sksNEW_SNI_1726.jsp

2. Shell Plate Each Shell 상세출력 [div id='divDetailView' display:none ] SHOW

CALC_SHOW_MODE = [0] [ 0=계산서 내용 내용 표시 안하기, 1=표시하기 ]
메뉴판 [SKS_MAKE_JAVASCRIPT() myBuf[2] = [

Design Data and Calculation Result

조회 가능 메뉴 (누르세요)

No.

Description

DESIGN
CODE

Containment
Type

INNER OR
OUTER

Shell
Material

Tank
Diameter
(m)

Tank
Height
(m)

DLL
(m)

Empty
Weight
(Ton)

Design
Pressure
(kPa)

Nominal
Volume
(m³)

Storage
Volume
(m³)

2
강도계산서

3
Weight
summary

4
Weld Metal
용접봉

8
Roof
Structure

강도계산
MS-WORD

TK-001 (VPDM)

API 650

N/A

OUTER

A537-CL2

60.000

23.000

21.440

1698.7

2.4517

65,031

60,620

view

Turkey SECL (1 ONE-FOOT)

API 650

N/A

OUTER

A516-70

31.600

15.200

239.5

2.4517

11,921

view

Turkey SECL (2 ONE-FOOT)

API 650

N/A

OUTER

A516-70

41.600

15.200

423.0

2.4517

20,660

view

TK-002 (ONE-FOOT)

API 650

N/A

OUTER

A537-CL2

40.000

23.000

21.440

657.3

2.4517

28,903

26,942

view

[SECL] LP Ethylene

API 620

FULL Containment

INNER

A553-TYPE1

42.000

35.800

35.500

578.7

49,599

49,183

view

[SECL] LP Ethylene *

API 620

FULL Containment

OUTER

A553-TYPE1

44.000

37.800

35.500

994.3

18.0

view

한화-대산 LPG

API 620

FULL Containment

INNER

A537-CL2+S5

62.200

40.230

36.200

1799.7

122,242

109,997

view

한화-대산 LPG *

API 620

FULL Containment

OUTER

A537-CL2+S5

64.200

42.200

33.980

2780.5

14.71

view

T-201 SUMBAWA 50000 KL LNG

API 620

FULL Containment

INNER

A553-TYPE1

60.000

23.370

20.240

582.5

66,077

57,227

view

T-201 SUMBAWA 50000 KL LNG *

API 620

FULL Containment

OUTER

A553-TYPE1

62.000

24.140

20.240

1369.1

22.0

view

[T201] CAP2 LP Ethylene

API 620

FULL Containment

INNER

A553-TYPE1

46.300

16.300

14.500

381.8

27,443

24,413

view

[T201] CAP2 LP Ethylene *

API 620

FULL Containment

OUTER

A553-TYPE1

48.300

18.400

14.500

721.0

19.6133

view

[301] CAP2 Propane(C3/C4)

API 620

FULL Containment

INNER

A537-CL2+S5

70.000

27.500

24.750

1507.2

105,832

95,249

view

[301] CAP2 Propane(C3/C4) *

API 620

FULL Containment

OUTER

A537-CL2+S5

72.000

30.000

20.189

2502.6

19.62

view

총 15 개 [GA 이미지] 전체조회

myBuf[2] END = SKS_MAKE_JAVASCRIPT() 계산결과 보기 테이블 메뉴판
myBuf[3] START = SKS_MAKE_JAVASCRIPT() GA 이미지 업로드후에 GA 모두 보여주기 (hidden div = 'fromSaveBase64' / div = 'atDiv_j_i' )
div id='atDiv_2_0', at[0].divRPT[2] Contents 내용 = TK-001 (VPDM)] 2.강도계산서] 100 [KB]
div id='atDiv_3_0', at[0].divRPT[3] Contents 내용 = TK-001 (VPDM)] 3.Weight summary] 73 [KB]
div id='atDiv_4_0', at[0].divRPT[4] Contents 내용 = TK-001 (VPDM)] 4.Weld Metal] 47 [KB]
div id='atDiv_8_0', at[0].divRPT[8] Contents 내용 = TK-001 (VPDM)] 8.Roof Structure] 0 [KB]
div id='atDiv_2_2', at[2].divRPT[2] Contents 내용 = Turkey SECL (1 ONE-FOOT)] 2.강도계산서] 34 [KB]
div id='atDiv_3_2', at[2].divRPT[3] Contents 내용 = Turkey SECL (1 ONE-FOOT)] 3.Weight summary] 46 [KB]
div id='atDiv_4_2', at[2].divRPT[4] Contents 내용 = Turkey SECL (1 ONE-FOOT)] 4.Weld Metal] 40 [KB]
div id='atDiv_8_2', at[2].divRPT[8] Contents 내용 = Turkey SECL (1 ONE-FOOT)] 8.Roof Structure] 0 [KB]
div id='atDiv_2_4', at[4].divRPT[2] Contents 내용 = Turkey SECL (2 ONE-FOOT)] 2.강도계산서] 34 [KB]
div id='atDiv_3_4', at[4].divRPT[3] Contents 내용 = Turkey SECL (2 ONE-FOOT)] 3.Weight summary] 52 [KB]
div id='atDiv_4_4', at[4].divRPT[4] Contents 내용 = Turkey SECL (2 ONE-FOOT)] 4.Weld Metal] 42 [KB]
div id='atDiv_8_4', at[4].divRPT[8] Contents 내용 = Turkey SECL (2 ONE-FOOT)] 8.Roof Structure] 0 [KB]
div id='atDiv_2_6', at[6].divRPT[2] Contents 내용 = TK-002 (ONE-FOOT)] 2.강도계산서] 41 [KB]
div id='atDiv_3_6', at[6].divRPT[3] Contents 내용 = TK-002 (ONE-FOOT)] 3.Weight summary] 65 [KB]
div id='atDiv_4_6', at[6].divRPT[4] Contents 내용 = TK-002 (ONE-FOOT)] 4.Weld Metal] 53 [KB]
div id='atDiv_8_6', at[6].divRPT[8] Contents 내용 = TK-002 (ONE-FOOT)] 8.Roof Structure] 0 [KB]
div id='atDiv_2_8', at[8].divRPT[2] Contents 내용 = [SECL] LP Ethylene] 2.강도계산서] 39 [KB]
div id='atDiv_3_8', at[8].divRPT[3] Contents 내용 = [SECL] LP Ethylene] 3.Weight summary] 22 [KB]
div id='atDiv_4_8', at[8].divRPT[4] Contents 내용 = [SECL] LP Ethylene] 4.Weld Metal] 0 [KB]
div id='atDiv_8_8', at[8].divRPT[8] Contents 내용 = [SECL] LP Ethylene] 8.Roof Structure] 0 [KB]
div id='atDiv_2_10', at[10].divRPT[2] Contents 내용 = [SECL] LP Ethylene] 2.강도계산서] 39 [KB]
div id='atDiv_3_10', at[10].divRPT[3] Contents 내용 = [SECL] LP Ethylene] 3.Weight summary] 40 [KB]
div id='atDiv_4_10', at[10].divRPT[4] Contents 내용 = [SECL] LP Ethylene] 4.Weld Metal] 41 [KB]
div id='atDiv_8_10', at[10].divRPT[8] Contents 내용 = [SECL] LP Ethylene] 8.Roof Structure] 0 [KB]
div id='atDiv_2_12', at[12].divRPT[2] Contents 내용 = 한화-대산 LPG] 2.강도계산서] 43 [KB]
div id='atDiv_3_12', at[12].divRPT[3] Contents 내용 = 한화-대산 LPG] 3.Weight summary] 23 [KB]
div id='atDiv_4_12', at[12].divRPT[4] Contents 내용 = 한화-대산 LPG] 4.Weld Metal] 0 [KB]
div id='atDiv_8_12', at[12].divRPT[8] Contents 내용 = 한화-대산 LPG] 8.Roof Structure] 0 [KB]
div id='atDiv_2_14', at[14].divRPT[2] Contents 내용 = 한화-대산 LPG] 2.강도계산서] 44 [KB]
div id='atDiv_3_14', at[14].divRPT[3] Contents 내용 = 한화-대산 LPG] 3.Weight summary] 39 [KB]
div id='atDiv_4_14', at[14].divRPT[4] Contents 내용 = 한화-대산 LPG] 4.Weld Metal] 42 [KB]
div id='atDiv_8_14', at[14].divRPT[8] Contents 내용 = 한화-대산 LPG] 8.Roof Structure] 0 [KB]
div id='atDiv_2_16', at[16].divRPT[2] Contents 내용 = T-201 SUMBAWA 50000 KL LNG] 2.강도계산서] 33 [KB]
div id='atDiv_3_16', at[16].divRPT[3] Contents 내용 = T-201 SUMBAWA 50000 KL LNG] 3.Weight summary] 19 [KB]
div id='atDiv_4_16', at[16].divRPT[4] Contents 내용 = T-201 SUMBAWA 50000 KL LNG] 4.Weld Metal] 0 [KB]
div id='atDiv_8_16', at[16].divRPT[8] Contents 내용 = T-201 SUMBAWA 50000 KL LNG] 8.Roof Structure] 0 [KB]
div id='atDiv_2_18', at[18].divRPT[2] Contents 내용 = T-201 SUMBAWA 50000 KL LNG] 2.강도계산서] 34 [KB]
div id='atDiv_3_18', at[18].divRPT[3] Contents 내용 = T-201 SUMBAWA 50000 KL LNG] 3.Weight summary] 36 [KB]
div id='atDiv_4_18', at[18].divRPT[4] Contents 내용 = T-201 SUMBAWA 50000 KL LNG] 4.Weld Metal] 34 [KB]
div id='atDiv_8_18', at[18].divRPT[8] Contents 내용 = T-201 SUMBAWA 50000 KL LNG] 8.Roof Structure] 0 [KB]
div id='atDiv_2_20', at[20].divRPT[2] Contents 내용 = [T201] CAP2 LP Ethylene] 2.강도계산서] 32 [KB]
div id='atDiv_3_20', at[20].divRPT[3] Contents 내용 = [T201] CAP2 LP Ethylene] 3.Weight summary] 18 [KB]
div id='atDiv_4_20', at[20].divRPT[4] Contents 내용 = [T201] CAP2 LP Ethylene] 4.Weld Metal] 0 [KB]
div id='atDiv_8_20', at[20].divRPT[8] Contents 내용 = [T201] CAP2 LP Ethylene] 8.Roof Structure] 0 [KB]
div id='atDiv_2_22', at[22].divRPT[2] Contents 내용 = [T201] CAP2 LP Ethylene] 2.강도계산서] 33 [KB]
div id='atDiv_3_22', at[22].divRPT[3] Contents 내용 = [T201] CAP2 LP Ethylene] 3.Weight summary] 36 [KB]
div id='atDiv_4_22', at[22].divRPT[4] Contents 내용 = [T201] CAP2 LP Ethylene] 4.Weld Metal] 32 [KB]
div id='atDiv_8_22', at[22].divRPT[8] Contents 내용 = [T201] CAP2 LP Ethylene] 8.Roof Structure] 0 [KB]
div id='atDiv_2_24', at[24].divRPT[2] Contents 내용 = [301] CAP2 Propane(C3/C4)] 2.강도계산서] 36 [KB]
div id='atDiv_3_24', at[24].divRPT[3] Contents 내용 = [301] CAP2 Propane(C3/C4)] 3.Weight summary] 21 [KB]
div id='atDiv_4_24', at[24].divRPT[4] Contents 내용 = [301] CAP2 Propane(C3/C4)] 4.Weld Metal] 0 [KB]
div id='atDiv_8_24', at[24].divRPT[8] Contents 내용 = [301] CAP2 Propane(C3/C4)] 8.Roof Structure] 0 [KB]
div id='atDiv_2_26', at[26].divRPT[2] Contents 내용 = [301] CAP2 Propane(C3/C4)] 2.강도계산서] 38 [KB]
div id='atDiv_3_26', at[26].divRPT[3] Contents 내용 = [301] CAP2 Propane(C3/C4)] 3.Weight summary] 38 [KB]
div id='atDiv_4_26', at[26].divRPT[4] Contents 내용 = [301] CAP2 Propane(C3/C4)] 4.Weld Metal] 38 [KB]
div id='atDiv_8_26', at[26].divRPT[8] Contents 내용 = [301] CAP2 Propane(C3/C4)] 8.Roof Structure] 0 [KB]
myBuf[3] END = SKS_MAKE_JAVASCRIPT() (hidden div = 'fromSaveBase64' / div = 'atDiv_j_i' )

[ GA 이미지 업로드 ] myBuf[0] START = SKS_MAKE_JAVASCRIPT() 이미지 업로드 [iframe + pgBar + form] 및 Display iframe name='myFrame'

1. myPgBar[0]	0 %	imgName.png
2. myPgBar[1]	0 %	imgName.png

imgFile	File Size (Byte)	pid = fileSize= Description
imgRoof 1
imgRoof 2
imgRoof 3
imgRoof 4
imgRoof 5
imgRoof 6
imgRoof 7
imgRoof 8
imgRoof 9
imgRoof 10
imgRoof 11
imgRoof 12
imgRoof 13
imgRoof 14
imgShell 1
imgShell 2
imgShell 3
imgShell 4
imgShell 5
imgShell 6
imgShell 7
imgShell 8
imgShell 9
imgShell 10
imgShell 11
imgShell 12
imgShell 13
imgShell 14
imgSpect 1	0 1 2 3 4
imgSpect 2	0 1 2 3 4
imgSpect 3	0 1 2 3 4
imgSpect 4	0 1 2 3 4
imgSpect 5	0 1 2 3 4
imgSpect 6	0 1 2 3 4
imgSpect 7	0 1 2 3 4
imgSpect 8	0 1 2 3 4
imgSpect 9	0 1 2 3 4
imgSpect 10	0 1 2 3 4
imgSpect 11	0 1 2 3 4
imgSpect 12	0 1 2 3 4
imgSpect 13	0 1 2 3 4
imgSpect 14	0 1 2 3 4

[New : divXhr (이미지 업로드 결과!!! 중요!!), old : iframe [

dbgTextArea :
]
myBuf[0] END = SKS_MAKE_JAVASCRIPT() 이미지 업로드 [iframe + pgBar + form]

myBuf[1] START = SKS_MAKE_JAVASCRIPT() CANVAS [SHELL / SEISMIC SPECT / GA 그림] 그리기 CANVAS 모듈 : example2.js + ROOF_STRU_Module.js
GA CANVAS SHOW/HIDE 폰트 SIZE : (10~16) DEBUG!! GA_DRAW_AND_SEISMIC_DRAW() div canvasRoof Start = [[[]]]] div canvasRoof close !!!
myBuf[1] END = SKS_MAKE_JAVASCRIPT() CANVAS [SHELL / SEISMIC SPECT / GA 그림] 그리기 CANVAS 모듈 : example2.js + ROOF_STRU_Module.js
Date : 2025-08-04 23:06:38.0877 ~ 2025-08-04 23:06:38.0877
TEST OF SAVE_LOCAL_STORAGE()

// CANVAS 이미지 그리기 예제 	https://itrooms.tistory.com/213  
// 로칼스토리지 사용 방법 		https://www.daleseo.com/js-web-storage/

이 파일의 총 크기는 [
] 입니다.

시작시간 = [2025-08-04 23:06:38.0877]
종료시간 = [2025-08-04 23:06:40.0853]

현재 커넥션 풀 수량 [1]개 입니다.
1 conn.getAutoCommit() Check!!! = [true]
2 conn.getAutoCommit() Check!!! = [true]

HTML END!!!

S-Tank Engineering	TANK STRENGTH CALCULATION	Page	[$CP] / [$TP]
		[AAA1]	[AAA2]
	Doc. No. : [AAA3]	Rev. No.	[AAA4]

	Sd : Allowable stress for Design Condition	Sd = Min( Fy x 2/3, Ft x 2/5)	API 650 5.6.2.1
	St : Allowable stress for Hydrostatic-test Condition	St = Min( Fy x 3/4, Ft x 3/7)	API 650 5.6.2.2

Shell Course No.	Material	Fy (MPa)	Ft (MPa)	Sd (MPa)	St (MPa)
#3 ~ #12	A516-70	485.0	260.0	173.0	195.0
#1 ~ #2	A537-CL2	550.0	415.0	220.0	236.0

S-Tank Engineering	TANK STRENGTH CALCULATION	Page	[$CP] / [$TP]
		[AAA1]	[AAA2]
	Doc. No. : [AAA3]	Rev. No.	[AAA4]

Design Condition : D=60.000 (m), H=23.000 (m), SG=1.0, Pg=2.4517 (kPa) HTL : Height from the bottom of the course under consideration to the top of the shell including the top angle. (m) TOP Angle(HT) = DLL = HTL = 23.000 (m) as per API 650 Design CODE API 650, CRT, OUTER, Pg= 2.452 (kPa) = 250 (mmWTR) 주의 : ( ) 내 두께 수치(붉은색)는 위험물안전관리 기준으로 계산된 두께 임 허용응력 : 항복강도의 60%, S = 0.6×Fy = 0.6×415 = 249 MPa												Tank D(m)=	60	H(m)=	23	DLL(m)=	21.44	Shutdown and Construction Condition [ 내부압력 없는 조건 Pd: 0.0 MPa ], T1s(ShutDown) = Max. Compression (-값) 압축 1) Roof Dead Load Wr = [0.0] Ton 2) Roof Live Load LL = [339.292] Ton = Max( LL, Vacuum, SnowLoad ) 120 kg/m²× At (2827.433)m²= [339.292] Ton Total Load : (1)+(2) Wsum = [339.292] Ton Note 1) : 탱크내부에 진공압력( Vacuum Pressure 0.005 MPa)이 걸렸을 경우에는 나중에 추가 예정 2022.07.15
Shell No. [n]	Material	W[i] (m)	Hd (m)	Ht (m)	Sd (MPa)	St (MPa)	ONE-FOOT td (mm)	ONE-FOOT tt (mm)	Used Thk. tu =Max(td,tt , tMin) (mm)	Weight (Ton)	Remark tu(input) (mm)	SKETCH	Each Wtr[n] (mm)	∑Wtr[1~n] 누적(mm)	Remark	tc =tu-CA (mm)	Ratio t / R	누적중량 Stacked Weight W (Ton)	Shell 단면적 Sectional Area A[n] (mm²)	T1=R/2× (P-W/A) (N/mm)	T2=P×R (N/mm)	Sc = T1/tc 수직응력 (-압축,+인장) (MPa)	St = T2/tc 원주막응력 (-압축,+인장) (MPa)	Sts (MPa)	Factor N =St/Sts	Factor M Fact(N)	Scs (MPa)	Sca = M×Scs (MPa)	Stress ratio SRc = Sc/Sca SRt = St/Sts SRtc < 1.0 OK	1. ASME D.1 Sca = M×0.0625×E×tPr (MPa), E = 204,000 (MPa) 2. EN_1993 Sca = 0.0605 × E × Cx(1.0) × tPr (MPa) 3. JIS_LNG Sca = (0.25/γ1=2.25)×E×tPr (MPa) Long-Term 4. JIS_LNG Sca = (0.25/γ2=1.50)×E×tPr (MPa) Short-Term
12	A516-70	1.000	1.250	1.250	173 (156)	195 (195)	8.0 (8.0)	8.0 (8.0)	8.00 (＋0.0)	11.840	8.0 (8.0)	dbgCanvas_650 shCanvas_650 [CANVAS SHOW]	1,000	2,726		5.0	0.000167	351.132	942478	(-) 18.268	367.749	-3.654	73.550	147.050	0.5002	0.6512	2.068	1.347	2.713 > 1.0 NG	ASME= 1.384, EN1993= 2.057, JIS(L)= 3.778, JIS(S)= 5.667
11	A516-70	2.000	3.250	3.250	173 (156)	195 (195)	8.506 (8.562)	8.0 (8.0)	9.50 (＋0.99)	28.112	9.5 (8.5)		1,038	1,726		6.5	0.000217	379.244	1225221	(-) 19.731	956.149	-3.035	147.100	147.050	1.0003	-0.0006	2.689	-0.002	-1881.407 > 1.0 NG	ASME= -0.002, EN1993= 2.674, JIS(L)= 4.911, JIS(S)= 7.367
10	A516-70	2.000	5.250	5.250	173 (156)	195 (195)	12.232 (12.333)	8.78 (8.784)	13.50 (＋1.27)	39.952	13.5 (12.5)		313	688		10.5	0.000350	419.196	1979203	(-) 21.809	1544.548	-2.077	147.100	147.050	1.0003	-0.0006	4.344	-0.003	-796.960 > 1.0 NG	ASME= -0.003, EN1993= 4.32, JIS(L)= 7.933, JIS(S)= 11.9
9	A516-70	2.000	7.250	7.250	173 (156)	195 (195)	16.097 (16.103)	12.328 (12.333)	17.50 (＋1.4)	51.808	17.5 (16.0)		140	375		14.5	0.000483	471.004	2733186	(-) 24.504	2132.947	-1.690	147.100	147.050	1.0003	-0.0006	5.998	-0.004	-469.558 > 1.0 NG	ASME= -0.004, EN1993= 5.965, JIS(L)= 10.956, JIS(S)= 16.433
8	A516-70	2.000	9.250	9.250	173 (156)	195 (195)	19.985 (19.874)	15.875 (15.881)	21.50 (＋1.51)	63.648	21.5 (20.0)		76	235		18.5	0.000617	534.652	3487168	(-) 27.816	2721.346	-1.504	147.100	147.050	1.0003	-0.0006	7.653	-0.005	-327.435 > 1.0 NG	ASME= -0.005, EN1993= 7.611, JIS(L)= 13.978, JIS(S)= 20.967
7	A516-70	2.000	11.250	11.250	173 (156)	195 (195)	23.891 (23.645)	19.423 (19.43)	25.50 (＋1.61)	75.488	25.5 (24.0)		47	159		22.5	0.000750	610.140	4241150	(-) 31.743	3309.745	-1.411	147.100	147.050	1.0003	-0.0006	9.308	-0.006	-252.618 > 1.0 NG	ASME= -0.006, EN1993= 9.257, JIS(L)= 17, JIS(S)= 25.5
6	A516-70	2.000	13.250	13.250	173 (156)	195 (195)	27.778 (27.416)	22.97 (22.979)	29.50 (＋1.72)	87.344	29.5 (27.5)		31	112		26.5	0.000883	697.484	4995132	(-) 36.287	3898.144	-1.369	147.100	147.050	1.0003	-0.0006	10.963	-0.007	-208.180 > 1.0 NG	ASME= -0.007, EN1993= 10.902, JIS(L)= 20.022, JIS(S)= 30.033
5	A516-70	2.000	15.250	15.250	173 (156)	195 (195)	31.817 (31.186)	26.518 (26.528)	33.50 (＋1.68)	99.184	33.5 (31.5)		22	81		30.5	0.001017	796.668	5749115	(-) 41.447	4486.543	-1.359	147.100	147.050	1.0003	-0.0006	12.617	-0.008	-179.505 > 1.0 NG	ASME= -0.008, EN1993= 12.548, JIS(L)= 23.044, JIS(S)= 34.567
4	A516-70	2.000	17.250	17.250	173 (156)	195 (195)	35.095 (34.957)	30.065 (30.077)	37.50 (＋2.4)	111.040	37.5 (35.0)		16	59		34.5	0.001150	907.708	6503097	(-) 47.224	5074.942	-1.369	147.100	147.050	1.0003	-0.0006	14.272	-0.009	-159.848 > 1.0 NG	ASME= -0.009, EN1993= 14.193, JIS(L)= 26.067, JIS(S)= 39.1
3	A516-70	2.000	19.250	19.250	173 (156)	195 (195)	34.697 (38.728)	33.613 (33.626)	(최대두께 확인) 47.50 (t<45 초과)	140.672	41.5 (39.0)		12	43		44.5	0.001483	1048.380	8388052	(-) 54.543	5663.342	-1.226	127.266	147.050	0.8655	0.2292	18.409	4.219	0.290 < 1.0 OK	ASME= 4.335, EN1993= 18.307, JIS(L)= 33.622, JIS(S)= 50.433
2	A537-CL2	2.000	21.250	21.250	220 (249)	236 (236)	34.697 (27.746)	30.704 (30.717)	36.50 (＋1.8)	108.080	36.5 (28.0)		17	31		33.5	0.001117	1156.460	6314601	(-) 60.166	6251.741	-1.796	186.619	187.000	0.9980	0.0040	13.858	0.055	32.399 > 1.0 NG	ASME= 0.057, EN1993= 13.782, JIS(L)= 25.311, JIS(S)= 37.967
1	A537-CL2	2.000	23.250	23.250	220 (249)	236 (236)	39.082 (34.988)	33.636 (39.706)	39.50 (＋0.42)	116.960	39.5 (35.0)		14	14		36.5	0.001217	1273.420	6880088	(-) 66.251	6840.140	-1.815	187.401	187.000	1.0021	-0.0042	15.100	-0.063	-28.621 > 1.0 NG	ASME= -0.065, EN1993= 15.016, JIS(L)= 27.578, JIS(S)= 41.367
∑W, Hd, Ht(m)=		23.000	23.250	23.250	Total Net Weight, NetWt =					934.128	Ton		∑Wtr=	2.726	(m)
			Total Gross Weight, GrsWt =							969.756	Ton
			Equivalent Shell Nominal Thickness (평균두께 부식전)							26.623	mm	Without CA
			Equivalent Shell Corroded Thickness (평균두께 부식후)							23.623	mm	With CA
			Shell Gravity Center from Bottom,(PV Hanbook : 434 Page) Xs = (Aa+Ba+Ca...Z) / (A+B+C..Z) =8.861 [m]							8.861	m

Where,

	Tank In-Diameter	D =	60.000	m
	Weld Joint Efficiency	E =	0.85
	Design Specific Gravity	G =	1.0
	Liquid Density (Design)	p =	1000	kg/m³
	Corrosion Allowance	CA =	3.0	mm
	Design Internal Pressure, Pg = 250.0 (mmWTR)	Pg =	250	mmWTR
	Additional Pressure at Hydrostatic-test, Pg/G = 250.0 (mmWTR)	Pg/G =	250	mmWTR
	Design Liquid Level (m)	DLL =	21.440	m
	Hydrostatic-test Liquid Level (m)	HLL =	23.000	m
	Design Liquid Depth of each shell welding point(mm) : Hd[0] = DLL + Pg/G	Hd =	Aboble Table	m
	Test Liquid Depth of each shell welding point(mm) : Ht[0] = HTL + Pg	Hd =	Aboble Table	m
	Height of each shell	W(i) =	Above Table	m
	Shell plate average thickness, tAvg = twt / (π×D×HT×7.85) tAvg = 934.128 / (π×60×23×7.85 )	tAvg =	26.623	mm
	Shell 무게중심위치 from Bottom	Xs =	8.861	m

API 650 3.4.2 and Annex K.2.2.1 Design Condition
tpd = 4.9 × D × (H - 0.3) × SG/(Sd×E) + CA = 39.082 mm	tpd =	39.082	mm
t1d = (1.06 - (0.0696 × D/H) × (HG/Sd)^0.5) × (4.9HDG/Sd)+CA = 39.432 mm	t1d =	39.432	mm
Lesser of tpd & t1d = Min( tpd, t1d ) = Min( 39.082, 39.432 ) = 39.082 mm	Min(tpd,t1d)=	39.082	mm
API 650 3.4.2 and Annex K.2.2.2 Hydrostatic Test Condition
tpt = 4.9 × D × (H - 0.3) / St×E = 33.636 mm	tpt =	33.636	mm
t1t = (1.06 - (0.0696 × D/H) × (H/StE)^0.5) × (4.9HD/StE) = 34.036 mm	t1t =	34.036	mm
Lesser of tpt & t1t = Min( tpt, t1t ) = Min( 33.636, 34.036 ) = 33.636 mm	Min(tpt,t1t)=	33.636	mm
Check L / H ≤ 1000/6 then OK L / H = (44.75) ≤ 166 OK.	44.75 ≤ 166 OK.
Where, L = (500 × D × t)^0.5 = 1040.41 m	L =	1040.41	m
H = 23.250 mm	H =	23.250	m
L / H = 44.749	L/H =	44.749
Corroded Thickness of 1st Shell Cource, tL = t1 = (t1d - CA) = 39.432 - 3.0	tL =	36.082	mm
Therefore, 1st Bottom Shell course Thickness ( CA 포함 사용두께 )	tUsed =	39.5	mm

Trial No.	Used Thk. tU (mm)	tL=t1 (mm)	K=tL/tU	C	x1 (mm)	x2 (mm)	x3 (mm)	x = Min(x1..x3) (mm)	Z = h1/√(r×t1) 1.375 < Z < 2.625	t2a (mm)	td[2]-CA (mm)	tdx[2]+CA VDPM Used(mm)		Used Thk tu (mm)	Used tu - VDPM(mm)
1	32.937	36.500	1.108	0.053	964.04	1117.75	1212.73	964.04	1.911	31.893	31.893
2	31.893	36.500	1.144	0.070	1069.28	1476.88	1193.35	1069.28	1.911	31.728	31.728
3	31.728	36.500	1.150	0.072	1086.09	1534.25	1190.26	1086.09	1.911	31.702	31.702
4	31.702	36.500	1.151	0.073	1088.57	1542.75	1189.77	1088.57	1.911	31.698	31.698
5	31.698	36.500	1.152	0.073	1089.21	1544.88	1189.70	1089.21	1.911	31.697	31.697
6	31.697	36.500	1.152	0.073	1089.20	1544.88	1189.68	1089.20	1.911	31.697	31.697	34.70 (1.366 in)	<	36.50	1.80

Trial No.	Used Thk. tU (mm)	tL=t2 (mm)	K=tL/tU	C	x1 (mm)	x2 (mm)	x3 (mm)	x = Min(x1..x3) (mm)	B L A N K	tdx[3] (mm)	td[3]-CA (mm)	tdx[3]+CA VDPM Used(mm)		Used Thk tu (mm)	Used tu - VDPM(mm)
1	37.887	31.697	0.837	-0.085	128.58	-1630.47	1300.67	-1630.47		41.747	41.747
2	41.747	31.697	0.759	-0.126	-94.73	-2429.35	1365.32	-2429.35		43.344	43.344
3	43.344	31.697	0.731	-0.141	-175.43	-2721.95	1391.19	-2721.95		43.929	43.929
4	43.929	31.697	0.722	-0.147	-202.79	-2822.05	1400.54	-2822.05		44.129	44.129
5	44.129	31.697	0.718	-0.148	-212.28	-2856.70	1403.73	-2856.70		44.198	44.198	34.70 (1.366 in)	<	41.50	6.80

Trial No.	Used Thk. tU (mm)	tL=t3 (mm)	K=tL/tU	C	x1 (mm)	x2 (mm)	x3 (mm)	x = Min(x1..x3) (mm)	B L A N K	tdx[4] (mm)	td[4]-CA (mm)	tdx[4]+CA VDPM Used(mm)		Used Thk tu (mm)	Used tu - VDPM(mm)
1	33.888	44.198	1.304	0.140	1385.65	2408.10	1230.11	1230.11		32.029	32.029
2	32.029	44.198	1.380	0.170	1538.00	2937.68	1195.89	1195.89		32.097	32.097
3	32.097	44.198	1.377	0.169	1532.01	2916.98	1197.16	1197.16		32.095	32.095
4	32.095	44.198	1.377	0.169	1532.55	2918.70	1197.12	1197.12		32.095	32.095	35.10 (1.382 in)	<	37.50	2.41

Trial No.	Used Thk. tU (mm)	tL=t4 (mm)	K=tL/tU	C	x1 (mm)	x2 (mm)	x3 (mm)	x = Min(x1..x3) (mm)	B L A N K	tdx[5] (mm)	td[5]-CA (mm)	tdx[5]+CA VDPM Used(mm)		Used Thk tu (mm)	Used tu - VDPM(mm)
1	29.890	32.095	1.074	0.036	754.29	552.05	1155.27	552.05		29.386	29.386
2	29.386	32.095	1.092	0.045	792.34	686.25	1145.49	686.25		29.118	29.118
3	29.118	32.095	1.102	0.050	812.66	757.93	1140.25	757.93		28.974	28.974
4	28.974	32.095	1.108	0.052	823.94	797.58	1137.43	797.58		28.895	28.895
5	28.895	32.095	1.111	0.054	830.00	818.93	1135.88	818.93		28.852	28.852
6	28.852	32.095	1.112	0.054	833.48	831.13	1135.03	831.13		28.828	28.828
7	28.828	32.095	1.113	0.055	835.68	838.75	1134.56	835.68		28.819	28.819
8	28.819	32.095	1.114	0.055	836.57	841.80	1134.38	836.57		28.817	28.817
9	28.817	32.095	1.114	0.055	836.55	841.80	1134.34	836.55		28.817	28.817	31.82 (1.253 in)	<	33.50	1.68

Trial No.	Used Thk. tU (mm)	tL=t5 (mm)	K=tL/tU	C	x1 (mm)	x2 (mm)	x3 (mm)	x = Min(x1..x3) (mm)	B L A N K	tdx[6] (mm)	td[6]-CA (mm)	tdx[6]+CA VDPM Used(mm)		Used Thk tu (mm)	Used tu - VDPM(mm)
1	25.891	28.817	1.113	0.055	769.96	726.10	1075.21	726.10		25.039	25.039
2	25.039	28.817	1.151	0.072	835.66	959.30	1057.37	835.66		24.820	24.820
3	24.820	28.817	1.161	0.077	853.27	1021.58	1052.74	853.27		24.785	24.785
4	24.785	28.817	1.163	0.078	855.87	1030.85	1052.00	855.87		24.780	24.780
5	24.780	28.817	1.163	0.078	856.24	1032.18	1051.89	856.24		24.779	24.779
6	24.779	28.817	1.163	0.078	856.66	1033.50	1051.87	856.66		24.778	24.778
7	24.778	28.817	1.163	0.078	856.64	1033.50	1051.85	856.64		24.778	24.778	27.78 (1.094 in)	<	29.50	1.72

Trial No.	Used Thk. tU (mm)	tL=t6 (mm)	K=tL/tU	C	x1 (mm)	x2 (mm)	x3 (mm)	x = Min(x1..x3) (mm)	B L A N K	tdx[7] (mm)	td[7]-CA (mm)	tdx[7]+CA VDPM Used(mm)		Used Thk tu (mm)	Used tu - VDPM(mm)
1	21.893	24.778	1.132	0.064	723.32	715.50	988.72	715.50		21.062	21.062
2	21.062	24.778	1.176	0.084	787.65	946.12	969.77	787.65		20.918	20.918
3	20.918	24.778	1.184	0.088	798.95	986.63	966.45	798.95		20.895	20.895
4	20.895	24.778	1.186	0.088	800.84	993.38	965.92	800.84		20.891	20.891
5	20.891	24.778	1.186	0.088	801.15	994.50	965.83	801.15		20.891	20.891	23.89 (0.941 in)	<	25.50	1.61

Trial No.	Used Thk. tU (mm)	tL=t7 (mm)	K=tL/tU	C	x1 (mm)	x2 (mm)	x3 (mm)	x = Min(x1..x3) (mm)	B L A N K	tdx[8] (mm)	td[8]-CA (mm)	tdx[8]+CA VDPM Used(mm)		Used Thk tu (mm)	Used tu - VDPM(mm)
1	17.894	20.891	1.168	0.080	683.73	740.00	893.87	683.73		17.127	17.127
2	17.127	20.891	1.220	0.103	743.32	956.45	874.50	743.32		17.008	17.008
3	17.008	20.891	1.228	0.107	753.04	991.60	871.46	753.04		16.988	16.988
4	16.988	20.891	1.230	0.108	754.56	997.15	870.95	754.56		16.985	16.985
5	16.985	20.891	1.230	0.108	754.82	998.08	870.87	754.82		16.985	16.985	19.98 (0.787 in)	<	21.50	1.52

Trial No.	Used Thk. tU (mm)	tL=t8 (mm)	K=tL/tU	C	x1 (mm)	x2 (mm)	x3 (mm)	x = Min(x1..x3) (mm)	B L A N K	tdx[9] (mm)	td[9]-CA (mm)	tdx[9]+CA VDPM Used(mm)		Used Thk tu (mm)	Used tu - VDPM(mm)
1	13.895	16.985	1.222	0.105	636.51	758.35	787.68	636.51		13.222	13.222
2	13.222	16.985	1.285	0.131	688.80	951.93	768.37	688.80		13.118	13.118
3	13.118	16.985	1.295	0.136	697.26	983.10	765.34	697.26		13.101	13.101
4	13.101	16.985	1.296	0.136	698.64	988.18	764.84	698.64		13.098	13.098
5	13.098	16.985	1.297	0.136	699.06	989.63	764.76	699.06		13.097	13.097
6	13.097	16.985	1.297	0.136	699.04	989.63	764.73	699.04		13.097	13.097	16.10 (0.634 in)	<	17.50	1.40

Trial No.	Used Thk. tU (mm)	tL=t9 (mm)	K=tL/tU	C	x1 (mm)	x2 (mm)	x3 (mm)	x = Min(x1..x3) (mm)	B L A N K	tdx[10] (mm)	td[10]-CA (mm)	tdx[10]+CA VDPM Used(mm)		Used Thk tu (mm)	Used tu - VDPM(mm)
1	9.897	13.097	1.323	0.148	580.19	774.38	664.77	580.19		9.336	9.336
2	9.336	13.097	1.403	0.179	624.05	941.33	645.66	624.05		9.249	9.249
3	9.249	13.097	1.416	0.184	631.11	968.10	642.64	631.11		9.235	9.235
4	9.235	13.097	1.418	0.185	632.21	972.30	642.15	632.21		9.232	9.232
5	9.232	13.097	1.419	0.185	632.50	973.35	642.05	632.50		9.232	9.232	12.23 (0.482 in)	<	13.50	1.27

Trial No.	Used Thk. tU (mm)	tL=t10 (mm)	K=tL/tU	C	x1 (mm)	x2 (mm)	x3 (mm)	x = Min(x1..x3) (mm)	B L A N K	tdx[11] (mm)	td[11]-CA (mm)	tdx[11]+CA VDPM Used(mm)		Used Thk tu (mm)	Used tu - VDPM(mm)
1	5.898	9.232	1.565	0.239	505.26	777.08	513.18	505.26		5.488	5.488
2	5.488	9.232	1.682	0.278	536.74	903.83	495.03	495.03		5.508	5.508
3	5.508	9.232	1.676	0.276	535.11	897.33	495.93	495.93		5.506	5.506
4	5.506	9.232	1.677	0.276	535.27	897.98	495.84	495.84		5.506	5.506	8.51 (0.335 in)	<	9.50	0.99

Trial No.	Used Thk. tU (mm)	tL=t11 (mm)	K=tL/tU	C	x1 (mm)	x2 (mm)	x3 (mm)	x = Min(x1..x3) (mm)	B L A N K	tdx[12] (mm)	td[12]-CA (mm)	tdx[12]+CA VDPM Used(mm)		Used Thk tu (mm)	Used tu - VDPM(mm)
1	1.899	5.506	2.899	0.545	363.52	681.00	291.19	291.19		1.917	1.917
2	1.917	5.506	2.872	0.541	362.57	675.87	292.57	292.57		1.914	1.914
3	1.914	5.506	2.877	0.541	362.73	676.75	292.34	292.34		1.915	1.915
4	1.915	5.506	2.875	0.541	362.69	676.50	292.42	292.42		1.915	1.915	4.92 (0.194 in)	<	8.00	3.08

1. [OUTER TANK] Shell Plate
Net Weight (설계중량)							Gross Weight (자재구매 중량)							자재구매가격 Shell Plate Purchsing Price					Remark
Shell Course No.	Material	Thk. (mm)	Width (mm)	Length (mm)	Qty (SHT)	Net WT (Ton)	Shell Course No.	Material	Thk. (mm)	Width (mm)	Length (mm)	Qty (SHT)	Gross WT (Ton)	Loss Grs/net Ratio(%)	수입 자재단가 (USD/Ton)	수입 자재금액 (USD)	내수 자재단가 (천원/Ton)	내수 자재금액 (천원)	Remark
12 th Shell Plate	A516-70	8.0	1000	11782	16	11.840	12	A516-70	8.0	1050	11830	17	13.260	11.99	1,284.17	17,028	1,541.00	20,434	Stiff and jig 부착 PAD PLATE 1 Sheet 포함
11 th Shell Plate	A516-70	9.0	2000	11782	16	26.640	11	A516-70	9.0	2050	11830	16	27.408	2.88	1,284.17	35,197	1,541.00	42,236
10 th Shell Plate	A516-70	13.0	2000	11783	16	38.480	10	A516-70	13.0	2050	11830	16	39.600	2.91	1,284.17	50,853	1,541.00	61,024
9 th Shell Plate	A516-70	16.5	2000	11784	16	48.848	9	A516-70	16.5	2050	11830	16	50.256	2.88	1,284.17	64,537	1,541.00	77,444
8 th Shell Plate	A516-70	20.5	2000	11785	16	60.688	8	A516-70	20.5	2050	11830	16	62.448	2.9	1,284.17	80,194	1,541.00	96,232
7 th Shell Plate	A516-70	24.5	2000	11785	16	72.528	7	A516-70	24.5	2050	11830	16	74.624	2.89	1,284.17	95,830	1,541.00	114,996
6 th Shell Plate	A516-70	28.5	2000	11786	16	84.384	6	A516-70	28.5	2050	11830	16	86.816	2.88	1,284.17	111,486	1,541.00	133,783
5 th Shell Plate	A516-70	32.5	2000	11787	16	96.224	5	A516-70	32.5	2050	11830	16	98.992	2.88	1,284.17	127,123	1,541.00	152,547
4 th Shell Plate	A516-70	35.5	2000	11788	16	105.120	4	A516-70	35.5	2050	11830	16	108.128	2.86	1,284.17	138,855	1,541.00	166,625
3 rd Shell Plate	A516-70	47.5	2000	11790	16	140.672	3	A516-70	47.5	2050	11840	16	144.800	2.93	1,284.17	185,948	1,541.00	223,137
2 nd Shell Plate	A537-CL2	35.0	2000	11788	16	103.648	2	A537-CL2	35.0	2050	11830	16	106.608	2.86	1,541.67	164,354	1,850.00	197,225
1 st Shell Plate	A537-CL2	39.5	2000	11788	16	116.960	1	A537-CL2	39.5	2050	11830	17	127.840	9.3	1,541.67	197,087	1,850.00	236,504	1st Shell Nozzzle and Openning PAD PLATE 1 Sheet 포함
[OUTER TANK] Shell Plate Total =					192	906.032	Total Qty and Weight =					194	940.780	3.84	1,348.34	1,268,492	1,618.00	1,522,186	(천원)
Shell 재질이 2개 일 경우 재질별 합계표
Part Name	Material	Shell Course No.			Qty (SHT)	Net WT (Ton)	Thickness Range (mm)			Width (mm)	Length (mm)	Qty (SHT)	Gross WT (Ton)	Loss Grs/net Ratio(%)	수입 자재단가 (USD/Ton)	수입 자재금액 (USD)	내수 자재단가 (천원/Ton)	내수 자재금액 (천원)	Remark
2 nd Material	A516-70	#3 ~ #12			161	685.424	t 47.5 ~ 8.0			2050	11840	161	706.332	3.05	1284.17	907,050	1541.00	1,088,458	2nd Material (#3 ~ #12 top shell course)
1 st Material	A537-CL2	#1 ~ #2			33	220.608	t 39.5 ~ 35.0			2050	11830	33	234.448	6.27	1,541.67	361,441	1,850.00	433,729	Primary Material (#1 ~ #2 Shell course)
2. [OUTER TANK] Bottom / Annular / Roof Plate / Compression Ring / Stiffener Ring
Net Weight (설계중량)							Gross Weight (자재구매 중량)							자재구매가격 Shell Plate Purchsing Price					Remark
Part Name	Material	Shell Course No.			Qty (SHT)	Net WT (Ton)	Thickness Range (mm)			Width (mm)	Length (mm)	Qty (SHT)	Gross WT (Ton)	Loss Grs/net Ratio(%)	수입 자재단가 (USD/Ton)	수입 자재금액 (USD)	내수 자재단가 (천원/Ton)	내수 자재금액 (천원)	Remark
1. Bottom Plate	A283-C	9.5	2438	6096	175.50	194.470	1	A283-C	9.5	2438	6096	186	206.088	5.97	1,137.00	234,322	1,690.00	348,289
2. Annular Plate	A516-60	26.0	2438	6096	17.10	51.730	2	A516-60	26.0	2438	6096	20	60.660	17.26	1,300.00	78,858	1,690.00	102,515
3. Roof Plate	A516-60	5.4	2438	6096	198.20	124.890	3	A516-60	5.4	2438	6096	213	134.190	7.45	1,300.00	174,447	1,690.00	226,781
4. Comp. Ring	A516-60	103.0	1400	4597	41.00	209.588	4	A516-60	103.0	1550	4747	43	255.807	22.05	1,300.00	332,549	1,690.00	432,314
6. Stiffener Ring	A283-C	L150x15		188.0 (m)	1 Rings	6.684	6	A283-C	ref.	역계산	역계산	1	7.687	15.01	5,090.00	39,127	6,108.00	46,952
[OUTER TANK] Bottom / Annular / Total =						587.362	Total Qty and Weight =						664.432			859,303	USD	1,156,851	(천원)
[OUTER TANK] Grand Total =						1493.394	Grand Total Qty and Weight =						1605.212			2,127,795	USD	2,679,038	(천원)

kid = 15	1	2	3	4	5	6	7	8	9	10	11	12	13	14	15	16	17	18	19	20	21	22	23	24	25
id	SIZE mm	H mm	B mm	t₁ mm	t₂ mm	r1 mm	r2 mm	A cm²	W Kg/m	Ix cm⁴	Iy cm⁴	rx cm	ry cm	Sx cm³	Sy cm³	ex cm	ey cm	Zx cm³	Zy cm³	Cw(비틀림) cm⁶x1000	J(뒤틀링) cm⁴	rts	λf=B/tf	λw=H-2tf/tw	L=5m/ry< 300 OK
15	H396X199X7X11	396	199	7	11	16		72.16	56.6	20000	1450	16.7	4.48	1010	145	19.8	9.95	1130	224	536000	27.1	5.25	9.05	53.43	L/r=60< 200 OK Limit: 33.4(M)
15	[CA=0] 적용 H396x199	396	199	7	11	16	0	72.16	56.6	20000	1450	16.7	4.48	1010	145	19.8	9.95	1130	224	536000	27.1	5.25	9.05	53.43	112

A. TK-001 (VPDM) TANK Net Weight (설계중량) 　　D= 60 (m), H= 23 (m)							Horizontal Weld (수평용접 : 2G) [자동:SAW or 수동:SMAW] [용착효율:SAW (95%) / 수동:SMAW (60%)]						Vertical Weld (수직용접) [ FCAW 용착효율: (90%) ]						합계중량	REMARK	[새창에서] A. TK-001 (VPDM) TANK 큰 이미지 로 보기 [새창에서] PDF 도면 보기 [새창에서] SHOP_WPS_PQR_SUMBAWA_50K PDF 보기
No.	Material	Thickness (mm)	Width (mm)	Length (mm)	Qty (SHT)	Weight (Ton)	Joint No.	수평용접 총길이 (m)	용입부 단면적 A(mm²)	용접봉 NET중량 (kg)	용착 효율 (%)	용접봉 발주예상 중량(kg)	Joint No.	shCirQty=[16] 수직용접 총길이 VL = 16 PCS × Each S.W(m)	용입부 단면적 A(mm²)	용접봉 NET중량 (kg)	용착 효율 (%)	용접봉 발주예상 중량(kg)	수평+수직 용접봉중량 (kg)	REMARK
12	A516-70 (Comp. Ring+Top Shell)	8.0	1000	11782	16	11.840	2G-H12	188	37.63	55.53	95	58.45	3G-V12	1m ×16= 16 m	-1.00	-0.13	90	-0.14	58.31
11	A516-70	9.5	2000	11782	16	28.112	2G-H11	188	-1.00	-1.48	95	-1.56	3G-V11	2m ×16= 32 m	-1.00	-0.25	90	-0.28	-1.84
10	A516-70	13.5	2000	11783	16	39.952	2G-H10	188	-1.00	-1.48	95	-1.56	3G-V10	2m ×16= 32 m	-1.00	-0.25	90	-0.28	-1.84
9	A516-70	17.5	2000	11784	16	51.808	2G-H9	188	-1.00	-1.48	95	-1.56	3G-V9	2m ×16= 32 m	-1.00	-0.25	90	-0.28	-1.84
8	A516-70	21.5	2000	11785	16	63.648	2G-H8	188	-1.00	-1.48	95	-1.56	3G-V8	2m ×16= 32 m	-1.00	-0.25	90	-0.28	-1.84
7	A516-70	25.5	2000	11785	16	75.488	2G-H7	188	-1.00	-1.48	95	-1.56	3G-V7	2m ×16= 32 m	-1.00	-0.25	90	-0.28	-1.84
6	A516-70	29.5	2000	11786	16	87.344	2G-H6	188	-1.00	-1.48	95	-1.56	3G-V6	2m ×16= 32 m	-1.00	-0.25	90	-0.28	-1.84
5	A516-70	33.5	2000	11787	16	99.184	2G-H5	188	-1.00	-1.48	95	-1.56	3G-V5	2m ×16= 32 m	-1.00	-0.25	90	-0.28	-1.84
4	A516-70	37.5	2000	11788	16	111.040	2G-H4	188	-1.00	-1.48	95	-1.56	3G-V4	2m ×16= 32 m	-1.00	-0.25	90	-0.28	-1.84
3	A516-70	47.5	2000	11790	16	140.672	2G-H3	188	-1.00	-1.48	95	-1.56	3G-V3	2m ×16= 32 m	-1.00	-0.25	90	-0.28	-1.84
2	A537-CL2	36.5	2000	11788	16	108.080	2G-H2	188	-1.00	-1.48	95	-1.56	3G-V2	2m ×16= 32 m	-1.00	-0.25	90	-0.28	-1.84
1	A537-CL2	39.5	2000	11788	16	116.960	2G-H1	188	-1.00	-1.48	98	-1.56	3G-V1	2m ×16= 32 m	-1.00	-0.25	90	-0.28	-1.84
A)	1st Shell + Annular Plate	t1st= 39.5 tAnn= 26	2000	11788	N/A	N/A	1F-An	188.0	382.26	564.14	60	940.23	-	-	-	-	-	-	-1.56
A. TK-001 (VPDM) TANK Total =					192	934.1	HLEN =	2444.0	408.89	603.39	98	981.52	VLEN =	368.000	-12.00	-2.88	90	-3.22	978.30

Design Condition : D=31.600 (m), H=15.200 (m), SG=1.0, Pg=2.4517 (kPa) HTL : Height from the bottom of the course under consideration to the top of the shell including the top angle. (m) TOP Angle(HT) = DLL = HTL = 15.200 (m) as per API 650 Design CODE API 650, DRT, OUTER, Pg= 2.452 (kPa) = 250 (mmWTR) 주의 : ( ) 내 두께 수치(붉은색)는 위험물안전관리 기준으로 계산된 두께 임 허용응력 : 항복강도의 60%, S = 0.6×Fy = 0.6×260 = 156 MPa												Tank D(m)=	31.6	H(m)=	15.2	DLL(m)=	15.2	Shutdown and Construction Condition [ 내부압력 없는 조건 Pd: 0.0 MPa ], T1s(ShutDown) = Max. Compression (-값) 압축 1) Roof Dead Load Wr = [0.0] Ton 2) Roof Live Load LL = [94.112] Ton = Max( LL, Vacuum, SnowLoad ) 120 kg/m²× At (784.267)m²= [94.112] Ton Total Load : (1)+(2) Wsum = [94.112] Ton Note 1) : 탱크내부에 진공압력( Vacuum Pressure 0.005 MPa)이 걸렸을 경우에는 나중에 추가 예정 2022.07.15
Shell No. [n]	Material	W[i] (m)	Hd (m)	Ht (m)	Sd (MPa)	St (MPa)	ONE-FOOT td (mm)	ONE-FOOT tt (mm)	Used Thk. tu =Max(td,tt , tMin) (mm)	Weight (Ton)	Remark tu(input) (mm)	SKETCH	Each Wtr[n] (mm)	∑Wtr[1~n] 누적(mm)	Remark	tc =tu-CA (mm)	Ratio t / R	누적중량 Stacked Weight W (Ton)	Shell 단면적 Sectional Area A[n] (mm²)	T1=R/2× (P-W/A) (N/mm)	T2=P×R (N/mm)	Sc = T1/tc 수직응력 (-압축,+인장) (MPa)	St = T2/tc 원주막응력 (-압축,+인장) (MPa)	Sts (MPa)	Factor N =St/Sts	Factor M Fact(N)	Scs (MPa)	Sca = M×Scs (MPa)	Stress ratio SRc = Sc/Sca SRt = St/Sts SRtc < 1.0 OK	1. ASME D.1 Sca = M×0.0625×E×tPr (MPa), E = 204,000 (MPa) 2. EN_1993 Sca = 0.0605 × E × Cx(1.0) × tPr (MPa) 3. JIS_LNG Sca = (0.25/γ1=2.25)×E×tPr (MPa) Long-Term 4. JIS_LNG Sca = (0.25/γ2=1.50)×E×tPr (MPa) Short-Term
7	A516-70	0.800	1.050	1.050	173 (156)	195 (195)	6.0 (6.0)	6.0 (6.0)	8.50 (＋2.5)	5.298	8.5 (6.0)	dbgCanvas_650 shCanvas_650 [CANVAS SHOW]	265	5,461		7.0	0.000443	99.410	694920	(-) 9.820	162.692	-1.403	23.242	173.000	0.1343	0.9261	5.498	5.092	0.276 < 1.0 OK	ASME= 5.231, EN1993= 5.468, JIS(L)= 10.042, JIS(S)= 15.063
6	A516-70	2.400	3.450	3.450	173 (156)	195 (195)	6.0 (6.0)	6.0 (6.0)	6.00 (＋0.0)	11.226	6.0 (6.0)		2,400	5,196		4.5	0.000285	110.636	446734	(-) 10.929	534.561	-2.429	118.791	173.000	0.6867	0.4606	3.535	1.628	1.492 > 1.0 NG	ASME= 1.673, EN1993= 3.515, JIS(L)= 6.456, JIS(S)= 9.684
5	A516-70	2.400	5.850	5.850	173 (156)	195 (195)	6.467 (7.011)	6.0 (6.0)	7.00 (＋0.53)	13.092	7.0 (7.0)		1,453	2,796		5.5	0.000348	123.728	546009	(-) 12.222	906.429	-2.222	164.805	173.000	0.9526	0.0889	4.320	0.384	5.786 > 1.0 NG	ASME= 0.395, EN1993= 4.296, JIS(L)= 7.89, JIS(S)= 11.835
4	A516-70	2.400	8.250	8.250	173 (156)	195 (195)	8.615 (9.394)	6.313 (6.315)	9.00 (＋0.38)	16.836	9.0 (9.5)		669	1,343		7.5	0.000475	140.564	744557	(-) 13.885	1278.297	-1.851	170.440	173.000	0.9852	0.0290	5.891	0.171	10.837 > 1.0 NG	ASME= 0.176, EN1993= 5.859, JIS(L)= 10.759, JIS(S)= 16.139
3	A516-70	2.400	10.650	10.650	173 (156)	195 (195)	10.764 (11.777)	8.218 (8.222)	11.50 (＋0.74)	21.516	11.5 (12.0)		326	674		10.0	0.000633	162.080	992743	(-) 16.011	1650.165	-1.601	165.017	173.000	0.9539	0.0866	7.855	0.680	2.354 > 1.0 NG	ASME= 0.699, EN1993= 7.811, JIS(L)= 14.346, JIS(S)= 21.519
2	A516-70	2.400	13.050	13.050	173 (156)	195 (195)	12.912 (14.16)	10.124 (10.128)	13.50 (＋0.59)	25.260	13.5 (14.5)		207	348		12.0	0.000759	187.340	1191292	(-) 18.506	2022.034	-1.542	168.503	173.000	0.9740	0.0501	9.426	0.472	3.266 > 1.0 NG	ASME= 0.485, EN1993= 9.374, JIS(L)= 17.215, JIS(S)= 25.823
1	A516-70	2.400	15.450	15.450	173 (156)	195 (195)	15.06 (19.251)	12.03 (14.201)	15.50 (＋0.44)	29.004	15.5 (19.5)		141	141		14.0	0.000886	216.344	1389841	(-) 21.371	2393.902	-1.527	170.993	173.000	0.9884	0.0228	10.997	0.251	6.088 > 1.0 NG	ASME= 0.258, EN1993= 10.936, JIS(L)= 20.084, JIS(S)= 30.127
∑W, Hd, Ht(m)=		15.200	15.450	15.450	Total Net Weight, NetWt =					122.232	Ton		∑Wtr=	5.461	(m)
			Total Gross Weight, GrsWt =							132.209	Ton
			Equivalent Shell Nominal Thickness (평균두께 부식전)							10.316	mm	Without CA
			Equivalent Shell Corroded Thickness (평균두께 부식후)							8.816	mm	With CA
			Shell Gravity Center from Bottom,(PV Hanbook : 434 Page) Xs = (Aa+Ba+Ca...Z) / (A+B+C..Z) =6.253 [m]							6.253	m

kid = 5	1	2	3	4	5	6	7	8	9	10	11	12	13	14	15	16	17	18	19	20	21	22	23	24	25
id	SIZE mm	H mm	B mm	t₁ mm	t₂ mm	r1 mm	r2 mm	A cm²	W Kg/m	Ix cm⁴	Iy cm⁴	rx cm	ry cm	Sx cm³	Sy cm³	ex cm	ey cm	Zx cm³	Zy cm³	Cw(비틀림) cm⁶x1000	J(뒤틀링) cm⁴	rts	λf=B/tf	λw=H-2tf/tw	L=5m/ry< 300 OK
5	H194X150X6X9	194	150	6	9	13		39.01	30.6	2690	507	8.3	3.61	277	67.6	9.7	7.5	309	104	43300	11	4.11	8.33	29.33	L/r=120 < 200 OK Limit:16.6(M)
5	[CA=0] 적용 H194x150	194	150	6	9	13	0	39.01	30.6	2690	507	8.3	3.61	277	67.6	9.7	7.5	309	104	43300	11	4.11	8.33	29.33	139

Design Condition : D=41.600 (m), H=15.200 (m), SG=1.0, Pg=2.4517 (kPa) HTL : Height from the bottom of the course under consideration to the top of the shell including the top angle. (m) TOP Angle(HT) = DLL = HTL = 15.200 (m) as per API 650 Design CODE API 650, DRT, OUTER, Pg= 2.452 (kPa) = 250 (mmWTR) 주의 : ( ) 내 두께 수치(붉은색)는 위험물안전관리 기준으로 계산된 두께 임 허용응력 : 항복강도의 60%, S = 0.6×Fy = 0.6×260 = 156 MPa												Tank D(m)=	41.6	H(m)=	15.2	DLL(m)=	15.2	Shutdown and Construction Condition [ 내부압력 없는 조건 Pd: 0.0 MPa ], T1s(ShutDown) = Max. Compression (-값) 압축 1) Roof Dead Load Wr = [0.0] Ton 2) Roof Live Load LL = [163.101] Ton = Max( LL, Vacuum, SnowLoad ) 120 kg/m²× At (1359.179)m²= [163.101] Ton Total Load : (1)+(2) Wsum = [163.101] Ton Note 1) : 탱크내부에 진공압력( Vacuum Pressure 0.005 MPa)이 걸렸을 경우에는 나중에 추가 예정 2022.07.15
Shell No. [n]	Material	W[i] (m)	Hd (m)	Ht (m)	Sd (MPa)	St (MPa)	ONE-FOOT td (mm)	ONE-FOOT tt (mm)	Used Thk. tu =Max(td,tt , tMin) (mm)	Weight (Ton)	Remark tu(input) (mm)	SKETCH	Each Wtr[n] (mm)	∑Wtr[1~n] 누적(mm)	Remark	tc =tu-CA (mm)	Ratio t / R	누적중량 Stacked Weight W (Ton)	Shell 단면적 Sectional Area A[n] (mm²)	T1=R/2× (P-W/A) (N/mm)	T2=P×R (N/mm)	Sc = T1/tc 수직응력 (-압축,+인장) (MPa)	St = T2/tc 원주막응력 (-압축,+인장) (MPa)	Sts (MPa)	Factor N =St/Sts	Factor M Fact(N)	Scs (MPa)	Sca = M×Scs (MPa)	Stress ratio SRc = Sc/Sca SRt = St/Sts SRtc < 1.0 OK	1. ASME D.1 Sca = M×0.0625×E×tPr (MPa), E = 204,000 (MPa) 2. EN_1993 Sca = 0.0605 × E × Cx(1.0) × tPr (MPa) 3. JIS_LNG Sca = (0.25/γ1=2.25)×E×tPr (MPa) Long-Term 4. JIS_LNG Sca = (0.25/γ2=1.50)×E×tPr (MPa) Short-Term
7	A516-70	0.800	1.050	1.050	173 (156)	195 (195)	8.0 (8.0)	8.0 (8.0)	11.50 (＋3.5)	9.440	11.5 (8.0)	dbgCanvas_650 shCanvas_650 [CANVAS SHOW]	273	6,402		10.0	0.000481	172.541	1306903	(-) 12.947	214.177	-1.295	21.418	173.000	0.1238	0.9323	5.967	5.563	0.233 < 1.0 OK	ASME= 5.715, EN1993= 5.934, JIS(L)= 10.897, JIS(S)= 16.346
6	A516-70	2.400	3.450	3.450	173 (156)	195 (195)	8.0 (8.0)	8.0 (8.0)	8.00 (＋0.0)	19.700	8.0 (8.0)		2,400	6,129		6.5	0.000312	192.241	849487	(-) 14.425	703.725	-2.219	108.265	173.000	0.6258	0.5275	3.878	2.046	1.085 > 1.0 NG	ASME= 2.102, EN1993= 3.857, JIS(L)= 7.083, JIS(S)= 10.625
5	A516-70	2.400	5.850	5.850	173 (156)	195 (195)	8.039 (8.755)	8.0 (8.0)	8.50 (＋0.46)	20.930	8.5 (9.0)		1,994	3,729		7.0	0.000337	213.171	914832	(-) 15.996	1193.273	-2.285	170.468	173.000	0.9854	0.0286	4.177	0.119	19.130 > 1.0 NG	ASME= 0.123, EN1993= 4.154, JIS(L)= 7.628, JIS(S)= 11.442
4	A516-70	2.400	8.250	8.250	173 (156)	195 (195)	10.867 (11.892)	8.31 (8.314)	11.50 (＋0.63)	28.320	11.5 (12.0)		818	1,735		10.0	0.000481	241.491	1306903	(-) 18.121	1682.821	-1.812	168.282	173.000	0.9727	0.0525	5.967	0.313	5.785 > 1.0 NG	ASME= 0.322, EN1993= 5.934, JIS(L)= 10.897, JIS(S)= 16.346
3	A516-70	2.400	10.650	10.650	173 (156)	195 (195)	13.695 (15.029)	10.819 (10.824)	14.00 (＋0.3)	34.480	14.0 (15.0)		468	917		12.5	0.000601	275.971	1633628	(-) 20.708	2172.370	-1.657	173.790	173.000	1.0046	-0.0093	7.458	-0.069	-23.884 > 1.0 NG	ASME= -0.071, EN1993= 7.417, JIS(L)= 13.622, JIS(S)= 20.433
2	A516-70	2.400	13.050	13.050	173 (156)	195 (195)	16.523 (18.167)	13.328 (13.333)	17.00 (＋0.48)	41.870	17.0 (18.5)		273	449		15.5	0.000745	317.841	2025699	(-) 23.850	2661.918	-1.539	171.737	173.000	0.9927	0.0144	9.248	0.133	11.554 > 1.0 NG	ASME= 0.137, EN1993= 9.197, JIS(L)= 16.891, JIS(S)= 25.337
1	A516-70	2.400	15.450	15.450	173 (156)	195 (195)	19.351 (24.869)	15.837 (18.695)	20.00 (＋0.65)	49.270	20.0 (25.0)		176	176		18.5	0.000889	367.111	2417770	(-) 27.547	3151.466	-1.489	170.349	173.000	0.9847	0.0299	11.038	0.330	4.512 > 1.0 NG	ASME= 0.339, EN1993= 10.977, JIS(L)= 20.16, JIS(S)= 30.24
∑W, Hd, Ht(m)=		15.200	15.450	15.450	Total Net Weight, NetWt =					204.01	Ton		∑Wtr=	6.402	(m)
			Total Gross Weight, GrsWt =							216.496	Ton
			Equivalent Shell Nominal Thickness (평균두께 부식전)							13.082	mm	Without CA
			Equivalent Shell Corroded Thickness (평균두께 부식후)							11.582	mm	With CA
			Shell Gravity Center from Bottom,(PV Hanbook : 434 Page) Xs = (Aa+Ba+Ca...Z) / (A+B+C..Z) =6.277 [m]							6.277	m

kid = 7	1	2	3	4	5	6	7	8	9	10	11	12	13	14	15	16	17	18	19	20	21	22	23	24	25
id	SIZE mm	H mm	B mm	t₁ mm	t₂ mm	r1 mm	r2 mm	A cm²	W Kg/m	Ix cm⁴	Iy cm⁴	rx cm	ry cm	Sx cm³	Sy cm³	ex cm	ey cm	Zx cm³	Zy cm³	Cw(비틀림) cm⁶x1000	J(뒤틀링) cm⁴	rts	λf=B/tf	λw=H-2tf/tw	L=5m/ry< 300 OK
7	H300X150X6.5X9	300	150	6.5	9	13		46.78	36.7	7210	508	12.4	3.29	481	67.7	15	7.5	542	105	107000	12.7	3.92	8.33	43.38	L/r=81 < 200 OK Limit:24.8(M)
7	[CA=0] 적용 H300x150	300	150	6.5	9	13	0	46.78	36.7	7210	508	12.4	3.29	481	67.7	15	7.5	542	105	107000	12.7	3.92	8.33	43.38	152

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B. Turkey SECL (1 ONE-FOOT) TANK Net Weight (설계중량) 　　D= 31.6 (m), H= 15.2 (m)							Horizontal Weld (수평용접 : 2G) [자동:SAW or 수동:SMAW] [용착효율:SAW (95%) / 수동:SMAW (60%)]						Vertical Weld (수직용접) [ FCAW 용착효율: (90%) ]						합계중량	REMARK	[새창에서] B. Turkey SECL (1 ONE-FOOT) TANK 큰 이미지 로 보기 [새창에서] PDF 도면 보기 [새창에서] SHOP_WPS_PQR_SUMBAWA_50K PDF 보기
No.	Material	Thickness (mm)	Width (mm)	Length (mm)	Qty (SHT)	Weight (Ton)	Joint No.	수평용접 총길이 (m)	용입부 단면적 A(mm²)	용접봉 NET중량 (kg)	용착 효율 (%)	용접봉 발주예상 중량(kg)	Joint No.	shCirQty=[6] 수직용접 총길이 VL = 6 PCS × Each S.W(m)	용입부 단면적 A(mm²)	용접봉 NET중량 (kg)	용착 효율 (%)	용접봉 발주예상 중량(kg)	수평+수직 용접봉중량 (kg)	REMARK
7	A516-70 (Comp. Ring+Top Shell)	8.5	800	16550	6	5.298	2G-H7	99	42.48	33.01	95	34.75	3G-V7	0.8m ×6= 4.8 m	-1.00	-0.04	90	-0.04	34.71
6	A516-70	6.0	2400	16548	6	11.226	2G-H6	99	-1.00	-0.78	95	-0.82	3G-V6	2.4m ×6= 14.4 m	-1.00	-0.11	90	-0.12	-0.94
5	A516-70	7.0	2400	16549	6	13.092	2G-H5	99	-1.00	-0.78	95	-0.82	3G-V5	2.4m ×6= 14.4 m	-1.00	-0.11	90	-0.12	-0.94
4	A516-70	9.0	2400	16550	6	16.836	2G-H4	99	-1.00	-0.78	95	-0.82	3G-V4	2.4m ×6= 14.4 m	-1.00	-0.11	90	-0.12	-0.94
3	A516-70	11.5	2400	16551	6	21.516	2G-H3	99	-1.00	-0.78	95	-0.82	3G-V3	2.4m ×6= 14.4 m	-1.00	-0.11	90	-0.12	-0.94
2	A516-70	13.5	2400	16552	6	25.260	2G-H2	99	-1.00	-0.78	95	-0.82	3G-V2	2.4m ×6= 14.4 m	-1.00	-0.11	90	-0.12	-0.94
1	A516-70	15.5	2400	16553	6	29.004	2G-H1	99	-1.00	-0.78	98	-0.82	3G-V1	2.4m ×6= 14.4 m	-1.00	-0.11	90	-0.12	-0.94
A)	1st Shell + Annular Plate	t1st= 15.5 tAnn= 10.5	2400	16553	N/A	N/A	1F-An	99.0	58.86	45.74	60	76.23	-	-	-	-	-	-	-0.82
B. Turkey SECL (1 ONE-FOOT) TANK Total =					42	122.2	HLEN =	792.0	95.34	74.07	98	106.06	VLEN =	91.200	-7.00	-0.70	90	-0.76	105.30
A. Turkey SECL (2 ONE-FOOT) TANK Net Weight (설계중량) 　　D= 41.6 (m), H= 15.2 (m)							Horizontal Weld (수평용접 : 2G) [자동:SAW or 수동:SMAW] [용착효율:SAW (95%) / 수동:SMAW (60%)]						Vertical Weld (수직용접) [ FCAW 용착효율: (90%) ]						합계중량	REMARK	[새창에서] A. Turkey SECL (2 ONE-FOOT) TANK 큰 이미지 로 보기 [새창에서] PDF 도면 보기 [새창에서] SHOP_WPS_PQR_SUMBAWA_50K PDF 보기
No.	Material	Thickness (mm)	Width (mm)	Length (mm)	Qty (SHT)	Weight (Ton)	Joint No.	수평용접 총길이 (m)	용입부 단면적 A(mm²)	용접봉 NET중량 (kg)	용착 효율 (%)	용접봉 발주예상 중량(kg)	Joint No.	shCirQty=[10] 수직용접 총길이 VL = 10 PCS × Each S.W(m)	용입부 단면적 A(mm²)	용접봉 NET중량 (kg)	용착 효율 (%)	용접봉 발주예상 중량(kg)	수평+수직 용접봉중량 (kg)	REMARK
7	A516-70 (Comp. Ring+Top Shell)	11.5	800	13072	10	9.440	2G-H7	130	77.76	79.35	95	83.53	3G-V7	0.8m ×10= 8 m	-1.00	-0.06	90	-0.07	83.46
6	A516-70	8.0	2400	13071	10	19.700	2G-H6	130	-1.00	-1.02	95	-1.07	3G-V6	2.4m ×10= 24 m	-1.00	-0.19	90	-0.21	-1.28
5	A516-70	8.5	2400	13071	10	20.930	2G-H5	130	-1.00	-1.02	95	-1.07	3G-V5	2.4m ×10= 24 m	-1.00	-0.19	90	-0.21	-1.28
4	A516-70	11.5	2400	13072	10	28.320	2G-H4	130	-1.00	-1.02	95	-1.07	3G-V4	2.4m ×10= 24 m	-1.00	-0.19	90	-0.21	-1.28
3	A516-70	14.0	2400	13073	10	34.480	2G-H3	130	-1.00	-1.02	95	-1.07	3G-V3	2.4m ×10= 24 m	-1.00	-0.19	90	-0.21	-1.28
2	A516-70	17.0	2400	13074	10	41.870	2G-H2	130	-1.00	-1.02	95	-1.07	3G-V2	2.4m ×10= 24 m	-1.00	-0.19	90	-0.21	-1.28
1	A516-70	20.0	2400	13075	10	49.270	2G-H1	130	-1.00	-1.02	98	-1.07	3G-V1	2.4m ×10= 24 m	-1.00	-0.19	90	-0.21	-1.28
A)	1st Shell + Annular Plate	t1st= 20 tAnn= 13	2400	13075	N/A	N/A	1F-An	130.0	98.00	100.01	60	166.68	-	-	-	-	-	-	-1.07
A. Turkey SECL (2 ONE-FOOT) TANK Total =					70	204.0	HLEN =	1040.0	169.76	173.24	98	243.79	VLEN =	152.000	-7.00	-1.20	90	-1.33	242.46

Design Condition : D=40.000 (m), H=23.000 (m), SG=1.0, Pg=2.4517 (kPa) HTL : Height from the bottom of the course under consideration to the top of the shell including the top angle. (m) TOP Angle(HT) = DLL = HTL = 23.000 (m) as per API 650 Design CODE API 650, DRT, OUTER, Pg= 2.452 (kPa) = 250 (mmWTR) 주의 : ( ) 내 두께 수치(붉은색)는 위험물안전관리 기준으로 계산된 두께 임 허용응력 : 항복강도의 60%, S = 0.6×Fy = 0.6×415 = 249 MPa												Tank D(m)=	40	H(m)=	23	DLL(m)=	21.44	Shutdown and Construction Condition [ 내부압력 없는 조건 Pd: 0.0 MPa ], T1s(ShutDown) = Max. Compression (-값) 압축 1) Roof Dead Load Wr = [0.0] Ton 2) Roof Live Load LL = [150.796] Ton = Max( LL, Vacuum, SnowLoad ) 120 kg/m²× At (1256.637)m²= [150.796] Ton Total Load : (1)+(2) Wsum = [150.796] Ton Note 1) : 탱크내부에 진공압력( Vacuum Pressure 0.005 MPa)이 걸렸을 경우에는 나중에 추가 예정 2022.07.15
Shell No. [n]	Material	W[i] (m)	Hd (m)	Ht (m)	Sd (MPa)	St (MPa)	ONE-FOOT td (mm)	ONE-FOOT tt (mm)	Used Thk. tu =Max(td,tt , tMin) (mm)	Weight (Ton)	Remark tu(input) (mm)	SKETCH	Each Wtr[n] (mm)	∑Wtr[1~n] 누적(mm)	Remark	tc =tu-CA (mm)	Ratio t / R	누적중량 Stacked Weight W (Ton)	Shell 단면적 Sectional Area A[n] (mm²)	T1=R/2× (P-W/A) (N/mm)	T2=P×R (N/mm)	Sc = T1/tc 수직응력 (-압축,+인장) (MPa)	St = T2/tc 원주막응력 (-압축,+인장) (MPa)	Sts (MPa)	Factor N =St/Sts	Factor M Fact(N)	Scs (MPa)	Sca = M×Scs (MPa)	Stress ratio SRc = Sc/Sca SRt = St/Sts SRtc < 1.0 OK	1. ASME D.1 Sca = M×0.0625×E×tPr (MPa), E = 204,000 (MPa) 2. EN_1993 Sca = 0.0605 × E × Cx(1.0) × tPr (MPa) 3. JIS_LNG Sca = (0.25/γ1=2.25)×E×tPr (MPa) Long-Term 4. JIS_LNG Sca = (0.25/γ2=1.50)×E×tPr (MPa) Short-Term
12	A516-70	1.000	1.250	1.250	173 (156)	195 (195)	8.0 (8.0)	8.0 (8.0)	13.00 (＋5.0)	12.830	13.0 (8.0)	dbgCanvas_650 shCanvas_650 [CANVAS SHOW]	177	4,024		10.0	0.000500	163.626	1256637	(-) 12.769	245.166	-1.277	24.517	147.050	0.1667	0.9062	6.205	5.623	0.227 < 1.0 OK	ASME= 5.777, EN1993= 6.171, JIS(L)= 11.333, JIS(S)= 17
11	A516-70	2.000	3.250	3.250	173 (156)	195 (195)	8.0 (8.0)	8.0 (8.0)	8.00 (＋0.0)	15.790	8.0 (8.0)		2,000	3,847		5.0	0.000250	179.416	628319	(-) 14.001	637.432	-2.800	127.486	147.050	0.8670	0.2270	3.103	0.704	3.976 > 1.0 NG	ASME= 0.724, EN1993= 3.086, JIS(L)= 5.667, JIS(S)= 8.5
10	A516-70	2.000	5.250	5.250	173 (156)	195 (195)	9.598 (9.222)	8.0 (8.0)	10.00 (＋0.4)	19.730	10.0 (9.5)		862	1,847		7.0	0.000350	199.146	879646	(-) 15.541	1029.698	-2.220	147.100	147.050	1.0003	-0.0006	4.344	-0.003	-851.872 > 1.0 NG	ASME= -0.003, EN1993= 4.32, JIS(L)= 7.933, JIS(S)= 11.9
9	A516-70	2.000	7.250	7.250	173 (156)	195 (195)	12.264 (11.736)	8.218 (8.222)	13.00 (＋0.74)	25.660	13.0 (12.0)		354	985		10.0	0.000500	224.806	1256637	(-) 17.544	1421.965	-1.754	142.196	147.050	0.9670	0.0630	6.205	0.391	4.488 > 1.0 NG	ASME= 0.402, EN1993= 6.171, JIS(L)= 11.333, JIS(S)= 17
8	A516-70	2.000	9.250	9.250	173 (156)	195 (195)	14.929 (14.249)	10.583 (10.588)	15.50 (＋0.57)	30.590	15.5 (14.5)		202	631		12.5	0.000625	255.396	1570796	(-) 19.931	1814.231	-1.594	145.138	147.050	0.9870	0.0255	7.757	0.198	8.061 > 1.0 NG	ASME= 0.203, EN1993= 7.714, JIS(L)= 14.167, JIS(S)= 21.25
7	A516-70	2.000	11.250	11.250	173 (156)	195 (195)	17.595 (16.763)	12.948 (12.954)	18.00 (＋0.4)	35.530	18.0 (17.0)		128	429		15.0	0.000750	290.926	1884956	(-) 22.704	2206.497	-1.514	147.100	147.050	1.0003	-0.0006	9.308	-0.006	-271.019 > 1.0 NG	ASME= -0.006, EN1993= 9.257, JIS(L)= 17, JIS(S)= 25.5
6	A516-70	2.000	13.250	13.250	173 (156)	195 (195)	20.261 (19.277)	15.313 (15.32)	21.00 (＋0.74)	41.450	21.0 (19.5)		81	301		18.0	0.000900	332.376	2261947	(-) 25.938	2598.763	-1.441	144.376	147.050	0.9818	0.0355	11.170	0.397	3.634 > 1.0 NG	ASME= 0.407, EN1993= 11.108, JIS(L)= 20.4, JIS(S)= 30.6
5	A516-70	2.000	15.250	15.250	173 (156)	195 (195)	22.927 (21.791)	17.678 (17.686)	23.50 (＋0.57)	46.390	23.5 (22.0)		59	220		20.5	0.001025	378.766	2576106	(-) 29.558	2991.029	-1.442	145.904	147.050	0.9922	0.0154	12.721	0.196	7.360 > 1.0 NG	ASME= 0.201, EN1993= 12.651, JIS(L)= 23.233, JIS(S)= 34.85
4	A516-70	2.000	17.250	17.250	173 (156)	195 (195)	25.592 (24.305)	20.043 (20.051)	26.00 (＋0.41)	51.330	26.0 (24.5)		44	161		23.0	0.001150	430.096	2890265	(-) 33.564	3383.295	-1.459	147.100	147.050	1.0003	-0.0006	14.272	-0.009	-170.416 > 1.0 NG	ASME= -0.009, EN1993= 14.193, JIS(L)= 26.067, JIS(S)= 39.1
3	A516-70	2.000	19.250	19.250	173 (156)	195 (195)	28.258 (26.819)	22.408 (22.417)	29.00 (＋0.74)	57.250	29.0 (27.0)		32	117		26.0	0.001300	487.346	3267256	(-) 38.032	3775.561	-1.463	145.214	147.050	0.9875	0.0245	16.134	0.395	3.701 > 1.0 NG	ASME= 0.406, EN1993= 16.045, JIS(L)= 29.467, JIS(S)= 44.2
2	A537-CL2	2.000	21.250	21.250	220 (249)	236 (236)	24.958 (19.497)	20.47 (20.478)	25.50 (＋0.54)	50.340	25.5 (19.5)		47	85		22.5	0.001125	537.686	2827433	(-) 41.960	4167.827	-1.865	185.237	187.000	0.9906	0.0185	13.962	0.258	7.220 > 1.0 NG	ASME= 0.265, EN1993= 13.885, JIS(L)= 25.5, JIS(S)= 38.25
1	A537-CL2	2.000	23.250	23.250	220 (249)	236 (236)	27.055 (24.325)	22.424 (26.471)	27.50 (＋0.44)	54.290	27.5 (24.5)		38	38		24.5	0.001225	591.976	3078761	(-) 46.197	4560.093	-1.886	186.126	187.000	0.9953	0.0093	15.203	0.141	13.336 > 1.0 NG	ASME= 0.145, EN1993= 15.119, JIS(L)= 27.767, JIS(S)= 41.65
∑W, Hd, Ht(m)=		23.000	23.250	23.250	Total Net Weight, NetWt =					441.18	Ton		∑Wtr=	4.024	(m)
			Total Gross Weight, GrsWt =							461.408	Ton
			Equivalent Shell Nominal Thickness (평균두께 부식전)							19.446	mm	Without CA
			Equivalent Shell Corroded Thickness (평균두께 부식후)							16.446	mm	With CA
			Shell Gravity Center from Bottom,(PV Hanbook : 434 Page) Xs = (Aa+Ba+Ca...Z) / (A+B+C..Z) =9.24 [m]							9.240	m

Descriptipon	SI Unit			USC Unit
Diameter of tank inside	D =	42000	mm	D =	137.795	ft
Height of tank	Htank =	35800	mm	Htank =	117.454	ft
Radius of tank in-diameter, Rc = D / 2	Rc =	21000	mm	Rc =	68.898	ft
Design liquid level	DLL =	35500	mm	DLL =	116.47	ft
Hydrostatic-test liquid level, HTL = 1.25 DLL × SG	HTL =	20160	mm	HTL =	66.142	ft
Corrosion allowance	C.A =	2.0	mm	C.A =	0.079	in
Min. Shell Thickness as per API 620 CODE	tMin =	6.350	mm	tMin =	0.25	inch
Design Temperature	DT =	-104.0	℃	DT =	-155.2	ºF
Design Specific Gravity(SG = 0.5677), Design Density(ρ)	ρ =	567.7	kg/m³	ρ =	35.44	lb/ft³
Cross-sectional area of the tank, At = π×D²/4	At =	1385.442	m²	At =	2,147,440	in²
Total weight of tank and its contents.	W =	0.0	Ton	Wr =	0.0	kN
Shell Plate Welding Joint Efficiency	E =	1.000		E =	1.000
Material of shell plate	MATL =	A553-TYPE1
Minimum Tensile strength (For WELD METAL)	Fu =	689.476	MPa	Fu =	100,000	psi
Minimum Yield strength　 (For WELD METAL)	Fy =	399.896	MPa	Fy =	58,000	psi
Allowable Stress for Design Condition [View] 　　(Design) Sts = Min( 1/3 × Ft, 2/3 × Fy)	Sts =	229.825	MPa	Sts =	33,333	psi
Allowable Stress for Test Condition 　　(Test) Sts = Min( 0.55 × Ft, 0.85 × Fy)	Sts =	339.912	MPa	Sts =	49,300	psi
Design internal pressure, Pg = 0 mmWTR	Pg =	0.0	MPa	Pg =	0.0	psi
Height from the bottom of the course under consideration to the Max. design liquid level(DLL), PL = ρ · g · Hd · 10^-3 (kPa) Gravity acceleration, g = 9.80665 m/sec²	PL =	See Below 3.1.1 Table(a)
Total pressure, P = Pg + PL	P =	See Below 3.1.1 Table(a)

Design Condition : D=42.000 (m), H=35.800 (m), SG=0.5677, Pg=0.0 (kPa) DLL=35.500 (m), HTL=DLL×SG×1.25 = 20.160 (m) Ht[i] = Hd[i] × SG × 1.25 API 620, FULL, INNER, Pg= 0.0 (kPa) = 0 (mmWTR)												Tank D(m)=	42	H(m)=	35.8	DLL(m)=	35.5	Shutdown and Construction Condition [ 내부압력 없는 조건 Pd: 0.0 MPa ], T1s(ShutDown) = Max. Compression (-값) 압축 1) Roof Dead Load Wr = [0.0] Ton 2) Roof Live Load LL = [0.0] Ton = Max( LL, Vacuum, SnowLoad ) 120 kg/m²× At (1385.442)m²= [0.0] Ton Total Load : (1)+(2) Wsum = [0.0] Ton Note 1) : 탱크내부에 진공압력( Vacuum Pressure 0.005 MPa)이 걸렸을 경우에는 나중에 추가 예정 2022.07.15
Shell No. [n]	Material	W[i] (m)	Hd (m)	Ht (m)	P=Pg+P_L (KPa)	T2=P×R (N/mm)	td (mm)	tt (mm)	Used Thk. tu =Max(td,tt , tMin) (mm)	Weight (Ton)	Remark tu(input) (mm)	SKETCH	Each Wtr[n] (mm)	∑Wtr[1~n] 누적(mm)	Remark	tc =tu-CA (mm)	Ratio t / R	누적중량 Stacked Weight W (Ton)	Shell 단면적 Sectional Area A[n] (mm²)	T1=R/2× (P-W/A) (N/mm)	T2=P×R (N/mm)	Sc = T1/tc 수직응력 (-압축,+인장) (MPa)	St = T2/tc 원주막응력 (-압축,+인장) (MPa)	Sts (MPa)	Factor N =St/Sts	Factor M Fact(N)	Scs (MPa)	Sca = M×Scs (MPa)	Stress ratio SRc = Sc/Sca SRt = St/Sts SRtc < 1.0 OK	1. ASME D.1 Sca = M×0.0625×E×tPr (MPa), E = 204,000 (MPa) 2. EN_1993 Sca = 0.0605 × E × Cx(1.0) × tPr (MPa) 3. JIS_LNG Sca = (0.25/γ1=2.25)×E×tPr (MPa) Long-Term 4. JIS_LNG Sca = (0.25/γ2=1.50)×E×tPr (MPa) Short-Term
11	A553-TYPE1	3.200	2.900	0.0	16.145	339.04	6.350	6.350	6.35 (＋0.0)	21.050	6.35 (0.0)	dbgCanvas_650 shCanvas_650 [CANVAS SHOW]	3,200	11,018		4.35	0.000207	21.050	573969	(-) 1.564	339.045	-0.360	77.941	229.825	0.3391	0.7864	2.571	2.022	0.178 < 1.0 OK	ASME= 2.077, EN1993= 2.557, JIS(L)= 4.695, JIS(S)= 7.043
10	A553-TYPE1	3.260	6.160	0.0	34.294	720.18	6.350	6.350	6.35 (＋0.0)	21.440	6.35 (0.0)		3,260	7,818		4.35	0.000207	42.490	573969	(-) 3.158	720.178	-0.726	165.558	229.825	0.7204	0.4213	2.571	1.083	0.670 < 1.0 OK	ASME= 1.113, EN1993= 2.557, JIS(L)= 4.695, JIS(S)= 7.043
9	A553-TYPE1	3.260	9.420	0.0	52.443	1101.31	6.792	6.350	7.50 (＋0.71)	25.330	7.5 (0.0)		1,814	4,558		5.5	0.000262	67.820	725708	(-) 5.041	1101.311	-0.916	200.238	229.825	0.8713	0.2206	3.250	0.717	1.278 > 1.0 NG	ASME= 0.737, EN1993= 3.232, JIS(L)= 5.937, JIS(S)= 8.905
8	A553-TYPE1	3.260	12.680	0.0	70.593	1482.44	8.450	6.350	9.00 (＋0.55)	30.400	9.0 (0.0)		992	2,744		7.0	0.000333	98.220	923628	(-) 7.300	1482.444	-1.043	211.778	229.825	0.9215	0.1419	4.137	0.587	1.777 > 1.0 NG	ASME= 0.603, EN1993= 4.114, JIS(L)= 7.556, JIS(S)= 11.333
7	A553-TYPE1	3.260	15.940	0.600	88.742	1863.58	10.109	6.350	10.50 (＋0.39)	35.460	10.5 (0.0)		611	1,752		8.5	0.000405	133.680	1121549	(-) 9.935	1863.577	-1.169	219.244	229.825	0.9540	0.0864	5.023	0.434	2.693 > 1.0 NG	ASME= 0.446, EN1993= 4.996, JIS(L)= 9.175, JIS(S)= 13.762
6	A553-TYPE1	3.260	19.200	3.860	106.891	2244.71	11.767	6.350	12.50 (＋0.73)	42.220	12.5 (0.0)		360	1,141		10.5	0.000500	175.900	1385442	(-) 13.073	2244.710	-1.245	213.782	229.825	0.9302	0.1274	6.205	0.791	1.575 > 1.0 NG	ASME= 0.812, EN1993= 6.171, JIS(L)= 11.333, JIS(S)= 17
5	A553-TYPE1	3.260	22.460	7.120	125.04	2625.84	13.425	6.350	14.00 (＋0.57)	47.290	14.0 (0.0)		258	781		12.0	0.000571	223.190	1583363	(-) 16.588	2625.843	-1.382	218.820	229.825	0.9521	0.0897	7.092	0.636	2.173 > 1.0 NG	ASME= 0.654, EN1993= 7.053, JIS(L)= 12.952, JIS(S)= 19.429
4	A553-TYPE1	3.260	25.720	10.380	143.189	3006.98	15.084	6.350	15.50 (＋0.42)	52.360	15.5 (0.0)		192	523		13.5	0.000643	275.550	1781283	(-) 20.480	3006.976	-1.517	222.739	229.825	0.9692	0.0590	7.978	0.471	3.223 > 1.0 NG	ASME= 0.484, EN1993= 7.934, JIS(L)= 14.571, JIS(S)= 21.857
3	A553-TYPE1	3.260	28.980	13.640	161.339	3388.11	16.742	8.264	17.50 (＋0.76)	59.120	17.5 (0.0)		136	331		15.5	0.000738	334.670	2045177	(-) 24.874	3388.109	-1.605	218.588	229.825	0.9511	0.0915	9.160	0.838	1.915 > 1.0 NG	ASME= 0.861, EN1993= 9.11, JIS(L)= 16.73, JIS(S)= 25.095
2	A553-TYPE1	3.260	32.240	16.900	179.488	3769.24	18.400	10.239	19.00 (＋0.6)	64.180	19.0 (0.0)		108	195		17.0	0.000810	398.850	2243097	(-) 29.644	3769.242	-1.744	221.720	229.825	0.9647	0.0672	10.047	0.675	2.583 > 1.0 NG	ASME= 0.694, EN1993= 9.991, JIS(L)= 18.349, JIS(S)= 27.524
1	A553-TYPE1	3.260	35.500	20.160	197.637	4150.37	20.059	12.214	20.50 (＋0.44)	69.250	20.5 (0.0)		87	87		18.5	0.000881	468.100	2441017	(-) 34.790	4150.375	-1.881	224.345	229.825	0.9762	0.0460	10.933	0.503	3.739 > 1.0 NG	ASME= 0.517, EN1993= 10.873, JIS(L)= 19.968, JIS(S)= 29.952
∑W, Hd, Ht(m)=		35.800	35.500	20.160	Total Net Weight, NetWt =					468.1	Ton		∑Wtr=	11.018	(m)
			Total Gross Weight, GrsWt =							486.103	Ton
			Equivalent Shell Nominal Thickness (평균두께 부식전)							12.626	mm	Without CA
			Equivalent Shell Corroded Thickness (평균두께 부식후)							10.626	mm	With CA
			Shell Gravity Center from Bottom,(PV Hanbook : 434 Page) Xs = (Aa+Ba+Ca...Z) / (A+B+C..Z) =13.966 [m]							13.966	m

1. [INNER TANK] Shell Plate
Net Weight (설계중량)							Gross Weight (자재구매 중량)							자재구매가격 Shell Plate Purchsing Price					Remark
Shell Course No.	Material	Thk. (mm)	Width (mm)	Length (mm)	Qty (SHT)	Net WT (Ton)	Shell Course No.	Material	Thk. (mm)	Width (mm)	Length (mm)	Qty (SHT)	Gross WT (Ton)	Loss Grs/net Ratio(%)	수입 자재단가 (USD/Ton)	수입 자재금액 (USD)	내수 자재단가 (천원/Ton)	내수 자재금액 (천원)	Remark
11 th Shell Plate	A553-TYPE1	6.35	3200	13196	10	21.050	11	A553-TYPE1	6.35	3250	13240	11	23.595	12.09	5,353.50	126,316	6,957.00	164,150	Stiff and jig 부착 PAD PLATE 1 Sheet 포함
10 th Shell Plate	A553-TYPE1	6.35	3260	13196	10	21.440	10	A553-TYPE1	6.35	3310	13240	10	21.850	1.91	5,353.50	116,974	6,957.00	152,010
9 th Shell Plate	A553-TYPE1	7.5	3260	13197	10	25.330	9	A553-TYPE1	7.5	3310	13240	10	25.800	1.86	5,353.50	138,120	6,957.00	179,491
8 th Shell Plate	A553-TYPE1	9.0	3260	13197	10	30.400	8	A553-TYPE1	9.0	3310	13240	10	30.960	1.84	5,353.50	165,744	6,957.00	215,389
7 th Shell Plate	A553-TYPE1	10.5	3260	13197	10	35.460	7	A553-TYPE1	10.5	3310	13240	10	36.120	1.86	5,353.50	193,368	6,957.00	251,287
6 th Shell Plate	A553-TYPE1	12.5	3260	13198	10	42.220	6	A553-TYPE1	12.5	3310	13240	10	43.000	1.85	5,353.50	230,200	6,957.00	299,151
5 th Shell Plate	A553-TYPE1	14.0	3260	13199	10	47.290	5	A553-TYPE1	14.0	3310	13240	10	48.160	1.84	5,353.50	257,825	6,957.00	335,049
4 th Shell Plate	A553-TYPE1	15.5	3260	13199	10	52.360	4	A553-TYPE1	15.5	3310	13240	10	53.320	1.83	5,353.50	285,449	6,957.00	370,947
3 rd Shell Plate	A553-TYPE1	17.5	3260	13200	10	59.120	3	A553-TYPE1	17.5	3310	13250	10	60.250	1.91	5,353.50	322,548	6,957.00	419,159
2 nd Shell Plate	A553-TYPE1	19.0	3260	13200	10	64.180	2	A553-TYPE1	19.0	3310	13250	10	65.410	1.92	5,353.50	350,172	6,957.00	455,057
1 st Shell Plate	A553-TYPE1	20.5	3260	13201	10	69.250	1	A553-TYPE1	20.5	3310	13250	11	77.638	12.11	5,353.50	415,635	6,957.00	540,128	1st Shell Nozzzle and Openning PAD PLATE 1 Sheet 포함
[INNER TANK] Shell Plate Total =					110	468.100	Total Qty and Weight =					112	486.103	3.85	5,353.50	2,602,352	6,957.00	3,381,819	(천원)
2. [INNER TANK] Bottom / Annular Plate / Stiffener Ring
Net Weight (설계중량)							Gross Weight (자재구매 중량)							자재구매가격 Shell Plate Purchsing Price					Remark
Part Name	Material	Shell Course No.			Qty (SHT)	Net WT (Ton)	Thickness Range (mm)			Width (mm)	Length (mm)	Qty (SHT)	Gross WT (Ton)	Loss Grs/net Ratio(%)	수입 자재단가 (USD/Ton)	수입 자재금액 (USD)	내수 자재단가 (천원/Ton)	내수 자재금액 (천원)	Remark
1. Bottom Plate	A553-TYPE1	7.0	3048	12192	34.30	70.030	1	A553-TYPE1	7.0	3048	12192	37	75.554	7.89	5,353.50	404,478	6,957.00	525,629
2. Annular Plate	A553-TYPE1	13.5	2438	6096	8.70	13.740	2	A553-TYPE1	13.5	2438	6096	11	17.325	26.09	5,353.50	92,749	6,957.00	120,530
6. Stiffener Ring	A553-TYPE1	L450x6.35+120x6.35 FB 170x6		132.0 (m)	17 Rings	26.852	6	A553-TYPE1	ref.	역계산	역계산	17	30.880	15.00	5,353.50	165,316	6,957.00	214,832
[INNER TANK] Bottom / Annular / Total =						110.622	Total Qty and Weight =						123.759			662,544	USD	860,991	(천원)
[INNER TANK] Grand Total =						578.722	Grand Total Qty and Weight =						609.862			3,264,896	USD	4,242,810	(천원)

Design Condition : D=44.000 (m), H=37.800 (m), SG=0.5677, Pg=18.0 (kPa) , Pg=18.0 (kPa) = 1,835 (mmWTR) DLL=35.500 (m), Hd[i] = DLL + Pg/SG (m) Ht[i] = Hd[i] × SG API 620, FULL, OUTER, Pg= 18.0 (kPa) = 1835.5 (mmWTR)												Tank D(m)=	44	H(m)=	37.8	DLL(m)=	35.5	Shutdown and Construction Condition [ 내부압력 없는 조건 Pd: 0.0 MPa ], T1s(ShutDown) = Max. Compression (-값) 압축 1) Roof Dead Load Wr = [339.4] Ton 2) Roof Live Load LL = [182.464] Ton = Max( LL, Vacuum, SnowLoad ) 120 kg/m²× At (1520.531)m²= [182.464] Ton Total Load : (1)+(2) Wsum = [521.864] Ton Note 1) : 탱크내부에 진공압력( Vacuum Pressure 0.005 MPa)이 걸렸을 경우에는 나중에 추가 예정 2022.07.15
Shell No. [n]	Material	W[i] (m)	Hd (m)	Ht (m)	P=Pg+P_L (KPa)	T2=P×R (N/mm)	td (mm)	tt (mm)	Used Thk. tu =Max(td,tt , tMin) (mm)	Weight (Ton)	Remark tu(input) (mm)	SKETCH	Each Wtr[n] (mm)	∑Wtr[1~n] 누적(mm)	Remark	tc =tu-CA (mm)	Ratio t / R	누적중량 Stacked Weight W (Ton)	Shell 단면적 Sectional Area A[n] (mm²)	T1=R/2× (P-W/A) (N/mm)	T2=P×R (N/mm)	Sc = T1/tc 수직응력 (-압축,+인장) (MPa)	St = T2/tc 원주막응력 (-압축,+인장) (MPa)	Sts (MPa)	Factor N =St/Sts	Factor M Fact(N)	Scs (MPa)	Sca = M×Scs (MPa)	Stress ratio SRc = Sc/Sca SRt = St/Sts SRtc < 1.0 OK	1. ASME D.1 Sca = M×0.0625×E×tPr (MPa), E = 204,000 (MPa) 2. EN_1993 Sca = 0.0605 × E × Cx(1.0) × tPr (MPa) 3. JIS_LNG Sca = (0.25/γ1=2.25)×E×tPr (MPa) Long-Term 4. JIS_LNG Sca = (0.25/γ2=1.50)×E×tPr (MPa) Short-Term
11	A553-TYPE1	1.800	0.0	0.0	18	396	7.938	7.938	35.00 (＋27.06)	68.420	35.0 (0.0)	dbgCanvas_650 shCanvas_650 [CANVAS SHOW]	25	12,011		33.0	0.001500	590.284	4561593	(-) 41.877	396.000	-1.269	12.000	229.825	0.0522	0.9729	18.616	18.111	0.070 < 1.0 OK	ASME= 18.607, EN1993= 18.513, JIS(L)= 34, JIS(S)= 51
10	A553-TYPE1	3.600	3.100	0.0	35.258	775.69	7.938	7.938	7.94 (＋0.0)	31.010	7.938 (0.0)		3,600	11,986		5.94	0.000270	621.294	820810	(-) 44.077	775.686	-7.423	130.631	229.825	0.5684	0.5863	3.350	1.964	3.780 > 1.0 NG	ASME= 2.018, EN1993= 3.331, JIS(L)= 6.118, JIS(S)= 9.177
9	A553-TYPE1	3.600	6.700	0.0	55.3	1216.61	7.938	7.938	8.00 (＋0.06)	31.260	8.0 (0.0)		3,508	8,386		6.0	0.000273	652.554	829380	(-) 46.295	1216.611	-7.716	202.768	229.825	0.8823	0.2040	3.385	0.690	11.175 > 1.0 NG	ASME= 0.709, EN1993= 3.366, JIS(L)= 6.182, JIS(S)= 9.273
8	A553-TYPE1	3.600	10.300	0.0	75.343	1657.54	9.212	7.938	10.00 (＋0.79)	39.070	10.0 (0.0)		1,709	4,878		8.0	0.000364	691.624	1105841	(-) 49.067	1657.536	-6.133	207.192	229.825	0.9015	0.1741	4.513	0.786	7.806 > 1.0 NG	ASME= 0.807, EN1993= 4.488, JIS(L)= 8.242, JIS(S)= 12.364
7	A553-TYPE1	3.600	13.900	0.0	95.385	2098.46	11.131	7.938	11.50 (＋0.37)	44.930	11.5 (0.0)		1,112	3,169		9.5	0.000432	736.554	1313186	(-) 52.254	2098.461	-5.500	220.891	229.825	0.9611	0.0737	5.359	0.395	13.926 > 1.0 NG	ASME= 0.406, EN1993= 5.33, JIS(L)= 9.788, JIS(S)= 14.682
6	A553-TYPE1	3.600	17.500	2.160	115.427	2539.39	13.049	7.938	13.50 (＋0.45)	52.750	13.5 (0.0)		690	2,057		11.5	0.000523	789.304	1589646	(-) 55.997	2539.386	-4.869	220.816	229.825	0.9608	0.0743	6.487	0.482	10.102 > 1.0 NG	ASME= 0.495, EN1993= 6.452, JIS(L)= 11.848, JIS(S)= 17.773
5	A553-TYPE1	3.600	21.100	5.760	135.469	2980.31	14.968	7.938	15.50 (＋0.53)	60.570	15.5 (0.0)		462	1,367		13.5	0.000614	849.874	1866106	(-) 60.294	2980.311	-4.466	220.764	229.825	0.9606	0.0746	7.616	0.568	7.861 > 1.0 NG	ASME= 0.584, EN1993= 7.574, JIS(L)= 13.909, JIS(S)= 20.864
4	A553-TYPE1	3.600	24.700	9.360	155.511	3421.24	16.886	7.938	17.50 (＋0.61)	68.390	17.5 (0.0)		327	905		15.5	0.000705	918.264	2142566	(-) 65.146	3421.236	-4.203	220.725	229.825	0.9604	0.0750	8.744	0.656	6.409 > 1.0 NG	ASME= 0.674, EN1993= 8.696, JIS(L)= 15.97, JIS(S)= 23.955
3	A553-TYPE1	3.600	28.300	12.960	175.553	3862.16	18.805	9.682	19.50 (＋0.69)	76.210	19.5 (0.0)		241	578		17.5	0.000795	994.474	2419026	(-) 70.552	3862.161	-4.032	220.695	229.825	0.9603	0.0752	9.872	0.742	5.431 > 1.0 NG	ASME= 0.763, EN1993= 9.818, JIS(L)= 18.03, JIS(S)= 27.045
2	A553-TYPE1	3.600	31.900	16.560	195.595	4303.09	20.723	11.967	21.50 (＋0.78)	84.020	21.5 (0.0)		184	337		19.5	0.000886	1078.494	2695486	(-) 76.513	4303.086	-3.924	220.671	229.825	0.9602	0.0753	11.000	0.828	4.737 > 1.0 NG	ASME= 0.851, EN1993= 10.94, JIS(L)= 20.091, JIS(S)= 30.136
1	A553-TYPE1	3.600	35.500	20.160	215.637	4744.01	22.642	14.252	23.00 (＋0.36)	89.890	23.0 (0.0)		153	153		21.0	0.000955	1168.384	2902832	(-) 82.890	4744.012	-3.947	225.905	229.825	0.9829	0.0334	11.846	0.396	9.976 > 1.0 NG	ASME= 0.406, EN1993= 11.781, JIS(L)= 21.636, JIS(S)= 32.455
∑W, Hd, Ht(m)=		37.800	35.500	20.160	Total Net Weight, NetWt =					646.52	Ton		∑Wtr=	12.011	(m)
			Total Gross Weight, GrsWt =							670.832	Ton
			Equivalent Shell Nominal Thickness (평균두께 부식전)							15.764	mm	Without CA
			Equivalent Shell Corroded Thickness (평균두께 부식후)							13.764	mm	With CA
			Shell Gravity Center from Bottom,(PV Hanbook : 434 Page) Xs = (Aa+Ba+Ca...Z) / (A+B+C..Z) =16.762 [m]							16.762	m

kid = 8	1	2	3	4	5	6	7	8	9	10	11	12	13	14	15	16	17	18	19	20	21	22	23	24	25
id	SIZE mm	H mm	B mm	t₁ mm	t₂ mm	r1 mm	r2 mm	A cm²	W Kg/m	Ix cm⁴	Iy cm⁴	rx cm	ry cm	Sx cm³	Sy cm³	ex cm	ey cm	Zx cm³	Zy cm³	Cw(비틀림) cm⁶x1000	J(뒤틀링) cm⁴	rts	λf=B/tf	λw=H-2tf/tw	L=5m/ry< 300 OK
8	H346X174X6X9	346	174	6	9	14		52.68	41.4	11100	792	14.5	3.88	642	91	17.3	8.7	716	140	224000	13.7	4.56	9.67	54.67	L/r=69 < 200 OK Limit:29.0(M)
8	[CA=0] 적용 H346x174	346	174	6	9	14	0	52.68	41.4	11100	792	14.5	3.88	642	91	17.3	8.7	716	140	224000	13.7	4.56	9.67	54.67	129

[SECL] LP Ethylene / INNER TANK Net Weight (설계중량) 　　D= 42 (m), H= 35.8 (m)							Horizontal Weld (수평용접 : 2G) [자동:SAW or 수동:SMAW] [용착효율:SAW (95%) / 수동:SMAW (60%)]						Vertical Weld (수직용접) [ FCAW 용착효율: (90%) ]						합계중량	REMARK	[새창에서] [SECL] LP Ethylene / INNER TANK 큰 이미지 로 보기 [새창에서] PDF 도면 보기 [새창에서] 저장탱크 용접 표준화 CAD 파일 (dwg) [새창에서] STE_저장탱크_용접부_개선표준_황상화 (pdf) [새창에서] SHOP_WPS_PQR_SUMBAWA_50K PDF 보기 [새창에서] 용접부_용입면적_산출_이한나.pdf
No.	Material	Thickness (mm)	Width (mm)	Length (mm)	Qty (SHT)	Weight (Ton)	Joint No.	수평용접 총길이 (m)	용입부 단면적 A(mm²)	용접봉 NET중량 (kg)	용착 효율 (%)	용접봉 발주예상 중량(kg)	Joint No.	shCirQty=[10] 수직용접 총길이 VL = 10 PCS × Each S.W(m)	용입부 단면적 A(mm²)	용접봉 NET중량 (kg)	용착 효율 (%)	용접봉 발주예상 중량(kg)	수평+수직 용접봉중량 (kg)	REMARK
11	A553-TYPE1	6.4	3200	13196	10	21.050	2G-H11	131	-1.00	-1.03	95	-1.08	3G-V11	3.2m ×10= 32 m	-1.00	-0.25	90	-0.28	-1.36
10	A553-TYPE1	6.4	3260	13196	10	21.440	2G-H10	131	-1.00	-1.03	95	-1.08	3G-V10	3.26m ×10= 32.6 m	-1.00	-0.26	90	-0.29	-1.37
9	A553-TYPE1	7.5	3260	13197	10	25.330	2G-H9	131	-1.00	-1.03	95	-1.08	3G-V9	3.26m ×10= 32.6 m	-1.00	-0.26	90	-0.29	-1.37
8	A553-TYPE1	9.0	3260	13197	10	30.400	2G-H8	131	-1.00	-1.03	95	-1.08	3G-V8	3.26m ×10= 32.6 m	-1.00	-0.26	90	-0.29	-1.37
7	A553-TYPE1	10.5	3260	13197	10	35.460	2G-H7	131	-1.00	-1.03	95	-1.08	3G-V7	3.26m ×10= 32.6 m	-1.00	-0.26	90	-0.29	-1.37
6	A553-TYPE1	12.5	3260	13198	10	42.220	2G-H6	131	-1.00	-1.03	95	-1.08	3G-V6	3.26m ×10= 32.6 m	-1.00	-0.26	90	-0.29	-1.37
5	A553-TYPE1	14.0	3260	13199	10	47.290	2G-H5	131	-1.00	-1.03	95	-1.08	3G-V5	3.26m ×10= 32.6 m	-1.00	-0.26	90	-0.29	-1.37
4	A553-TYPE1	15.5	3260	13199	10	52.360	2G-H4	131	-1.00	-1.03	95	-1.08	3G-V4	3.26m ×10= 32.6 m	-1.00	-0.26	90	-0.29	-1.37
3	A553-TYPE1	17.5	3260	13200	10	59.120	2G-H3	132	-1.00	-1.04	95	-1.09	3G-V3	3.26m ×10= 32.6 m	-1.00	-0.26	90	-0.29	-1.38
2	A553-TYPE1	19.0	3260	13200	10	64.180	2G-H2	132	-1.00	-1.04	95	-1.09	3G-V2	3.26m ×10= 32.6 m	-1.00	-0.26	90	-0.29	-1.38
1	A553-TYPE1	20.5	3260	13201	10	69.250	2G-H1	132	-1.00	-1.04	98	-1.09	3G-V1	3.26m ×10= 32.6 m	-1.00	-0.26	90	-0.29	-1.38
A)	1st Shell + Annular Plate	t1st= 20.5 tAnn= 13.5	3260	13201	N/A	N/A	1F-An	132.0	102.96	106.69	60	177.82	-	-	-	-	-	-	-1.09
[SECL] LP Ethylene / INNER TANK Total =					110	468.1	HLEN =	1576.0	91.96	95.33	98	165.91	VLEN =	358.000	-11.00	-2.85	90	-3.18	162.73
[SECL] LP Ethylene / OUTER TANK Net Weight (설계중량) 　　D= 44 (m), H= 37.8 (m)							Horizontal Weld (수평용접 : 2G) [자동:SAW or 수동:SMAW] [용착효율:SAW (95%) / 수동:SMAW (60%)]						Vertical Weld (수직용접) [ FCAW 용착효율: (90%) ]						합계중량	REMARK	[새창에서] [SECL] LP Ethylene / OUTER TANK 큰 이미지 로 보기 [새창에서] PDF 도면 보기 [새창에서] SHOP_WPS_PQR_SUMBAWA_50K PDF 보기
No.	Material	Thickness (mm)	Width (mm)	Length (mm)	Qty (SHT)	Weight (Ton)	Joint No.	수평용접 총길이 (m)	용입부 단면적 A(mm²)	용접봉 NET중량 (kg)	용착 효율 (%)	용접봉 발주예상 중량(kg)	Joint No.	shCirQty=[10] 수직용접 총길이 VL = 10 PCS × Each S.W(m)	용입부 단면적 A(mm²)	용접봉 NET중량 (kg)	용착 효율 (%)	용접봉 발주예상 중량(kg)	수평+수직 용접봉중량 (kg)	REMARK
11	A553-TYPE1 (Comp. Ring+Top Shell)	35.0	1800	13834	10	68.420	2G-H11	138	720.30	780.30	95	821.37	3G-V11	1.8m ×10= 18 m	-1.00	-0.14	90	-0.16	821.21
10	A553-TYPE1	7.9	3600	13825	10	31.010	2G-H10	138	-1.00	-1.08	95	-1.14	3G-V10	3.6m ×10= 36 m	-1.00	-0.28	90	-0.31	-1.45
9	A553-TYPE1	8.0	3600	13825	10	31.260	2G-H9	138	-1.00	-1.08	95	-1.14	3G-V9	3.6m ×10= 36 m	-1.00	-0.28	90	-0.31	-1.45
8	A553-TYPE1	10.0	3600	13826	10	39.070	2G-H8	138	-1.00	-1.08	95	-1.14	3G-V8	3.6m ×10= 36 m	-1.00	-0.28	90	-0.31	-1.45
7	A553-TYPE1	11.5	3600	13826	10	44.930	2G-H7	138	-1.00	-1.08	95	-1.14	3G-V7	3.6m ×10= 36 m	-1.00	-0.28	90	-0.31	-1.45
6	A553-TYPE1	13.5	3600	13827	10	52.750	2G-H6	138	-1.00	-1.08	95	-1.14	3G-V6	3.6m ×10= 36 m	-1.00	-0.28	90	-0.31	-1.45
5	A553-TYPE1	15.5	3600	13827	10	60.570	2G-H5	138	-1.00	-1.08	95	-1.14	3G-V5	3.6m ×10= 36 m	-1.00	-0.28	90	-0.31	-1.45
4	A553-TYPE1	17.5	3600	13828	10	68.390	2G-H4	138	-1.00	-1.08	95	-1.14	3G-V4	3.6m ×10= 36 m	-1.00	-0.28	90	-0.31	-1.45
3	A553-TYPE1	19.5	3600	13829	10	76.210	2G-H3	138	-1.00	-1.08	95	-1.14	3G-V3	3.6m ×10= 36 m	-1.00	-0.28	90	-0.31	-1.45
2	A553-TYPE1	21.5	3600	13829	10	84.020	2G-H2	138	-1.00	-1.08	95	-1.14	3G-V2	3.6m ×10= 36 m	-1.00	-0.28	90	-0.31	-1.45
1	A553-TYPE1	23.0	3600	13830	10	89.890	2G-H1	138	-1.00	-1.08	98	-1.14	3G-V1	3.6m ×10= 36 m	-1.00	-0.28	90	-0.31	-1.45
A)	1st Shell + Annular Plate	t1st= 23 tAnn= 15	3600	13830	N/A	N/A	1F-An	138.0	129.60	140.40	60	234.00	-	-	-	-	-	-	-1.14
[SECL] LP Ethylene / OUTER TANK Total =					110	646.5	HLEN =	1656.0	839.90	909.90	98	1043.97	VLEN =	378.000	-11.00	-2.94	90	-3.26	1040.71

Design Condition : D=62.200 (m), H=40.230 (m), SG=0.5814, Pg=0.0 (kPa) DLL=36.200 (m), HTL=DLL×SG×1.25 = 21.033 (m) Ht[i] = Hd[i] × SG × 1.25 API 620, FULL, INNER, Pg= 0.0 (kPa) = 0 (mmWTR)												Tank D(m)=	62.2	H(m)=	40.23	DLL(m)=	36.2	Shutdown and Construction Condition [ 내부압력 없는 조건 Pd: 0.0 MPa ], T1s(ShutDown) = Max. Compression (-값) 압축 1) Roof Dead Load Wr = [0.0] Ton 2) Roof Live Load LL = [0.0] Ton = Max( LL, Vacuum, SnowLoad ) 120 kg/m²× At (3038.58)m²= [0.0] Ton Total Load : (1)+(2) Wsum = [0.0] Ton Note 1) : 탱크내부에 진공압력( Vacuum Pressure 0.005 MPa)이 걸렸을 경우에는 나중에 추가 예정 2022.07.15
Shell No. [n]	Material	W[i] (m)	Hd (m)	Ht (m)	P=Pg+P_L (KPa)	T2=P×R (N/mm)	td (mm)	tt (mm)	Used Thk. tu =Max(td,tt , tMin) (mm)	Weight (Ton)	Remark tu(input) (mm)	SKETCH	Each Wtr[n] (mm)	∑Wtr[1~n] 누적(mm)	Remark	tc =tu-CA (mm)	Ratio t / R	누적중량 Stacked Weight W (Ton)	Shell 단면적 Sectional Area A[n] (mm²)	T1=R/2× (P-W/A) (N/mm)	T2=P×R (N/mm)	Sc = T1/tc 수직응력 (-압축,+인장) (MPa)	St = T2/tc 원주막응력 (-압축,+인장) (MPa)	Sts (MPa)	Factor N =St/Sts	Factor M Fact(N)	Scs (MPa)	Sca = M×Scs (MPa)	Stress ratio SRc = Sc/Sca SRt = St/Sts SRtc < 1.0 OK	1. ASME D.1 Sca = M×0.0625×E×tPr (MPa), E = 204,000 (MPa) 2. EN_1993 Sca = 0.0605 × E × Cx(1.0) × tPr (MPa) 3. JIS_LNG Sca = (0.25/γ1=2.25)×E×tPr (MPa) Long-Term 4. JIS_LNG Sca = (0.25/γ2=1.50)×E×tPr (MPa) Short-Term
12	A537-CL2+S5	3.347	0.0	0.0	0	0	9.525	9.525	11.00 (＋1.47)	56.480	11.0 (0.0)	dbgCanvas_650 shCanvas_650 [CANVAS SHOW]	3,347	12,636		9.5	0.000305	56.480	1856367	(-) 2.834	0.0	-0.298	0.0	165.474	0.0000	1.0000	3.791	3.791	0.079 < 1.0 OK	ASME= 3.895, EN1993= 3.77, JIS(L)= 6.924, JIS(S)= 10.386
11	A537-CL2+S5	3.353	2.670	0.0	15.223	473.44	9.525	9.525	12.00 (＋2.47)	61.728	12.0 (0.0)		2,611	9,289		10.5	0.000338	118.208	2051774	(-) 5.932	473.443	-0.565	45.090	165.474	0.2725	0.8355	4.190	3.501	0.161 < 1.0 OK	ASME= 3.597, EN1993= 4.167, JIS(L)= 7.653, JIS(S)= 11.479
10	A537-CL2+S5	3.353	6.023	0.0	34.341	1067.99	9.525	9.525	12.00 (＋2.47)	61.728	12.0 (0.0)		2,611	6,678		10.5	0.000338	179.936	2051774	(-) 9.030	1067.995	-0.860	101.714	165.474	0.6147	0.5392	4.190	2.259	0.381 < 1.0 OK	ASME= 2.321, EN1993= 4.167, JIS(L)= 7.653, JIS(S)= 11.479
9	A537-CL2+S5	3.353	9.376	0.0	53.458	1662.55	11.547	9.525	14.00 (＋2.45)	72.016	14.0 (0.0)		1,688	4,067		12.5	0.000402	251.952	2442588	(-) 12.644	1662.546	-1.012	133.004	165.474	0.8038	0.3160	4.988	1.576	0.642 < 1.0 OK	ASME= 1.619, EN1993= 4.961, JIS(L)= 9.11, JIS(S)= 13.666
8	A537-CL2+S5	3.353	12.729	0.0	72.576	2257.1	15.140	9.525	18.00 (＋2.86)	92.608	18.0 (0.0)		843	2,379		16.5	0.000531	344.560	3224217	(-) 17.292	2257.098	-1.048	136.794	165.474	0.8267	0.2848	6.584	1.875	0.559 < 1.0 OK	ASME= 1.927, EN1993= 6.548, JIS(L)= 12.026, JIS(S)= 18.039
7	A537-CL2+S5	3.353	16.082	0.915	91.693	2851.65	18.733	9.525	22.00 (＋3.27)	113.184	22.0 (0.0)		490	1,536		20.5	0.000659	457.744	4005845	(-) 22.972	2851.650	-1.121	139.105	165.474	0.8406	0.2653	8.181	2.170	0.516 < 1.0 OK	ASME= 2.23, EN1993= 8.135, JIS(L)= 14.941, JIS(S)= 22.412
6	A537-CL2+S5	3.353	19.435	4.268	110.81	3446.2	22.326	9.525	26.00 (＋3.67)	133.776	26.0 (0.0)		314	1,046		24.5	0.000788	591.520	4787473	(-) 29.686	3446.202	-1.212	140.661	165.474	0.8501	0.2517	9.777	2.461	0.492 < 1.0 OK	ASME= 2.528, EN1993= 9.723, JIS(L)= 17.856, JIS(S)= 26.785
5	A537-CL2+S5	3.353	22.788	7.621	129.928	4040.75	25.919	9.525	29.00 (＋3.08)	149.216	29.0 (0.0)		235	732		27.5	0.000884	740.736	5373694	(-) 37.174	4040.754	-1.352	146.937	165.474	0.8880	0.1952	10.974	2.142	0.631 < 1.0 OK	ASME= 2.201, EN1993= 10.913, JIS(L)= 20.043, JIS(S)= 30.064
4	A537-CL2+S5	3.353	26.141	10.974	149.045	4635.31	29.512	11.032	33.00 (＋3.49)	169.808	33.0 (0.0)		167	497		31.5	0.001013	910.544	6155322	(-) 45.696	4635.306	-1.451	147.153	165.474	0.8893	0.1932	12.570	2.429	0.597 < 1.0 OK	ASME= 2.495, EN1993= 12.501, JIS(L)= 22.958, JIS(S)= 34.437
3	A537-CL2+S5	3.353	29.494	14.327	168.163	5229.86	33.105	14.403	36.00 (＋2.9)	185.264	36.0 (0.0)		133	330		34.5	0.001109	1095.808	6741544	(-) 54.994	5229.858	-1.594	151.590	165.474	0.9161	0.1507	13.767	2.075	0.768 < 1.0 OK	ASME= 2.131, EN1993= 13.691, JIS(L)= 25.145, JIS(S)= 37.717
2	A537-CL2+S5	3.353	32.847	17.680	187.28	5824.41	36.698	17.774	39.00 (＋2.3)	200.704	39.0 (0.0)		108	197		37.5	0.001206	1296.512	7327765	(-) 65.066	5824.409	-1.735	155.318	165.474	0.9386	0.1132	14.964	1.694	1.024 > 1.0 NG	ASME= 1.74, EN1993= 14.882, JIS(L)= 27.331, JIS(S)= 40.997
1	A537-CL2+S5	3.353	36.200	21.033	206.397	6418.96	40.291	21.145	42.00 (＋1.71)	216.160	42.0 (0.0)		89	89		40.5	0.001302	1512.672	7913986	(-) 75.915	6418.961	-1.874	158.493	165.474	0.9578	0.0796	16.162	1.286	1.457 > 1.0 NG	ASME= 1.322, EN1993= 16.072, JIS(L)= 29.518, JIS(S)= 44.277
∑W, Hd, Ht(m)=		40.230	36.200	21.033	Total Net Weight, NetWt =					1512.672	Ton		∑Wtr=	12.636	(m)
			Total Gross Weight, GrsWt =							1558.355	Ton
			Equivalent Shell Nominal Thickness (평균두께 부식전)							24.513	mm	Without CA
			Equivalent Shell Corroded Thickness (평균두께 부식후)							23.013	mm	With CA
			Shell Gravity Center from Bottom,(PV Hanbook : 434 Page) Xs = (Aa+Ba+Ca...Z) / (A+B+C..Z) =15.075 [m]							15.075	m

1)	지진계수 Seismic Data ( KGS GC203 2018년 + KDS 41 17 00)
	KGS GC 203 내진설계 성능수준		기능수행	붕괴방지	Unit
	중요도 등급 : GC203 표2.2.1.2.2		특	특
	내진 등급 : GC203 표2.2.3.1 내진등급 분류		내진 특	내진 특
	- 재현주기 : GC203 표2.4 가스시설 내진성능목표	RYEAR =	200	2400	년
	- 위험도계수 ( I ) : GC203 표2.5.3.2 위험도 계수	I =	0.73	2
	지역 계수 ( Z ) : GC203 표2.5.3.1 지진구역계수(Z)	Z =	0.201	0.11	g
	유효수평 지반가속도 S = Z × I	S =	0.1467	0.2200	g
	지반의 분류 : 표.2.5.5 지반의 분류 ( Ground Type )	SOIL =	S4	S4
	단주기 증폭계수 : 지반증폭 계수 (GC203 표 2.5.6.1.2)	Fa =	1.5066	1.36
	장주기 증폭계수 : 지반증폭 계수 (GC203 표 2.5.6.1.2)	Fv =	2.1066	1.96
	유효 지반가속도 : EGA = Fa × S	EGA =	0.221	0.2992	g
2)	표준설계응답스펙트럼 설계수평 지반가속도 계산
	단주기 설계 스펙트럼 가속도, S_DS = 2.5 · Fa · S	S_DS =	0.5525	0.7480	g
	1 sec. 설계 스펙트럼 가속도, S_D1 = Fv · S	S_D1 =	0.3090	0.4312	g
	전이주기의 계산 : To = 0.2 · Ts	To =	0.1119	0.1153	sec
	전이주기의 계산 : Ts = Fv / (2.5 · Fa)	Ts =	0.5593	0.5765	sec
	장 주기, GC203 표 2.5.6.1.1(1)	TL =	3	3	sec