in] - outside diameter of head L [in] - inside crown radius (note 1) IKR [in] - inside knuckle radius (note 2) tb [in] - thickness before forming tf [in] - thickness after forming Corr [in] - corrosion allowance Skirt [in] - straight skirt length

S [psi] - allowable stress

E - head longitudinal efficiency P [psi] - interior pressure

nt [in] = tf-Corr ~~ thickness with corrosion allowance removedD [in] = Di+2*Corr ~~ ID with corrosion allowance removedL/r =M =

Ro [in] =

Required Thickness: App. 1-4(a), App. 1-4(d)App1-4(f) =

App1-4(f)Calc =

Treq [in] = (P*L*M)/(2*S*E-0.2*P)+Corr ~~ required minimum thickness

CheckTreq =

Maximum Pressure: App. 1-4(a), App. 1-4(d)Pmax [psi] = (2*S*E*nt)/(L*M+0.2*nt) ~~ maximum allowed design pressure

CheckPMax =

B15

If not specified use value indicated by note 3

B22




Shell Nozzle and Repad (Not Required) 4/22/2023 Page 1 of 2 #VALUE!NOZZLE 1 -- NOT USED 0 INCH/PSI OTHER

JOB NO: 0 NOZZLE ID. QUANTITY= 0

Shell Inputs: FLANGE/COUPLING RATING OTHER PSIINHERENT Material

#N/A0.65

0.0000.000#N/A0.0000.063

Nozzle Inputs:INHERENT Material

01.00

0.0000.0000

0.0000.0000.0000.0%

0.0

Reinforcement:INHERENT Material

#N/A0.0000 0.000

0.0000.0000.0000.0000.000

Variables:Nwall*UTP 0*0 = 0.000Do/2 - (Nwall-nca) + UT 0/2 - (0-0) + 0 = 0.000Nwall-2*nca 0-2*0 = 0.000MIN(Ip-sca,2.5*nt,2.5*ti) MIN(0-0,2.5*0,2.5*0) = 0.000Nwall-nca 0-0 = 0.000Do-2*tn 0-2*0 = 0.000MIN(Sn/Sv,1) #N/A #N/AMIN(Sn/Sv,1) #N/A #N/AMIN(Sn/Sv,Sp/Sv,1) #N/A #N/AMIN(Sp/Sv,1) #N/A #N/A

(0*0)/(0*1 - 0.6*0)+0 = #DIV/0!(Pn*Rn)/(Sn*1 - 0.6*Pn) (0*0)/(0*1 - 0.6*0) = #DIV/0!TreqN <= Nwall #DIV/0! #DIV/0!

thickness standard wall pipe VLOOKUP(0,PIpeWall,2) = #N/ANwall * (1-UTP) 0 * (1-0) = 0.000

#DIV/0! #DIV/0!trnR + nca #DIV/0! #DIV/0!Min(UG45b3,UG45b4) #N/A #N/A

Sv [psi] - allowable stress E1 - efficiency of shell at nozzle

Ds [in] - inside diameter of shell nt [in] - nominal shell wall thickness Treq [in] - required shell wall thickness sca [in] - shell corrosion allowance tUG16(b) [in] - minimum thickness per UG-16 b

Sn [psi] - allowable stress E - nozzle efficiency

Do [in] - outside diameter of nozzle Nwall [in] - nominal wall thickness of nozzle Lp [in] - exterior projection of nozzle Ip [in] - interior projection of nozzle nca [in] - nozzle corrosion allowance UTP [%] - undertolerance allowance Pn [psi] - interior pressure

Sp [psi] - allowable stress of repad te [in] - repad thickness Dp [in] - outside diameter Leg41 [in] - fillet size Leg42 [in] - fillet size Leg43 [in] - fillet size LegG [in] - depth of groove

UT [in] = Rn [in] =

ti [in] = h [in] =

tn [in] = d [in] = fr1 = fr2 = fr3 = fr4 =

Required Thickness: UG-27(c)(1,2)TreqN [in] = (Pn*Rn)/(Sn*E - 0.6*Pn)+nca ~~ required minimum thickness

trnR [in] = CheckTreqN =

UG-45: Tstd [in] = Nact [in] =

UG45 [in] = Max(UG45a, UG45b) ~~ required thickness per UG-45 UG45a [in] = UG45b [in] =

D9

ITEM OR ID. USED ON DRAWING FOR THIS NOZZLE.

B30


Shell Nozzle 1 Page 2 of 2

Max(Treq+sca,tUG16(b) + sca) #N/A #N/A0 0 = 0.000Max(UG45b1,UG45b2) #N/A #N/ATstd*0.875 + nca #N/A #N/AUG45 <= Nact #DIV/0! #DIV/0!

Minimum thickness per UG-45 [in] = #N/A #N/A

#N/A #N/Amax(d, 2*(nt+tn)) * (E1*nt-1*Treq)-2*tn*(E1*nt-1*Treq)*(1-fr1)

#N/A #N/Amin((tn-trnR)*fr2*min(5*nt,2*Lp),(tn-trnR)*(Min(2.5*tn+te,2*Lp)*fr2*2))

#DIV/0! #DIV/0!Min(5*nt*ti*fr2,5*ti*ti*fr2,2*h*ti*fr2)

#N/A #N/A(Dp-d-2*tn)*te*fr4 #N/A #N/ALeg41^2*fr3 #N/A #N/ALeg42^2*fr4 #N/A #N/A(Leg43-nca)^2*fr2 #N/A #N/A

#N/A #N/A#N/A #N/A

smaller of 0.75, nt, or Nwall 0.000 0.000 0.000 = 0.0000smaller of 0.25 or (tmin * 0.7) / 0.7 0 = 0.0000

0 >= 0 = Acceptable(smaller of 0.5nt or te) 0.000 = 0.0000(smaller of 0.25 or (temin * 0.7) / 0.7) 0 = 0.0000

0 >= 0 = Acceptable(smaller of 0.25 or (tmin * 0.7) / 0.7) + sca = 0.0000

0 >= 0 = AcceptableMinimum design temperature check: Impact testing exempt per UG20(F)

UCS-66 CURVE 'B' RATING [F]: #N/A

UG45b1 [in] = UG45b2 [in] = UG45b3 [in] = UG45b4 [in] =

CheckUG45 =

Area Replacement: Ar [in^2] = 1*d*Treq*1+2*tn*Treq*1*(1-fr1) ~~ required Area

A1 [in^2] =

A2 [in^2] =

A3 [in^2] =

A5 [in^2] = A41 [in^2] = A42 [in^2] = A43 [in^2] =

Aa [in^2] = A1+A2+A3+A5+A41+A42+A43 ~~ actual area

CheckA = Aa >= Ar ~~ check area replacement

Nozzle Weld Strength: per UW-16(a), (b)Weld 41 tmin [in] = Weld 41 Leg [in] =

Weld 42 tmin [in] = Weld 42 Leg [in] =

Weld 43 Leg [in] =



Shell Nozzle and Repad (Not Required) 4/22/2023 Page 1 of 2NOZZLE 2 -- NOT USED 0 INCH/PSI OTHER

JOB NO: 0 NOZZLE ID. QUANTITY= 0Shell Inputs: FLANGE/COUPLING RATING OTHER PSI

INHERENT Material #N/A0.65

0.0000.000#N/A0.0000.063


01.00

0.0000.00000.0000

0.0000.0000.0000.0%

0.0


#N/A0.0000 0.000

0.0000.0000.0000.0000.000

Variables:Nwall*UTP 0*0 = 0.000Do/2 - (Nwall-nca) + UT 0/2 - (0-0) + 0 = 0.000Nwall-2*nca 0-2*0 = 0.000MIN(Ip-sca,2.5*nt,2.5*ti) MIN(0-0,2.5*0,2.5*0) = 0.000Nwall-nca 0-0 = 0.000((Tangent Do+Do)/2)-(2*tn) (0+0)/2)-(2*0) = 0.000 REQUIREDMIN(Sn/Sv,1) #N/A #N/AMIN(Sn/Sv,1) #N/A #N/AMIN(Sn/Sv,Sp/Sv,1) #N/A #N/AMIN(Sp/Sv,1) #N/A #N/A



#DIV/0! #DIV/0!trnR + nca #DIV/0! #DIV/0!




Do [in] - outside diameter of nozzle Nwall [in] - nominal wall thickness of nozzle CLn [in] - nozzle offset from vessel centerline Lp [in] - exterior projection of nozzle Ip [in] - interior projection of nozzle nca [in] - nozzle corrosion allowance UTP [%] - undertolerance allowance Pn [psi] - interior pressure


UT [in] = Rn [in] =

ti [in] = h [in] =





UG45 [in] = Max(UG45a, UG45b) ~~ required thickness per UG-45 UG45a [in] =

D9


B27

Tangent nozzle offset from centerline

B31



Min(UG45b3,UG45b4) #N/A #N/AMax(Treq+sca,tUG16(b) + sca) #N/A #N/A0 0 = 0.000Max(UG45b1,UG45b2) #N/A #N/ATstd*0.875 + nca #N/A #N/AUG45 <= Nact #DIV/0! #DIV/0!






#N/A #N/A#N/A #N/A




0 >= 0 = Acceptable

Minimum design temperature check: CURVE "D"UCS-66 CURVE 'B' RATING [F]: #N/A

Shell tangent nozzle: Large nozzle diameter 0.000 (in)

Note: Attached piping to be externally supported. Calculations are limited to materials listed in this sheet.

UG45b [in] = UG45b1 [in] = UG45b2 [in] = UG45b3 [in] = UG45b4 [in] =

CheckUG45 =


A1 [in^2] =

A2 [in^2] =

A3 [in^2] =

A5 [in^2] = A41 [in^2] = A42 [in^2] = A43 [in^2] =





Weld 43 Leg [in] =






#N/A0.65

0.0000.000#N/A0.0000.063


01.00

0.0000.00000.0000

0.0000.0000.0000.0%

0.0


#N/A0.0000 0.0000

0.0000.0000.0000.0000.000

Variables:Nwall*UTP 0*0 = 0.000Do/2 - (Nwall-nca) + UT 0/2 - (0-0) + 0 = 0.000Nwall-2*nca 0-2*0 = 0.000MIN(Ip-sca,2.5*nt,2.5*ti) MIN(0-0,2.5*0,2.5*0) = 0.000Nwall-nca 0-0 = 0.000((Tangent Do+Do)/2)-(2*tn) (0+0)/2)-(2*0) = 0.000 REQUIREDMIN(Sn/Sv,1) #N/A #N/AMIN(Sn/Sv,1) #N/A #N/AMIN(Sn/Sv,Sp/Sv,1) #N/A #N/AMIN(Sp/Sv,1) #N/A #N/A







Do [in] - outside diameter of nozzle Nwall [in] - nominal wall thickness of nozzle CLn [in] - nozzle offset from vessel centerline Lp [in] - exterior projection of nozzle Ip [in] - interior projection of nozzle nca [in] - nozzle corrosion allowance UTP [%] - undertolerance allowance Pn [psi] - interior pressure


UT [in] = Rn [in] =

ti [in] = h [in] =






D9


B27


B31



Min(UG45b3,UG45b4) #N/A #N/AMax(Treq+sca,tUG16(b) + sca) #N/A #N/A0 0 = 0.000Max(UG45b1,UG45b2) #N/A #N/ATstd*0.875 + nca #N/A #N/AUG45 <= Nact #DIV/0! #DIV/0!






#N/A #N/A#N/A #N/A






Shell tangent nozzle: Large nozzle diameter 0.000 (in)


CheckUG45 =


A1 [in^2] =

A2 [in^2] =

A3 [in^2] =

A5 [in^2] = A41 [in^2] = A42 [in^2] = A43 [in^2] =





Weld 43 Leg [in] =






#N/A0.65

0.0000.000#N/A0.0000.063


01.00

0.0000.00000.00000.00000.0000.0000.0000.0%

0.0


#N/A0.0000 0.0000.0000.0000.0000.0000.000

Variables:Nwall*UTP 0*0 = 0.000Do/2 - (Nwall-nca) + UT 0/2 - (0-0) + 0 = 0.000Nwall-2*nca 0-2*0 = 0.000MIN(Ip-sca,2.5*nt,2.5*ti) MIN(0-0,2.5*0,2.5*0) = 0.000Nwall-nca 0-0 = 0.000((Tangent Do+Cone Do)/2)-(2*tn) (0+0)/2)-(2*0) = 0.000 REQUIREDMIN(Sn/Sv,1) #N/A #N/AMIN(Sn/Sv,1) #N/A #N/AMIN(Sn/Sv,Sp/Sv,1) #N/A #N/AMIN(Sp/Sv,1) #N/A #N/A



#DIV/0! #DIV/0!trnR + nca #DIV/0! #DIV/0!Min(UG45b3,UG45b4) #N/A #N/A


Ds [in] - inside diameter of shell/cone at nozzle nt [in] - nominal shell wall thickness Treq [in] - required shell wall thickness at nozzle sca [in] - shell corrosion allowance tUG16(b) [in] - minimum thickness per UG-16 b

Sn [psi] - allowable stress E - nozzle efficiency Do [in] - outside diameter of nozzle Nwall [in] - nominal wall thickness of nozzle Ln [in] - nozzle distance from cone ODL CLn [in] - nozzle offset from vessel centerline Lp [in] - exterior projection of nozzle Ip [in] - interior projection of nozzle nca [in] - nozzle corrosion allowance UTP [%] - undertolerance allowance Pn [psi] - interior pressure


UT [in] = Rn [in] =

ti [in] = h [in] =






D9


B28


B32



Max(Treq+sca,tUG16(b) + sca) #N/A #N/A0 0 = 0.000Max(UG45b1,UG45b2) #N/A #N/ATstd*0.875 + nca #N/A #N/AUG45 <= Nact #DIV/0! #DIV/0!






#N/A #N/A#N/A #N/A




0 >= 0 = Acceptable

#DIV/0! N/AO.D. of cone at nozzle: 0 Cone ODL side of nozzle 0 (in)

0.000 Center of nozzle 0 (in)0 0 Cone ODS side of nozzle 0 (in)

Shell or cone straight nozzle: Large nozzle diameter 0.000 (in)Shell or cone tangent nozzle: Large nozzle diameter 0.000 (in)Added nozzle cut length: 0.000 (in)

Minimum design temperature check: Impact testing exempt per UG20(F)UCS-66 CURVE 'B' RATING [F]: #N/A



CheckUG45 =


A1 [in^2] =

A2 [in^2] =

A3 [in^2] =

A5 [in^2] = A41 [in^2] = A42 [in^2] = A43 [in^2] =





Weld 43 Leg [in] =

Cone Required Thickness at Nozzle 4: VIII-1 App 1-4 e)Treq [in] = P*ODL/(2*COS(a)*(S*E+0.4*P)) + Corr ~~required minimum thickness




JOB NO: 0 NOZZLE ID. QUANTITY= 0Shell Inputs: FLANGE/COUPLING RATING OTHER PSI

INHERENT Material #N/A0.65

0.0000.000#N/A0.0000.063


01.00

0.0000.00000.00000.0000

0.0000.0000.0000.0%

0.0Reinforcement:

INHERENT Material #N/A

0.0000 0.0000.0000.0000.0000.0000.000

Variables:Nwall*UTP 0*0 = 0.000Do/2 - (Nwall-nca) + UT 0/2 - (0-0) + 0 = 0.000Nwall-2*nca 0-2*0 = 0.000MIN(Ip-sca,2.5*nt,2.5*ti) MIN(0-0,2.5*0,2.5*0) = 0.000Nwall-nca 0-0 = 0.000((Tangent Do+Cone Do)/2)-(2*tn) (0+0)/2)-(2*0) = 0.000 REQUIREDMIN(Sn/Sv,1) #N/A #N/AMIN(Sn/Sv,1) #N/A #N/AMIN(Sn/Sv,Sp/Sv,1) #N/A #N/AMIN(Sp/Sv,1) #N/A #N/A



Sv [psi] - allowable stress E1 - efficiency of shell at nozzle Ds [in] - inside diameter of shell/cone at nozzle nt [in] - nominal shell wall thickness Treq [in] - required shell wall thickness at nozzle sca [in] - shell corrosion allowance tUG16(b) [in] - minimum thickness per UG-16 b

Sn [psi] - allowable stress E - nozzle efficiency Do [in] - outside diameter of nozzle Nwall [in] - nominal wall thickness of nozzle Ln [in] - nozzle distance from cone ODL CLn [in] - nozzle offset from vessel centerline Lp [in] - exterior projection of nozzle Ip [in] - interior projection of nozzle nca [in] - nozzle corrosion allowance UTP [%] - undertolerance allowance Pn [psi] - interior pressure


UT [in] = Rn [in] =

ti [in] = h [in] =



TreqN [in] = (Pn*Rn)/(Sn*E - 0.6*Pn)+nca ~~ required minimum thickness



D9


B26


B30


Shell nozzle 5 Page 2 of 2

#DIV/0! #DIV/0!trnR + nca #DIV/0! #DIV/0!Min(UG45b3,UG45b4) #N/A #N/AMax(Treq+sca,tUG16(b) + sca) #N/A #N/A0 0 = 0.000Max(UG45b1,UG45b2) #N/A #N/ATstd*0.875 + nca #N/A #N/AUG45 <= Nact #DIV/0! #DIV/0!






#N/A #N/A#N/A #N/A




0 >= 0 = Acceptable

#DIV/0! N/AO.D. of cone at nozzle: 0 Cone ODL side of nozzle 0 (in)

0.000 Center of nozzle 0 (in)0 0 Cone ODS side of nozzle 0 (in)

Shell or cone straight nozzle: Large nozzle diameter 0.000 (in)Shell or cone tangent nozzle: Large nozzle diameter 0.000 (in)Added nozzle cut length: 0.000 (in)



UG45 [in] = Max(UG45a, UG45b) ~~ required thickness per UG-45

UG45a [in] = UG45b [in] =


CheckUG45 =


A1 [in^2] =

A2 [in^2] =

A3 [in^2] =

A5 [in^2] = A41 [in^2] = A42 [in^2] = A43 [in^2] =



Nozzle Weld Strength: per UW-16(a), (b)



Weld 43 Leg [in] =

Cone Required Thickness at Nozzle: VIII-1 App 1-4 e)

Treq [in] = P*ODL/(2*COS(a)*(S*E+0.4*P)) + Corr ~~required minimum thickness



Head Nozzle and Repad (Not Required) 4/22/2023 Page 1 of 2HEAD A NOZZLE 1 -- NOT USED NOZZLE ID. 0 INCH/PSI OTHER

JOB NO: 0 QTY= 0 FLANGE/COUPLING RATING OTHER PSIHead Inputs: HEAD A (END) ELLIPTICAL (Nozzles within 80% limit only)

SA-36 Material 16,600

0.70

0.000 Ds [in] - inside head dish diameter0.000

#DIV/0! Treq [in] - required head wall thickness at nozzle0.0000.063

Nozzle Inputs: N/AINHERENT Material

01.00

0.0000.000

0.00000.0000

0.0000.0000.0000.0%

0.0


16,6000.0000 0.000

0.0000.0000.0000.0000.000

Variables:Nwall*UTP 0*0 = 0.000Do/2 - (Nwall-nca) + UT 0/2 - (0-0) + 0 = 0.000Nwall-2*nca 0-2*0 = 0.000MIN(Ip-sca,2.5*nt,2.5*ti) MIN(0-0,2.5*0,2.5*0) = 0.000Nwall-nca 0-0 = 0.000((Tangent or nozzle Do+Cone Do)/2)-(2*tn) (0+0)/2)-(2*0) = 0.000 REQUIREDMIN(Sn/Sv,1) MIN(0/16600,1) = 0.000MIN(Sn/Sv,1) MIN(0/16600,1) = 0.000MIN(Sn/Sv,Sp/Sv,1) MIN(0/16600,16600/16600,1) = 0.000MIN(Sp/Sv,1) MIN(16600/16600,1) = 1.000


thickness s thickness standard wall pipe VLOOKUP(0,PIpeWall,2) = #N/ANwall * (1-UTP) 0 * (1-0) = 0.000


Sv [psi] - allowable stress E1 - efficiency of head at nozzle

nt [in] - nominal head wall thickness

sca [in] - shell/head corrosion allowance tUG16(b) [in] - minimum thickness per UG-16 b


Do [in] - outside diameter of nozzle Nwall [in] - nominal wall thickness of nozzle Ln [in] - nozzle distance from cone ODL CLn [in] - nozzle offset from Cone centerline Lp [in] - exterior projection of nozzle Ip [in] - interior projection of nozzle nca [in] - nozzle corrosion allowance UTP [%] - undertolerance allowance Pn [psi] - interior pressure


UT [in] = Rn [in] =

ti [in] = h [in] =






E8


B13

Typically E1=1

B16

Use nt from the corresponding head or pipe and shell program

B17

Use one of the following based on nozzle location: nozzle in pipe/shell - See Treq from pipe and shell program nozzle in head - See Treq from corresponding head program

B28

Tangent nozzle offset from centerline of Cone only. NOT FOR HEAD USE.

B32


Head A Nozzle 1 Page 2 of 2

Min(UG45b3,UG45b4) #DIV/0! #DIV/0!Max(Treq+sca,tUG16(b) + sca) #DIV/0! #DIV/0!0 0 = 0.000Max(UG45b1,UG45b2) #DIV/0! #DIV/0!Tstd*0.875 + nca #N/A #N/AUG45 <= Nact #DIV/0! #DIV/0!


#DIV/0! #DIV/0!max(d, 2*(nt+tn)) * (E1*nt-1*Treq)-2*tn*(E1*nt-1*Treq)*(1-fr1)

#DIV/0! #DIV/0!min((tn-trnR)*fr2*min(5*nt,2*Lp),(tn-trnR)*(Min(2.5*tn+te,2*Lp)*fr2*2))


MIN(5*0*0*0,5*0*0*0,2*0*0*0) = 0.000(Dp-d-2*tn)*te*fr4 (0-0-2*0)*0*1 = 0.000Leg41^2*fr3 0^2*0 = 0.000Leg42^2*fr4 0^2*1 = 0.000(Leg43-nca)^2*fr2 (0-0)^2*0 = 0.000

#DIV/0! #DIV/0!#DIV/0! #DIV/0!




0 >= 0 = Acceptable

#DIV/0! 0.000O.D. of cone at nozzle: 0 Cone ODL side of nozzle N/A (in)

0.000 Center of nozzle N/A (in)#VALUE! 0 Cone ODS side of nozzle N/A (in)

Cone straight nozzle: Large nozzle diameter 0.000 (in)Cone tangent nozzle: Large nozzle diameter 0.000 (in)Added nozzle cut length: 0.000




CheckUG45 =


A1 [in^2] =

A2 [in^2] =

A3 [in^2] =

A5 [in^2] = A41 [in^2] = A42 [in^2] = A43 [in^2] =





Weld 43 Leg [in] =

Cone Required Thickness at Head A Nozzle 1: VIII-1 App 1-4 e)Treq [in] = P*ODL/(2*COS(a)*(S*E+0.4*P)) + Corr ~~required minimum thickness






0.70


#DIV/0!0.0000.063


01.00

0.0000.000

0.00000.0000

0.0000.0000.0000.0%

0.0


16,6000.0000 0.000

0.0000.0000.0000.0000.000



thickness thickness standard wall pipe VLOOKUP(0,PIpeWall,2) = #N/ANwall * (1-UTP) 0 * (1-0) = 0.000



nt [in] - nominal head wall thickness Treq [in] - required wall thickness at nozzle sca [in] - shell/head corrosion allowance tUG16(b) [in] - minimum thickness per UG-16 b




UT [in] = Rn [in] =

ti [in] = h [in] =






E8


B13

Typically E1=1

B16


B17


B28


B32













0 >= 0 = Acceptable


0.000 Center of nozzle N/A (in)### 0 Cone ODS side of nozzle N/A (in)





CheckUG45 =


A1 [in^2] =

A2 [in^2] =

A3 [in^2] =

A5 [in^2] = A41 [in^2] = A42 [in^2] = A43 [in^2] =





Weld 43 Leg [in] =

Cone Required Thickness at Head A Nozzle 2: VIII-1 App 1-4 e)Treq [in] = P*ODL/(2*COS(a)*(S*E+0.4*P)) + Corr ~~required minimum thickness






0.70

0.0000.0000

#DIV/0!0.0000.063

Nozzle Inputs: HEADINHERENT Material

01.00

0.0000.0000.0000.0000.0000.0%

0.0


16,6000.0000 0.0000.0000.0000.0000.0000.000

Variables:Nwall*UTP 0*0 = 0.000Do/2 - (Nwall-nca) + UT 0/2 - (0-0) + 0 = 0.000Nwall-2*nca 0-2*0 = 0.000MIN(Ip-sca,2.5*nt,2.5*ti) MIN(0-0,2.5*0,2.5*0) = 0.000Nwall-nca 0-0 = 0.000Do-2*tn 0-2*0 = 0.000MIN(Sn/Sv,1) MIN(0/16600,1) = 0.000MIN(Sn/Sv,1) MIN(0/16600,1) = 0.000MIN(Sn/Sv,Sp/Sv,1) MIN(0/16600,16600/16600,1) = 0.000MIN(Sp/Sv,1) MIN(16600/16600,1) = 1.000





Ds [in] - inside head dish/cone diameter at nozzle nt [in] - nominal head wall thickness Treq [in] - required wall thickness at nozzle sca [in] - shell/head corrosion allowance tUG16(b) [in] - minimum thickness per UG-16 b




UT [in] = Rn [in] =

ti [in] = h [in] =






E8


B13

Typically E1=1

B17


B30


Min(UG45b3,UG45b4) #DIV/0! #DIV/0!


Max(Treq+sca,tUG16(b) + sca) #DIV/0! #DIV/0!0 0 = 0.000Max(UG45b1,UG45b2) #DIV/0! #DIV/0!Tstd*0.875 + nca #N/A #N/AUG45 <= Nact #DIV/0! #DIV/0!













UG45b [in] =


CheckUG45 =


A1 [in^2] =

A2 [in^2] =

A3 [in^2] =

A5 [in^2] = A41 [in^2] = A42 [in^2] = A43 [in^2] =





Weld 43 Leg [in] =



Head Nozzle and Repad (Not Required) 4/22/2023 Page 1 of 2HEAD B NOZZLE 1 -- NOT USED NOZZLE ID. 0 INCH/PSI OTHER

JOB NO: 0 QTY= 0 FLANGE/COUPLING RATING OTHER PSIHead Inputs: HEAD B (END) ELLIPTICAL (Nozzles within 80% limit only)


0.70


#DIV/0!0.0000.063


01.00

0.0000.000

0.00000.00000.0000.0000.0000.0%

0.0


16,6000.0000 0.0000.0000.0000.0000.0000.000




#DIV/0! #DIV/0!


nt [in] - nominal head wall thickness Treq [in] - required head wall thickness sca [in] - shell/head corrosion allowance tUG16(b) [in] - minimum thickness per UG-16 b




UT [in] = Rn [in] =

ti [in] = h [in] =





UG45 [in] = Max(UG45a, UG45b) ~~ required thickness per UG-45

E8


B16


B17


B28


B32


trnR + nca #DIV/0! #DIV/0!

HEAD B NOZZLE 1 Page 2 of 2











0 >= 0 = Acceptable


0.000 Center of nozzle N/A (in)#VALUE! 0 Cone ODS side of nozzle N/A (in)




UG45a [in] =


CheckUG45 =


A1 [in^2] =

A2 [in^2] =

A3 [in^2] =

A5 [in^2] = A41 [in^2] = A42 [in^2] = A43 [in^2] =





Weld 43 Leg [in] =

Cone Required Thickness at Head B Nozzle 1: VIII-1 App 1-4 e)




Head Nozzle and Repad (Not Required) 4/22/2023 Page 1 of 2HEAD B NOZZLE 2 -- NOT USED NOZZLE ID. 0 INCH/PSI OTHER

JOB NO: 0 QTY= 0 FLANGE/COUPLING RATING 3,500 PSI

Head Inputs: HEAD B (END) ELLIPTICAL (Nozzles within 80% limit only)SA-36 Material 16,600

0.70


#DIV/0!0.0000.063

Nozzle Inputs: HEADINHERENT Material

01.00

0.0000.0000.0000.0000.0000.0%

0.0


16,6000.0000 0.000

0.0000.0000.0000.0000.000

Variables:Nwall*UTP 0*0 = 0.000Do/2 - (Nwall-nca) + UT 0/2 - (0-0) + 0 = 0.000Nwall-2*nca 0-2*0 = 0.000MIN(Ip-sca,2.5*nt,2.5*ti) MIN(0-0,2.5*0,2.5*0) = 0.000Nwall-nca 0-0 = 0.000Do-2*tn 0-2*0 = 0.000MIN(Sn/Sv,1) MIN(0/16600,1) = 0.000MIN(Sn/Sv,1) MIN(0/16600,1) = 0.000MIN(Sn/Sv,Sp/Sv,1) MIN(0/16600,16600/16600,1) = 0.000MIN(Sp/Sv,1) MIN(16600/16600,1) = 1.000


thickness sthickness standard wall pipe VLOOKUP(0,PIpeWall,2) = #N/ANwall * (1-UTP) 0 * (1-0) = 0.000

#DIV/0! #DIV/0!trnR + nca #DIV/0! #DIV/0!Min(UG45b3,UG45b4) #DIV/0! #DIV/0!


nt [in] - nominal head wall thickness Treq [in] - required head wall thickness sca [in] - shell/head corrosion allowance tUG16(b) [in] - minimum thickness per UG-16 b




UT [in] = Rn [in] =

ti [in] = h [in] =






E8


B13

Typically E1=1

B17


B30


HEAD B NOZZLE 2 Page 2 of 2

Max(Treq+sca,tUG16(b) + sca) #DIV/0! #DIV/0!0 0 = 0.000Max(UG45b1,UG45b2) #DIV/0! #DIV/0!Tstd*0.875 + nca #N/A #N/AUG45 <= Nact #DIV/0! #DIV/0!










0 >= 0 = Acceptable




CheckUG45 =


A1 [in^2] =

A2 [in^2] =

A3 [in^2] =

A5 [in^2] = A41 [in^2] = A42 [in^2] = A43 [in^2] =





Weld 43 Leg [in] =


PRESSURE VESSEL CALCULATIONSSPREADSHEET VERSION: 09082015e Page 1 of 1

4/22/2023Conical Section per Appendix 1-5 0.000 PageJOB NO: 0Dimensions:

0.0000.0000.0000.0000.0000.000 #DIV/0! 0.0000.000


#N/A65%

0.0Calculated Properties: 0.000

Approx. cone weight based on steel, lbs = 0.0Approx. cone volume , cuft = 0.00

ATAN((0-0)/(2*0)) = #DIV/0!#DIV/0! #DIV/0!

0-0 = 0.000

#DIV/0! #DIV/0!Treq <= t #DIV/0! #DIV/0!

#N/A #N/APmax >= P #N/A #N/A


All UG-16 minimum thickness requirements have not been taken into consideration here.

ODL [in] - outside diameter of large end IDL [in] - inside diameter of large end ODS [in] - outside diameter of small end IDS [in] - inside diameter of small end t [in] - thickness L [in] -length Corr [in] - corrosion allowance

S [psi] - allowable stress E - long seam efficiency = P [psi] - interior pressure

a [rad] = ATAN((ODL-ODS)/(2*L)) ~~ alpha angle in radiansangle [deg] = Degrees(a) ~~ alpha angle in degrees

nt [in] = t-Corr ~~ thickness with corrosion allowance removed Required Thickness: VIII-1 App 1-4 e)


CheckTreq = Maximum Pressure: VIII-1 App 1-4(e)Pmax [psi] = 2*S*E*nt*cos(a)/(ODL-0.8*nt*cos(a)) ~~maximum allowed design pressure

CheckPMax =

B14

Defaults to main shell thickness.

B20

Enter joint efficiency if not the same as the main shell here.

F20

Efficiency used in calculations. If entry is left blank or zero, this will default to the shell efficiency



Page 1 of 1HEAD ON BOOT 2:1 RATIO ELLIPTICAL Page 4/22/2023

JOB NO. 0Dimensions:

0.0000 t [in] - nominal wall thickness t= 0.000

0.0000.0000.000


#N/A0.0%0.70

0.0 0.000Calculated Properties: #N/Anote 1: Suggested thickness after forming Approx. head weight based on steel, lbs = 0.00


0*0 = 0.0000-0+0 = 0.000

0+2*0-(0*2) = 0.0000/4 = 0.000




nt >= 0.0625+Corr 0 >= 0.0625 = ERROR



All UG-16(b) minimum thickness requirements have not been taken into consideration here.Nozzles may be subject to a smaller required thickness depending on location in the head.

Heads may be subject to stress relief if large elongation occurs - UCS-79(d), UNF-79(d), UHA-44(d)

Do [in] - outside diameter of head Di [in] - inside diameter of head

tf [in] - thickness after forming (note 1) Corr [in] - corrosion allowance Skirt [in] - straight skirt length


ut [in] = tf*UTP ~~ undertorlerance allowance

nt [in] = tf-(Corr+ut) ~~ thickness with corrosion allowance removedD [in] = Do-2*nt ~ ID with corrosion allowance removed

h [in] = D/4 ~~ inside crown heightho [in] =D/2h =

Do/2ho =K =

Kone =Kzero =


App1-4(f) =




CheckPMax =

B11

Make entry here only if head is used as head on BOOT.

B13

Code requires that heads be at least as thick as the shell or cone they are attached to.

B14


B18

If thiskness is pipe schedule, material must be Weld Cap material.

B20


B21



PRESSURE VESSEL CALCULATIONSSPREADSHEET VERSION: 08092015

Page 1 of 1Bolted Closure Formed 2:1 Elliptical head used 8/15/2015

JOB NO. 0Dimensions: Closure on shell or nozzle

0.000.000

0 t [in] - nominal wall thickness 0.0000.0000.0000.000

Material and Conditions:INHERENT Material INHERENT used

#N/A0.0%0.700.0

Calculated Properties:note 1: Suggested thickness after forming Approx. head weight based on steel, lbs = 0.00


0*0 = 0.0000-0+0 = 0.000

0+2*0-(0*2) = 0.0000/4 = 0.000




nt >= 0.0625+Corr 0 >= 0.0625 = ERROR


Calculations for swing bolted heads:INHERENT Flange or ring Material

#N/A0.000 #N/A0.000 PRESSUR LOADING0.000

SA-193 B725,000

#N/A #N/A 0 #N/A#N/A

0 #N/A0.000 hg = 0.0000.0000.000

INHERENT Lug material #N/A #N/A#N/A

1.00Thickness required for flat circular bolted heads or rings using C = 0.3t = [d * square root {(CP/SE)+(1.9Whg/SEd3)}]+Corr #N/A (in)

0#N/A #N/A#N/A (in)#N/A

#N/A #N/AMinimum design temperature check: Impact testing exempt per UG20(F)

UCS-66 CURVE 'B' RATING [F]: #N/A / 'D' [F]: #N/A

Do [in] - outside diameter of closure head = Di [in] - inside diameter of closure head

tf [in] - thickness after forming (note 1) Corr [in] - corrosion allowance Skirt [in] - straight skirt length



ho [in] =D/2h =

Do/2ho =K =

Kone =Kzero =


App1-4(f) =




CheckPMax =

S [psi] - allowable stress Ft [in] - flange or ring thickness Bc [in] - bolt circle centerline diameter B [in] - bolt diameter (0.5" to 2.5" max.) Bm - bolt material Bs (psi) - bolt allowable stress value Bl [in] - bolt loading Bt (ft/lbs) - bolt torque Bn - number of bolts used Gc [in] - gasket centerline diameter (d) Lw [in] - Lug width at hole (w) Lt [in] - Lug thickness

Ls (psi) - Lug allowable stress value E - efficiency if joint present

Required clamping force (LB)= (Gc/2)*(Gc/2)*(22/7)*P=Bolt clamping force (LB)= Bn*Bl=Required lug thickness (in) = Bl/(2Ls(Lw-B)) =

Maximum lug load (LB)= Bl*(Lt/Rt)

B11

If Head A is not the closure head, enter O.D.

B13

Code requires that heads be at least as thick as the shell or cone they are attached to. If Head A is part of closure leave blank or zero.

B14


B18

If thiskness is pipe schedule, material must be Weld Cap material.

B20


B21


B55

If a ring is being used for sealing a head or shell, enter the height of the ring. If a flat plate is being used as a flange, enter the plate thickness. If there is no ring or flange, use the head straight flange height of 2".



Circular Unstayed Flat Head per UG-34 4/22/2023 1 of 1Figure UG-34 sketch (e) and othersJOB NO: 0Dimensions:

SHELL #1 0.0000.000#N/A85%

0.000Material and Conditions:

* INHERENT Head or Flange Material #N/A

* 0.0000

Calculations for sketches (b-2), (e), (f), (g), (i):Thickness required for flat unstayed circular heads using C = #N/A #N/Atr = [d * square root (CP/SE)] + Corr tr = #N/A in

Maximum allowable design pressure= P*(t/tr) = #N/A psiMinimum design temperature:UCS-66 CURVE "B" CURVE "D"

#N/A #N/A #N/A #N/ACalculations for sketches (h), (r), (s):Thickness required for flat unstayed circular heads using C = 0.33tr = [d * square root (CP/SE)] + Corr tr = #N/A in

Maximum allowable design pressure= P*(t/tr) = #N/A psiMinimum design temperature:UCS-66 CURVE "B" CURVE "D"

#N/A #N/A

* 0.000 * 0.000 #N/A * 0.000 PRESSURLOADING * 0.000 * SA-193 B7

25,000#N/A#N/A

* 0 * 0.000 hg = 0.000

Thickness required for flat unstayed circular bolted heads using C = 0.3 #N/A #N/Atr = [d * square root {(CP/SE)+(1.9Whg/SEd3)}]+Corr tr = #N/A in

0#N/A #N/A

Thickness maximum allowable design pressure= P*(t/tr) = #N/A psiBolt clamping force maximum allowable pressure= #N/A

Minimum design temperature:UCS-66 CURVE "B" CURVE "D"

#N/A #N/A #N/A #N/A

* Requires input

d [in] - inside diameter ts [in] - shell nominal wall thickness tr [in] - required shell thickness E - joint efficiency Corr [in] - corrosion allowance

S [psi] - allowable stress t [in] - head nominal thickness P [psi] - interior pressure

D [in] - flange/head outside diameter t [in] - flange/head nominal thickness Bc [in] - bolt circle centerline diameter B [in] - bolt diameter (0.5" to 2.5" max.) Bm - bolt material Bs (psi) - bolt allowable stress value Bl [in] - bolt loading Bt (ft/lbs) - bolt torque Bn - number of bolts used Gc [in] - gasket centerline diameter (d)

Required clamping force (LB)= (Gc/2)*(Gc/2)*(22/7)*P=Bolt clamping force (LB)= Bn*Bl=

B16

Enter material for main shell. Shell #2 is entered in Shell #2 sheet.



4/22/2023Straight Pipe or Shell under external pressureUG-28 Calculations 0 Rings requiredJOB NO: 0Dimensions:

0.0000.0000.0000.000

* 0.0000.000


#N/A * 29,000,000

0.650.65

12.5%0.0

* 15.0

Inputs from Charts: * 0.000124 Do/ts = #DIV/0! L/Do= #DIV/0! * 3,625

Calculations:Pa (External Allowable pressure) for A value left of line:

Acceptable At shell corroded condition: N/A psiPa (External Allowable pressure) for A value right of line:

#DIV/0! At shell corroded condition: #DIV/0! psi

Inputs from Charts: * 3,625 #DIV/0!

Calculations:Pa (External Allowable pressure) #REF! #REF! #DIV/0! #DIV/0!

#DIV/0! At shell nominal thickness less CA: #DIV/0! psi #DIV/0! * Requires change or input

Di [in] - inside diameter Do [in] - outside diameter ts [in] - nominal wall thickness less UTP t [in] - corroded wall thickness L [in] -length of section Corr [in] - corrosion allowance

S [psi] - allowable stress E - modulus of elasticity El - long seam efficiency (circ stress) Ec - circ seam efficiency (long stress) UTP [%] - undertolerance allowance P [psi] - interior pressure Px [psi] - external pressure

(where Do/t > 10) A - from Figure G below using B - from Figure CS-2 below

(where Do/t > 10)

(where Do/t < 10) B - from Figure CS-2 below using A value:

(where Do/t < 10)

t

Do

Leng

th

Long

Sea

m

B20


B21


B22


TOWER/ANCHOR BOLT/LIFTING LUG DESIGN CALCULATIONS BOLT TABLEFOR VERTICAL VESSELS ONLY Page 1 of 1CUSTOMER: COMPANY NAME JOB#: 0

DESIGN INPUTS CALCULATION OUTPUTSTOTAL REQ, SHELL THICKNESS #N/A

VESSEL O.D.(IN.): 0 VESSEL SHELL WEIGHT DRY: 0SHELL HEIGHT (IN.): 0 VESSEL SHELL WEIGHT WET: 0SHELL WALL THICKNESS: 0 MAWP MIN. THICKNESS LS: #N/ACORROSION ALLOWANCE: 0 WIND/MAWP REQ. THICKNESS: #N/ASHELL STRESS VALUE: #N/A SKIRT WIND+WEIGHT REQ.TK: #VALUE!JOINT EFFICIENCY: 0.65 BOLT LOAD (WIND+WEIGHT): #VALUE!SKIRT O.D. (IN.): 0.000 BASE RING REQ. TKNESS: #DIV/0!SKIRT HEIGHT (IN.): 0.000 LIFTING LUG REQ.TKNESS: 0SKIRT THICKNESS: #VALUE! FILLET WELD REQ.TKNESS: 0BASE RING O.D.: 6.000 MAX.FILLET WELD LOAD: 20160BASE RING I.D.: -3.000 MAX.LIFTING LUG LOAD: #DIV/0!CORROSION ALLOWANCE: 0 DEFLECTION AT TOP (IN.): #VALUE!SKIRT MATERIAL: SA-36 MAX.ALLOWABLE DEFLECTION: 0.000 INSULATION THICKNESS: ______ VIBRATION PERIOD (SEC.) #DIV/0!INTERNAL WEIGHT: 0 MAX.ALLOWABLE VIB.PERIOD: #DIV/0!BOLT SIZE 0.500 SEISMIC SHEAR AT BASE: #DIV/0!BOLT ROOT AREA 0.126 SEISMIC MOMENT AT BASE: #DIV/0!NUMBER OF BOLTS 0 BUCKLING SKIRT/SHELL #N/ABOLT CIRCLE (IN.) 0.00 INCREASE 16,600INTERNAL DESIGN MAWP: 0WIND FORCE (PSF): 0 CALCULATIONS ARE BASED ON FORMULAS SIESMIC ZONE FACTOR: 0.1875 FROM THE ELEVENTH EDITION OF THEHEIGHT COEFFICIENT: 1 PRESSURE VESSEL HANDBOOKSITE COEFFICIENT: 1LIFTING LUG HOLE: 1LUG CROWN RADIUS: 2LUG BASE LENGTH: 4LUG THICKNESS: 0.375LUG STRESS VALUE: 14612.5FILLET WELD LEG: 0.2625

1 Pressure Vessel2 ASME Code Section II3

4 Material Database and Temperatures Page 1 of 15 Material Properties:6 0 UCS-66 CURVE WITH ALLOWABLE TEMPERATURE REDUCTION UCS-66 TABLE

0 (SEE TABLE FOR MATERIAL EXEMPT TEMPERATURE) MATERIAL CURVE7 Material Materials less than 1" thickness may be exempt per UG-20(f). THICKNESS A B C D8 SA-36 Plate 16,600 16,600 900 Carbon Steels CURVE "B" WITH REDUCTION 39 #N/A #N/A 0.25 18 -20 -55 -55

SA-53 EB Welded Pipe 14,600 14,600 900 SHELL #N/A F #N/A #N/A 2 0.00 #N/A #N/A 0.3125 18 -20 -55 -559 SA-106 B Seamless Pipe 17,100 17,100 1,000 NOZZLE 1 #N/A F 0 3 0 #N/A 0.375 18 -20 -55 -55

SA-106 C Seamless Pipe 20,000 20,000 1,000 NOZZLE 2 #N/A F 0 4 0 #N/A 0.4375 25 -13 -40 -55SA-193 B7 Studs 25,000 25,000 1,000 NOZZLE 3 #N/A F 0 5 0 #N/A 0.5 32 -7 -34 -55

10 SA-234 WPB Fittings 17,100 17,100 1,000 NOZZLE 4 #N/A F 0 40 0 #N/A 0.5625 37 -1 -26 -5111 SA-105 Forging 20,000 20,000 1,000 NOZZLE 5 #N/A F 0 38 0 #N/A 0.625 43 5 -22 -4812 SA-516 70 Plate 20,000 20,000 1,000 37 #N/A #N/A 0.6875 48 10 -18 -4513 SA-414 G Sheet 21,400 21,400 900 HEAD A #N/A F #DIV/0! #N/A 27 0.00 #N/A #N/A 0.75 53 15 -15 -4214 SA-213 TP316L Sms Tube 16,700 16,700 850 Stainless Steel 316L NOZZLE 1 #N/A F 0 41 0 #N/A 0.875 61 23 -9 -3615 SA-240 316L Plate 16,700 16,700 850 NOZZLE 2 #N/A F 0 7 0 #N/A 1 68 31 -3 -3016 SA-312 TP316L Sms. and Wld. Pipe 16,700 16,700 850 NOZZLE 3 #N/A F 0 17 0 #N/A 1.125 75 37 2 -2617 SA-403 316L Sms and Weld Fittings 16,700 16,700 850 45 1.1875 77 40 2 -2318 SA-479 316L Bar 16,700 16,700 850 HEAD B #N/A F #DIV/0! #N/A 29 #N/A #N/A 1.25 80 43 6 -2119 SA-213 TP316 Sms Tube 20,000 20,000 1,500 Stainless Steel 316 NOZZLE 1 #N/A F 0 42 0 #N/A 1.375 84 47 10 -1820 SA-240 316 Plate 20,000 20,000 1,500 NOZZLE 2 #N/A F 0 8 0 #N/A 1.5 88 51 14 -1421 SA-312 TP316 Sms. and Wld. Pipe 20,000 20,000 1,500 18 #N/A #N/A 1.625 92 55 17 -1122 SA-403 316 Sms and Weld Fittings 20,000 20,000 1,500 SHELL #2 #N/A F #N/A #N/A 46 0.00 #N/A #N/A 1.6875 93 57 19 -1023 SA-479 316 Bar 20,000 20,000 1,500 HEAD C #N/A F #DIV/0! #N/A 30 0.00 #N/A #N/A 1.75 94 58 20 -824 SA-213 TP304L Sms Tube 16,700 16,700 1,200 Stainless Steel 304L 43 #N/A #N/A 1.875 97 61 23 -625 SA-240 304L Plate 16,700 16,700 1,200 CLOSURE #N/A F #DIV/0! #N/A 9 0.00 #N/A #N/A 2 99 63 26 -426 SA-312 TP304L Sms. and Wld. Pipe 16,700 16,700 1,200 19 #N/A #N/A 2.125 101 65 28 -227 SA-403 304L Sms and Weld Fittings 16,700 16,700 1,200 The above temperatures and curves #N/A 47 2.25 102 67 30 028 SA-479 304L Bar 16,700 16,700 1,200 are for carbon steels only. 32 2.375 104 69 32 229 SA-213 TP304 Sms Tube 20,000 20,000 1,500 Stainless Steel 304 #DIV/0! 44 2.5 105 71 34 430 SA-240 304 Plate 20,000 20,000 1,500 #DIV/0! 10 2.625 106 73 36 631 SA-312 TP304 Sms. and Wld. Pipe 20,000 20,000 1,500 Note: SA-36 is a curve "A" material. 20 2.75 108 74 38 832 SA-403 304 Sms and Weld Fittings 20,000 20,000 1,500 48 2.875 109 76 40 933 SA-479 304 Bar 20,000 20,000 1,500 33 3 110 77 41 1134 SB-209 6061-T6 plate 0.051-0.249", wld 6,000 6,000 400 Aluminum 49 3.125 111 79 43 1235 SB-209 6061-T651 plate 0.25-5", wld 6,000 6,000 400 50 3.25 112 80 44 1436 SB-209 6061-T6 plate 0.051-0.249" 10,900 10,900 400 51 3.375 113 82 46 1537 SB-209 6061-T651 plate 0.25-4.0" 10,900 10,900 400 52 3.5 114 83 47 1738 SB-209 6061-T651 plate 4.0-5.0" 10,300 10,300 400 53 3.625 115 85 49 1839 SB-211 A96061-T6 bar 0.125-0.249", wld 6,000 6,000 400 57 3.75 116 86 50 2040 SB-234 A96061-T6 tubes 0.025-0.200", wld 6,000 6,000 400 59 3.875 116 88 51 2141 SB-241 A96061-T6 sms. Pipe, wld 6,000 6,000 400 61 4 117 89 52 2342 SB-247 A96061-T6 forging, wld 6,000 6,000 400 62 4.125 118 90 54 2443 SB-308 A96061-T6 shapes, wld 6,000 6,000 400 64 4.25 118 91 55 2544 Material properties are compliant with ASME Section IID Table 1A 4.375 119 93 56 27

4.5 119 94 57 28Impact Requirements For Low Temperature Applications 4.625 119 95 58 29The rules in ASME 8 Div 1 Section UCS 66 provide a good guide to reducing the risk of brittle fracture. 4.75 119 96 59 30

4.875 119 97 60 31Materials are divided into 4 groups: A) high risk to D) low risk:- 5 119 97 60 32

5.125 119 98 61 33A) Materials with low toughness or materials that don’t fit into the other groups. 5.25 119 99 62 34B) Most materials fit into this group 5.375 119 100 63 35C) Low strength materials; such as an SA516 Grade 60, note: grade 70 goes in B 5.5 119 100 63 36D) Tough fine grain steels, all normalised grades of SA516. 5.625 119 101 64 37

5.75 120 102 65 38If in doubt assume A 5.875 120 103 66 38

6 120 104 66 39As thickness is increases so does the risk of brittle fracture; therefore the temperature before impacts tests are required must get warmer.This is the basis of Fig UCS 66, which plots each material group between MDMT (Minimum Design Metal Temperature) and thickness. If the MDMT falls below the appropriate material curve (A to D), Impact testing is mandatory.However if the item is not highly stressed there is less risk of brittle fracture, UCS-66 permits the impact test temperature to be raised if the full material thickness is not required. If the resulting test temperature exceeds the values in the UCS 66 table, impact testing is not required.Residual stresses are present in all welded structures and can be up to yield point in magnitude. Whilst these stresses will not cause failure byyielding, they could drive a brittle fracture. Therefore stress relief is mandatory on thick material that is prone to brittle fracture (UCS 56). Allowances for stress relief is built into the code rules, but stress relief of any item when its not required will permit an increase in the impact test exemption temperature (UCS68c).Welding defects can also cause brittle fracture; therefore when material thickness exceeds a certain limit, full radiography is required. (Table UCS 57). The toughness of weld metal must also be demonstrated by production test plates, which are mandatory if impact testing is required.As the strength of the material increases so does the risk of brittle fracture, particularly as thickness increases. Therefore higher absorbed energy is required from strong materials above a certain thickness. (Fig UG 84.1).

UCS66, UG20, and UG84 MUST be read very carefully before any decision is made concerning impact testing, as both sections contain many exceptions and exemptions.

Temp [°F] - maximum design temperature Temp [°F] - minimum design temperature

Ambient

Strength

Design Streng

thMax ºF

150#Nom. Y No. & WNFLG.

Pipe O C Weld Slip on Lap Bolt Size of Wt.Size INCHES INCHES Neck Thrd. Joint Circle Holes Lbs 1/2 3 1/2 7/16 1 7/8 5/8 5/8 2 3/8 4 - 5/8 2 3/4 3 7/8 1/2 2 1/16 5/8 5/8 2 3/4 4 - 5/8 2

1 4 1/4 9/16 2 3/16 11/16 11/16 3 1/8 4 - 5/8 2.51 1/4 4 5/8 5/8 2 1/4 13/16 13/16 3 1/2 4 - 5/8 2.51 1/2 5 11/16 2 7/16 7/8 7/8 3 7/8 4 - 5/8 4

2 6 3/4 2 1/2 1 1 4 3/4 4-3/4 62 1/2 7 7/8 2 3/4 1 1/8 1 1/8 5 1/2 4-3/4 10

3 7 1/2 15/16 2 3/4 1 3/16 1 3/16 6 4-3/4 11.54 9 15/16 3 1 5/16 1 5/16 7 1/2 8-3/4 16.55 10 15/16 3 1/2 1 7/16 1 7/16 8 1/2 8-7/8 216 11 1 3 1/2 1 9/16 1 9/16 9 1/2 8-7/8 268 13 1/2 1 1/8 4 1 3/4 1 3/4 11 3/4 8-7/8 4210 16 1 3/16 4 1 15/16 1 15/16 14 1/4 12-1 5412 19 1 1/4 4 1/2 2 3/16 2 3/16 17 12-1 8814 21 1 3/8 5 2 1/4 3 1/8 18 3/4 12-1 1/8 11416 23 1/2 1 7/16 5 2 1/2 3 7/16 21 1/4 16-1 1/8 14218 25 1 9/16 5 1/2 2 11/16 3 13/16 22 3/4 16-1 1/4 16520 27 1/2 1 11/16 5 11/16 2 7/8 4 1/16 25 20-1 1/4 19724 32 1 7/8 6 3 1/4 4 3/8 29 1/2 20-1 3/8 268

300#Nom. Y No. & WNFLG.

Pipe O C Weld Slip on Lap Bolt Size of Wt.Size INCHES INCHES Neck Thrd. Joint Circle Holes Lbs 1/2 3 3/4 9/16 2 1/16 7/8 7/8 2 5/8 4 - 5/8 2 3/4 4 5/8 5/8 2 1/4 1 1 3 1/4 4 - 3/4 3

1 4 7/8 11/16 2 7/16 1 1/16 1 1/16 3 1/2 4 - 3/4 41 1/4 5 1/4 3/4 2 9/16 1 1/16 1 1/16 3 7/8 4 - 3/4 51 1/2 6 1/8 13/16 2 11/16 1 3/16 1 3/16 4 1/2 4 -7/8 7

2 6 1/2 7/8 2 3/4 1 5/16 1 5/16 5 8-3/4 82 1/2 7 1/2 1 3 1 1/2 1 1/2 5 7/8 8-7/8 12

3 8 1/4 1 1/8 3 1/8 1 11/16 1 11/16 6 5/8 8-7/8 184 10 1 1/4 3 3/8 1 7/8 1 7/8 7 7/8 8-7/8 26.55 11 1 3/8 3 7/8 2 2 9 1/4 8-7/8 36

150 LB. FLANGES - INCHES

300 LB. FLANGES - INCHES

6 12 1/2 1 7/16 3 7/8 2 1/16 2 1/16 10 5/8 12-7/8 458 15 1 5/8 4 3/8 2 7/16 2 7/16 13 12-1 6910 17 1/2 1 7/8 4 5/8 2 5/8 3 3/4 15 1/4 16-1 1/8 10012 20 1/2 2 5 1/8 2 7/8 4 17 3/4 16-1 1/4 14214 23 2 1/8 5 5/8 3 4 3/8 20 1/4 20-1 1/4 20616 25 1/2 2 1/4 5 3/4 3 1/4 4 3/4 22 1/2 20-1 3/8 24918 28 2 3/8 6 1/4 3 1/2 5 1/8 24 3/4 24-1 3/8 30620 30 1/2 2 1/2 6 3/8 3 3/4 5 1/2 27 24-1 3/8 36924 36 2 3/4 6 5/8 4 3/16 6 32 24-1 5/8 519

400 #Nom. No. & WNFLG.

Pipe O C Weld Slip on Lap Bolt Size of Wt.Size INCHES INCHES Neck Thrd. Joint Circle Holes Lbs 1/2 3 3/4 9/16 2 1/16 7/8 7/8 2 5/8 4 - 5/8 3 3/4 4 5/8 5/8 2 1/4 1 1 3 1/4 4 - 3/4 3.5

1 4 7/8 11/16 2 7/16 1 1/16 1 1/16 3 1/2 4 - 3/4 41 1/4 5 1/4 13/16 2 5/8 1 1/8 1 1/8 3 7/8 4 - 3/4 5.51 1/2 6 1/8 7/8 2 3/4 1 1/4 1 1/4 4 1/2 4 -7/8 8

2 6 1/2 1 2 7/8 1 7/16 1 7/16 5 8-3/4 102 1/2 7 1/2 1 1/8 3 1/8 1 5/8 1 5/8 5 7/8 8-7/8 14

3 8 1/4 1 1/4 3 1/4 1 13/16 1 13/16 6 5/8 8-7/8 184 10 1 3/8 3 1/2 2 2 7 7/8 8-1 305 11 1 1/2 4 2 1/8 2 1/8 9 1/4 8-1 396 12 1/2 1 5/8 4 1/16 2 1/4 2 1/4 10 5/8 12-1 498 15 1 7/8 4 5/8 2 11/16 2 11/16 13 12-1 1/8 7810 17 1/2 2 1/8 4 7/8 2 7/8 4 15 1/4 16-1 1/4 11012 20 1/2 2 1/4 5 3/8 3 1/8 4 1/4 17 3/4 16-1 3/8 16014 23 2 3/8 5 7/8 3 5/16 4 5/8 20 1/4 20-1 3/8 23316 25 1/2 2 1/2 6 3 11/16 5 22 1/2 20-1 1/2 29418 28 2 5/8 6 1/2 3 7/8 5 3/8 24 3/4 24-1 1/2 26020 30 1/2 2 3/4 6 5/8 4 5 3/4 27 24-1 5/8 44524 36 3 6 7/8 4 1/2 6 1/4 32 24-1 7/8 640


Pipe O C Weld Slip on Lap Bolt Size of Wt.Size INCHES INCHES Neck Thrd. Joint Circle Holes Lbs 1/2 3 3/4 9/16 2 1/16 7/8 7/8 2 5/8 4 - 5/8 3 3/4 4 5/8 5/8 2 1/4 1 1 6 1/4 4 - 3/4 3.5

1 4 7/8 11/16 2 7/16 1 1/16 1 1/16 3 1/2 4 - 3/4 41 1/4 5 1/4 13/16 2 5/8 1 1/8 1 1/8 3 7/8 4 - 3/4 5.51 1/2 6 1/8 7/8 2 3/4 1 1/4 1 1/4 4 1/2 4 -7/8 8

2 6 1/2 1 2 7/8 1 7/16 1 7/16 5 8-3/4 102 1/2 7 1/2 1 1/8 3 1/8 1 5/8 1 5/8 5 7/8 8-7/8 14

3 8 1/4 1 1/4 3 1/4 1 13/16 1 13/16 6 5/8 8-7/8 184 10 3/4 1 1/2 4 2 1/8 2 1/8 8 1/2 8-1 375 13 1 3/4 4 1/2 2 3/8 2 3/8 10 1/2 8-1 1/8 686 14 1 7/8 4 5/8 2 5/8 2 5/8 11 1/2 12-1 1/8 73

** The 1/4" raised face is not included in the thickness "Y" or "C"400 LB. FLANGES - INCHES **Y (See Note Above)


8 16 1/2 2 3/16 5 1/4 3 3 13 3/4 12-1 1/4 11210 20 2 1/2 6 3 3/8 4 3/8 17 16-1 3/8 18912 22 2 5/8 6 1/8 3 5/8 4 5/8 19 1/4 20-1 3/8 22614 23 3/4 2 3/4 6 1/2 3 11/16 5 20 3/4 20-1 1/2 26816 27 3 7 4 3/16 5 1/2 23 3/4 20-1 5/8 48118 29 1/4 3 1/4 7 1/4 4 5/8 6 25 3/4 20-1 3/4 55520 32 3 1/2 7 1/2 5 6 1/2 28 1/2 24-1 3/4 69024 37 4 8 5 1/2 7 1/4 33 24-2 977


Pipe O C Weld Slip on Lap Bolt Size of Wt.Size INCHES INCHES Neck Thrd. Joint Circle Holes Lbs 1/2 4 3/4 7/8 2 3/8 1 1/4 1 1/4 3 1/4 4 - 7/8 7 3/4 5 1/8 1 2 3/4 1 3/8 1 3/8 3 1/2 4 - 7/8 7

1 5 7/8 1 1/8 2 7/8 1 5/8 1 5/8 4 4 - 1 8.51 1/4 6 1/4 1 1/8 2 7/8 1 5/8 1 5/8 4 3/8 4 - 1 101 1/2 7 1 1/4 3 1/4 1 3/4 1 3/4 4 7/8 4 -1 1/8 14

2 8 1/2 1 1/2 4 2 1/4 2 1/4 6 1/2 8-1 242 1/2 9 5/8 1 5/8 4 1/8 2 1/2 2 1/2 7 1/2 8-1 1/8 36

3 9 1/2 1 1/2 4 2 1/8 2 1/8 7 1/2 8-1 294 11 1/2 1 3/4 4 1/2 2 3/4 2 3/4 9 1/4 8-1 1/4 515 13 3/4 2 5 3 1/8 3 1/8 11 8-1 3/8 866 15 2 3/16 5 1/2 3 3/8 3 3/8 12 1/2 12-1 1/4 1108 18 1/2 2 1/2 6 3/8 4 4 1/2 15 1/2 12-1 1/2 18710 21 1/2 2 3/4 7 1/4 4 1/4 5 18 1/2 16-1 1/2 26812 24 3 1/8 7 7/8 4 5/8 5 5/8 21 20-1 1/2 37214 25 1/4 3 3/8 8 3/8 5 1/8 6 1/8 22 20-1 5/8 56216 27 3/4 3 1/2 8 1/2 5 1/4 6 1/2 24 1/4 20-1 3/4 68518 31 4 9 6 7 1/2 27 20-2 92420 33 3/4 4 1/4 9 3/4 6 1/4 8 1/4 29 1/2 24-2 1/8 116424 41 5 1/2 11 1/2 8 10 1/2 35 1/2 24-2 5/8 2107


Pipe O C Weld Slip on Lap Bolt Size of Wt.Size INCHES INCHES Neck Thrd. Joint Circle Holes Lbs 1/2 4 3/4 7/8 2 3/8 1 1/4 1 1/4 3 1/4 4 - 7/8 7 3/4 5 1/8 1 2 3/4 1 3/8 1 3/8 3 1/2 4 - 7/8 7

1 5 7/8 1 1/8 2 7/8 1 5/8 1 5/8 4 4 - 1 8.51 1/4 6 1/4 1 1/8 2 7/8 1 5/8 1 5/8 4 3/8 4 - 1 101 1/2 7 1 1/4 3 1/4 1 3/4 1 3/4 4 7/8 4 -1 1/8 14

2 8 1/2 1 1/2 4 2 1/4 2 1/4 6 1/2 8-1 242 1/2 9 5/8 1 5/8 4 1/8 2 1/2 2 1/2 7 1/2 8-1 1/8 36

3 10 1/2 1 7/8 4 5/8 2 7/8 2 7/8 8 8-1 1/4 484 12 1/4 2 1/8 4 7/8 3 9/16 3 9/16 9 1/2 8-1 3/8 695 14 3/4 2 7/8 6 1/8 4 1/8 4 1/8 11 1/2 8-1 5/8 1326 15 1/2 3 1/4 6 3/4 4 11/16 4 11/16 12 1/2 12-1 1/2 164



8 19 3 5/8 8 3/8 5 5/8 5 5/8 15 1/2 12-1 3/4 27310 23 4 1/4 10 6 1/4 7 19 12-2 45412 26 1/2 4 7/8 11 1/8 7 1/8 8 5/8 22 1/2 16-2 1/8 69014 29 1/2 5 1/4 11 3/4 9 1/2 25 16-2 3/816 32 1/2 5 3/4 12 1/4 10 1/4 27 3/4 16 - 2 5/818 36 6 3/8 12 7/8 10 7/8 30 1/2 16- 2 7/820 38 3/4 7 14 11 1/2 32 3/4 16-3 1/824 46 8 16 13 39 16 -3 5/8

SCREWED FITTINGS

3000#SIZE A B C D E F G H * 1/2 1 5/16 1 1/2 1 2 1/8 2 3/16 1 7/8 1 1/8 1/2 3/4 1 1/2 1 13/16 1 1/8 2 5/16 2 9/16 2 1 3/8 9/16

1 1 3/4 2 3/16 1 5/16 2 1/2 2 15/16 2 3/8 1 3/4 11/161 1/2 2 3/8 3 1 11/16 3 1/8 3 11/16 3 1/8 2 1/2 11/16

2 2 1/2 3 5/16 1 3/4 3 1/2 4 9/16 3 3/8 3 3/4 2 1/2 3 1/4 4 2 1/16 4 5/8 5 1/4 3 5/8 3 5/8 15/16

6000#SIZE A B C D E F G H * 1/2 1 1/2 1 13/16 1 1/8 2 7/8 2 13/16 1 7/8 1 1/2 1/2 3/4 1 3/4 2 3/16 1 5/16 3 3/8 3 1/8 2 1 3/4 9/16

1 2 2 7/16 1 3/8 3 5/8 3 13/16 2 3/8 2 1/4 11/161 1/2 2 1/2 3 5/16 1 3/4 4 3/16 4 3/4 3 1/8 3 11/16

2 3 1/4 4 2 1/16 4 5/8 5 1/4 3 3/8 3 5/8 3/4 2 1/2 3 3/4 4 3/4 2 1/2 - - 3 5/8 4 1/4 15/16

* Thread engagement typical for H, J & K

Nominal Outside Desig- Wall WeightPipe Size Dia. nation Thickness Lbs/ Ft.

150# 150# 150# 1/8 0.405 Std. 0.068 0.244SO-FLG. Lap-FLG. Blind-FLG. 1/8 0.405 X-Stg. 0.095 0.314

Wt. Wt. Wt.Lbs Lbs Lbs 1/4 0.540 Std. 0.088 0.424

1 1 2 1/4 0.540 X-Stg. 0.119 0.5351.5 1.5 22 2 2 3/8 0.675 Std. 0.091 0.567

2.5 2.5 3 3/8 0.675 X-Stg. 0.126 0.7383 3 35 5 4 1/2 0.840 Std. 0.109 0.8508 8 7 1/2 0.840 X-Stg. 0.147 1.0879 9 9 1/2 0.840 160 0.138 1.31013 12 17 1/2 0.840 XX-Stg. 0.294 1.71415 13 2017 18 27 3/4 1.050 Std. 0.113 1.13028 28 47 3/4 1.050 X-Stg. 0.154 1.47340 36 67 3/4 1.050 160 0.219 1.94061 60 102 3/4 1.050 XX-Stg. 0.308 2.44083 77 139

106 104 187 1 1.315 Std. 0.133 1.678109 146 217 1 1.315 X-Stg. 0.179 2.171148 159 283 1 1.315 160 0.250 2.850204 195 415 1 1.315 XX-Stg. 0.358 3.659

1 1/4 1.660 Std. 0.140 2.272300# 300# 300# 1 1/4 1.660 X-Stg. 0.191 2.996

SO-FLG. Lap-FLG. Blind-FLG. 1 1/4 1.660 160 0.250 3.764

Wt. Wt. Wt. 1 1/4 1.660 XX-Stg. 0.382 5.214Lbs Lbs Lbs1.5 1.5 2 1 1/2 1.900 Std. 0.145 2.7172.5 2.5 3 1 1/2 1.900 X-Stg. 0.200 3.6313 3 4 1 1/2 1.900 160 0.281 4.862

4.5 4.5 6 1 1/2 1.900 XX-Stg. 0.400 6.4086.5 6.5 77 7 8 2 2.375 Std. 0.154 3.65210 10 12 2 2.375 X-Stg. 0.218 5.02213 14.5 16 2 2.375 160 0.344 7.450

23.5 24 28 2 2.375 XX-Stg. 0.436 9.02929 26 37

36 38 48 2 1/2 2.875 Std. 0.203 5.79056 55 79 2 1/2 2.875 X-Stg. 0.276 7.66077 88 122 2 1/2 2.875 160 0.375 10.010

113 139 183 2 1/2 2.875 XX-Stg. 0.552 13.690159 184 241210 234 315 3 3.5 Std. 0.216 7.57253 305 414 3 3.5 X-Stg. 0.300 10.25307 375 515 3 3.5 160 0.438 14.32490 530 800 3 3.5 XX-Stg. 0.600 18.58

4 4.5 Std. 0.237 10.79

400 # 400 # 400 # 4 4.5 X-Stg. 0.337 14.98SO-FLG. Lap-FLG. Blind-FLG. 4 4.5 120 0.438 19.00

Wt. Wt. Wt. 4 4.5 160 0.531 22.60Lbs Lbs Lbs 4 4.5 XX-Stg. 0.674 27.54

2 2 2 3 3 3 5 5.563 Std. 0.258 14.62

3.5 3.5 4 5 5.563 X-Stg. 0.375 20.784.5 4.5 6 5 5.563 120 0.500 27.106.5 6.5 8 5 5.563 160 0.625 32.968 8 10 5 5.563 XX-Stg. 0.750 38.5512 11 15 15 14 20 6 6.625 Std. 0.280 18.9724 22 33 6 6.625 X-Stg. 0.432 28.5731 29 44 6 6.625 120 0.562 36.4039 37 61 6 6.625 160 0.719 45.3063 59 100 6 6.625 XX-Stg. 0.864 53.1691 95 155

129 152 226 8 8.625 Std. 0.322 28.55191 210 310 8 8.625 60 0.406 35.70253 280 398 8 8.625 X-Stg. 0.500 43.39310 345 502 8 8.625 100 0.594 50.90378 420 621 8 8.625 120 0.719 60.70539 615 936 8 8.625 140 0.812 67.80

8 8.625 XX-Stg. 0.875 72.428 8.625 160 0.906 74.70

600 # 600 # 600 # SO-FLG. Lap-FLG. Blind-FLG. 10 10.750 Std. 0.365 40.48

Wt. Wt. Wt. 10 10.750 X-Stg. 0.500 54.74Lbs Lbs Lbs 10 10.750 80 0.594 64.40

2 2 2 10 10.750 100 0.719 77.003 3 3 10 10.750 120 0.844 89.20

3.5 3.5 4 10 10.750 140 1.000 104.204.5 4.5 6 10 10.750 160 1.125 116.006.5 6.5 8 8 8 10 12 12.750 Std. 0.375 49.6012 11 15 12 12.750 40 0.406 53.6015 14 20 12 12.750 X-Stg. 0.500 65.4033 31 41 12 12.750 60 0.562 73.2056 63 68 12 12.750 80 0.688 88.6066 78 86 12 12.750 100 0.844 108.00

97 112 139 12 12.750 XX-Stg. 1.000 125.50177 195 231 12 12.750 140 1.125 140.00215 240 295 12 12.750 160 1.312 161.00259 290 378 366 400 527 14 14.000 Std. 0.375 54.45476 469 665 14 14.000 40 0.438 63.30612 604 855 14 14.000 X-Stg. 0.500 71.93876 866 1175 14 14.000 80 0.750 109.50

14 14.000 160 1.406 188.70

900 # 900 # 900 # 16 16.000 Std. 0.375 62.44SO-FLG. Lap-FLG. Blind-FLG. 16 16.000 40 0.500 82.59

Wt. Wt. Wt. 16 16.000 X-Stg. 0.500 82.59Lbs Lbs Lbs 16 16.000 80 0.844 136.32

6 6 4 16 16.000 160 1.594 244.726 6 6

7.5 7.5 9 18 18.000 Std. 0.375 70.4410 10 10 18 18.000 40 0.562 104.4414 14 14 18 18.000 X-Stg. 0.500 93.2522 21 25 18 18.000 80 0.938 170.5636 29 35 18 18.000 160 1.781 307.8431 25 32 53 51 54 20 20.000 Std. 0.375 78.4383 81 87 20 20.000 40 0.594 122.84

108 105 113 20 20.000 X-Stg. 0.500 103.91172 188 197 20 20.000 80 1.031 208.42245 277 290 20 20.000 160 1.969 378.35326 371 413 380 397 494 24 24.000 Std. 0.375 94.41459 488 619 24 24.000 40 0.688 170.80647 670 880 24 24.000 X-Stg. 0.500 125.22792 868 1107 24 24.000 80 1.219 295.94

1480 1659 2099 24 24.000 160 2.344 540.96

1500 # 1500 # 1500 #SO-FLG. Lap-FLG. Blind-FLG.

Wt. Wt. Wt.Lbs Lbs Lbs

6 6 76 6 10

7.5 7.5 1210 10 1814 14 2522 21 3936 29 5648 38 8673 75 133

132 138 223164 170 345

258 286 533436 485 1025667 749 1464

SCREWED FITTINGS

3000#J * K *

1/2 1/2 9/16 9/16 11/16 11/16 11/16 11/16 3/4 3/4

15/16 15/16

6000#J * K *

1/2 1/2 9/16 9/16 11/16 11/16 11/16 11/16 3/4 3/4

15/16 15/16

Date post:	10-Feb-2016
Category:	Documents
Upload:	bob-fitcher
View:	365 times
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Pressure Vessel Design

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