Do not print this sheet, it contains only information as how to design elements of pressure vessel INPUTS INPUT CELLS (UNLOCKED)
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CALCULATIONS BY PROGRAM RESULTS
STEPS 1
Select sheet what you need to design (e-g: For shell design select shell sheet)
2
Input values in yellow cells ----->
3
Results
or thru
are shown for every item at end of the sheet
Histroy: 0 Reviewed with ARC
cells
USA
05.11.07
sign select shell sheet)
Inputs
THICKNESS OF CYLINDRICAL SHELL (Internal Pressure & Inside Dimensions)
Cylindrical Shell
Dsign Code: Cylinder Construction Material
ASME Sec VIII, Div.1, 2004 SA-516 Gr. 70 See Section II Part D for other materials
Internal Design Pressure
P
107.00
psi
Inner Diameter of Shell
Di
4580.00
mm
Temp
315.00
°F
Design Temperature Corrosion Allowance Allowable Stress
CA
3.00
S
20000 20000.00
Shell thickness per UG-27
psi
Full
Radiography Type Joint Efficiency
mm
E
1.00
t
PDi 2( SE 0.6 P)
Result: Min. Req. Design Thickness of Shell Mill Undertolerence per UG-16 Min. req'd thickness of Shell Select shell thickness
t = 15.2910 0.300 to= 15.5910 16.0000
mm mm mm mm
or Recommended thickness is adequate
Stress Releif per UCS-79 tnom=
16.00
mm
Final Centre Linre Radius
Rf=
2298.00
mm
Original Centreline radius
Ro=
Nominal thickness of Vessel
Percent Extreme fiber Elongation
0.348%
infinity for straight plate Stress Releif Not Required
Inputs
THICKNESS OF CYLINDRICAL SHELL (Internal Pressure & Outside Dimensions)
Cylindrical Shell
Dsign Code: Cylinder Construction Material
ASME Sec VIII, Div.1, 2004 SA-106 Gr. B See Section II Part D for other materials
Internal Design Pressure
P
1440.00
psi
Inner Diameter of Shell
Do
219.00
mm
Temp
120.00
°F
Design Temperature Corrosion Allowance Allowable Stress
CA
3.00
S
17115 20000.00
Shell thickness per UG-27
psi
Full
Radiography Type Joint Efficiency
mm
E
1.00
PD o 2 ( SE 0 . 4 P )
t
Result: Min. Req. Design Thickness of Shell Mill Undertolerence per UG-16 Min. req'd thickness of Shell Select shell thickness
t = 11.9131 1.489 to= 13.4023 16.0000
mm mm mm mm
or Recommended thickness is adequate
Stress Releif per UCS-79 tnom=
16.00
mm
Final Centre Linre Radius
Rf=
117.50
mm
Original Centreline radius
Ro=
Nominal thickness of Vessel
Percent Extreme fiber Elongation
infinity for straight plate
6.809% Stress Releif Required. To Avoid Stress Releif Increase The Thickness
Inputs
THICKNESS OF BOOT (Internal Pressure & Inside Dimensions)
Boot
Dsign Code:
ASME Sec VIII, Div.1, 2004 As Desired
Cylinder Construction Material
See Section II Part D for other materials
Internal Design Pressure
P
350.00
psi
Inner Diameter of Shell
Di
1524.00
mm
Height of Liquid Level in Boot
H
3.00
ft
100.00
°F
Design Temperature
Temp
Corrosion Allowance
CA
3.00
mm
Total Internal Pressure in Boot
Pi
351.30
psi
Allowable Stress
S
0 20000.00
psi
To be entered by user
Full
Radiography Type Joint Efficiency
E
Thickness per UG-27
t
1.00
Pi D i 2 ( SE 0 . 6 P )
Result: Min. Req. Design Thickness of Boot Mill Undertolerence per UG-16 Min. req'd thickness of Boot Select Boot thickness
t = 16.5271 0.300 to= 16.8271 17.0000
mm mm mm mm
or Recommended thickness is adequate
Stress Releif per UCS-79 Nominal thickness of Boot
tnom=
Final Centre Linre Radius
Rf=
Original Centreline radius
Ro =
Percent Extreme fiber Elongation
1.10%
17.00
mm
770.50
mm
infinity for straight plate Stress Releif Not Required
Inputs
THICKNESS OF ELLIPSOIDAL HEAD
Dsign Code: Cylinder Construction Material
Ellipsoidal Head
Ellipsoidal Head
(Internal Pressure & Inside Dimensions)
ASME Sec VIII, Div.1, 2004 SA-516 Gr. 70 See Section II Part D for other materials
Internal Design Pressure
P
1440.00
psi
Inner Diameter of Head
Di
3300.00
mm
Temp
170.00
°F
Design Temperature Corrosion Allowance Allowable Stress
CA
3.00
S
20000 20000.00
psi
Spot
Radiography Type Joint Efficiency
mm
E
0.85
Thickness per UG-32
t
PD i 2 SE 0 . 2 P
Result: Min. Req. Design Thickness of Head Mill Undertolerence per UG-16 Min. req'd thickness of Head Select Head thickness
t = 145.1705 0.300 to= 145.4705 14.0000
mm mm mm mm
or Recommend a higher thickness
Stress Releif per UCS-79 Nominal thickness of Vessel
tnom=
Final Centre Linre Radius
Rf=
Original Centreline radius
Ro=
Percent Extreme fiber Elongation
1.86%
14.00
mm
563.38
mm
infinity for straight plate Stress Releif Not Required
Inputs
THICKNESS OF ELLIPSOIDAL HEAD
Dsign Code: Cylinder Construction Material
Ellipsoidal Head
Ellipsoidal Head
(Internal Pressure & Inside Dimensions)
ASME Sec VIII, Div.1, 2004 SA-516 Gr. 70 See Section II Part D for other materials
Internal Design Pressure
P
1440.00
psi
Inner Diameter of Head
D0
273.00
mm
Temp
120.00
°F
Design Temperature Corrosion Allowance Allowable Stress
CA
3.00
S
20000 20000.00
psi
Full
Radiography Type Joint Efficiency
mm
E
1.00
Thickness per UG-32
PD o 2 SE 1 . 8 P
t Result: Min. Req. Design Thickness of Head Mill Undertolerence per UG-16 Min. req'd thickness of Head Select Head thickness
t = 12.2271 0.300 to= 12.5271 14.0000
mm mm mm mm
or Recommended thickness is adequate
Stress Releif per UCS-79 tnom=
14.00
mm
Final Centre Linre Radius
Rf=
48.79
mm
Original Centreline radius
Ro=
Nominal thickness of Vessel
Percent Extreme fiber Elongation
infinity for straight plate
21.52% Stress Releif Required. To Avoid Stress Releif Increase The Thickness
Inputs
THICKNESS OF ELLIPSOIDAL HEAD (Internal Pressure & Inside Dimensions)
Boot
Dsign Code: Cylinder Construction Material
ASME Sec VIII, Div.1, 2004 As Desired
Add SA 105 as Boot cap
See Section II Part D for other materials
Internal Design Pressure
P
386.30
psi
Inner Diameter of Head
Di
457.20
mm
Temp
150.00
°F
Design Temperature Corrosion Allowance Allowable Stress
CA
3.00
S
0 20000.00
psi
To be entered by user
Full
Radiography Type Joint Efficiency
mm
E
1.00
Thickness per UG-32
t
PD i 2 SE 0 . 2 P
Result: Min. Req. Design Thickness of Head Mill Undertolerence per UG-16 Min. req'd thickness of Head Select Head thickness
t = 7.4297 0.300 to= 7.7297 7.9375 5/16
mm mm mm mm in
or Recommended thickness is adequate
Stress Releif per UCS-79 tnom=
7.94
mm
Final Centre Linre Radius
Rf=
79.07
mm
Original Centreline radius
Ro=
Nominal thickness of Vessel
Percent Extreme fiber Elongation
infinity for straight plate
7.53% Stress Releif Required. To Avoid Stress Releif Increase The Thickness
Inputs
THICKNESS OF HEMISPHERICAL HEAD
Spherical Head
Spherical Head
(Internal Pressure & Inside Dimensions)
Dsign Code:
ASME Sec VIII, Div.1, 2004 As Desired
Cylinder Construction Material
See Section II Part D for other materials
Internal Design Pressure
P
100.00
psi
Inner Diameter of Head
Di
2438.40
mm
Temp
650.00
°F
Design Temperature Corrosion Allowance Allowable Stress
CA
0.00
S
0 20000.00
psi
To be entered by user
Full
Radiography Type Joint Efficiency
mm
E
1.00
Thickness per UG-32
PD i 2 ( 2 SE 0 . 2 P )
t Result: Min. Req. Design Thickness of Head Mill Undertolerence per UG-16 Min. req'd thickness of Head Select Head thickness
t = 3.0495 0.300 to= 3.3495 4.0000
mm mm mm mm
or Recommended thickness is adequate
Stress Releif per UCS-79 tnom=
4.00
mm
Final Centre Linre Radius
Rf=
1221.20
mm
Original Centreline radius
Ro=
Nominal thickness of Vessel
Percent Extreme fiber Elongation
0.25%
infinity for straight plate Stress Releif Not Required
Inputs
THICKNESS OF CONICAL SECTION (Internal Pressure & Inside Dimensions)
Note:
α to be less than 30 degree
α
Dsign Code:
Conical Section
ASME Sec VIII, Div.1, 2004 SA-106 Gr. B
Cylinder Construction Material
See Section II Part D for other materials
Internal Design Pressure
P
100.00
psi
Inner Diameter of Conical section
Di
2438.40
mm
Temp
650.00
°F
Design Temperature Corrosion Allowance
CA
0.00
mm
α
35.00
Degree
Cone Half Apex Angle
Formula is not valid. See Div I for special analysis Allowable Stress
17115 20000.00
S
psi
Full
Radiography Type Joint Efficiency
E
1.00
Thickness per UG-32
t
PDi 2Cos ( SE 0.6 P )
Result: t = 8.7270 1.091 to= 9.8179 7.9375 5/16
Min. Req. Design Thickness of Conical section
Mill Undertolerence per UG-16 Min. req'd thickness of Conical section Select Conical section thickness
mm mm mm mm in
or Recommend a higher thickness
Stress Releif per UCS-79 Nominal thickness of Vessel
tnom=
7.94
mm
Final Centre Linre Radius
Rf= Ro=
1223.17
mm
Original Centreline radius Percent Extreme fiber Elongation
0.49%
infinity for straight plate Stress Releif Not Required
Inputs
THICKNESS OF TORISPHERICAL HEAD (Internal Pressure & Inside Dimensions)
Torispherical Head
Dsign Code:
ASME Sec VIII, Div.1, 2004 As Desired
Cylinder Construction Material
See Section II Part D for other materials
Internal Design Pressure
P
100.00
psi
Inner Diameter of Head
L
2438.40
mm
Temp
650.00
°F
Design Temperature Corrosion Allowance
CA
3.18
mm
Knuckle radius
r
152.40
mm
Allowable Stress
S
0 15000.00
psi
To be entered by user
Full
Radiography Type Joint Efficiency
E
1.00
Ratio
L/r
16.00
Case 1: when L/r= 16 Thickness per UG-32
t
0.885PL This Formula Is Valid ( SE 0.1P )
Result: Min. Req. Design Thickness of Head Mill Undertolerence per UG-16 Min. req'd thickness of Head Select Head thickness
t = 17.5762 0.300 to= 17.8762 14.2875 9/16
mm mm mm mm in
or Recommend a higher thickness
Case 2: when L/r < 16 Thickness per UG-32
t
PLM This Formula Is Not Valid 2SE 0.2 P
t Result:
PLM 2SE 0.2 P M= 1.75 t = 17.41 0.300 to= 17.71 14.2875 9/16
Factor M Min. Req. Design Thickness of Head Mill Undertolerence per UG-16 Min. req'd thickness of Head Select Head thickness SA-516 Gr. 70
mm mm mm mm mm in
or Recommend a higher thickness
SA-106 Gr. B
Case 3:
SA-285 Gr. C
when L/r > 16 SA-240 Gr. 304
Thickness per UG-32 As Desired
1 (3 L ) r 4 PLM t This Formula Is Not Valid 2SE 0.2 P
M
Result: Factor M Min. Req. Design Thickness of Head Mill Undertolerence per UG-16 Min. req'd thickness of Head Select Head thickness
M= 1.75 t = 17.41 0.300 to= 17.71 14.2875 9/16
mm mm mm mm mm in
or Recommend a higher thickness
Stress Releif per UCS-79 Nominal thickness of Vessel
tnom=
Final Centre Linre Radius
Rf=
Original Centreline radius
Ro=
Percent Extreme fiber Elongation
17.88
mm
170.28
mm
infinity for straight plate
7.87% Stress Releif Required. To Avoid Stress Releif Increase The Thickness
Inputs
THICKNESS OF HEMISPHERICAL HEAD (Internal Pressure & Inside Dimensions)
Circular Flat Head
Dsign Code:
ASME Sec VIII, Div.1, 2004
Cylinder Construction Material
As Desired See Section II Part D for other materials
Internal Design Pressure
P
300.00
psi
Inner Diameter of Head
Di
609.60
mm
Temp
450.00
°F
Design Temperature Corrosion Allowance Allowable Stress
CA
3.00
S
FALSE 20000.00
mm psi
Full
Radiography Type Joint Efficiency
E
1.00
Required thickness of Shell
tr
-505.00
mm
Actual thickness of Shell
ts
-505.00
mm
Thickness per UG-34
Result: C Factor Min. Req. Design Thickness of Head Mill Undertolerence per UG-16 Min. req'd thickness of Head Select Head thickness
To be entered by user
t C 0.33 r ts CP t D SE C= 0.33 t = 45.8892 0.300 to= 46.1892 46.0000
mm mm mm mm mm
or Recommend a higher thickness
Stress Releif per UCS-79 Nominal thickness of Vessel
tnom=
46.19
mm
Final Centre Linre Radius
Rf=
Original Centreline radius
Ro=
Percent Extreme fiber Elongation
327.89
mm
infinity for straight plate
10.56% Stress Releif Required. To Avoid Stress Releif Increase The Thickness
SADDLE DIMENSIONS
Dia of Vessel (mm)
304.8 355.6 406.4 457.2 508 558.8 609.6 660.4 711.2 762 812.8 863.6 914.4 965.2 1016 1066.8 1219.2 1371.6 1524
Max.Weight of Vessel (Kg)
19,051 22,680 25,402 28,123 31,752 34,474 38,102 40,824 44,453 47,174 50,803 58,061 60,782 65,318 95,256 99,792 114,307 127,915 141,523
Length A (mm)
266.7 317.5 355.6 393.7 444.5 482.6 533.4 571.5 622.3 660.4 711.2 736.6 774.7 838.2 889 927.1 1066.8 1193.8 1320.8
Base Plate Web Plate Wear Plate Width Thickness Height Thickness Width Thickness Width C (mm) G (mm) (mm) H (mm) D (mm) K (mm) (mm)
101.6 101.6 101.6 101.6 101.6 101.6 101.6 101.6 101.6 101.6 101.6 152.4 152.4 152.4 152.4 152.4 152.4 152.4 152.4
6.35 6.35 6.35 6.35 6.35 6.35 6.35 6.35 12.7 12.7 12.7 12.7 12.7 12.7 12.7 12.7 19.05 19.05 19.05
6.35 6.35 6.35 6.35 6.35 6.35 6.35 6.35 6.35 6.35 6.35 6.35 6.35 6.35 9.525 9.525 9.525 9.525 9.525
101.6 101.6 101.6 101.6 101.6 152.4 152.4 152.4 152.4 152.4 152.4 279.4 279.4 279.4 279.4 279.4 279.4 279.4 279.4
6.35 6.35 6.35 6.35 6.35 6.35 6.35 9.525 9.525 9.525 9.525 9.525
Ribs Dist. Of centre Thickness from Base Plate H (mm) (B)
6.35 6.35 6.35 6.35 6.35 6.35 6.35 6.35 6.35 6.35 6.35 6.35 6.35 6.35 9.525 9.525 9.525 9.525 9.525
304.8 330.2 355.6 381 406.4 431.8 457.2 482.6 508 533.4 558.8 584.2 609.6 635 660.4 685.8 762 914.4 990.6
Bolt Dist.
Bolt Dia
E (mm)
(mm)
88.9 101.6 127 152.4 165.1 177.8 190.5 203.2 215.9 228.6 241.3 254 279.4 304.8 330.2 355.6 406.4 457.2 508
12.70 12.70 12.70 12.70 12.70 12.70 12.70 12.70 12.70 12.70 12.70 12.70 12.70 19.05 19.05 19.05 19.05 19.05 19.05
1676.4 1828.8 1981.2 2133.6 2286 2438.4 2590.8 2743.2 2895.6 3048 3200.4 3352.8 3505.2 3657.6
156,038 182,347 197,770 213,192 227,707 243,130 344,736 365,602 386,467 406,426 426,384 447,250 467,208 488,074
1460.5 1587.5 1727.2 1854.2 1981.2 2120.9 2247.9 2374.9 2527.3 2641.6 2781.3 2908.3 3048 3175
152.4 228.6 228.6 228.6 228.6 228.6 228.6 228.6 228.6 228.6 228.6 228.6 228.6 228.6
19.05 19.05 19.05 19.05 19.05 25.4 25.4 25.4 25.4 25.4 25.4 25.4 25.4 25.4
9.525 9.525 12.7 12.7 12.7 12.7 12.7 12.7 19.05 19.05 19.05 19.05 19.05 19.05
279.4 457.2 457.2 457.2 457.2 457.2 457.2 457.2 609.6 609.6 609.6 609.6 609.6 609.6
9.525 9.525 9.525 9.525 9.525 9.525 12.7 12.7 12.7 12.7 12.7 12.7 12.7 12.7
9.525 9.525 12.7 12.7 12.7 12.7 12.7 12.7 19.05 19.05 19.05 19.05 19.05 19.05
1066.8 1143 1219.2 1295.4 1371.6 1447.8 1524 1600.2 1676.4 1752.6 1828.8 1905 1981.2 2057.4
558.8 609.6 660.4 711.2 762 812.8 863.6 914.4 965.2 1016 1066.8 1117.6 1168.4 1219.2
19.05 19.05 19.05 25.40 25.40 25.40 25.40 25.40 25.40 31.75 31.75 31.75 31.75 31.75
THICKNESS OF SKIRT
LATER Inputs * Wind Load (From PVElite) * Height of Vessel
P H MT R E
* Moment * Outside Radius of Skirt * Joint Efficiency * Stress Value of Head or Skirt
Mat. Whichever is smaller * Weight of Tower above Skirt
W
lbs ft 493,000.00 lbs-ft 28.00 in 8500.00 58.00
0.70
Skirt
20000.00
psi
78000.00
lbs 516 Gr-70 Temp(F) S (psi)
Formula used :
t
12 M T 2W R ² SE RSE
Resuslt: Required Thickness of Skirt
Required Thickness of Skirt
0.30
7.58
in
mm
(-20)
20,000
50
20,000
100
20,000
200
20,000
300 400
20,000 20,000
500 600
20,000 19,400
650
18,800
700 750
18,100 14,800
800 850
12,000 9,300
900 950 1000
6,700 4,000 2,500
Note: For other materials see section 2 part D
THICKNESS OF NOZZLE AS PER UG-45 NB 3/4" (DN 20)
Nozzle Size :
Inputs UG-45 b(1) for Internal Pressure Internal Design Pressure Diameter of Shell/Head Design Temperature Allowable Stress of Shell Joint Efficiency Corrosion Allowance Formula used
Inputs UG-45 b(2) for External Pressure P D Temp S E CA t
Result Thickness
LATER
Nozzle on Sump of PV-221 ( R22 Receiver )
259.00 2168.00 140.00 17100.00 1.00 3.00
psi mm F psi mm
Formula used
PD 2( SE 0.6 P )
t
19.5691
External Design Pressure Diameter of Shell/Head Design Temperature Allowable Stress of Shell Joint Efficiency Corrosion Allowance t
P D Temp S E CA
15.00
2168.00 140.00 17100.00 1.00 3.00
psi mm F psi mm
PD 2( SE 0.6 P )
Result mm
Inputs UG-16(b)
Thickness
t
3.9514
mm
t t CA
2.87
2.5113 3.00
mm mm mm
t
5.5113
mm
P D Temp S E CA
259.00 20.00 140.00 17100.00 1.00 3.00
psi mm F psi
Inputs UG-45 b(4) Minimum thickness Minimum thickness Corrosion Allowance
t t CA
1/16 1.59 3.00
in mm mm
t
4.5875
mm
Result
Standard Wall Thk of pipe Minimum thickness Corrosion Allowance Result
Thickness
Final Result
Thickness
Inputs UG-45 a for Internal Pressure
Step 1:
Max ( UG 45b(1) , UG 16b)
t
19.5691
mm
Step 2:
Max ( UG 45b(2) , UG 16b)
t
4.5875
mm
Step 3:
Max ( Step1 , Step 2)
t
19.5691
mm
Step 4:
Min ( Step3 , UG-45 b(4))
t
5.5113
mm
Step 5:
Max ( Step4 , UG-45 (a))
t
5.5113
mm
Internal Design Pressure Diameter of Pipe Design Temperature Allowable Stress Joint Efficiency Corrosion Allowance Formula used
t
mm
PD 2( SE 0.6 P )
Result
Min Required thickness of Nozzle
t Sch
5.5113
mm
Thickness
t
3.1529
mm
THICKNESS OF NOZZLE AS PER UG-45 11.75
Nozzle Size :
in
Inputs UG-45 b(1) for Internal Pressure Internal Design Pressure Diameter of Shell/Head Design Temperature Allowable Stress of Shell Joint Efficiency Corrosion Allowance Formula used
t
Inputs UG-45 b(2) for External Pressure P D Temp S E CA
400.00 60.00 250.00 14300.00 1.00 0.00
psi in F psi
External Design Pressure Diameter of Shell/Head Design Temperature Allowable Stress of Shell Joint Efficiency Corrosion Allowance
in
Formula used
PD 2( SE 0.6 P )
Result
t
P D Temp S E CA
15.00 60.00 250.00 14300.00 1.00 0.00
psi in F psi
t
0.0315
in
t t CA
8.3738 0.00
mm mm mm
t t
8.3738 0.3297
mm in
P D Temp S E CA
400.00
in
PD 2( SE 0.6 P )
Result Thickness
t
0.8535
in
Inputs UG-16(b)
Thickness
Inputs UG-45 b(4) Minimum thickness Minimum thickness Corrosion Allowance
Result
LATER
ASME Section VIII Index L-7.2 Example 2
Thickness Thickness
t t CA
1/16 1.59 3.00
in mm mm
t t
4.5875 0.1806
mm in
Final Result
Standard Wall Thk of pipe Minimum thickness Corrosion Allowance Result
Thickness Thickness
9.57
Inputs UG-45 a for Internal Pressure
Step 1:
Max ( UG 45b(1) , UG 16b)
t
0.8535
mm
Step 2:
Max ( UG 45b(2) , UG 16b)
t
0.1806
mm
Step 3:
Max ( Step1 , Step 2)
t
0.8535
mm
Step 4:
Min ( Step3 , UG-45 b(4))
t
0.3297
mm
Step 5:
Max ( Step4 , UG-45 (a))
t
0.3297
mm
Min Required thickness of Nozzle
t
0.3297
mm
Internal Design Pressure Diameter of Pipe Design Temperature Allowable Stress Joint Efficiency Corrosion Allowance Formula used
t
psi in 250.00 F 16600.00 psi 11.75
1.00
0.00
in
0.14
in
PD 2( SE 0.6 P )
Result
Actual Thickness of Pipe
=
Actual Thickness of Pipe
Thickness
Sch
Pipe Schedule Thickness x 0.875 (12.5% Undertolerance )
should be greater than
Minimum Required Thickness
t
PIPE SCHEDULE CHART ND (in)
OD
0.50 0.75 1.00 1.25 1 1/2 2.00 2 1/2 3.00 3 1/2 4.00 5.00 6.00 8.00 10.00 12.00 14.00 16.00 18.00 20.00 22.00 24.00 26.00 28.00 30.00 32.00 34.00 36.00
21.30 26.70 33.4 42.2 48.3 60.3 73 88.9 101.6 114.3 141.3 168.3 219.1 273.1 323.9 355.6 406.4 457.2 508 558.8 609.6 660.4 711.2 762 812.8 863.6 914.4
Sch 10
Sch. 20
Sch. 30
2.11 2.77 2.77 2.77 2.77 3.05 3.05 3.05 3.05 3.4
6.35 6.35 6.35 6.35 6.35 6.35 7.92 7.92 7.92 7.92 7.92 7.92
6.35 6.35 6.35 7.92 7.92 7.92 9.52 9.52 9.52 12.7 12.7 12.7 12.7 12.7 12.7
7.04 7.8 8.38 9.52 9.52 11.12 12.7 12.7 14.27 15.87 15.87 15.87 15.87 15.87
Std. Wall
Sch. 40
2.77 2.87 3.38 3.56 3.69 3.91 5.16 5.49 5.74 6.02 6.55 7.11 8.18 9.27 9.57 9.52 9.52 9.52 9.52 9.52 9.52 9.52 9.52 9.52 9.52 9.52 9.52
2.77 2.87 3.38 3.56 3.69 3.91 5.16 5.49 5.74 6.02 6.55 7.11 8.18 9.27 10.31 11.12 12.7 14.27 15.06 15.87 17.48
17.48 17.48 19.05
Sch. 60
10.34 12.7 14.27 15.06 16.66 19.05 20.62 22.22 24.59
Extra Strong
Sch. 80
3.73 3.91 4.55 4.85 5.08 5.54 7.01 7.62 8.08 8.56 9.52 10.97 12.7 12.7 12.7 12.7 12.7 12.7 12.7 12.7 12.7 12.7 12.7 12.7 12.7 12.7 12.7
3.73 3.91 4.55 4.85 5.08 5.54 7.01 7.62 8.08 8.56 9.52 10.97 12.7 15.06 17.45 19.05 21.41 23.8 26.19 28.57 30.94
Sch. 100
15.06 18.24 21.41 23.8 26.19 29.36 32.54 34.92 38.89
Sch. 120
11.3 12.7 14.27 18.24 21.41 23.8 27.76 30.94 34.92 38.1 41.27
Sch. 140
20.62 25.4 28.57 31.75 36.53 39.67 44.45 47.64
Sch 160
XX Strong
ND
4.75 5.54 6.35 6.35 7.14 8.71 9.52 11.13
7.47 7.82 9.09 9.7 10.16 11.07 14.02 15.24 16.15 17.12 19.05 21.95 22.22
1/2 3/4 1.00 1 1/4 1 1/2 2.00 2 1/2 3.00 3 1/2 4.00 5.00 6.00 8.00 10.00 12.00 14.00 16.00 18.00 20.00 22.00 24.00 26.00 28.00 30.00 32.00 34.00 36.00
13.49 15.87 18.24 23.01 28.57 33.32 35.71 40.46 45.24 49.99 53.97
LIFTING LUG DIMENSIONS
Vessel Weight
Dia of Hole
Thickness of Lug
Radius of Outer
Height of Lug
Length of Lug
Weld
(Kg) 5,443 9,072 13,608 22,680 31,752 45,360 68,040 90,720 113,400 136,080
D (mm) 25.4 28.702 35.052 41.402 54.102 63.5 76.2 101.6 107.95 114.3
T (mm) 12.7 19.05 25.4 31.75 31.75 38.1 44.45 50.8 50.8 63.5
arc R (mm) 38.1 50.8 54.102 63.5 88.9 114.3 127 152.4 165.1 177.8
H (mm) 127 152.4 152.4 177.8 203.2 228.6 254 304.8 330.2 355.6
L (mm) 254 254 254 304.8 304.8 406.4 406.4 457.2 457.2 508
(Min) 12.7 mm Full Penetration Fillet
19.05 mm Full Penetration Fillet
LATER Butt Weld Input Thickness of the Plate
Pressure Conditions t
16.00
mm
Design Pressure
P
400.00
psi
Theta
56.00
degree
Diameter
D
1375
mm
Diameter to be Weld
D
1375.00
mm
Area for Pressure
A
1484140.63
mm2
Total Area of Weld
A
Area for Pressure
A
2300.42
in2
Total Area of Weld
A
836.80
in2
Load induced
F
920169
lbs
Allowable Stress of Material
S
20000.00
psi
Bearable Load for Butt Weld
F
16735938 lbs
Bevel Angle
Strength of Weld Result
2 539867.88 mm
1718.79 % Weld is O.K.
ANCHOR BOLT DESIGN LATER Inputs Bolt Area
Wind Load (From PVElite) Height of Vessel with Skirt Moment Weight of Vessel Bolt Circle Area within Bolt Circle Circumference of Bolt Circle Maximum Tension Allow. Stress Value of Bolt Mat. No. of Anchor Bolts Req.Area of one Bolt
P H M W
lbs 21.00 ft 63,000.00 lbs-ft 11000.00 lbs 84.00 in 2 5,538.96 in 264 in 94.78 lb/in 15,000.00 psi
AB CB T SB N BA
Dia of Bolt from Table against Root Area Induced Stress in Anchor Bolts
d Sind
Corrosion Allowance for Bolt
CA
3000.00
8.00
0.21
2
in
in 10,191.08 psi 0.63 0.13
in
Formulas Used M W AB CB
i Maximum Tension ( lb/in )
T 12
ii Req. Area of One Bolt ( Sq.in )
BA
TC B SB N
SB
TC B BA N
iii Stress in Anchor Bolt ( psi ) Resuslt: Required Diameter of Anchor Bolt
0.75
Required Diameter of Anchor Bolt
19.05
in mm
Table Bolt Size
in2
in
0.126
0.500
0.202
0.625
0.302
0.750
0.419
0.875
0.551
1.000
0.693
1.125
0.89
1.250
1.054
1.375
1.294
1.500
1.515
1.625
1.744
1.750
2.049
1.875
2.3
2.000
3.02
2.250
3.715 4.618
2.500 2.750
5.621
3.000
LATER Nominal Thickness
Nominal Thickness
Temperature (F)
(in)
(mm)
0.1 0.2
2.54 5.08
-55 -55
2.54 5.08
-55 -55
0.3
7.62
-55
7.62
-55
0.4
10.16
-55
10.16
-55
0.5
12.7
-55
12.7
-55
0.6 0.7 0.8 0.9
15.24 17.78 20.32 22.86
-50 -45 -40 -35
15.24 17.78 20.32 22.86
-50 -45 -40 -35
1 1.3 1.5 1.7 2.2 2.5 2.9 3.4 3.8 4.2 4.7 5.3 5.4 6
25.4 33.02 38.1 43.18 55.88 63.5 73.66 86.36 96.52 106.68 119.38 134.62 137.16 152.4 0 0 0 0 0 0
-30 -20 -15 -10 0 5 10 15 20 25 30 35 35 38
25.4 33.02 38.1 43.18 55.88 63.5 73.66 86.36 96.52 106.68 119.38 134.62 137.16 152.4
-30 -20 -15 -10 0 5 10 15 20 25 30 35 35 38
INTERPOLATION Temp (F)
Thickness
X1
-50
Y1
15.24
X
?
Y
16
X2
-45
Y2
17.78
X
-48.5
INTERPOLATION X1
340.57
Y1
81.35
X
?
Y
85
X2
359.93
Y2
85.95
X
355.9317
