SUVIDYA INSTITUTE OF TECHNOLOGY Mumbai : 400055
SAMPLE DESIGN CALCULATION - SKIRT SUPPORT DESIGN OF VERTICAL COLUMN REFE REFERE RENC NCE E
Pres Pressu sure re Vesse essell Des Desig ign n Man Manua uall by Denn Dennis is R M!ss M!ss
VESSEL DES IGN DATA AND "EIGHT CALCULATION CALCULATION CODE
ASME SEC. VIII, DIV. DIV. 1 LATEST LATEST
P
DESIGN PRESSURE
T
DESIGN TEMPERATURE
%50
E
' EL ELD (OINT EFFCIENC)
0.85
CA
CORROSION ALLO'ANCE
.0 ! F.V
"a#$ D&$. C
1.5
mm
1.5
M&-
30.4
M&-
5
M&-
MATERIAL OF CONSTRUCTION S*ELL
SA 515 GR. +0
SIRT
IS : %0% GR. A
CONSTRUCTION DETAILS D
S*ELL ID
*
Oa// C/um *&i$2-
2
SIRT *EIG*T
OTHER INFORMATION Li#ui$ H!l$ u% & '()) ** +r!* ,!--!* TL Ty%e !+ $is.e$ en$ & / & '0 Elli%s!i$al Insula-i!n & Yes 1HOT2 ')) ** In-ernals & 3) Trays 1Val4e Ty%e2 Cm/&-& /um i6 7ii7&7 i- 6&-i a6 62 i -2& 69&-2 b&/ Sr N!
LEVELS
uni-s
I
II
III
IV
V
VI
T!-al
1
M&a Diam&-
mm
153
151%
151%
1510
1510
1508
%
*&i$2-
mm
5000
5000
5000
5000
5000
530
3
S2&//!Di62
$
%+50
%%40
%%40
180
180
155
4
"7; F/a$&
$
0
0
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0
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0
5
N<&6
$
100
10
10
10
10
10
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$
0
400
+00
00
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+
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$
0
3530
10
+80
10
+80
8
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$
0
%00
8830
8830
8830
%00
I6u/a-i!A--a2m& $
500
300
300
300
300
300
10
E#&-i '&i$2-
$
%850
%400
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%0%0
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1815
'3()())
11
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3350
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4310
3+00
330
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/(5'())
1%
T&6-i$ '& '&i$2-
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1130
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1115
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S2u- D &i$2-
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3100
Cal9ula-i!n is base$ !n a
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$
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b
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/(5'())
T&6- &i$2- : 3 > 4 > 5 >>8
$
6'37())
7
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$
'8()())
1 OF 8
SUVIDYA INSTITUTE OF TECHNOLOGY Mumbai : 400055
SAMPLE DESIGN CALCULATION - SKIRT SUPPORT DESIGN OF VERTICAL COLUMN REFERENCE
Pressure Vessel Design Manual by Dennis R M!ss
"IND MOMENT CALCULATION CODE
IS : 8+5
D!
V&66&/ Ou-6i7& Diam&-
In
I6u/a-i T2i9&66
1.51% M&-
De
E??&-i& V&66&/ 7iam&- @ D& > %. IB
Si-e
N&a# Mumbai
Vb
"a6i 'i7 6&&7 F#m IS : 8+5 ?# 6i-& &a# MumbaiB
:'
Ri69 Fa-#
:/
T#ai *&i$2- Fa-#
0.1 M&1.+1% M&-
40 ,m!6 1
L&&/ I
1
L&&/ II
1
L&&/ III
1
L&&/ IV
1
L&&/ V
1
L&&/ VI
1
:3
T$#a2; Fa-#
V;
D&6i$ 'i7 6&&7 1 Vb :' :/ :3 2
1.0 m!S&
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H
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M&-
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5.3
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03.01 %5.00 %+.5 %5008.881 %433.%4%%4
V
40.00
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5.00
8.5
83+.8 %0.00 %%.500 1884+.+04 04%.8815%05
53+%.11
IV
40.00
+.8
1.+1%
5.00
8.5
83+.8 15.00 1+.500 145.3%+% 1840.5%8%05505
1434%.5
III
40.00
+.8
1.+1%
5.00
8.5
83+.8 10.00 1%.500
104+0.48 348%.540001%
%51+5.30
II
40.00
+.8
1.+1%
5.00
8.5
83+.8
5.00
+.500
%8%.5881 54000.40001%
303+.34
I
40.00
+.8
1.+1%
5.00
8.5
83+.8
0.00
%.500
%04.18 ++33.+%8%05505
55%+1.+
V
()7'37
Mb
1+5%.
==363=/8/
% OF 8
SUVIDYA INSTITUTE OF TECHNOLOGY Mumbai : 400055
SAMPLE DESIGN CALCULATION - SKIRT SUPPORT DESIGN OF VERTICAL COLUMN REFERENCE
Pressure Vessel Design Manual by Dennis R M!ss
SEISMIC MOMENT CALCULATION FIND OUT ,ASE SHEAR ? 1 V. 2
1As %er %r!9e$ure gi4en in IS&'873@/))/2
SITE
MUM"AI, INDIA
ONE
III
ONE FACTOR
I
IMPORTANCE FACTOR Tab/& IS:183%00%B
1
R
RESPONSE REDUCTION FACTOR Tab/& + IS:183%00%B
4
Sa!$
0.1
AVERAGE RESPONSE ACCELERATION COEFFICIENT
%.5
C/. .4.5 IS:183 %00%, Si/ M&7ium 6i/ 6i-&6 A2 A2 '
DESIGN *ORIONTAL ACCELERATION SPECTRUM H I B ! R H Sa!$BB
0.01
T-a/ '&i$2- ? &66&/ , Oa-i$
%5415.00 /b 5014. /b
V.
*#i<-a/ S&i6mi F#& A2 . ' B
H
Oa// *&i$2- ? &66&/
.+% ?&&-
D
Ui?#m /um Diam&-
5.153 ?&&-
-
T2i9&66 ? 62&//
0.%3%%05 i
.-
% ! 3 B . *
5+.48+1 ?&&-
T
Pi7 ? Vib#a-i @ 0.0000%5 . *! DB % . '. D ! 2- B
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0.5
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1%.%353 /b
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1%.%353 /b
F
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Mb
O-u#i$ Mm&- a- ba6& F- . *B > %!3 . F. *B
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C!*%aring Mb B Mb @@ G!4erning M!*en- is e++e9-i4e $ue -! in$ Use Mb +!r +ur-.er 9al9ula-i!n
3 OF 8
SUVIDYA INSTITUTE OF TECHNOLOGY Mumbai : 400055
SAMPLE DESIGN CALCULATION - SKIRT SUPPORT DESIGN OF VERTICAL COLUMN COM,INED STRESS ANALYSIS COM,INED STRESS ANALYSIS TO ,E CARRIED OUT FOR FOLLO"ING CONDITION A
ERECTION CONDITION
"
OPERATING CONDITION
C
TESTING CONDITON
STRESS SHALL ,E CALCULATED INDUCED DUE TO A
DEAD 'EIG*T
"
INTERNAL PRESSURE
C
' IND OR SEISMIC EFFECT
<<9
Pi . D ! 4 - B > 48. M- ! i . D %. - B ' 2! Pi. D. -B
L!ngi-u$inal s-ress0 Tensi!n L!ngi-u$inal s-ress0 C!*%ressi!n
B P&. D ! 4 - B 48. M- ! i . D %. - B '2! Pi. D. -B
LOADING CONDTION & ERECTION LEVELS
"eig.- !+ ea9. Se9-i!n lb
lb
lb+-
in
in
PSI
PSI
VI
4000.%
4000.%
1+5%.
5.53
0.%3
%30.%
1+000
411.+
11000.00
V
445%.08
845%.34
53+%.11
5.53
0.%3
100%.10
1+000
1384.84
11000.00
IV
445%.08
1%04.4%
1434%.5
5.53
0.%3
%3%.3
1+000
%10.+0
11000.00
III
5%8.
1814.0%
%51+5.30
5.53
0.%3
4184.44
1+000
5008.31
11000.00
II
5%8.
%3483.%
303+.34
5.53
0.315
44.48
1+000
5+44.0%
11000.00
I
%81.4
%+5.0%
55%+1.+
5.53
0.4+%
4+8.%4
1+000
544%.15
11+.+
NOTE
S.ear L!a$ ".
M-
D
- 1Ne2
<-
All!able Li*iS'E'
All!able Li*iFa9-!r ,
<9
PSI
PSI
EFFECT DUE TO INTERNAL AND EKTERNAL PRESSURE TO "E IGNORED DURING ERECTION STAGE ALLO'A"LE STRESS CALCULATED AT AM"IENT CONDITION 'ELD EFFICIENT) : 0.85
LOADING CONDTION & SHUTDO"N LEVELS
"eig.- !+ ea9. Se9-i!n
S.ear L!a$
lb
lb
lb+-
in
in
PSI
PSI
VI
583.8
583.8
1+5%.
5.53
0.1++
%4+.1
1+000
08.8
11000.00
V
5.08
1%3.4
53+%.11
5.53
0.1++
1%0.+%
1+000
1+%.8+
11000.00
".
M-
D
- 1C!rr!$e$2
<-
All!able Li*iS'E'
All!able Li*iFa9-!r ,
<9
PSI
PSI
IV
435.8
10+5.%
1434%.5
5.53
0.1++
%15.5%
1+000
40+.%4
11000.00
III
+43.0
%5.%%
%51+5.30
5.53
0.1++
53%.43
1+000
30.5+
11000.00
II
83%.40
33401.%
303+.34
5.53
0.%5
5880.
1+000
+%+.84
11000.00
I
+383.40
40+85.0%
55%+1.+
5.53
0.413
530.84
1+000
3%.18
11+.+
NOTE
EFFECT DUE TO INTERNAL AND EKTERNAL PRESSURE TO "E IGNORED DURING ERECTION STAGE ALLO'A"LE STRESS CALCULATED AT AM"IENT CONDITION 'ELD EFFICIENT) : 0.85
LOADING CONDTION & OPERATING LEVELS
"eig.- !+ ea9. Se9-i!n
S.ear L!a$
lb
lb
lb+-
in
in
PSI
PSI
VI
++0%.8
++0%.8
1+5%.
5.53
0.1++
.+1
148+5
+44.+
11000.00
V
81.+%
134.+0
53+%.11
5.53
0.1++
101.%8
148+5
%1.31
11000.00
".
M-
D
- 1C!rr!$e$2
<-
All!able Li*iS'E'
All!able Li*iFa9-!r ,
<9
PSI
PSI
IV
8154.80
%451.50
1434%.5
5.53
0.1++
3%55.18
148+5
4315.58
11000.00
III
4.%4
34018.+4
%51+5.30
5.53
0.1++
505.54
148+5
+%3.4
11000.00
II
141%.5%
4831.%
303+.34
5.53
0.%5
511.3%
148+5
+53.%8
11000.00
I
+383.40
5014.
55%+1.+
5.53
0.413
53%5.81
148+5
55.%1
11+.+
D
- 1Ne2
NOTE
ALLO'A"LE STRESS CALCULATED AT DESIGN TEMPERATURE. 'ELD EFFICIENT) : 0.85
LOADING CONDTION & TEST LEVELS
"eig.- !+ ea9. Se9-i!n lb
lb
lb+-
in
in
PSI
PSI
VI
%55.4
%55.4
1+5%.
5.53
0.%3
34%.55
148+5
%58.41
V
%545.%0
51055.
53+%.11
5.53
0.%3
.8
148+5
3+.5%
11000.00
IV
%5%35.80
+%1.4
1434%.5
5.53
0.%3
1555.1+
148+5
81.%%
11000.00
III
%%3.+%
10%585.18
%51+5.30
5.53
0.%3
%.%0
148+5
%%+3.+4
11000.00
II
%448.00
1%033.18
303+.34
5.53
0.315
3.38
148+5
3154.1
11000.00
I
%81.40
135314.58
55%+1.+
5.53
0.4+%
35%.5
148+5
35+3.3
11+.+
NOTE
S.ear L!a$ ".
M-
<-
All!able Li*iS'E'
All!able Li*iFa9-!r ,
<9
PSI
PSI
ALLO'A"LE STRESS CALCULATED AT DESIGN TEMPERATURE. 'ELD EFFICIENT) : 0.85 *)DROSTATIC TEST PRESSURE IS 1.5 TIMES DESIGN PRESSURE > EFFECT DUE TO STATIC *EAD SUC* "IG COLUMN *)DROTESTD IN *ORIONTAL CONDITION IN 'ORS*OP EKTERNAL PRESSURE 'ILL "E ERO IN A"OVE CALCULATION
CONCLUSION STRESSES INDUCED DURING DIFFERENT CONDITIONS ARE "ELL "ITHIN IN ALLO"A,LE LIMITED AND HENCE PROVIDE THIC:NESS ARE ADEUATE
11000.00
SUVIDYA INSTITUTE OF TECHNOLOGY Mumbai : 400055
SAMPLE DESIGN CALCULATION - SKIRT SUPPORT DESIGN OF VERTICAL COLUMN REFERENCE Pressure Vessel Design Manual by Dennis R M!ss
ANCHOR ,OLT CALCULATION @ EUIVALENT AREA METHOD REFER TA,LE 333 FOR NO OF ,OLTS SHELL O>D
N
RECOMMENDED MINIMUM NOOF ANCHOR ,OLTS
8 N6
RECOMMENDED MAIMUM NOOF ANCHOR ,OLTS
1% N6.
NO OF ,OLTS ASSUMED
1% N6.
MATERIAL OF CONSTRUCITON FOR ANCHOR ,OLTS Fs
ALLO"A,LE TENSILE STRESS FOR ANCHOR ,OTLS0 1REFER TA,LE 3352
F9
ALLO"A,LE COMPRESSIVE STRESS FOR CONCRETE0 1REFER TA,LE 33(2
n Mb "b $ r
5.45 i
RATIO OF MODULUS OF ELASTICITY OF STEEL TO CONCRETE 1REFER TA,LE 33(2 OVERTURNING MOMENT DUE TO "IND "EIGHT OF VESSEL AT ,ASE @ TEST "EIGHT OUTSIDE DIAMETER OF S:IRT OUTSIDE RADIUS OF S:IRT "IDTH OF ,ASE PLATE
SA3 1000 PSI 1000 PSI 1% ((7/='6= /b.?135314.58 /b 4.00 i 3%.00 i 5.00 i
APPROIMATE VALUE OF : :
' > 1 ' 1Fs > nF922
0.38+
COEFFICIENT FROM C*ART C9
1.4
C-
%.33
0.+83
J
0.4%+
TENSILE LOAD IN STEEL ? 1 T 2 T
1Mb @ "b @ J$ 2> $
845.5 /b
REUIRED ROOT AREA ? 1Ab2 Ab
1 T %i $ > Fs r C- 2
ROOT AREA OF ONE ,OLT & Ab > N Ra
PROVIDED ROOT AREA
1.%00 i% 0.1000 i% 0.30% i%
SELECTED ,OLT DIAMETER & )=(K HENCE O: STRESS IN EUIVALENT STEEL ,AND ? 1 -s 2 -s
1 N Ra 2 > 1 %i $ 2
0.0180 i
EUIVALENT TENSILE STRESS IN ANCHOR ,OLT ? 1 +s 2 +s
T > 1-s r C- 2
%3.+ PSI
COMPRESSIVE LOAD IN CONCRETE ? 1 C 2 C
T "b
143++4.%3 /b
EUIVALENT COMPRESSIVE STRESS IN CONCRETE ? 1 +9 2 +9
C > 1 1 @ - s 2n -srC9 2
5%+.0% /b
RECHEC:ING : USING ACTUAL +s an$ +9 :
' > 1 ' 1+s > n+922
0.501 /b
SINCE THIS VALUE OF : IS DIFFERENT THAN THAT "AS ASSUMED HENCE RECALCULATE
5 OF 8
SUVIDYA INSTITUTE OF TECHNOLOGY Mumbai : 400055
SAMPLE DESIGN CALCULATION - SKIRT SUPPORT DESIGN OF VERTICAL COLUMN REFERENCE Pressure Vessel Design Manual by Dennis R M!ss
ANCHOR ,OLT CALCULATION @ EUIVALENT AREA METHOD TRIAL @ / APPROIMATE VALUE OF :
'IDT* OF "ASE PLATE
: n
5.50 i 0.300
RATIO OF MODULUS OF ELASTICIT) OF STEEL TO CONCRETE REFER TA"LE 3.35B
1%
COEFFICIENT FROM C*ART C9
1.51
C-
%.44%
0.+81
J
0.438
TENSILE LOAD IN STEEL ? 1 T 2 T
1Mb @ "b @ J$ 2> $
8481.3 /b
REUIRED ROOT AREA ? 1Ab2 Ab
1 T %i $ > Fs r C- 2
ROOT AREA OF ONE ,OLT & Ab > N Ra
PROVIDED ROOT AREA
1.148 i% 0.05+ i% 0.30% i%
SELECTED ,OLT DIAMETER & )=(K HENCE O: STRESS IN EUIVALENT STEEL ,AND ? 1 -s 2 -s
1 N Ra 2 > 1 %i $ 2
0.0180 i
EUIVALENT TENSILE STRESS IN ANCHOR ,OLT ? 1 +s 2 +s
T > 1-s r C- 2
0%0.4 PSI
COMPRESSIVE LOAD IN CONCRETE ? 1 C 2 C
T "b
143+5.88 /b
EUIVALENT COMPRESSIVE STRESS IN CONCRETE ? 1 +9 2 +9
C > 1 1 @ -s 2n - srC9 2
5%%.%4 /b
RECHEC:ING : USING ACTUAL +s an$ +9 :
' > 1 ' 1+s > n+922
0.510 /b
NO" CALCULATED VALUE OF : IS VERY CLOSE TO ASSUMED VALUE AND SIJING IS ADEUATE SUMMARY $b
SIE OF "OLT DIAMTER
N
NO. OF "OLTS
'IDT* OF "ASE PLATE MOC OF SELECTED "OLTS
0.+5 i 8 N6. 5.50 i SA3
OF 8
SUVIDYA INSTITUTE OF TECHNOLOGY Mumbai : 400055
SAMPLE DESIGN CALCULATION - SKIRT SUPPORT DESIGN OF VERTICAL COLUMN REFERENCE Pressure Vessel Design Manual by Dennis R M!ss
DESIGN OF ANCHOR CHAIR SELECTED T)PE OF ANC*OR C*AIR T)PE 3
R -s
OUT SIDE RADIUS OF S:IRT SH ELL S:IRT SHEL L THIC:NESS
30.000 i 0.4+% i
a
% i
9
1.5 i
e
9 @ 1$b>/2
. l
1.1%5 i 1% i
a9
3.5 i
-9
COMPRESSION PL AT E T HIC:NESS
1.00 i
-b
,ASE RING THIC:NESS
1.00 i
"i$-. !+ ,ase Ring
b
SPACING ,ET "EEN T "O GUSSETS
A
COMPRESSION PLATE "IDTH
-g
GUSSETS THIC:NESS
0.5 i
$
,OLT CIRCLE DIAMETER
4 i
N
NOOF ANCHOR ,OLTS
$b
DIAMTER OF ,OLT HOLE IN ,ASE PLATE
bs
SPACING ,ET"EEN ANCHOR CHAIR
Fs
ALLO"A,LE TENSILE STRESS FOR ANCHOR ,OTLS0 1REFER TA,LE 3352
Ra
PROVIDED ROOT AREA
5.5 i %.500 i 4.5000 i
8 N6. 1.+5 i %1.3 i 1000 PSI 0.30% i%
+ OF 8
SUVIDYA INSTITUTE OF TECHNOLOGY Mumbai : 400055
SAMPLE DESIGN CALCULATION - SKIRT SUPPORT DESIGN O F VERTICAL COLUMN REFERENCE Pressure Vessel Design Manual by Dennis R M!ss
DESIGN OF ANCHOR CHAIR
,ASE PLATE DESIGN @ TYPE 3 CHEC:ING THIC:NESS ,ET"EEN T"O GUSSETS MAIMUM ANCHOR ,OLT FORCE ? 1P2 P
Fs Ra
5+38 /b
,ENDING MOMENT ? 1M!2 M!
P b > 8
1+3.1%5 /b. i
REUIRED THIC:NESS ? 1 -b2 -b
1 6 M!2 > 1 1@$b2Fs2 )(
0.38 i
CHEC:ING THIC:NESS ,ET"EEN T"O ANCHOR CHAIR RATIO
l >
bs
0.1%
,ENDING MOMENT PER UNIT LENGTH @ REFER TA,LE 336 M<
)))3=7 +9 b /
My
@)56( +9 l
M!
GREATER OF M< !r My
1%.3+ /b. i
/
%+4.83 /b.i
%+4.835 /b.i
REUIRED THIC:NESS ? 1 -b2 -b
1 6 M!2 > Fs )(
0. i
-b
GREATER OF A,OVE
0. i
PROVIDED ,ASE PLATE THIC:NESS ? 1 -b 2
1.00 i
COMPRESSION PLATE THIC:NESS CHEC: @ TYPE 3 MINIMUM THIC:NESS OF TOP PLATE ? -9 -9
1 P > Fs e 21)3=(b @ )// $b2 )(
0.385 i
PROVIDED TOP COMPRESSION PLATE THIC:NESS ? 1-92
1.00 i
GUSSET PLATE THIC:NESS CHEC: @ TYPE @3 REUIRED GUSSET THIC:NESS ? 1 -g 2 -g
P > 1 '8))) l2 3>8 K
0.011 i
PROVIDED GUSSET PLATE THIC:NESS ? 1-g2
0.50 i
S:IRT SHELL THIC:NESS CHEC: @ TYPE 3 J
' /
0.000+3% )(
/
1'== A . 2> 1R -s2 1-b > -s2 '
4%4.00 PSI S
SINCE S /())) PSI0 HENCE PROVIDED SHELL THIC:NESS IS ADEUATE
8 OF 8