Vessel ID
D
6000 mm
Vessel Height
H
17115 mm
Design Internal Pressure
Pi
0.015 mPa
Design External Pressure
Pe
0.018 mPa
Specifc ra!it" #$ %i&ui'
sg
%i&ui' Height
H$
1600 mm
*l+mate ,ensile Strength
St
10-.)1 mPa
,ensile /#'ulus
Et
10-).1 mPa
*l+mate lexural strength
S$
151.6 mPa
lexural m#'ulus
E$
68(.7 mPa
%i!e l#a' #n r##$
Pl
0.0007-5 mPa
,#p Hea' ,hicness
t
0 mm
Shell ,hicness
t
-5 mm
2#3#m Hea' ,hicness
t
0 mm
4#rr#si#n all#ance
4a
5.)) mm
Depth #$ Hea'
h
157) mm
4r#n a'ius #$ Hea'
4r
800 mm
rea Densit" #$ P
0.((7)
5-.1) g s&m
Thickness Calculaton for 2:1 Ellipsodial Top Head Inernal Pressure Calculaton Insi'e Diameter
Di
6000
Internal Pressure
Pi
0.015
*l+mate ,ensile Strength
Su
10-.)1
Design act#r $#r Sustaine' l#a'
F
10
Thickness Calculaton for 2:1 Ellipsodial Head e&uire' thicness $#r Internal Pressure
t ; PDi)SuF
.-5
Exernal Pressure calculaton External Presure
Pe
0.018
9utsi'e Diameter #$ shell
D#
6080
lexural m#'ulus #$ elas+cit" $#r hea'
E$
68(.7
4#rr#'e' ,hicness
tc
-.78
Design act#r
F
5
D#h <# ll#a:le external pressure
Pa ; 0.-6=E$ F >=t<#D#>@
e&uire' ,hicness $#r external Pressure
t ; <#D#=P'0.-6E$>?0.5
1.885( 0.855 0.0)))
-1.-
Design for loads on Top Head Loads 2!" l#s$1% in&' Insi'e ra'ius #$ 4r#n
800
=t>?0.5
08.5(
A00
Stress
S1
A0.--07
,#tal Stress
a:s= S1 Pt>
ll#a:le stress
SuF
).81 )0.68
(axi)u) Corrosion Liner *arrier +rain due o inernal Pressure ,ensile m#'ulus #$ elas+cit"
E
10-).1
4#rr#si#n %iner 2arrier ,hicness
t
5.))
Strain in c#rr#si#n liner 2arrier
PD=)tBE>
ll#a:le strain $#r sustaine' l#a's
0.0008--55 0.001
Pressure Tes Vessel shall :e teste' :" flling upt# $ull 'esignate' li&ui' capacit" ,est Pressure
Pt
0.018
%i&ui' Hea' Pressure
Ph
0.0160-1
,#tal test Pressure
P
0.0-0-1
Design act#r $#r intermi3ent l#a'
5
e&uire' thicness $#r )C1 Ellips#i'al Hea'
t ; PDi)SuF
Strain in c#rr#si#n liner 2arrier 'ue t# test Pressure
P'=)tBE>
ll#a:le strain $#r sustaine' l#a's
.( 0.0018( 0.00)
,eigh calculaton rea #$ )C1 ellips#i'al Hea'
1.08D@
-(0)000
rea Densit" #$ P
5-.1)
eight #$ Hea'
)07).(55
Summar" #$ ,#p Hea' ,hicness Summar"
e&uire'
Pr#!i'e'
Design
#r Internal pressure
.-5
-.78
Sa$e
#r External Pressure
-1.-
-.78
Sa$e
#r test Pressure
.(
-.78
Sa$e
Summar" #$ 4#rr#si#n %iner 2arrier Strain #r Internal pressure #r test Pressure eight #$ Hea'
In'uce'
ll#e'
Design
0.0008--55
0.001
Sa$e
0.0018(
0.00)
Sa$e
)07- gs
mm mPa mPa ,PA1A)01- -A1))
mm
-A)0
mPa mm mPa mm ) 0.(
1.8 0.81
1.6 0.7-
0 )
0 0
0 0
1.8 0.(
0 0
0 0
mpa
0.81
0
0
mm
0 ) 0.(
1.8 0.81
-A10
-./-0" 0.855 mm
mm
F/11A00 ig F/11A1
/pa mPa
F/11A00
mPa
F/11A00
mPa mm
-A1-0 %/!"
mPa mPa mPa ,PA1A)01- -A1)) mm
-A)0
-A1-0
mm@
gS&m gs
1. 0.65
1.) 0.57
1 0.5
0 0
0 0
0
0 0
0 0
0
0
Thickness Calculaton for 2:1 Ellipsodial *oo) Head Inernal Pressure Calculaton Insi'e Diameter
Di
6000
Internal Pressure
Pi
0.015
Sta+c Hea' Pressure
Ph
0.0-11
,#tal internal pressure
P
0.061
*l+mate ,ensile Strength
Su
10-.)1
Design act#r $#r Sustaine' l#a'
F
10
e&uire' thicness $#r Internal Pressure
t ; PDi)SuF
1-.-7
External Presure
Pe
0.018
9utsi'e Diameter #$ shell
D#
6080
lexural m#'ulus #$ elas+cit" $#r hea'
E$
68(.7
4#rr#'e' ,hicness
tc
-.78
Design act#r
F
5
Exernal Pressure calculaton
D#h <# ll#a:le external pressure
Pa ; 0.-6=E$ F >=t<#D#>@
e&uire' ,hicness $#r external Pressure
t ; <#D#=P'0.-6E$>?0.5
Design for loads on Top Head Loads 2!" l#s$1% in&'
1.885( 0.855 0.0)))
-1.-
Insi'e ra'ius #$ 4r#n
=t>?0.5
800 08.5(
-00
Stress
S1
0.)8
,#tal Stress
a:s= S1 Pt>
ll#a:le stress
SuF
6.11 )0.68
(axi)u) Corrosion Liner *arrier +rain due o inernal Pressure ,ensile m#'ulus #$ elas+cit"
E
10-).1
4#rr#si#n %iner 2arrier ,hicness
t
5.))
Strain in c#rr#si#n liner 2arrier
PD=)tBE>
ll#a:le strain $#r sustaine' l#a's
0.0008--55 0.001
Pressure Tes Vessel shall :e teste' :" flling upt# $ull 'esignate' li&ui' capacit" ,est Pressure
Pt
0.018
%i&ui' Hea' Pressure
Ph
0.1(87
,#tal test Pressure
P
0.)167
Design act#r $#r intermi3ent l#a'
5
e&uire' thicness $#r )C1 Ellips#i'al Hea'
t ; PDi)SuF
Strain in c#rr#si#n liner 2arrier 'ue t# test Pressure
P'=)tBE>
ll#a:le strain $#r sustaine' l#a's
,eigh calculaton
-1.0.01)0 0.00)
rea #$ )C1 ellips#i'al Hea'
1.08D@
-(0)000
rea Densit" #$ P
5-.1)
eight #$ Hea'
)07).(55
Summar" #$ ,#p Hea' ,hicness Summar"
e&uire'
Pr#!i'e'
Design
#r Internal pressure
1-.-7
-.78
Sa$e
#r External Pressure
-1.-
-.78
Sa$e
-1.-
-.78
Sa$e
#r test Pressure Summar" #$ 4#rr#si#n %iner 2arrier Strain #r Internal pressure #r test Pressure eight #$ Hea'
In'uce'
ll#e'
Design
0.0008--55
0.001
Sa$e
0.01)0
0.00)
F#t Sa$e
)07- gs
mm mPa mPa mPa mPa ,PA1A)01- -A1)) mm
-A)0
mPa mm mPa mm ) 0.(
1.8 0.81
1.6 0.7-
0 )
0 0
0 0
1.8 0.(
0 0
0 0
mpa
0.81
0
0
mm
0 ) 0.(
1.8 0.81
-A10
-./-0" 0.855
mm mm
F/11A00 ig F/11A1
/pa mPa
F/11A00
mPa
F/11A00
mPa mm
-A1-0 %/!"
mPa mPa mPa ,PA1A)01- -A1)) mm
-A)0
-A1-0
mm@ gS&m gs
1. 0.65
1.) 0.57
1 0.5
0 0
0 0
0
0 0
0 0
0
0
