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

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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