[SKS] IMO TYPE C TANK DATA LIST

IMO TYPE C TANK DATA LIST π × (ø ｍ²ｍ³ ㄷ ＋－ × ÷ ± ≤ ≥ ^C ℃ ▶ ㅊ

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1. SHI CP 11매 2. SHI Comment_C-Type LNG Fuel Tank 생산 개선아이디어

query[0] = [Select HTML FROM IMO_STD Where headType=0 and (sid=0 or (sid=1 and jNo=4)) Order By sid, headType, jNo, rNo]
IMO TYPE C - STANDARD SIZE and Volume Table

Head Type ; Spherical-Head

Material Selection for IMO TYPE C TANK (재질을 선택하세요,) Unit : MPa
MATERIAL	Weld Metal(용접봉강도)			Allowable Membrane Stress(f) (by IGC, IGF)
MATERIAL	Tensile Re (=St)	Yield Rm (=Sy)	Div.1 S	f = Min(Rm/A, Re/B)	f (Mpa)	A	B
A1106(Hign Mn)	660	400	N/A	f = Min(660/3.5, 400/1.5)	188.6	3.5	1.5
A553-TYPE1	690	420	187.0	f = Min(690/3.0, 420/1.5)	230.0	3.0	1.5
LT-FH32(TM)	440~570	315	N/A	f = Min(440/3.0, 315/1.5)	146.67
LT-FH36(TM)	490~630	355	N/A	f = Min(490/3.0, 355/1.5)	163.33
SA240-304	515	205	138	f = Min(515/3.5, 205/1.5)	136.66	3.5	1.5
SA240-304L	485	170	115	f = Min(485/3.5, 170/1.5)	113.33
SA240-316	515	205	138	f = Min(515/3.5, 205/1.5)	136.66
SA240-316L	485	170	115	f = Min(485/3.5, 170/1.5)	113.33
[Allowable Stress 계산 식 참고하기]

Design Data :

Class Society

Liquid

Material

Head Type

Design Pressure
Po, MARVS(bar.g)

Design External
Pressure MAEP(bar.g)

Corrosion
Allowance
CA (mm)

BOR Limit
(%/day)

Insulation Thk.
tInsu (mm)

Vacuum Ring
Pitch (mm)

Weld Metal
Tensile Stress
Rm (MPa)

Weld Metal
Yield Stress
Re (MPa)

Allowable Stress
f=Min(Rm/A, Re/B)
f = Min(660/3.5, 400/1.5)

REMARK

KR (한국선급)

LNG

A1106(Hign Mn)

[HH] Hemi-Spherical Head

4.0

0.45

0.75

0.35

400

3500

660

400

188.6

No.	Description	Symbol	TNO-1	TNO-2	TNO-3	TNO-4	TNO-5	TNO-6	TNO-7	TNO-8	TNO-9	TNO-10	TNO-11	TNO-12	TNO-13	TNO-14	TNO-15	TNO-16	TNO-17	TNO-18	Unit
1	TANK In-Diameter	Di =	4000	4800	5800	6000	7500	8000	8000	8250	8500	9000	10000	9200	11000	11250	12000	12500	12000	12500	mm
2	Hemi-Spherical Depth	*z = 0.5D**	2000	2400	2900	3000	3750	4000	4000	4125	4250	4500	5000	4600	5500	5625	6000	6250	6000	6250	mm
3	Cylinder Straight Length (TL to TL : 10mm 단위올림)	TL =	13250	16150	15060	22530	18770	19540	24510	27240	29580	22300	16260	31480	24240	27720	25160	22230	27370	24270	mm
4	Total Length ( Head End to End ), L = 2*z +TL	L =	17250	20950	20860	28530	26270	27540	32510	35490	38080	31300	26260	40680	35240	38970	37160	34730	39370	36770	mm
5	Design Liquid Level	DLL =	3327	3993	4816	4994	6226	6640	6651	6862	7072	7471	8270	7654	9122	9338	9948	10347	9955	10355	mm
6
7	Gross Volume, Vnom = Vcyl+Vhead	Vnom =	200	350	500	750	1050	1250	1500	1750	2000	1800	1800	2500	3000	3500	3750	3750	4000	4000	m³
8	Net Volume ( Vnet = 0.98*Vnom)	Vnet =	179.0	313.3	447.5	671.3	939.8	1118.8	1342.5	1566.3	1790.0	1611.0	1611.0	2237.5	2685.0	3132.5	3356.3	3356.3	3580.0	3580.0	0.98*Vnom
9	Vhead = πD³ / 6	Vhead =	33.5	57.9	102.2	113.1	220.9	268.1	268.1	294.0	321.6	381.7	523.6	407.7	696.9	745.5	904.8	1022.7	904.8	1022.7	m³
10	Vcyl = πD² / 4 * L	Vcyl =	166.5	292.1	397.8	636.9	829.1	981.9	1231.9	1456.0	1678.4	1418.3	1276.4	2092.3	2303.1	2754.5	2845.2	2727.3	3095.2	2977.3	m³
11	Storage Ratio = Vnet / Vnom * 100	Sratio =	89.5	89.5	89.5	89.5	89.5	89.5	89.5	89.5	89.5	89.5	89.5	89.5	89.5	89.5	89.5	89.5	89.5	89.5	%
12	Static Head Pressure, Ps = ρgh(h=DLL)	Ps =	0.0163	0.0196	0.0236	0.0245	0.0305	0.0326	0.0326	0.0336	0.0347	0.0366	0.0406	0.0375	0.0447	0.0458	0.0488	0.0507	0.0488	0.0508	MPa
13	[ASME] Total Design Pressure, P = Po+Ps	P_ASME =	0.4163	0.4196	0.4236	0.4245	0.4305	0.4326	0.4326	0.4336	0.4347	0.4366	0.4406	0.4375	0.4447	0.4458	0.4488	0.4507	0.4488	0.4508	MPa
14	[ASME] Cylinder Shell Thickness	t_Cyl =	5.17	6.1	7.27	7.51	9.32	9.94	9.94	10.25	10.56	11.19	12.45	11.44	13.74	14.07	15.05	15.71	15.05	15.71	mm
15	[ASME] Hemi-Spherical Head Thickness	t_HHead =	2.96	3.42	4.01	4.13	5.03	5.34	5.34	5.49	5.65	5.96	6.59	6.09	7.24	7.4	7.89	8.22	7.89	8.22	mm
16	[ASME] Cylinder Shell Thk (Vacuum Ring Pitch: 3.5m )	t_CylPe =	10.0	11.0	12.0	12.5	14.0	14.5	14.5	14.5	15.0	15.0	16.0	15.5	17.0	17.0	17.5	18.0	17.5	18.0	mm
17	[ASME] Allowable External Pressure(Shell), Pe < Pa_Cyl	Pa_Cyl =	0.0525	0.0519	0.049	0.0519	0.051	0.0507	0.0507	0.0481	0.0503	0.0473	0.0486	0.0497	0.05	0.0485	0.0476	0.0483	0.0476	0.0483	MPa
18	[ASME] Allowable External Pressure(Head ), Pe < Pa_Head	Pa_Head =	0.0998	0.0829	0.0698	0.0689	0.0688	0.0688	0.0688	0.0689	0.0689	0.0689	0.0688	0.0688	0.0688	0.0689	0.0689	0.0689	0.0689	0.0689	MPa
19	[Class] Dynamic Pressure(Ship Motion)	Pgd(max) =	0.1363	0.1396	0.1436	0.1245	0.1305	0.1326	0.1326	0.1336	0.1347	0.1366	0.1206	0.1375	0.1247	0.1258	0.1288	0.1307	0.1288	0.1308	MPa
20	[Class] Total Design Pressure, P = Po+Pgd(max)	P_Class =	0.5363	0.5396	0.5436	0.5245	0.5305	0.5326	0.5326	0.5336	0.5347	0.5366	0.5206	0.5375	0.5247	0.5258	0.5288	0.5307	0.5288	0.5308	MPa
21	[Class] Cylinder Shell Thickness	t_Cyl =	6.45	7.63	9.12	9.11	11.32	12.07	12.07	12.44	12.82	13.58	14.57	13.88	16.08	16.46	17.6	18.37	17.6	18.37	mm
22	[Class] Hemi-Spherical Head Thickness	t_HHead =	3.59	4.18	4.93	4.92	6.03	6.4	6.4	6.59	6.78	7.15	7.65	7.31	8.4	8.59	9.16	9.55	9.16	9.55	mm
23	[LR] Cylinder Shell Thk (Vacuum Ring: 3.5m )	t_CylPe =	10.0	11.5	12.5	13.0	14.5	15.0	15.0	15.5	15.5	16.0	17.0	16.0	18.0	18.0	19.0	19.0	19.0	19.0	mm
24	[DNV-GL] Hemi-Spherical Head Thk (For Vacuum ) Pc=2.4Et(t-c/Ro)²/ 3.7 [DNV-GL Pt4-Ch7]	t_HeadPe =	3.15	3.62	4.22	4.34	5.24	5.54	5.54	5.69	5.84	6.14	6.74	6.26	7.34	7.49	7.94	8.23	7.94	8.23	mm
25	[LR] Allowable External Pressure (Shell DNV-GL, LR, GV)	Pcr =	0.0473	0.053	0.0494	0.0521	0.0505	0.0493	0.0493	0.0513	0.0488	0.0491	0.0494	0.0471	0.0501	0.0479	0.0496	0.047	0.0496	0.047	MPa
26	[NK] Allowable External Pressure (ClassNk equal ASME Div2. )	Pa_div2 =	0.0204	0.0227	0.0276	0.0263	0.0358	0.0403	0.0403	0.0386	0.0408	0.0454	0.0464	0.044	0.0514	0.0498	0.0566	0.0571	0.0566	0.0571	MPa
27	PUF Insulation Volume	Vinsu =	98.05	140.11	166.36	233.58	265.87	296.18	348.81	391.64	432.04	376.02	349.93	497.49	512.64	578.62	587.66	571.84	622.2	605.01	m³
28	Min. Thickness for Internal Pressure 　tMinPo(DNV-GL) = 3+Di/1500+CA	tMinPo =	6.42	6.95	7.62	7.75	8.75	9.08	9.08	9.25	9.42	9.75	10.42	9.88	11.08	11.25	11.75	12.08	11.75	12.08	mm
29	Min. Thickness for Internal Pressure, (IGC_LR_ASME)	tMinBase =	3.0	3.0	3.0	3.0	3.0	3.0	3.0	3.0	3.0	3.0	3.0	3.0	3.0	3.0	3.0	3.0	3.0	3.0	mm
30	Min. Thickness for External Pressure, tMinPe = Do/850 ASME SECTION II, PART D - SUBPART 3 (METRIC), FIG. G	tMinPe =	5.46	6.4	7.57	7.81	9.57	10.16	10.16	10.46	10.75	11.34	12.51	11.57	13.69	13.99	14.87	15.46	14.87	15.46	mm
31
32	[Calc] Shell Thickness	tCyl =	6.45	7.63	9.12	9.11	11.32	12.07	12.07	12.44	12.82	13.58	14.57	13.88	16.08	16.46	17.60	18.37	17.60	18.37	mm
33	[Calc] Head Thickness	tHead =	6.42	6.95	7.62	7.81	9.57	10.16	10.16	10.46	10.75	11.34	12.51	11.57	13.69	13.99	14.87	15.46	14.87	15.46	mm
34	Nominal Shell Thickness (벤딩마진포함)	tu_Cyl =	7.00	8.00	9.50	9.50	12.00	13.00	13.00	13.00	13.50	14.50	15.50	14.50	17.00	17.00	18.50	19.00	18.50	19.00	mm
35	Nominal Head Thickness (성형마진포함)	tu_Head =	7.00	7.50	8.50	8.50	10.50	11.00	11.00	11.50	11.50	12.00	13.50	12.50	14.50	15.00	15.50	16.50	15.50	16.50	mm
36	Shell Thickness Margin, tMarginCyl = tuCyl - tCyl	tMarginCyl =	0.55	0.37	0.38	0.39	0.68	0.93	0.93	0.56	0.68	0.92	0.93	0.62	0.92	0.54	0.90	0.63	0.90	0.63	mm
37	Head Thickness Margin, tMarginHead = tuHead - tHead	tMarginHead =	0.58	0.55	0.88	0.69	0.93	0.84	0.84	1.04	0.75	0.66	0.99	0.93	0.81	1.01	0.63	1.04	0.63	1.04	mm
38
39
40	Shell Segment 수량	sQty =	4.0	5.0	5.0	7.0	6.0	6.0	8.0	9.0	9.0	7.0	5.0	10.0	8.0	9.0	8.0	7.0	9.0	8.0	sheets
41	Shell Segment Width	sWidth =	3337.5	3250.0	3032.0	3232.86	3145.0	3273.33	3076.25	3037.78	3297.78	3200.0	3272.0	3158.0	3042.5	3091.11	3157.5	3190.0	3052.22	3046.25	mm
42	Shell Cutting Plan Length, @SegmentWidth * sQty=	cpLength =	@3337.5x4 EA = 13350	@3250.0x5 EA = 16250	@3032.0x5 EA = 15160	@3232.86x7 EA = 22630	@3145.0x6 EA = 18870	@3273.33x6 EA = 19640	@3076.25x8 EA = 24610	@3037.78x9 EA = 27340	@3297.78x9 EA = 29680	@3200.0x7 EA = 22400	@3272.0x5 EA = 16360	@3158.0x10 EA = 31580	@3042.5x8 EA = 24340	@3091.11x9 EA = 27820	@3157.5x8 EA = 25260	@3190.0x7 EA = 22330	@3052.22x9 EA = 27470	@3046.25x8 EA = 24370	mm
43	Actual inertia moment of Saddle Ring	Ig_Saddle =	93387.0	99304.0	163003.0	163696.0	380938.0	397566.0	397566.0	611519.0	622941.0	646530.0	1049092.0	1010293.0	1436487.0	1603172.0	1678416.0	1970352.0	1678416.0	1970352.0	cm⁴
44	Saddle Ring (Qty) Saddle Ring (Size)	SRqty = SIZE =	2 S/Rings T600x22+300x22	2 S/Rings T600x22+300x22	2 S/Rings T700x23+300x23	2 S/Rings T700x23+300x23	2 S/Rings T900x25+350x25	2 S/Rings T900x25+350x25	2 S/Rings T900x25+350x25	2 S/Rings T1000x30+400x30	2 S/Rings T1000x30+400x30	2 S/Rings T1000x30+400x30	2 S/Rings T1200x30+400x30	2 S/Rings T1200x30+400x30	2 S/Rings T1300x32+430x32	2 S/Rings T1350x32+450x32	2 S/Rings T1350x32+450x32	2 S/Rings T1400x34+470x34	2 S/Rings T1350x32+450x32	2 S/Rings T1400x34+470x34	Rings
45	Vacuum Ring (Qty) Vacuum Ring (Size)	VRqty = SIZE =	5 V/Rings FB150x20	6 V/Rings FB200x20	5 V/Rings FB230x25	8 V/Rings FB230x25	7 V/Rings T300x15+100x15	7 V/Rings T300x15+100x15	9 V/Rings T300x15+100x15	9 V/Rings T300x15+100x15	10 V/Rings T300x15+100x15	8 V/Rings T300x15+100x15	6 V/Rings T300x15+100x15	11 V/Rings T300x15+100x15	8 V/Rings T350x15+200x15	10 V/Rings T350x15+200x15	9 V/Rings T350x15+200x15	8 V/Rings T400x20+250x15	9 V/Rings T350x15+200x15	8 V/Rings T400x20+250x15	Rings
46	Vacuum Ring @pitch	VR_pitch =	@2810×4 +2×1005	@2830×5 +2×1000	@3270×4 +2×990	@2930×7 +2×1010	@2800×6 +2×985	@2920×6 +2×1010	@2810×8 +2×1015	@3160×8 +2×980	@3060×9 +2×1020	@2900×7 +2×1000	@2850×5 +2×1005	@2950×10 +2×990	@3180×7 +2×990	@2860×9 +2×990	@2900×8 +2×980	@2890×7 +2×1000	@3170×8 +2×1005	@3180×7 +2×1005	mm
47	Required inertia moment of Stiff. Ring 　Ix = 0.18 * D * Pe_MPa * L * Ds² / E ×10E-5	Ix =	1018.4	1760.6	3108.1	3440.2	6725.1	8164.6	8164.6	8952.3	9792.6	11627.7	15948.5	12418.4	21231.4	22708.6	27568.4	31158.4	27568.4	31158.4	cm⁴
48	Actual inertia moment of Vacuum Ring	Ig =	1118.6	2637.8	5002.4	5031.8	13654.9	14459.4	14459.4	14537.6	14925.7	15676.3	16522.2	15733.2	33953.8	34086.3	36106.7	58209.4	36106.7	58209.4	cm⁴
49	Ix / Ig < 1.0 OK		0.9	0.7	0.6	0.7	0.5	0.6	0.6	0.6	0.7	0.7	1.0	0.8	0.6	0.7	0.8	0.5	0.8	0.5
50	Weight Summary
51	1) Shell Weight	wShell =	11.523	18.032	23.608	35.019	45.787	55.456	68.073	77.337	89.409	77.719	68.686	109.598	118.822	137.911	145.582	138.312	157.544	150.092	ton
52	2) Head Weight	wHead =	2.762	4.261	7.051	7.547	14.566	17.362	17.362	19.303	20.491	23.971	33.293	26.092	43.269	46.819	55.044	63.58	55.044	63.58	ton
53	3) Saddle Rins(Inside)	WsaddleRing =	4.653	5.772	8.056	8.477	14.216	15.635	15.635	20.406	21.151	22.663	28.103	25.555	35.265	37.314	41.176	46.739	41.176	46.739	ton
54	4) Vacuum Rings(Inside)	WvacuumRing =	1.618	2.748	3.746	6.509	7.25	7.894	10.092	11.04	12.495	10.654	9.302	15.081	17.74	22.682	22.52	28.596	22.52	28.596	ton
55	5) Swash Bulk Head and Attachment	WbulkHead =	5.799	7.19	9.221	10.022	14.153	15.995	15.995	16.616	17.378	18.958	22.057	19.5	25.583	26.382	29.81	31.732	29.81	31.732	ton
56	6) Saddle(CS/Bottom)	Wsaddle_CS =	3.194	4.953	7.199	7.798	12.109	13.883	13.883	14.954	16.025	18.561	25.059	19.636	34.751	37.749	48.879	57.18	48.879	57.18	ton
57	7) Accessory(CS/PlatForm)	Waccy_CS =																			ton
58	8) PUF ( Insulation ) Winsu = Vinsu * Density [ 40 kg/m³]	Winsu =	3.922	5.604	6.654	9.343	10.635	11.847	13.952	15.666	17.282	15.041	13.997	19.9	20.506	23.145	23.506	22.874	24.888	24.2	Ton
59	Empty Steel Weight(1~7)	Wempty =	33.471	48.56	65.535	84.715	118.716	138.072	154.992	175.322	194.231	187.567	200.497	235.362	295.936	332.002	366.517	389.013	379.861	402.119	Ton
60	at Operating Condition	Woper =	89.5	156.65	223.75	335.65	469.9	559.4	671.25	783.15	895.0	805.5	805.5	1118.75	1342.5	1566.25	1678.15	1678.15	1790.0	1790.0	Ton
61	at Hydrostatic-test Condition	Wtest =	200.0	350.0	500.0	750.0	1050.0	1250.0	1500.0	1750.0	2000.0	1800.0	1800.0	2500.0	3000.0	3500.0	3750.0	3750.0	4000.0	4000.0	Ton
62	Dynamic Pressure due to Ship mortion)	PgdMax =																			bar.g
63	Surface Area Calculation for Net Weight
64	Shell Plate Surface Area (OD 기준)	suf_Shell =																			m2
65	Head Plate Surface Area (OD 기준)	suf_Head =																			m2
66
67
68
69	Surface Area Total	SArea																			m2
Weight Summary			[조 회]	[조 회]	[조 회]	[조 회]	[조 회]	[조 회]	[조 회]	[조 회]	[조 회]	[조 회]	[조 회]	[조 회]	[조 회]	[조 회]	[조 회]	[조 회]	[조 회]	[조 회]	Unit

[TNO-5] Tank Size : ø7500 x 18770 (L = 26270 mm ) Weight Summary

5. Tank Capacity : 1050 ｍ³ 　Head Type ; [HH] Spherical-Head		Tank Size : ø7500 x 18770 (L = 26270 mm )						Plate 발주폭(Max) : 3400 mm Head Plate Surface Area(표면적) : 176.715 m²		Head Type ; [HH] Spherical-Head
No.	Name	MATERIAL	SIZE t x W X L (mm)			Quantity (SHT)	Weight (kg)	표면적 ｍ²/ pcs	Remark	SKETCH
1	Shell Plate (Center Part 일반부)	A1106(Hign Mn)	12.00	3,145	11,803	8	27,974	37.12044	길이분할: @3145.0×6 shts = 18870 > 18770 mm
2	Shell Plate (Saddle Support Part)	A1106(Hign Mn)	14.00	3,145	11,803	4	16,318	37.12044	원주분할: L=π×ø7514 = 23606mm / 2분할= 11803mm
3	Shell Plate (Dome Reinforcement)	A1106(Hign Mn)	14.00	3,400	4,000	1	1,495	13.60000	Dome Part
4	[HH] Hemi-Head Plate (Side)	A1106(Hign Mn)	10.50	2,359	3,174	20	10,653	129.24087	Angle = (#4WP: 47º, CP : 48.431º) [deg]
5	[HH] Hemi-Head Plate (Center)	A1106(Hign Mn)	10.50	2,818	5,637	4	3,913	47.47372	Angle = (#4WP: 47º + 43º : #5WP,CP) = 90º [deg]
6				0	0	0	0		(Head Plate 표면적)Surface Area : 176.715 m²
7	Wear Plate and 지지금구(Fix / Sliding)	A1106(Hign Mn)	14.00	1,200	11,847	2	3,125	14.21640	For Saddle Support
8				0	0	0	0		8
9	SWASH Bulk Head ( Baffle Plate - Hole 중량 포함 )	A1106(Hign Mn)	10.00	4,776	7,200	2	5,399	34.38720	Baffle Plate Net Surface Area = 29.50906 ｍ²(Hole 면적포함)
10	Bulk Head (Baffle Stiffener Plate)	A1106(Hign Mn)	15.00	1,200	11,852	2	3,349	14.22240	10
11	Bulk Head (U-BAND Spring : 충격완화금구)	A1106(Hign Mn)	25.00	400	660	44	2,280	0.26400
12	Vacuum Ring (Web) T300x15+100x15	A1106(Hign Mn)	15.00	285	0	6	4,564	6.46000	A = π× (OD 7500²- ID : 6930²) / 4 = 6.46 m²
13	Vacuum Ring (Flange) T300x15+100x15	A1106(Hign Mn)	15.00	100	22,667	6	1,601	2.26670	L = π × (ø7215 ) = 22667 mm
14	Vacuum Ring (Rib Plate)	A1106(Hign Mn)	25.00	162	850	40	1,084	0.13813
15	Saddle Ring (Web) T900x25+350x25	A1106(Hign Mn)	25.00	875	0	2	7,148	18.21100	A = π× (OD 7500²- ID : 5750²) / 4 = 18.211 m²
16	Saddle Ring (Flange) T900x25+350x25	A1106(Hign Mn)	25.00	350	20,813	2	2,859	7.28455	L = π × (ø6625 ) = 20813 mm
17	Saddle Ring (Rib Plate)	A1106(Hign Mn)	25.00	162	850	40	1,084	0.13813
18				0	0	0	0
19				0	0	0	0
20				0	0	0	0
21	Saddle Support (Base Plate)	DH32 OR A516-60	41.00	920	9,300	2	5,507	8.55600	Base Plate : t41 mm
22	Saddle Support (Rib & Etc)	DH32 OR A516-60	35.00	3,048	7,883	1	6,602	24.02738	Rib Plate Thick. J=35.0 (mm) , tg=32.0 (mm)
23				0	0	0	0
24				0	0	0	0
[ONLY] Shell and head Plate Quentity						37 sht
Total Weight							104,956	kg

Vacuuring Ring (Stiffener) Size : T300x15+100x15　
Tank OD (Da) = 7524 mm, Shell Plate: t12 x W:330mm W=1.1*SQRT(D*t)
( IxReqd = 6725.1 < 13654.9 = IxActual ) OK

Memb	b	d	A=b*d	Y	A*Y	h=ABS(y-C1)	A*h²	Ig = b*d³/12	SKETCH
No.	(cm)	(cm)	(cm²)	(cm)	(cm³)	(cm)	(cm⁴)	(cm⁴)
3	10.0	1.5	15.0	30.45	456.75	18.73	5261.63	2.81
2	1.5	28.5	42.75	15.45	660.49	3.73	594.46	2893.64
Shell	33.0	1.2	39.6	0.6	23.76	11.12	4897.59	4.75
	SUM	∑ =	97.35		1141.0		10753.68	2901.21

C1	= ∑(AY) / ∑(A) (무게중심 위치)	C1 =	11.721	cm	무게중심에서 FLANGE 하단 까지 떨어진 거리
C2	= H - C1	C2 =	19.479	cm	무게중심에서 FLANGE 상단 까지 떨어진 거리
∑(A)	= Sum of Section Area (단면적)	∑(A)=	97.35	cm²	단면적 (빗금전체)
Ix	= ∑(Ah²) + ∑(Ig)	Ix =	13654.89	cm⁴	X축 단면2차모멘트 (Moment of inertia)
Zx	= Ix / Max(C1, C2)	Zx =	701.01	cm³	X축 단면계수(Section Modulus)
Iy	= ∑(Iy)	Iy =	3726.72	cm⁴	Y축 단면2차모멘트(Moment of inertia)
Zy	= 나중에 무게중심 위치가 중앙 ??	Zy =	191.32	cm³	Y축 단면계수 (Section Modulus)
Rx	= SQRT( Ix / A )	Ry =	11.84	cm	X축 회전반경
Ry	= SQRT( Iy / A )	Ry =	6.19	cm	Y축 회전반경
Ring 단면적 (Shell 제외)		ARing =	57.75	cm²	Ring 단면적 (Shell 제외)
Ring 원주길이		Leng =	10.0	m	Ring 길이(m)
Ring 단위중량 (kg/m),		WTm =	45.33	kg/m	단위중량(kg/m)
Ring Weight, Shell(1) 제외 중량		WT =	453.34	kg	Ring 1 PCS 중량(kg)

Saddle Ring Size : T900x25+350x25　
Tank OD (Da) = 7524 mm, Shell Plate: t12 x W:330mm W=1.1*SQRT(D*t)
( IxReqd = 6725.1 < 380938.2 = IxSadAct ) OK

Memb	b	d	A=b*d	Y	A*Y	h=ABS(y-C1)	A*h²	Ig = b*d³/12	SKETCH
No.	(cm)	(cm)	(cm²)	(cm)	(cm³)	(cm)	(cm⁴)	(cm⁴)
3	35.0	2.5	87.5	89.95	7870.63	38.69	131000.47	45.57
2	2.5	87.5	218.75	44.95	9832.81	6.31	8701.49	139567.06
Shell	33.0	1.2	39.6	0.6	23.76	50.66	101618.81	4.75
	SUM	∑ =	345.85		17727.2		241320.78	139617.38

C1	= ∑(AY) / ∑(A) (무게중심 위치)	C1 =	51.257	cm	무게중심에서 FLANGE 하단 까지 떨어진 거리
C2	= H - C1	C2 =	39.943	cm	무게중심에서 FLANGE 상단 까지 떨어진 거리
∑(A)	= Sum of Section Area (단면적)	∑(A)=	345.85	cm²	단면적 (빗금전체)
Ix	= ∑(Ah²) + ∑(Ig)	Ix =	380938.16	cm⁴	X축 단면2차모멘트 (Moment of inertia)
Zx	= Ix / Max(C1, C2)	Zx =	7431.92	cm³	X축 단면계수(Section Modulus)
Iy	= ∑(Iy)	Iy =	12639.92	cm⁴	Y축 단면2차모멘트(Moment of inertia)
Zy	= 나중에 무게중심 위치가 중앙 ??	Zy =	246.6	cm³	Y축 단면계수 (Section Modulus)
Rx	= SQRT( Ix / A )	Ry =	33.19	cm	X축 회전반경
Ry	= SQRT( Iy / A )	Ry =	6.05	cm	Y축 회전반경
Ring 단면적 (Shell 제외)		ARing =	306.25	cm²	Ring 단면적 (Shell 제외)
Ring 원주길이		Leng =	10.0	m	Ring 길이(m)
Ring 단위중량 (kg/m),		WTm =	240.41	kg/m	단위중량(kg/m)
Ring Weight, Shell(1) 제외 중량		WT =	2404.06	kg	Ring 1 PCS 중량(kg)

query[0] = [Select sid, headType, jNo, rNo, DESCR, SYMBOL, VALUE, UNIT FROM IMO_STD Where sid=2 and headType=0 and jNo=4 Order By sid, jNo, rNo]
getResult[2] = [

번호	0 sid	1 headType	2 jNo	3 rNo	4 DESCR	5 SYMBOL	6 VALUE	7 UNIT
1	2	0	4	1	TANK In-Diameter	Di =	7500.0	mm
2	2	0	4	2	Hemi-Spherical Depth	z = 0.5*D	3750.0	mm
3	2	0	4	3	Cylinder Straight Length (TL to TL : 10mm 단위올림)	TL =	18770.0	mm
4	2	0	4	4	Total Length ( Head End to End ), L = 2*z +TL	L =	26270.0	mm
5	2	0	4	5	Design Liquid Level	DLL =	6226.0	mm
6	2	0	4	6			0.0
7	2	0	4	7	Gross Volume, Vnom = Vcyl+Vhead	Vnom =	1050.0	m³
8	2	0	4	8	Net Volume ( Vnet = 0.98*Vnom)	Vnet =	939.8	0.98*Vnom
9	2	0	4	9	Vhead = πD³ / 6	Vhead =	220.9	m³
10	2	0	4	10	Vcyl = πD² / 4 * L	Vcyl =	829.1	m³
11	2	0	4	11	Storage Ratio = Vnet / Vnom * 100	Sratio =	89.5	%
12	2	0	4	12	Static Head Pressure, Ps = ρgh(h=DLL)	Ps =	0.0305	MPa
13	2	0	4	13	[ASME] Total Design Pressure, P = Po+Ps	P_ASME =	0.4305	MPa
14	2	0	4	14	[ASME] Cylinder Shell Thickness	t_Cyl =	9.32	mm
15	2	0	4	15	[ASME] Hemi-Spherical Head Thickness	t_HHead =	5.03	mm
16	2	0	4	16	[ASME] Cylinder Shell Thk (Vacuum Ring Pitch: 3.5m )	t_CylPe =	14.0	mm
17	2	0	4	17	[ASME] Allowable External Pressure(Shell), Pe < Pa_Cyl	Pa_Cyl =	0.051	MPa
18	2	0	4	18	[ASME] Allowable External Pressure(Head ), Pe < Pa_Head	Pa_Head =	0.0688	MPa
19	2	0	4	19	[Class] Dynamic Pressure(Ship Motion)	Pgd(max) =	0.1305	MPa
20	2	0	4	20	[Class] Total Design Pressure, P = Po+Pgd(max)	P_Class =	0.5305	MPa
21	2	0	4	21	[Class] Cylinder Shell Thickness	t_Cyl =	11.32	mm
22	2	0	4	22	[Class] Hemi-Spherical Head Thickness	t_HHead =	6.03	mm
23	2	0	4	23	[LR] Cylinder Shell Thk (Vacuum Ring: 3.5m )	t_CylPe =	14.5	mm
24	2	0	4	24	[DNV-GL] Hemi-Spherical Head Thk (For Vacuum ) Pc=2.4Et(t-c/Ro)²/ 3.7 [DNV-GL Pt4-Ch7]	t_HeadPe =	5.24	mm
25	2	0	4	25	[LR] Allowable External Pressure (Shell DNV-GL, LR, GV)	Pcr =	0.0505	MPa
26	2	0	4	26	[NK] Allowable External Pressure (ClassNk equal ASME Div2. )	Pa_div2 =	0.0358	MPa
27	2	0	4	27	PUF Insulation Volume	Vinsu =	265.87	m³
28	2	0	4	28	Min. Thickness for Internal Pressure 　tMinPo(DNV-GL) = 3+Di/1500+CA	tMinPo =	8.75	mm
29	2	0	4	29	Min. Thickness for Internal Pressure, (IGC_LR_ASME)	tMinBase =	3.0	mm
30	2	0	4	30	Min. Thickness for External Pressure, tMinPe = Do/850 ASME SECTION II, PART D - SUBPART 3 (METRIC), FIG. G	tMinPe =	9.57	mm
31	2	0	4	31			0.0
32	2	0	4	32	[Calc] Shell Thickness	tCyl =	11.32	mm
33	2	0	4	33	[Calc] Head Thickness	tHead =	9.57	mm
34	2	0	4	34	Nominal Shell Thickness (벤딩마진포함)	tu_Cyl =	12.0	mm
35	2	0	4	35	Nominal Head Thickness (성형마진포함)	tu_Head =	10.5	mm
36	2	0	4	36	Shell Thickness Margin, tMarginCyl = tuCyl - tCyl	tMarginCyl =	0.68	mm
37	2	0	4	37	Head Thickness Margin, tMarginHead = tuHead - tHead	tMarginHead =	0.93	mm
38	2	0	4	38			0.0
39	2	0	4	39			0.0
40	2	0	4	40	Shell Segment 수량	sQty =	6.0	sheets
41	2	0	4	41	Shell Segment Width	sWidth =	3145.0	mm
42	2	0	4	42	Shell Cutting Plan Length, @SegmentWidth * sQty=	cpLength =	0.0	mm
43	2	0	4	43	Actual inertia moment of Saddle Ring	Ig_Saddle =	380938.0	cm⁴
44	2	0	4	44	Saddle Ring (Qty) Saddle Ring (Size)	SRqty = SIZE =	0.0	Rings
45	2	0	4	45	Vacuum Ring (Qty) Vacuum Ring (Size)	VRqty = SIZE =	6.0	Rings
46	2	0	4	46	Vacuum Ring @pitch	VR_pitch =	2800.0	mm
47	2	0	4	47	Required inertia moment of Stiff. Ring 　Ix = 0.18 * D * Pe_MPa * L * Ds² / E ×10E-5	Ix =	6725.1	cm⁴
48	2	0	4	48	Actual inertia moment of Vacuum Ring	Ig =	13654.9	cm⁴
49	2	0	4	49	Ix / Ig < 1.0 OK		0.5
50	2	0	4	50	Weight Summary		0.0
51	2	0	4	51	1) Shell Weight	wShell =	45.787	ton
52	2	0	4	52	2) Head Weight	wHead =	14.566	ton
53	2	0	4	53	3) Saddle Rins(Inside)	WsaddleRing =	14.216	ton
54	2	0	4	54	4) Vacuum Rings(Inside)	WvacuumRing =	7.25	ton
55	2	0	4	55	5) Swash Bulk Head and Attachment	WbulkHead =	14.153	ton
56	2	0	4	56	6) Saddle(CS/Bottom)	Wsaddle_CS =	12.109	ton
57	2	0	4	57	7) Accessory(CS/PlatForm)	Waccy_CS =	0.0	ton
58	2	0	4	58	8) PUF ( Insulation ) Winsu = Vinsu * Density [ 40 kg/m³]	Winsu =	10.635	Ton
59	2	0	4	59	Empty Steel Weight(1~7)	Wempty =	118.716	Ton
60	2	0	4	60	at Operating Condition	Woper =	469.9	Ton
61	2	0	4	61	at Hydrostatic-test Condition	Wtest =	1050.0	Ton
62	2	0	4	62	Dynamic Pressure due to Ship mortion)	PgdMax =	0.0	bar.g
63	2	0	4	63	Surface Area Calculation for Net Weight		0.0
64	2	0	4	64	Shell Plate Surface Area (OD 기준)	suf_Shell =	0.0	m2
65	2	0	4	65	Head Plate Surface Area (OD 기준)	suf_Head =	0.0	m2
66	2	0	4	66			0.0
67	2	0	4	67			0.0
68	2	0	4	68			0.0
69	2	0	4	69	Surface Area Total	SArea	0.0	m2

]

매크로포함_SHI_SN2430_D12m_견적강도계산 (견적원가).xlsm - [PV4th SADDLES] Sheet 참고

Pressure Vessel Design Manulal (4th edition) / Table 4-27 Large diameter saddle supports

Vessel DIA.		BASE PLATE LENGTH	SADDLE HEIGHT	Bolt Hole Dia.	INNER RIB PITCH	BASE PLATE Width	BOLT PITCH	Saddle BTM Width	Saddle Top Width	Wear Plate Width	Rib Plate 두께	RIB 수량	BOLT 수량	Base Plate 두께	Gusset Plate 두께	Wear Plate 두께	Approx wt for 2 Saddles (kg)	Saddle RIB Height(Center)
DIA(ft)	DIA(mm)	A	B	D	E	F	G	GB=F-50.8	GT	H	J	N	n	tb	tg	tw	wt	h=B-D/2
14	4267	3937	2337	35	483	457	229	406	711	864	19	8	8	25	19	19	3175	203.2
15	4572	4343	2540	35	533	457	229	406	711	864	19	8	8	25	19	19	3629	254
16	4877	4648	2743	35	457	457	235	406	711	864	25	10	8	29	22	22	4536	304.8
17	5182	4902	2896	41	483	533	273	483	787	940	25	10	8	32	25	25	4990	304.8
18	5486	5258	3099	41	432	533	279	483	787	940	29	12	12	35	29	25	5443	355.6
20	6096	5258	3353	41	432	533	279	483	787	940	29	12	12	35	29	29	7031	304.8
22	6706	5563	3658	48	457	610	318	559	864	1016	32	12	12	38	32	32	8618	304.8
24	7315	6121	3962	48	432	610	318	559	864	1016	32	14	12	38	32	32	9979	304.8
26	7925	6477	4369	48	457	610	318	559	864	1016	35	14	12	41	32	32	11793	406.4
28	8534	6985	4674	54	432	686	356	635	940	1092	35	16	16	41	35	32	14061	406.4
30	9144	7823	4978	54	483	686	362	635	940	1092	38	16	16	44	38	35	16783	406.4
32	9754	8331	5283	54	457	686	362	635	940	1092	38	18	16	44	38	35	19958	406.4
34	10363	8788	5588	60	483	787	406	737	1041	1194	44	18	16	51	44	35	24494	406.4
36	10973	9246	5842	60	457	787	406	737	1041	1194	44	20	16	51	44	35	29937	355.6
38	11582	9754	6198	60	483	813	413	762	1067	1219	51	20	16	57	51	38	36287	406.4
40	12192	10262	6502	67	508	864	451	813	1118	1270	51	20	20	64	51	38	45359	406.4

Notes: [SADDLE STANDARD DWG(pdf)]
　1. All dimensions are in inches unless noted otherwise
　2. All saddles in this size range must be fully designed. The dimensions shown are a starting place or to be used for estimating only!
　3. Assume that anchor bolts diameter is d - 0.125, where d is the diameter of the hole. Assume that slots for sliding saddle are 6 d long.
　4. N = Number of ribs
　5. n = Number of anchor bolts

매크로포함_SHI_SN2430_D12m_견적강도계산 (견적원가).xlsm - [PV4th SADDLES] Sheet 참고

시작시간 = [2025-04-06 09:12:55.0129]
종료시간 = [2025-04-06 09:12:55.0168]

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