Copy Of Hemispherical Calcu.
This document was uploaded by user and they confirmed that they have the permission to share it. If you are author or own the copyright of this book, please report to us by using this DMCA report form. Report DMCA
Overview
Download & View Copy Of Hemispherical Calcu. as PDF for free.
More details
- Words: 375
- Pages: 1
Prepaired uby:www.parstechnic.com
2
Hemispherical Head ver 1.1 Prepared By Pars Technic Co.
3
ASME Code VIII Div I 2001 no addenda
4
Verification Calculation #1
5
ASME L-1.5.1
1
<- vessel <- Component
6 7 8 9 10 11
Dimensions: 0.000 <- Outside Diameter (in.) 0.000 <- Thickness Before Forming 0.000 <- Thickness After Forming 0.125 <- Corrosion Allowance
www.parstechnic.com
In s id e R a d iu s
In s id e P r e s s u r iz e d
(in.) (in.) (in.)
12
T h ic k
13 14 15 16 17 18
Material Properties:
OD
A 516-70 <- Material 1.0 <- Design Pressure(psig) 20,000 <- Allowable Stress Level (psi) 0.70 <- Efficiency (UW-12(d))
0.0 <- Approximate blank diameter (in.) 0.0 <- Approximate weight for steel (lb.) 0.00 <- Volume (cuft)
19 20 21
Required Wall Thickness and Maximum Working Pressure
UG-32 (f)
-0.125 <- t (Nominal Thickness = Thickness after forming - Corrosion) 0.13 <- L (Inside Radius) (in.)
22 23
(in.)
24 25 26 27
PL tMin = ---------------2SE - 0.2P
1 * 0.125 = ---------------------------------------------2 * 20000 * 0.7 - 0.2 * 1
t = 0.000 ERROR
(in.)
2SEt PMax = ---------------L + 0.2t
2 * 20000 * 0.7 * -0.125 = ---------------------------------------------0.125 + 0.2 * -0.125
PMax = ERROR
(psi)
28 29 30 31
-35000
32 33 34 35 36 37 38 39 40 41 42
Head stress relief [UCS-79 (d) - carbon and low alloy steel only] Yes <- Head is cold formed(Yes/no) #DIV/0! <- Fiber elongation (see below) Required no <- Vessel carries lethal substances(Yes/no) no no <- Impact testing is required (Yes/no) no no <- Formed between 250 and 900 Degrees F no #DIV/0! <- Greater than 10% reduction in thickness #DIV/0! no <- Head is greater than 5/8" thick before forming no Stress Relieve ?
#DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0!
43 44 45 46 47
fiber elongation calculation UCS-79 (5) 0 <- Rf (Final center line radius, use radius) 0 <- Thickness ### <- Ro (Initial center line radius = Infinity, start with a flat plate)
48 49
elongation =
((75*t)/Rf)*(1-Rf/Ro)= ((75 * 0) / 0) * 1
= #DIV/0!
50 51 52
1
07/03/2009
2
Hemispherical Head ver 1.1 Prepared By Pars Technic Co.
3
ASME Code VIII Div I 2001 no addenda
4
Verification Calculation #1
5
ASME L-1.5.1
1
<- vessel <- Component
6 7 8 9 10 11
Dimensions: 0.000 <- Outside Diameter (in.) 0.000 <- Thickness Before Forming 0.000 <- Thickness After Forming 0.125 <- Corrosion Allowance
www.parstechnic.com
In s id e R a d iu s
In s id e P r e s s u r iz e d
(in.) (in.) (in.)
12
T h ic k
13 14 15 16 17 18
Material Properties:
OD
A 516-70 <- Material 1.0 <- Design Pressure(psig) 20,000 <- Allowable Stress Level (psi) 0.70 <- Efficiency (UW-12(d))
0.0 <- Approximate blank diameter (in.) 0.0 <- Approximate weight for steel (lb.) 0.00 <- Volume (cuft)
19 20 21
Required Wall Thickness and Maximum Working Pressure
UG-32 (f)
-0.125 <- t (Nominal Thickness = Thickness after forming - Corrosion) 0.13 <- L (Inside Radius) (in.)
22 23
(in.)
24 25 26 27
PL tMin = ---------------2SE - 0.2P
1 * 0.125 = ---------------------------------------------2 * 20000 * 0.7 - 0.2 * 1
t = 0.000 ERROR
(in.)
2SEt PMax = ---------------L + 0.2t
2 * 20000 * 0.7 * -0.125 = ---------------------------------------------0.125 + 0.2 * -0.125
PMax = ERROR
(psi)
28 29 30 31
-35000
32 33 34 35 36 37 38 39 40 41 42
Head stress relief [UCS-79 (d) - carbon and low alloy steel only] Yes <- Head is cold formed(Yes/no) #DIV/0! <- Fiber elongation (see below) Required no <- Vessel carries lethal substances(Yes/no) no no <- Impact testing is required (Yes/no) no no <- Formed between 250 and 900 Degrees F no #DIV/0! <- Greater than 10% reduction in thickness #DIV/0! no <- Head is greater than 5/8" thick before forming no Stress Relieve ?
#DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0!
43 44 45 46 47
fiber elongation calculation UCS-79 (5) 0 <- Rf (Final center line radius, use radius) 0 <- Thickness ### <- Ro (Initial center line radius = Infinity, start with a flat plate)
48 49
elongation =
((75*t)/Rf)*(1-Rf/Ro)= ((75 * 0) / 0) * 1
= #DIV/0!
50 51 52
1
07/03/2009
Related Documents
Copy Of Hemispherical Calcu.
May 2020 5
Stat Calcu
November 2019 8
Elec Calcu
June 2020 7
Calcu Challenge.docx
November 2019 11
Copy Of Copy Of Flip
November 2019 71