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8/17/2019 mechanical design of column
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DESIGN OF COLUMN WALL THICKNESS
1. Design pressure of the process:
• P = 1200 kN/m2 = 1.2 N/mm2
2. Wall thickness of shell:
t = Pi Di
2 SE−0.2 Pi
Pi = Desig !"ess#"e = 1.2 N/mm2
Di = ie" $i%me&e" '( &)e *'+#m = 1,00 mm
S = &)e $esig s&"ess '( &)e m%&e"i%+ '( *'s&"#*&i'
E = &)e -e+$ 'i& e((i*ie* = 1.0
T)e -e+$ 'i& is $'#+e -e+$e$ #&& '" e#i%+e& 'i& %$ 100 !e"*e& $eg"ee '(
"%$i'g"%!).
F"'m &%+e 13.24 T!i*%+ M%5im#m A++'-%+e S&"esses ('" P+%&e #$e" ASME 6P7 *'$e Se*.7III D.I
Desig &em!e"%"e4 1,0 0C→
802 0F
Tem!e"%"e M%5 %++'-%+e s&"ess9 S
800 1,
802 :
,00 12.;
: = 13.;< 1, ksi
1, ksi =108.322 N/mm2
t = 1.2(1500)
2 (103.422 ) (1 )−1.2(1.2)
1
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= ?mm
@ T)e +eg&) '( *+i$"i*%+ *'+#m %& &)e %se '( *'+#m is 8>m. i& is +ike+ &)%& &)e *'+#m -i++
#*k+e9 &)#s -e +e& &)e &)i*kess e 10mm.
N'&e4
A m#*) &)i*ke" -%++ %& &)e %se '( *'+#m is &' -i&)s&%$ &)e -i$ +'%$ %$ $e%$ -eig)& '( *'+#m.
As &)e (i"s& &"i%+9 -e $ii$e &)e *'+#m i&' , se*&i's -i&) &)i*kess i*"e%sig 2mm !e" se*&i'.
@ T)i*kess '& i*+#$e &)e $'me
F'" %++ '&)e" *%+*#+%&i's9 &)e %e"%ge &)i*kess is #se$.
T %g =
t 1+ t 2+t 3+t 4+ t 55
=10+12+14+16+18
5
T %g = 13 mm
2
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3. Dead weight load of DC
C'sis& '(4
• Weig)& '( me&%+ m%ke #! &)e m%i '$ WB
• Weig)& '( siee !+%&e %$ %**ess'"
• Weig)& '( is#+%&i' m%&e"i%+
F'" se*&i' 19
Ci"*#m(e"e*e = 2 π
"
=π
$ = π (1500 )=4712.39mm
•F'" s&ee+ esse+4
Wv=240CwDw ( Hv+0.8 Dm ) t
W)e"e4
W = &'&%+ -eig)& '( s)e++
C- = 1.1, ('" *'+#m -i&) m%)'+e
H = )eig)& '( *'+#m =8>m
T= &%g
Dm = me% $i%me&e" '( esse+
Dm= Di+ t X 10−3
Dm = 1., 13 5 108B
3
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= 1.,13 m
• W = 230 : 1.1, : 1.,13 8> 0.< : 1.,13B 13
= 2289,8;.1
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4. %ffect of wind load
P- = 0.0> U-2 ('" *+i$e" -i&) %&&%*)me&
T%ke $%mi* -i$ !"ess#"e %s 1>;2 N/m29 *'""es!'$ig &' 1?0 k!) 100 m!)B ('"
!"e+imi%" $esig s$ies.
5. &ean dia'eter of (essel including thickness and insulation:
¿ Di+2 (tavg+ tins ) X 10−3
= 1., 213,0B 5 108
=1.!2$ '
!. )oading per linear 'eter* +w
W= 1>;2 N/m
2
5 1.?2< m = 2#1,.3$ N-'
,. ending 'o'ent at /otto' colu'n*&0
M5 = FW
2 x Hv 2
= 2;1>.8< N/mB/2B 5 8>B2 m
= 1* ##!*#43.$,2 N.'
$. nalsis of stress:
C'sis& '(4
• Ci"*#m(e"e&i%+ s&"ess
5
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• +'gi$i%+ s&"ess
Ci"*#m(e"e&i%+ s&"ess4
) = PiDi2 t N/mm
2B =1.2 x15002 x18 = 5 N-''
2
L'gi$i%+ s&"ess4
L = PiDi
4 t N/mm2B =
1.2 x1500
4 x 18 = 25 N-''2
#. Dead weight stress* w
- =Wv
π ( Di+t )t N/mm2B
=223.54 x10
3 N
π (1500mm+18mm)18mm
= 2.!4 N-''2
1. ending stress* /
=±
M
Iv ( Di2 +t )
W)e"e4
M= e$ig m'me& %& '&&'m *'+#m
I= se*'$ m'me& %"e%
6
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( =
D
π
64¿ o
4 Di46
Do= Di+2 t
= 1,00 2 1
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D'--i$4
= L - −¿
$'--i$B = 2, 2.?03B ?2.0; = 8;> N/mm2
@- is *'m!"essie &)e"e('"e i& is eg%&ie.
= ,0 N/mm2
=,0 8;.>B
= N/mm2
8
84.5 N/mm2
Upwind
50
N/mm2
Downwind
50
N/mm2
8/17/2019 mechanical design of column
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12. Conclusion
T)e s&"ess $i((e"e*es ('" #!-i$ %$ $'--i$ *'$i&i' %"e +ess &)% S= 108.32 kN/mm 2. T)e"e('"e
&)e $esig &)i*kess9 & '&&'m = 1< mm is s%&is(%*&'".
DESIGN ON 7ESSEL SUPPOJT
S = m%5 %++'-%+e s&"ess =
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¿ π
4(1.5 )2 X 37 x
1000kg
mm2 x
9.81
1000kN
= ?31.32 kN
M%5 $e%$ -eig)& = ?31.32 8,1.;<
= ;;8.3 kN
2. Wi$ +'%$ = 2;1>.8>? N/m
8. 6e$ig m'me& %& %se '( ski"&4
¿1
2 X
2W
¿1
2 X 2.92 X (37+2.5 )2
¿2277.97 kN
3. 6e$ig s&"ess i &)e ski"&9 s
s = 3@Ms/π ¿ @Ds &B@&@Ds
= 3@ 22>>.;> @ 108 @ 108B/π
1,8?1
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=993.4 x10
3
π (1536+18) (18)
= 11.80 N/mm2
-s '!e"%&igB 4 -i&)'#& -%&e"
=351.98 x10
3
π (1536+18) (18)
=
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CO7EJ DESIGN
S&%$%"$ e++i!s'i$%+ &!e
t = Pi Di
2 SE−0.2 Pi
t = 1.2(1500)
2 (89) (1)−0.2(1.2)
= 10.12 mm
A$$ 2 mm ('" *'""'si' %++'-%*e4
10.12 2
= 12.18 mm
12