Material Selection for IMO TYPE "C" TANK Unit : MPa
MATERIALWeld Metal(¿ëÁ¢ºÀ°­µµ)Allowable Membrane Stress(f) ¼±±ÞKR/LR
Tensile
Rm (=St)
Yield
Re (=Sy)
Div.1
S
f = Min(Re/A, Rm/1.5) f (Mpa) A
A1106(Hign Mn) 660400 N/A f = Min(660/3.5, 400/1.5) 188.6 3.5
A553-TYPE1 640420187.0f = Min(640/3.0, 420/1.5) 213.3 3.0
LT-FH32 440~570315 N/A f = Min(440/3.0, 315/1.5) 146.67
LT-FH36-TM 490~630355 N/A f = Min(490/3.0, 355/1.5) 163.33
SA240-304 515205138f = Min(515/3.5, 205/1.5) 136.66 3.5
SA240-304L 485170115f = Min(485/3.5, 170/1.5) 113.33
SA240-316 515205138f = Min(515/3.5, 205/1.5) 136.66
SA240-316L 485170115f = Min(485/3.5, 170/1.5) 113.33
SA516-60 410215118ASME SEC. VIII Div.1
Allowable Stress
SA516-70 485260138
SA537-CL1 485345138
SA537-CL2 550415158
/*  ³×À̹ö ºí·Î±× 
https://m.blog.naver.com/back511/70032286820
https://blog.naver.com/jicsmlove/222390087093

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	±× Èê¼ö¼±À» ¸¸ÀçÈê¼ö¼±(Load Line)À̶ó°í ÇÑ´Ù. ¸¸ÀçÈê¼ö¼±¿¡¼­ °ÇÇö°©ÆÇ
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// Design draft vs Scantling draft
// https://amarineblog.com/2017/08/12/design-draft-vs-scantling-draft/			
mode = new MaxSid = [11]
IMO TYPE C Fuel Tank [°ßÀû°­µµ°è»ê] ( 2021³â 10¿ù 15ÀÏ ¼öÁ¤ )           ( £í©÷¡¡£í©ø ¤§ £« £­ ¡¿ ¡À ¡¾ ¡Â ¡Ã ^C ¡É ¢º ¤º )

mode = new sid = 11,     tid=1
PJTNO : PJTNAME : OWNER: Units : °ßÀûÀÚ¸í : ³¯Â¥ :

[ ¸ñ ·Ï ]¡¡¡¡¡¡[ Á¶ ȸ ]¡¡¡¡¡¡[Calc ]¡¡¡¡¡¡[Calc and Save]

No.o Ship Dimension and Data¡¡¡¡[¡ä¿À¹«¸®] [¡âÆîÄ¡±â]UnitExample[ #1 ]
[Del]
[ #2 ]
[CP] [Del]
[ #3 ]
[CP] [Del]
[ #4 ]
[CP] [Del]
[ #5 ]
[CP] [Del]
[ #6 ]
[CP] [Del]
[ #7 ]
[CP] [Del]
[ #8 ]
[CP] [Del]
[ #9 ]
[CP] [Del]
[ #10 ]
[CP] [Del]
Unit

A* 11. °í°´»ç (ȸ»ç¸í)
A* 22. Ship Naumber
A* 33. Ship Description
A* 44. Dead Weight (ÀçÇÏÁß·®)
A* 55. Fuel Tank ¿ë·®
A* 66. Tank Dia(m) x T.L~T.L
A* 77. ÅÊÅ©¼ö·®
A* 88. ´ã´çÀÚ ¸í
A* 99. Note Space
A* 1010. Note Space

11, 0o Ship Dimension Data¡¡TNO = SN-XXXX
12, 1Length overall (˟ˌ)Loa =m114.89m
13, 2Breadth moulded (ÇüÆø)B =m16.8m
14, 3Metacentric height (Unknown=0 ÀÔ·Â, ÀÚµ¿°è»ê)GM =m0m
15, 4Factor K=13*GM/B (Unknown K ¡Ã 1 ÀÔ·Â)K =1.0
16, 5Longitudinal distance (m) x =m9.5m
17, 6Transverse distance (m)y =m0.0m
18, 7Vertical distance (m)z =m-0.677m
19, 8Block coefficientCB =0.709
20, 9Service speedV =knote16knote

[21, 10]Acceleration due to ship's motions :UnitExample[#1][#2][#3][#4][#5][#6][#7][#8][#9][#10]Unit

22, 11Logitudinal Acceleration
Transverse Acceleration
Vertical Acceleration
Formula A
Formula ao
ax =
ay =
az =
A =
ao=
g
g
g

g
g
g
g

g
23, 12X-Z Longitudinal Direction ¥â =
a¥â =
Z¥â =
Pgd_XZ=
deg
g
m
bar.g
deg
g
m
bar.g
24, 13Y-Z Transverse Direction¥â =
a¥â =
Z¥â =
Pgd_YZ=
deg
g
m
bar.g
deg
g
m
bar.g
25, 14Pgd : Internal liquid pressure ( IGC 4.28.1.2 )
Pgd = a¥â¡¤Z¥â¡¤( ¥ñ / 10-4 ) [bar.g]
Pgd(Max) =bar.gbar.g

Ship Schematic Diagram :

x : ¼±¹ÚÀÇ Áß¾ÓÀ¸·ÎºÎÅÍ ÀûÀç¹°À» Æ÷ÇÔÇÑ ÅÊÅ©ÀÇ Áß½ÉÀ§Ä¡±îÁöÀÇ ¼±¹Ú ±æÀ̹æÇ⠰Ÿ®(m ), x´Â ¼±¹ÚÀÇ Áß¾ÓÀ¸·Î ºÎÅÍ ¼±¼ö¹æÇâÀ» Á¤(+), ¼±¹Ì¹æÇâÀ» ºÎ(-)·Î Ç¥½ÃÇÑ´Ù.
y : ¼±¹ÚÀÇ Á߽ɼ±À¸·ÎºÎÅÍ ÀûÀç¹°À» Æ÷ÇÔÇÑ ÅÊÅ©ÀÇ ¹«°ÔÁ߽ɱîÁö Ⱦ¹æÇ⠰Ÿ®(m).
z : ¼±¹ÚÀÇ ½ÇÁ¦ÀÇ È¦¼ö¼±À¸·ÎºÎÅÍ ÀûÀçÅÊÅ©Á߽ɱîÁöÀÇ ¼öÁ÷°Å¸®(m ), z´Â Ȧ¼ö¼±»óÀ¸·ÎºÎÅÍ »óÀ» Á¤(+), Çϸ¦ ºÎ(-)·Î Ç¥½ÃÇÑ´Ù.

Head Type (¼³¸í) : [H/H]= Hemi-Spherical,¡¡¡¡[E/E]=2:1 Ellipsodial,¡¡¡¡[10%D/D]= 10% Dish Head

[26, 16]o Fuel Tank Design DataUnitExample[#1][#2][#3][#4][#5][#6][#7][#8][#9][#10]Unit

27, 17Class Society ( KR, LR, ABS, DNV-GL, GV,(ASME VIII, Div.1)Class =LR
28, 18Fuel Type (LNG, LPG, AMMONIA, BUTANE)Liquid =LNG
29, 19Design temperature (-163 ~ +45 deg C)DTemp =deg C-163deg C
30, 21In-Diameter of TankD =m9.5m
31, 22Design Liquid LevelDLL =m[Auto]m
32, 23Length(T.L~T.L)L =m29.29m
33, 24[USED] Shell ThicknesstuShell =mm16.0mm
34, 25[USED] Head ThicknesstuHead =mm9.0mm
35, 26Corrosion AllowanceCA =mm0.75mm
36, 27Design DensitypDensitykg/m©ø500kg/m©ø
37, 28Head Type , [HH, EE, H+E, EE, 10%DD]Head =HH
38, 29Nominal Volume Vnom =m©ø[Auto] m©ø
39, 30Net Volume,(Vnet = Vnom¡¿89.5%)Vnet =m©ø[Auto] ¢º ¢º ¢º ¢º ¢º ¢º ¢º ¢º ¢º ¢ºm©ø
40, 31Storage RatioSratio =%[Auto] ¢º ¢º ¢º ¢º ¢º ¢º ¢º ¢º ¢º ¢º%
41, 32Tank materialMATL =A1106 ¡å ¡å ¡å ¡å ¡å ¡å ¡å ¡å ¡å ¡å
42, 34Yield stressRe =MPa390MPa
43, 35Tensile strengthRm =MPa540MPa
44, 36Allowable membrane stressf = MPa180MPa
45, 38(For Bilobe) Tank center to Swash Bulk HeadC =m2.65m

[46, 40]o Design (Internal / External) Pressure UnitExample[#1][#2][#3][#4][#5][#6][#7][#8][#9][#10]Unit

47, 41Design vapour pressure, IMO*Po =bar4.5bar
48, 42Maximum Allowed ReliveValve Setting MARVS =bar3.2bar
49, 44Dynamic Pressure for ship mortionPgd=bar0.8bar
50, 45Design Pressure Peq = Po+Pgd(max)Peq =bar5.3bar
51, 46Test pressure Pt = Po x 1.5Pt =bar6.75bar
52, 47Design External pressurePe =bar0.45bar
53, 48Vacuuum Ring Pitch [ÀÔ·Â]Pitch =m3.0m
54, 49Vacuuum Ring Q'ty [ÀÚµ¿°è»ê]qtyRing =Rings[Auto]Rings
55, 50[¾ÆÁ÷] ¡¤Head Thk for External Pressure (Class)tcH_LR = mmmm
56, 51[¾ÆÁ÷] ¡¤Head Thk for External Pressure (ASME) tcH_ASME = mmmm
57, 52[¾ÆÁ÷] Check For External PressureCheck =

[58, 53]o BOR & Insulation DataUnitExample[#1][#2][#3][#4][#5][#6][#7][#8][#9][#10]Unit

59, 54BOR(POS)BOR =%/day0.3%/day
60, 55PUF (Insulation Thickness)tInsu =mm400mm
61, 56PUF DensitypInsu =kg/m340kg/m3
62, 57Thermal Conductivityk =W/m¡¤K0.023W/m¡¤K
63, 58PUF (or Insulation) VolumeVinsu =m3[Auto]m3
64, 5922
65, 6033
66, 6144

[ ¸ñ ·Ï ]¡¡¡¡¡¡[ Á¶ ȸ ]¡¡¡¡¡¡[Calc ]¡¡¡¡¡¡[Calc and Save]

o Calculation Result
DescriptionSymbolUnitExample[#1][#2][#3][#4][#5][#6][#7][#8][#9][#10]Unit
AA°­µµ°è»ê °á°ú Á¶È¸[Àüü]
[Weight Summary]
[Strength Calculation]
[Dynamic Pressure]
[External Pressure]
[Àüü]
[WS]
[Stength]
[Dynamic]
[Vacuum]
[Àüü]
[WS]
[Stength]
[Dynamic]
[Vacuum]
[Àüü]
[WS]
[Stength]
[Dynamic]
[Vacuum]
[Àüü]
[WS]
[Stength]
[Dynamic]
[Vacuum]
[Àüü]
[WS]
[Stength]
[Dynamic]
[Vacuum]
[Àüü]
[WS]
[Stength]
[Dynamic]
[Vacuum]
[Àüü]
[WS]
[Stength]
[Dynamic]
[Vacuum]
[Àüü]
[WS]
[Stength]
[Dynamic]
[Vacuum]
[Àüü]
[WS]
[Stength]
[Dynamic]
[Vacuum]
[Àüü]
[WS]
[Stength]
[Dynamic]
[Vacuum]


query[0] = [Select sid,no,Descr,Symbol,Unit,A1,A2,A3,A4,A5,A6,A7,A8,A9,A10 FROM IMO_DATA Where sid='11' and no in (24, 25, 50, 51, 103, 106, 110, 113, 116, 121, 103, 103, 103, 104, 107, 111, 114, 120, 125) Order By no]
¹øÈ£0
sid
1
no
2
Descr
3
Symbol
4
Unit
5
A1
6
A2
7
A3
8
A4
9
A5
10
A6
11
A7
12
A8
13
A9
14
A10
ERROR MESSAGE:[java.lang.ArrayIndexOutOfBoundsException: 1]


Ãâó : ASME SHELL THICKNESS CALCULATION Ãâó

 
Wall thickness calculation of Sphere
according ASME
 
     
  Allowable stress S = 175.2 = 175.20 N/mm©÷  
  Corroded thickness tc = t - Ca - tol = 8.2 - 1 - 1.03 = 6.17 mm  
           
  Sphere:        
           
  Corroded inside radius
R =
Do
2
- tc=
219.1
2
- 6.17 =
103.38 mm  
1.Cylinder Shell : £«£­¡¿¡À
Required wall thickness
tr=
P · R
S¡¿E £­ 0.6¡¿P
£« CA
=
0.5 ¡¿ 103.38
2 ¡¿ 175.2 ¡¿ 1.0 £­ 0.2 ¡¿ 0.5
£« CA
0.15 mm 
2.Spherical Head :
Required wall thickness
tr=
P · R
2SE £­ 0.2P
£« CA
=
0.5 ¡¿ 103.38
2 ¡¿ 175.2 ¡¿ 1.0 £­ 0.2 ¡¿ 0.5
£« CA
0.15 mm 
3.2:1 Ellipsoidal Head :
Required wall thickness
tr=
P ⋅ D
2 ⋅ S ⋅ E - 0.2 ⋅ P
+ CA
=
0.5 * 103.38
2 * 175.2 * 1.0 - 0.2 * 0.5
+ CA
0.15 mm 
3.10% Dish Head :
Required wall thickness
tr=
P ⋅ D ⋅ K
2 * S * E - 0.2 * P
+ CA
=
0.5 * 103.38
2 * 175.2 * 1.0 - 0.2 * 0.5
+ CA
0.15 mm 
  Nominal required thickness trn = tr + Ca + tol = 0.148 + 1 + 1.03 = 2.18 mm  
  Max. Allowable Working Press.
MAWP =
2 ⋅S ⋅ E ⋅ tc
R + 0.2 ⋅ tc
=
2 ⋅ 175.2 ⋅ 1 ⋅ 6.17
103.38 + 0.2 ⋅ 6.17
=
20.67 N/mm©÷  
  Thickness analysis, t > trn ? t = 8.2 mm is OK      
           
  Weight     9.00 kg  
  Enclosed volume     0.004 m3  
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Rho (·Î¿ì) Çѱ¹¾î '»ç¶û' ÀÇ '¤©' (¿µ¾î r)
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Tau (Ÿ¿ì) ¿µ¾î t (Çѱ¹¾î µÈ¼Ò¸® '¤¨')
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Phi (ÆÄÀÌ) Çѱ¹¾î '¤½' (³ªÁß¿¡ ¿µ¾î f ·Î ¹Ù²ñ)
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Ä«ÀÌ (xhi) Çѱ¹¾î '¤»' (³ªÁß¿¡ µ¶ÀϾî Buch ÀÇ ch ·Î ¹Ù²ñ)
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ÇÁ»çÀÌ (psi) ¿µ¾î ps
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Omega (¿À¸Þ°¡) Çѱ¹¾î '¿À' (¿µ¾î tone ÀÇ o)

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¿µ¾î boy ÀÇ ÀÌÁ߸ðÀ½°ú °°½À´Ï´Ù.
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¿µ¾î too ÀÇ Àå¸ðÀ½°ú °°½À´Ï´Ù.
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¿µ¾î quit ÀÇ ui ¼Ò¸®¿Í °°½À´Ï´Ù.
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¿µ¾î finger ÀÇ ng ¹ßÀ½ÀÔ´Ï´Ù.
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