DOCUMENT TYPE:
CALCULATION REPORT DOCUMENT TITLE:
FURNACE STRUCTURE CALCULATION REPORT
4 3 2 1
-
REV.
DATE
-
-
-
PRE.
CHK.
APP.
CONTRACTOR
GEG
-
Issue For Approval
Client
Description
Purpose of Issue
PROJECT TITLE :
GOL-E-GOHAR MEGA MODULE PROJECT Client :
Contractor: MINES & METALS TECHNOLOGICAL ENGINEERING CO.
Client ‘S Project
Project Code
GEG
7
Main Area Code Plant Group Equipment Document Contractor Code Type
119 NAME
1003
7 DATE
FU
Eng. Discipline
Serial No.
S
001
15 MMTE No.
SHEET
REV.
PREPARED
GGMMSF10C4-001 CHECKED APPROVED
B
Contract No. : 90/1942
This document and the information disclosed are the property of MMTE and are not to be used to furnish any information for making of documents or apparatus except where approved by written agreement.
GOL-E-GOHAR MEGA MODULE PROJECT DOCUMENT TITLE
MMTE
Document No: Client Document NO: MMTE Document NO:
FURNACE STRUCTURE CALCULATION REPORT
Rev.
DATE: 1
GGMMSF10C4-001
Page:
REVISION RECORD SHEET P 0 0 0 0 0 0 0 0 0 1 1 1 1 1 1 1 1 1 1 2 2 2 2 2 2 2 2 2 2 3 3 3 3 3 3 3 3 3 3 4 4 4 4 4 4 4 4 4 4 5
R
R
R
Note: This Table is use for External Comments.
P 5 5 5 5 5 5 5 5 5 6 6 6 6 6 6 6 6 6 6 7 7 7 7 7 7 7 7 7 7 8 8 8 8 8 8 8 8 8 8 9 9 9 9 9 9 9 9 9 9 1
R
R
R
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GOL-E-GOHAR MEGA MODULE PROJECT DOCUMENT TITLE
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Table of Contents 1. INTRODUCTION ............................................................................................................................................4 2. GENERAL VIEW ...........................................................................................................................................4 3. STRUCTURAL SYSTEM .................................................................................................................................7 3.1 FOUNDATION ................................................................................................................................. 7 3.2 SUPER STRUCTURE ....................................................................................................................... 7
3.2.1 VERTICAL LOADS ...................................................................................................................... 7 3.2.2 LATERAL LOADS ....................................................................................................................... 7 3.2.3 FLOORS .................................................................................................................................. 7 4. LOADS........................................................................................................................................................8 4.1 DEAD LOAD ................................................................................................................................... 8 4.2 SUPER DEAD LOAD ........................................................................................................................ 8 4.3 LIVE LOAD ..................................................................................................................................... 8 4.4 VESSELS AND EQUIPMENT LOAD ..................................................................................................... 8 4.5 SEISMIC LOAD: ............................................................................................................................. 18
4.5.1 EVALUATION OF SEISMIC LOAD: ............................................................................................... 18 4.6 WIND LOAD: ................................................................................................................................ 19 4.7 THERMAL LOAD ............................................................................................................................ 19 4.8 ERECTION AND MAINTENANCE LOAD ............................................................................................. 19 5. LOAD COMBINATIONS ...............................................................................................................................20 6. ANALYSIS & DESIGN .................................................................................................................................23 6.1 MODELING ................................................................................................................................... 23
6.1.1 STRUCTURE MODELING .......................................................................................................... 23 6.2 DEFORMATIONS ........................................................................................................................... 23 6.3 DYNAMIC ANALYSIS ...................................................................................................................... 23 7.1 INTERNAL FORCES ....................................................................................................................... 24 7.2 DESIGN RATIO ............................................................................................................................. 24
GOL-E-GOHAR MEGA MODULE PROJECT DOCUMENT TITLE
FURNACE STRUCTURE CALCULATION REPORT
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MMTE Rev.
DATE: 1
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Page:
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1. INTRODUCTION This document contains Calculation Report for analysis and design of Furnace structure. For material characteristics and construction considerations, refer to Document No. GGMMSF10C0-001 and GGMMCF10C0-001. Overall structural systems Foundation Reinforced Concrete Grade slab Reinforced Concrete Structure Steel Structure above GL+ (0.00) m Stairs Steel Structure + Grating Walkways and platforms Steel Structure + Grating
2. GENERAL VIEW Location of structure in plant site is shown in Figure 1.
Figure 1: Location in Plant Site
GOL-E-GOHAR MEGA MODULE PROJECT DOCUMENT TITLE
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MMTE Rev.
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In Figure 2 and Figure 3, three dimensional views of the structure are shown:
second Part
Main Part
Figure 2: 3D View A
Page:
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Figure 3: 3D View B
Page:
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GOL-E-GOHAR MEGA MODULE PROJECT DOCUMENT TITLE
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In Figure 4 the foundation configuration is shown.
Figure 4 - Furnace Foundation
3. STRUCTURAL SYSTEM 3.1 FOUNDATION Foundation structural system is a 3 m thick reinforced concrete mat foundation. The top level of the foundation is 1 m under the finished ground level.
3.2 SUPER STRUCTURE 3.2.1 VERTICAL LOADS Vertical loads are supported by Steel Frames.
3.2.2 LATERAL LOADS According to ISIRI No. 2800 Iranian code of seismic resistant design of buildings for structures with height of 70m and more, Dual system composed of special moment resisting frames and braces should be used. For this type of structural systems, behavior factor is R=9 and there are some restrictions on columns to be stronger than beams. But in this structure, at some points such as beams under the furnace equipment, this cannot be achieved. Because at that level there are heavy beams to support the furnace equipment which are much stronger than the columns. On the other hand at that level there are still other columns that satisfy the beam to column strength ratio, so even if there may hinges occur in some columns, only part of lateral stability will be lost. Knowing that the main masses are below 70m level, and the above mentioned characteristics of this structure and applying all requirements of special moment resisting frames in members and connection design (except for the above mentioned points), behavior factor will be considered R=7 instead of 9. 3.2.3 FLOORS All floors are mainly covered by 32mm grating and there is a platform covered with 8mm chequered plate at the top of elevator.
GOL-E-GOHAR MEGA MODULE PROJECT DOCUMENT TITLE
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4. LOADS 4.1 DEAD LOAD Weight of structural components is included in analytical model based on specific weight of 25KN/m3 for concrete and 78.5KN/m3 for steel parts.
4.2 SUPER DEAD LOAD Super dead loads are dead load of non-structural components such as following items: Grating floors: Chequered plate floors
0.55 KN/m2 0.65 KN/m2
4.3 LIVE LOAD Live loads include the followings: Main Platforms: Auxiliary Platforms: Gangways and stairs: Roof
5.0 KN/m² 5.0 KN/m² 3.5 KN/m² 1.5 KN/m²
4.4 VESSELS AND EQUIPMENT LOAD Location and amount of each vessel or equipment point loads for individual cases are tabulated in Table 1.
GOL-E-GOHAR MEGA MODULE PROJECT DOCUMENT TITLE
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Page:
Table 1 - Vessels and Equipments
Item
Description
Mecha nical Weight (Ton)
Weight Of Material (Ton)
Refractory Weight (Ton)
Operationa l Weight (Ton)
Elevation and Centre Of Gravity (mm)
13360 1
7.6
18.4
-
56
(COG)
26245 2
Product Discharge Chamber Duct
3
Product Discharge Chamber
24
10
6
40
4
Bottom Discharge Bubbler
5
-
-
-
5
Product Cooler
38
-
-
38
(+100 0 COG) 21110 (COG)
21110 (COG)
26245 75
870
48
993
(+154 6 COG)
3D Shape from Analytical Model
9 of 24
GOL-E-GOHAR MEGA MODULE PROJECT DOCUMENT TITLE
Document No:
1
GGMMSF10C4-001
26245
6
Cooling Gas Scrubber
86
500
-
-
7
CGS offtake
-
-
-
12
36135
8
Cooling Gas Duct
-
-
-
80
36135
9
Spring Hanger
-
-
-
13.5
37810
10
Top Gas Scrubber
(-1806 COG
37810 122
-
-
Rev.
DATE:
Client Document NO: MMTE Document NO:
FURNACE STRUCTURE CALCULATION REPORT
MMTE
710
(-1026 COG)
Page:
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Rev.
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FURNACE STRUCTURE CALCULATION REPORT
MMTE
1
GGMMSF10C4-001
50500 (+502 5 COG)
11
Reduction Furnace
358
1500
516
2500
12
Top Gas Scrubber Duct
13
-
53
-70
60150
13
Top Gas Scrubber Ventrury
21
-
8
29
56170
14
Burden Feeder Water Tank
5
12.4
-
18
62350
Page:
11 of 24
GOL-E-GOHAR MEGA MODULE PROJECT DOCUMENT TITLE
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GGMMSF10C4-001
15
Charge Hopper
41
16
Bucket Elevator
See Attached Drawing recieved from Mechanical Discipline.
17
18
19
Bustle Gas Duct
327
-
Rev.
DATE:
Client Document NO: MMTE Document NO:
FURNACE STRUCTURE CALCULATION REPORT
MMTE
370
88550
15060 21110 97210
-
-
-
94
15960
-
-
-
20.5
50500
-
-
-
8.9
61870
Page:
12 of 24
GOL-E-GOHAR MEGA MODULE PROJECT DOCUMENT TITLE
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20
Monorail
-
-
-
3.5
25110
21
Maintenanc e Hoist (one of the three parallel monorails)
-
-
-
15
56170
22
Maintenanc e Hoist
-
-
-
10
56170
23
Shaft Furnace Hoist
-
-
-
10
10375 0
24
Elevator Hoist
-
-
-
2.5
59112
25
Elevator
-
-
-
10
-
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GOL-E-GOHAR MEGA MODULE PROJECT DOCUMENT TITLE
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26
-
MMTE
-
-
Rev.
DATE: 1
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-
Fz=-18
-
Fz= -16 Fx=14. 7
34740
Fz= -2 Fx= 1.2
34740
Page:
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34740
26
27
-
28
-
-
-
-
-
-
28
27
Important Note: -All equipments are assumed rigid in analytical model. -All piping loads are tabulated as below. Refer to appendices which show the location of loads. (x,y = 0,0 refers to Grids : "1,DT" and also z=0 refers to elevation +0.000.) TABLE: Joint Coordinates Joint
CoordSys
CoordType
XorR
Y
Z
F3
Text
Text
Text
m
m
m
KN -68.67
PS-1001
GLOBAL
Cartesian
12.8002
30.9502
50.5
PS-1002E
GLOBAL
Cartesian
9.5
32.91587
37.81
-10.8
PS-1002F
GLOBAL
Cartesian
8.80103
34.24189
37.81
-78.5
PS-1003
GLOBAL
Cartesian
1.5003
30.9505
26.245
-88.3
PS-1003A
GLOBAL
Cartesian
1.5003
34.2505
26.245
-176.6
PS-1004
GLOBAL
Cartesian
4.5003
30.9505
32.635
-200
PS-1004A
GLOBAL
Cartesian
4.5003
34.9455
32.635
-147.15 -1.77
PS-1004B
GLOBAL
Cartesian
4.5003
32.5955
32.635
PS-1005
GLOBAL
Cartesian
11.33
30.1755
50.5
-5
PS-1010
GLOBAL
Cartesian
11.33
32.0065
50.5
-4.9
PS-1012
GLOBAL
Cartesian
10.49973
17.96218
70.15
-13.73
PS-1013
GLOBAL
Cartesian
10.5
17.81162
76.05
-3.73
PS-1014
GLOBAL
Cartesian
10.5
20.5272
76.05
-3.92
PS-1015
GLOBAL
Cartesian
17.01791
21.3754
79.95
-10.8
PS-1017
GLOBAL
Cartesian
24.3917
14.85
34.74
-26.5
PS-1018
GLOBAL
Cartesian
24.39
14.8501
50.5
-200
PS-1020
GLOBAL
Cartesian
23.5
14.95275
76.05
-210
PS-1023
GLOBAL
Cartesian
1.5005
37.4508
8.6
-88.3
PS-1024
GLOBAL
Cartesian
7.6367
39.929
14.42
-32.4
PS-1027
GLOBAL
Cartesian
10.98
40.4083
44.35
-117.7
PS-1029
GLOBAL
Cartesian
-2.09
17.96656
26.245
-55.9
PS-1030
GLOBAL
Cartesian
11.524
32.5004
60.15
-18.15
PS-1031B
GLOBAL
Cartesian
11.524
36.0004
60.15
-21.58
PS-1031C
GLOBAL
Cartesian
11.524
30.3004
60.15
-18.15
PS-1032
GLOBAL
Cartesian
12.9001
28.6504
65.85
-28.45
PS-1033
GLOBAL
Cartesian
8.03207
16.50022
26.245
-23.55
PS-1035
GLOBAL
Cartesian
10.5
17.99458
50.5
-5.89
GOL-E-GOHAR MEGA MODULE PROJECT DOCUMENT TITLE
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FURNACE STRUCTURE CALCULATION REPORT
Client Document NO: MMTE Document NO:
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DATE: 1
GGMMSF10C4-001
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PS-1037
GLOBAL
Cartesian
20.377
30.8732
26.245
PS-1038
GLOBAL
Cartesian
24.59629
35.78787
30.85
-88.3 -9.8
PS-1039
GLOBAL
Cartesian
24.5748
41.4221
28.745
-103
PS-1047
GLOBAL
Cartesian
10.49982
38.03396
20.11
-5.89
PS-1048
GLOBAL
Cartesian
9.7627
37.8
14.96
-5.65
PS-1051
GLOBAL
Cartesian
4.24268
29.50026
26.245
-11.77
PS-1052
GLOBAL
Cartesian
5.7767
36.2703
15.06
-117.7
PS-1056
GLOBAL
Cartesian
20.60886
35.0005
26.245
-29.4
PS-1093
GLOBAL
Cartesian
0.775
40.4083
30.85
-187
PS-1094
GLOBAL
Cartesian
8.55117
40.46946
37.81
-20
PS-1106B
GLOBAL
Cartesian
10.5
31.90157
44.35
-10.8
PS-1106C
GLOBAL
Cartesian
10.5
32.29364
44.35
-3.14
PS-1106F
GLOBAL
Cartesian
10.5
34.03929
44.35
-98.1
PS-11072
GLOBAL
Cartesian
26.732
23.0003
15.06
-3
PS-11075
GLOBAL
Cartesian
11.3753
37.0005
37.81
-6.87
PS-11080
GLOBAL
Cartesian
-5.064E-13
28.0203
8.6
-5.89
PS-11083
GLOBAL
Cartesian
1.57843
19.1503
13.36
-3.52
PS-11084
GLOBAL
Cartesian
7.65638
19.1503
13.36
-3.48
PS-1125
GLOBAL
Cartesian
3.149
17.3372
8.6
-8.95
PS-1126
GLOBAL
Cartesian
5.324
17.3372
8.6
-9.4
PS-1127
GLOBAL
Cartesian
7.5005
17.3372
8.6
-5.06
PS-1155
GLOBAL
Cartesian
13.65
17.3393
26.245
-5.2
PS-1171
GLOBAL
Cartesian
17.8001
28.6504
65.85
-28.45
PS-1186A
GLOBAL
Cartesian
23.4998
38.2071
15.06
-3.92
PS-1242
GLOBAL
Cartesian
21.2001
34.2504
50.5
-7.36
PS-1246
GLOBAL
Cartesian
23
32.7005
45
-11.77
PS-1247
GLOBAL
Cartesian
24.203
32.8502
44.35
-11.77
PS-1248
GLOBAL
Cartesian
23.08783
32.7005
44.35
-58.9
PS-1250
GLOBAL
Cartesian
24.4003
32.8005
30.85
-93.2
PS-1252
GLOBAL
Cartesian
21.85
36.8222
50.5
-13.73
PS-1253
GLOBAL
Cartesian
20.1002
38.05712
50.5
-19.6
PS-1254
GLOBAL
Cartesian
24.4928
37.0441
44.35
-14.7
PS-1254A
GLOBAL
Cartesian
24.4928
36.0301
44.35
-34.33
PS-1255
GLOBAL
Cartesian
12.2502
35.5003
50.5
-11.77
PS-1258
GLOBAL
Cartesian
7.637
29.5002
32.635
-24.5
PS-1259
GLOBAL
Cartesian
7.6502
27.6005
36.135
-16.68
PS-1260
GLOBAL
Cartesian
7.60791
20.0005
36.135
-9.8
PS-1266
GLOBAL
Cartesian
22.798
36.0005
26.245
-9.8
PS-1269
GLOBAL
Cartesian
22.798
32.5005
26.245
-9.8
PS-1272
GLOBAL
Cartesian
22.798
34.2505
26.245
-9.8
PS-1273
GLOBAL
Cartesian
23.4997
38.1292
29.045
-13.73
PS-1281
GLOBAL
Cartesian
24.7418
39.9241
28.745
-31.4
PS-1283
GLOBAL
Cartesian
24.7418
36.0311
37.81
-22.56
PS-1287
GLOBAL
Cartesian
12.95671
15.0005
34.74
-27.6
PS-1288
GLOBAL
Cartesian
8.2213
29.5005
36.135
-3.43
PS-1289
GLOBAL
Cartesian
12.934
12.5003
34.74
-25.5
PS-1290
GLOBAL
Cartesian
2.4403
17.7455
32.635
-60
PS-1306
GLOBAL
Cartesian
11.6502
32.69384
50.5
-5.89
PS-1310
GLOBAL
Cartesian
1.7
27.5503
32.635
-5
PS-1319
GLOBAL
Cartesian
23.16363
32.7005
44.35
-5.89
PS-1328A
GLOBAL
Cartesian
25.25
17.52394
20.11
-8.83
PS-1329A
GLOBAL
Cartesian
25.25
22.15976
20.11
-8.92
GOL-E-GOHAR MEGA MODULE PROJECT DOCUMENT TITLE
Document No:
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Client Document NO: MMTE Document NO:
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DATE: 1
GGMMSF10C4-001
Page:
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PS-1330
GLOBAL
Cartesian
24.8401
29.5003
20.11
-4.02
PS-1330A
GLOBAL
Cartesian
25.09311
29.5003
20.11
-12.16 -4.02
PS-1330B
GLOBAL
Cartesian
24.33011
29.5003
20.11
PS-1331
GLOBAL
Cartesian
24.8947
38.66338
20.11
-4.4
PS-1334
GLOBAL
Cartesian
11.19646
40.5859
26.245
-26.5
PS-1336
GLOBAL
Cartesian
12.556
36.4253
26.245
-5.89
PS-1337
GLOBAL
Cartesian
7.64796
39.0003
26.245
-34.33
PS-1343A
GLOBAL
Cartesian
24.504
28.5673
97.21
-25.5
PS-1344
GLOBAL
Cartesian
24.52421
27.6121
83.35
-0.8
PS-1344A
GLOBAL
Cartesian
24.325
28.2103
83.35
-25
PS-1345
GLOBAL
Cartesian
24.596
27.7262
76.05
-35 -34.33
PS-1345A
GLOBAL
Cartesian
24.504
28.5672
76.05
PS-1346
GLOBAL
Cartesian
24.306
30.8732
56.17
-35
PS-1348
GLOBAL
Cartesian
24.316
30.8732
37.81
-78.5
PS-1350
GLOBAL
Cartesian
-1.1902
26.2901
35.495
-450
PS-1352
GLOBAL
Cartesian
17.025
27.1005
26.245
-3.43
PS-1354
GLOBAL
Cartesian
12.0502
24.08
26.245
-4.9
PS-1356
GLOBAL
Cartesian
-1.2797
23.798
26.245
-19.62
PS-1357
GLOBAL
Cartesian
-1.2874
23.80735
18.36
-98.1
PS-1359
GLOBAL
Cartesian
-5.124E-13
32.43913
15.06
-9.8
PS-1362A
GLOBAL
Cartesian
4.25
28.6003
18.36
-9.8
PS-1376
GLOBAL
Cartesian
16.6502
28.2754
56.17
-3.92
PS-1377
GLOBAL
Cartesian
22.23145
24.37705
56.17
-5.89
PS-1386
GLOBAL
Cartesian
7.5777
39
15.06
-4.905
PS-1388
GLOBAL
Cartesian
7.5777
32.08
15.06
-4.9
PS-1400
GLOBAL
Cartesian
10.5
35.86677
56.17
-3.92
PS-1405
GLOBAL
Cartesian
21.7002
27.9754
50.5
-3.92
PS-1407
GLOBAL
Cartesian
10.5
33.64311
50.5
-3.92
PS-1408
GLOBAL
Cartesian
9.12182
34.25035
26.245
-8.15
PS-1409
GLOBAL
Cartesian
9.122
39.0003
26.245
-7.35
PS-1410
GLOBAL
Cartesian
10.49991
33.59791
20.11
-14.7
PS-1411
GLOBAL
Cartesian
10.49987
35.49651
20.11
-7.85
PS-1412A
GLOBAL
Cartesian
-0.0002
36.1001
20.11
-5.89
PS-1423
GLOBAL
Cartesian
1.5
30.9503
8.6
-120
PS-1424
GLOBAL
Cartesian
1.5
25.7713
8.6
-30.6
PS-1425
GLOBAL
Cartesian
1.5005
22.5008
8.6
-67.9
PS-1426
GLOBAL
Cartesian
5.7767
29.909
15.06
-49.05
PS-1460
GLOBAL
Cartesian
18.485
30.8003
60.15
-4.9
PS-1460A
GLOBAL
Cartesian
17.9
30.8003
60.15
-8.2
PS-1460B
GLOBAL
Cartesian
17.35
30.8003
60.15
-6.8
PS-1460C
GLOBAL
Cartesian
16.8
30.8003
60.15
-4.42
PS-1460D
GLOBAL
Cartesian
16.3
30.8003
60.15
-4.42
PS-1460E
GLOBAL
Cartesian
15.8
30.8003
60.15
-4.42
PS-1461
GLOBAL
Cartesian
20.743
31.2703
60.15
-4.42
PS-1462
GLOBAL
Cartesian
21.95005
33.56317
56.17
-4.905
PS-1463
GLOBAL
Cartesian
21.95
34.9002
56.17
-11.77
PS-1465
GLOBAL
Cartesian
23.17732
30.4504
56.17
-8.83
PS-1465A
GLOBAL
Cartesian
22.5575
31.4004
56.17
-3.24
PS-1466
GLOBAL
Cartesian
23.5
36.96228
60.15
-13.25
PS-1467
GLOBAL
Cartesian
21.774
33.4364
60.15
-31.4
PS-1486
GLOBAL
Cartesian
15.53713
39.87128
15.06
-3.43
PS-1486B
GLOBAL
Cartesian
14.90366
39.8713
15.06
-5.89
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PS-1487
GLOBAL
Cartesian
15.5148
39.6721
26.245
PS-1487B
GLOBAL
Cartesian
14.9068
39.6721
26.245
-5.89 -7.85
PS-1488
GLOBAL
Cartesian
15.61719
39.55706
37.81
-5.89
PS-1488B
GLOBAL
Cartesian
14.98751
39.55706
37.81
-4.22
PS-1488C
GLOBAL
Cartesian
14.41225
39.55706
37.81
-3.35
PS-1489B
GLOBAL
Cartesian
14.9606
39.85273
44.35
-11.6
PS-1490
GLOBAL
Cartesian
15.50106
39.00026
56.17
-3.14
PS-1490B
GLOBAL
Cartesian
14.70194
39.00027
56.17
-3.92
PS-1491
GLOBAL
Cartesian
14.80386
36.1504
56.17
-5.89 -5.89
PS-1497
GLOBAL
Cartesian
2.87942
39.0001
20.11
PS-1498A
GLOBAL
Cartesian
9.666
30.2252
26.245
-3.92
PS-1507
GLOBAL
Cartesian
14
0.0002
8.6
-3.92
PS-1517A
GLOBAL
Cartesian
24.23526
31.63564
44.35
-3.92
PS-1518A
GLOBAL
Cartesian
23.5
31.81882
56.17
-19.6
PS-1526B
GLOBAL
Cartesian
19.3001
30.1484
60.15
-22.95
PS-1526C
GLOBAL
Cartesian
19.3001
29.9244
60.15
-39.73
PS-1526D
GLOBAL
Cartesian
19.3001
29.6744
60.15
-29.45
PS-1526E
GLOBAL
Cartesian
19.3001
29.5004
60.15
-9.8
PS-1535
GLOBAL
Cartesian
14.56653
39.00027
60.15
-39.25
PS-1536
GLOBAL
Cartesian
12.5
28.55439
97.21
-34.33
PS-1536A
GLOBAL
Cartesian
10.5
27.78918
88.55
-18.85
PS-1537
GLOBAL
Cartesian
10.5
27.72735
76.05
-36.3
PS-1538
GLOBAL
Cartesian
10.50009
27.59887
65.85
-14.7
PS-1539
GLOBAL
Cartesian
10.5
27.41443
56.17
-88.3
PS-1540
GLOBAL
Cartesian
10.5
27.68986
44.35
-11.78
PS-1541
GLOBAL
Cartesian
8.5003
28.93777
32.635
-19.6
PS-1542
GLOBAL
Cartesian
9.375
29.0252
26.245
-14.7
PS-1543
GLOBAL
Cartesian
9.33402
29.5003
13.36
-4.9
PS-1544
GLOBAL
Cartesian
8.5005
29.03819
8.6
-5.89
PS-1562
GLOBAL
Cartesian
3.45
39.0003
15.06
-7.85
PS-1565
GLOBAL
Cartesian
15.7588
12.1221
8.6
-11.77
PS-1573
GLOBAL
Cartesian
2.25
25.8533
8.6
-9
PS-1574
GLOBAL
Cartesian
9.503
39.0003
30.85
-3.63
PS-1577
GLOBAL
Cartesian
24.2028
38.1291
44.35
-5.4
PS-1627
GLOBAL
Cartesian
15.1001
32.63111
56.17
-8.15
PS-1635
GLOBAL
Cartesian
2.0503
19.0505
36.135
-5.5
PS-1636
GLOBAL
Cartesian
3.8503
19.0505
36.135
-35.3
PS-1655
GLOBAL
Cartesian
13.9002
38.05182
50.5
-47
PS-1683
GLOBAL
Cartesian
3.9
17.0173
13.36
-9.8
PS-1684
GLOBAL
Cartesian
6.884
17.0173
13.36001
-49
PS-1685
GLOBAL
Cartesian
9.338
17.0173
13.36001
-44.65
PS-1686
GLOBAL
Cartesian
9.3375
17.3397
18.36
-93.2
PS-1713
GLOBAL
Cartesian
13.7
16.5003
8.6
-3.43
PS-1714
GLOBAL
Cartesian
13.7
12.7502
8.6
-3.14
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4.5 SEISMIC LOAD: According to ISIRI No. 2800 Iranian code of seismic resistant design of buildings for structures with height of 70m and more, Dual system composed of special moment resisting frames and braces should be used. For this type of structural systems, behavior factor is R=9 and there are some restrictions on columns to be stronger than beams. But in this structure, at some points such as beams under the furnace equipment, this cannot be achieved. Because at that level there are heavy beams to support the furnace equipment which are much stronger than the columns. On the other hand at that level there are still other columns that satisfy the beam to column strength ratio, so even if there may hinges occur in some columns, only part of lateral stability will be lost. Knowing that the main masses are below 70m level, and the above mentioned characteristics of this structure and applying all requirements of special moment resisting frames in members and connection design (except for the above mentioned points), behavior factor will be considered R=7 instead of 9.
4.5.1 EVALUATION OF SEISMIC LOAD: Important Note: Shear base in Flexible Model should be more than that in Fixed Base Model. Soil Type : To Ts S Mass x = Mass y = T x dyn (Flexible Model) = T y dyn (Flexible Model) = T x dyn (Fixed Base) = T y dyn (Fixed Base) = H= I= Ct x = Ct y = Rx= Ry= A=
X Direction T 1x = Ct x x H3/4 Static Period Multiplier (0.8 or 1) T x st
II 0.1 0.5 1.5 97668 97668 1.912 Sec. 1.540 Sec. 1.249 Sec. 1.105 Sec. 107 m 1.2 0.05 0.05 7 7 0.30 g
T = MIN(1.25 x T x st ,T Bx1 Bx min=0.1 x Rx Bx Cx (Flexible)=ABI/Rx Vx
x dyn
)
Y Direction T 1y = Ct y x H3/4 Period Multiplier (0.8 or 1) T y st T = MIN(1.25 x T y st ,T y dyn ) B By min=0.1xRy By Cy (Flexible)=ABI/Ry Vy
Flexible Model
Fixed Base
1.663 Sec 1.0 1.663 Sec. 1.912 Sec. 1.022 0.700 1.022 0.05258 5135 KN
1.663 Sec 1.0 1.663 Sec. 1.249 Sec. 1.358 0.700 1.358 0.06984 6821 KN
1.663 S1.0
1.663 Sec. 1.0 1.663 Sec. 1.105 Sec. 1.473 0.700 1.473
1.663 S 1.540 S 1.181 0.700 1.181 0.06074 5932 KN
Spectrum Diagram
B
3.0 2.5 2.0 1.5 1.0 0.5 0.0 0.0
0.5
1.0
1.5
2.0
Period (T Sec.)
2.5
3.0
3.5
4.0
0.07578 7401 KN
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4.6 WIND LOAD: Wind loads are evaluated as mentioned in General Design Criteria and are applied on analytical model of the structure. INBC Part 6: V= 130 km/h q = 0.005 x V2= 0.005 x 1302 = 84.5 Kg/m2 P = Ce x Cq x q C e = According to table below C q = As shown below
P (Kg/m2) Height
Ce
V
q
cq= 0.5
cq= 0.7
cq= 0.8
0-10
2
130
84.5
84.5
118.3
135.2
10-20
2.2
130
84.5
93.0
130.1
148.7
20-30
2.4
130
84.5
101.4
142.0
162.2
30-40
2.5
130
84.5
105.6
147.9
169.0
40-50
2.6
130
84.5
109.9
153.8
175.8
50-60
2.7
130
84.5
114.1
159.7
182.5
60-80
2.8
130
84.5
118.3
165.6
189.3
80-100
2.9
130
84.5
122.5
171.5
196.0
100-120
3
130
84.5
126.8
177.5
202.8
4.7 THERMAL LOAD Effect of +/-30 degrees Celsius change in steel parts will be taken into account.
4.8 ERECTION AND MAINTENANCE LOAD No special erection load is noted on drawings. Refractory lining is assumed to be completed gradually and in a symmetrical pattern.
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5. LOAD COMBINATIONS Following tables describe the load cases and combination factors for design of foundation, concrete and steel parts. Table 2, includes load cases and Table 3, includes load combination factors that are used in this structure. In tables 1 & 2 env (…) means the envelop effect of loads written in parentheses Table 2: Load Cases Definition Load Cases Structural Loads
Type
Description
Intermediate Load cases
Dead00
Dead
Weight of structure alone
ALLDead= Soil+Dead00+Supd100+EMDL100
Supd100
Dead
Soil
Dead
Live20
Live
SpecX* SpecY*
Weight of floors+grating+internal walls+finishing+… Weight of the soil over the foundation Live loads that contribute in Earthquake 20% Earthquake Loads in X dir: Spectrum Analysis Earthquake Loads in Y dir: Spectrum Analysis Earthquake Loads in X dir: Auto Lateral Loading Earthquake Loads in Y dir: Auto Lateral Loading
EQX
Quake
EQY
Quake
WLX
Wind
Wind Load in +X dir
WLXN
Wind
Wind Load in -X dir
WLY
Wind
Wind Load in +Y dir
WLY
Wind
Wind Load in -Y dir
TL
Thermal
-------
Main Load cases
ALLLive=Live20+ EMLL100
Fv=( 0.7AI=0.2625) x ALLDead (Seismic Vertical Effect) FvN= - Fv
FvEnv=env(Fv, FvN)
Equipment Loads EMDL100
Dead
EMLL100
Live
EMEXLO
Quake
EMEYLO
Quake
CRV1 ~ CRV6
Other
Equipment Dead Loads that contribute in Earthquake 100% Equipment Live loads that contribute in Earthquake100% Equipment Earthquake Load in X dir (Local Earthquake) Equipment Earthquake Load in Y dir (Local Earthquake) Vertical Crane load at different levels (including impact factor : 1.25)
CRV= ENV(CRV1 ~ CRV6)
*: This note should be taken into account that in Load Combinations The positive and negative sign of SpecX and SpecY will be considered by software SAP2000.
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Table 3: Load Combination Factors
Design Combinations (for Soil Pressure Evaluation and Steel Design)
Design Combinations (for Equipment Supporting Elements Design) *
ALLDead
ALLLive
CRV
ASD1
1
1
1
ASD2
1
ASD3
0.75
0.75
0.375
ASD4
0.75
0.75
0.375
ASD5
0.75
0.75
0.375
ASD6
0.75
0.75
0.375
ASD7
0.75
ASD8
0.75
ASD9
0.75
ASD10
0.75
ASD11
0.75
0.75
ASD12
0.75
0.75
ASD13
0.75
0.75
ASD14
TL
WLX
WLY
WLXN
WLYN
SpecX
SpecY
FvEnv
0.375
0.75
0.225
0.225
0.375
0.225
0.75
0.225
0.375
0.225
0.225
0.75
0.75
0.75
0.225
0.225
ASD15
0.75
0.225
0.75
0.225
ASD16
0.75
0.225
0.225
0.75
ASD17-1
1
ASD17-2
0.67
0.67
0.67
0.67
ASD17-3
0.67
0.67
0.67
ASD17-4
0.67
0.67
0.67
ASD17-5
0.67
ASD17-6 ASD17-7
EMEYLO
EMEXLO
0.75 0.75 0.75 0.75 0.75 0.75 0.75 0.75
0.9 0.201
0.201
0.201
0.67
0.201
0.201
0.201
0.67
0.67
0.67
0.201
0.201
0.67
0.67
0.201
0.67
0.201
0.67
0.67
0.201
0.201
0.67
ASD18
0.75
0.75
0.375
0.225
0.75
0.225
ASD19
0.75
0.75
0.375
0.225
0.75
-0.225
ASD20
0.75
0.75
0.375
0.225
-0.75
0.225
ASD21
0.75
0.75
0.375
0.225
-0.75
-0.225
ASD22
0.75
0.75
0.375
0.225
0.225
0.75
ASD23
0.75
0.75
0.375
0.225
0.225
-0.75
ASD24
0.75
0.75
0.375
0.225
-0.225
0.75
ASD25
0.75
0.75
0.375
0.225
-0.225
-0.75
ASD26
0.75
0.75
0.375
0.75
0.225
0.225
ASD27
0.75
0.75
0.375
0.75
0.225
-0.225
ASD28
0.75
0.75
0.375
0.75
-0.225
0.225
ASD29
0.75
0.75
0.375
0.75
-0.225
-0.225
ASD30
0.75
0.225
0.75
0.225
ASD31
0.75
0.225
0.75
-0.225
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ASD32
0.75
0.225
-0.75
0.225
ASD33
0.75
0.225
-0.75
-0.225
ASD34
0.75
0.225
0.225
0.75
ASD35
0.75
0.225
0.225
-0.75
ASD36
0.75
0.225
-0.225
0.75
ASD37
0.75
0.225
-0.225
-0.75
ASD38
0.75
0.75
0.225
0.225
ASD39
0.75
0.75
0.225
-0.225
ASD40
0.75
0.75
-0.225
0.225
ASD41
0.75
0.75
-0.225
-0.225
Design Combinations
ASDF1
0.75
0.75
1.8
0.54
0.225
ASDF2
0.75
0.75
0.54
1.8
0.225
(With Over Strength Factor)
ASDF3
0.75
1.8
0.54
0.225
ASDF4
0.75
0.54
1.8
0.225
USD1
1.4
USD2
1.4
USD3
1.05
1.275
USD4
1.05
1.275
USD5
1.05
1.275 1.275
1.7
1.275 1.275 1.275
USD6
1.05
Design Combinations
USD7
0.9
(for Concrete Design)
USD8
0.9
USD9
0.9
USD10
0.9
USD11
1.05
1.275
1.4025
0.4208
USD12
1.05
1.275
0.4208
1.4025
USD13
1.05
1.4025
0.4208
USD14
1.05
0.4208
1.4025
USD15 Checking Combinations
ASD USD
1.4 env(ASD1 to ASD16) env(USD1 to USD15)
1.275 1.3 1.3 1.3 1.3
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6. ANALYSIS & DESIGN 6.1 MODELING According to standard No. 2800-05 3rd editions in Dual system, Flexural Frame must resist against 25% of Seismic Loads.
6.1.1 STRUCTURE MODELING In order for the purpose which goes in the previous section to be satisfied two Different SAP Analysis Model is prepared. Furthermore, the other model -Fixed Base Model- was prepared for comparing the design results between Flexible Model and Fixed Base one.
6.2 DEFORMATIONS Height of structure H=107 m In X and Y direction: Max ∆ W = (0.02x107)/(0.7x7)= 0.436 m For more information about the lateral drift refer to the appendices.
6.3 DYNAMIC ANALYSIS Dynamic analysis of structure will be performed in order to evaluate the seismic effect on structural components. 90 percent of the mass in each direction should be activated. TABLE: Modal Participating Mass Ratios OutputCase StepType StepNum Period UX UY UZ SumUX SumUY Text Text Unitless Sec Unitless Unitless Unitless Unitless Unitless MODAL Mode 1 1.912 0.727 0.006 0.000 0.727 0.006 MODAL Mode 2 1.540 0.006 0.723 0.000 0.733 0.730 MODAL Mode 3 1.267 0.000 0.005 0.000 0.733 0.734 MODAL Mode 4 1.081 0.000 0.000 0.000 0.733 0.734 MODAL Mode 5 1.052 0.001 0.000 0.000 0.734 0.734 MODAL Mode 6 0.975 0.000 0.000 0.000 0.734 0.734 MODAL Mode 7 0.967 0.006 0.000 0.000 0.739 0.734 MODAL Mode 8 0.926 0.003 0.000 0.000 0.742 0.735 MODAL Mode 9 0.913 0.000 0.002 0.000 0.742 0.737 MODAL Mode 10 0.803 0.009 0.000 0.000 0.751 0.737 MODAL Mode 11 0.719 0.098 0.000 0.000 0.848 0.737 MODAL Mode 12 0.706 0.000 0.002 0.000 0.849 0.739 MODAL Mode 13 0.670 0.000 0.003 0.000 0.849 0.741 MODAL Mode 14 0.665 0.000 0.000 0.000 0.849 0.742 MODAL Mode 15 0.652 0.002 0.014 0.000 0.851 0.756 MODAL Mode 16 0.644 0.000 0.076 0.000 0.851 0.832 MODAL Mode 17 0.601 0.000 0.001 0.000 0.851 0.833 MODAL Mode 18 0.595 0.000 0.000 0.000 0.851 0.833 MODAL Mode 19 0.578 0.000 0.000 0.000 0.851 0.833 MODAL Mode 20 0.576 0.000 0.001 0.000 0.851 0.834 MODAL Mode 21 0.560 0.000 0.000 0.000 0.851 0.834 MODAL Mode 22 0.558 0.000 0.000 0.000 0.851 0.834 MODAL Mode 23 0.551 0.000 0.003 0.000 0.851 0.837 MODAL Mode 24 0.542 0.001 0.000 0.000 0.852 0.837 MODAL Mode 25 0.519 0.000 0.001 0.000 0.852 0.838 MODAL Mode 26 0.511 0.000 0.000 0.000 0.852 0.838
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MODAL MODAL MODAL MODAL MODAL MODAL MODAL MODAL MODAL MODAL MODAL MODAL MODAL MODAL MODAL MODAL MODAL MODAL MODAL MODAL MODAL MODAL MODAL MODAL
Mode Mode Mode Mode Mode Mode Mode Mode Mode Mode Mode Mode Mode Mode Mode Mode Mode Mode Mode Mode Mode Mode Mode Mode
27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50
MMTE Rev.
DATE: 1
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0.496 0.492 0.489 0.488 0.484 0.483 0.475 0.475 0.473 0.471 0.469 0.466 0.457 0.455 0.447 0.444 0.442 0.440 0.433 0.431 0.425 0.424 0.416 0.412
0.000 0.001 0.002 0.000 0.000 0.000 0.001 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.001 0.033 0.000 0.000 0.000 0.005 0.017
0.000 0.000 0.000 0.000 0.000 0.001 0.000 0.000 0.000 0.000 0.000 0.001 0.004 0.017 0.000 0.000 0.000 0.003 0.000 0.000 0.000 0.002 0.001 0.007
Page:
0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.003 0.002 0.001 0.000 0.000 0.000 0.000 0.002 0.008 0.000 0.000 0.006 0.032
0.853 0.853 0.855 0.855 0.855 0.855 0.856 0.856 0.856 0.856 0.856 0.856 0.857 0.857 0.857 0.857 0.857 0.859 0.891 0.891 0.891 0.891 0.896 0.913
24 of 24
0.838 0.838 0.838 0.839 0.839 0.839 0.839 0.840 0.840 0.840 0.840 0.841 0.845 0.862 0.862 0.862 0.862 0.865 0.865 0.865 0.865 0.867 0.868 0.875
TABLE: Modal Load Participation Ratios OutputCase ItemType Item Static Dynamic Text Text Text Percent Percent MODAL Acceleration UX 99.846 91.307 MODAL Acceleration UY 99.461 87.462 MODAL Acceleration UZ 7.1176 5.671
As the result show, almost 90% of the mass in each direction is activated.
7.1 INTERNAL FORCES For internal forces in ASD and ASDF level refer to SAP analysis Model.
7.2 DESIGN RATIO For all design results refer to GGMM-Furnace-Flexible Model and also GGMMFurnace-Fixed Base Model. In fact, these two Model were prepared to compare their design results.(Monorail Loads was considered in Fixed Base Model.) For Design results of Flexural Frame refer to GGMM-Furnace-C=25% Model.