Staad Model Import To Tekla-Submited By Atul Saxena B.E(Structures),AIV, AMIE(Civil) Chartered Engineer. 1
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First open Tekla India environment---> Open new model---> File----> Import----> FEM--->Properties--->STADD---Select material IS2062 or don't change it material we will change it after importing it To Tekla ---> Parameter--->Access input file as std file (which is pasted on desktop-Use same std file which is attached herewith)
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--->Type--> STADD---Apply--OK (Of same Import FEM window) ----Select OK (Import model window)
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Click Import in above window
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Select accept all Click Yes to save the model. Double click in model outside to view ---view properties Adjust depth to view entire model.
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Right click in model----> fit work as shown below
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\ *Transmission Tower Design With Connetions.Example. (Input File) Copy and paste these commands to your staad input file browser ************************************************************************ STAAD TRUSS START JOB INFORMATION ENGINEER DATE 25-Mar-09 END JOB INFORMATION INPUT WIDTH 79 INPUT WIDTH 79 UNIT METER KN JOINT COORDINATES 1
3.000
0.000
3.000
2
1.200
27.000
3
2.800
3.000
2.800
4
2.600
6.000
2.600
5
2.400
9.000
2.400
6
2.200
12.000
2.200
7
2.000
15.000
2.000
8
1.800
18.000
1.800
1.200
13
9
1.600
21.000
1.600
10
1.400
24.000
1.400
11
-3.000
0.000
3.000
12
-1.200
27.000
13
-2.800
3.000
2.800
14
-2.600
6.000
2.600
15
-2.400
9.000
2.400
16
-2.200
12.000
2.200
17
-2.000
15.000
2.000
18
-1.800
18.000
1.800
19
-1.600
21.000
1.600
20
-1.400
24.000
1.400
21
3.000
0.000
22
1.200
27.000
23
2.800
3.000
1.200
-3.000 -1.200 -2.800
14
24
2.600
6.000
-2.600
25
2.400
9.000
-2.400
26
2.200
12.000
-2.200
27
2.000
15.000
-2.000
28
1.800
18.000
-1.800
29
1.600
21.000
-1.600
30
1.400
24.000
-1.400
31
-3.000
0.000
-3.000
32
-1.200
27.000
33
-2.800
3.000
-2.800
34
-2.600
6.000
-2.600
35
-2.400
9.000
-2.400
36
-2.200
12.000
-2.200
37
-2.000
15.000
-2.000
38
-1.800
18.000
-1.800
-1.200
15
39
-1.600
21.000
-1.600
40
-1.400
24.000
-1.400
41
1.200
30.000
1.200
42
-1.200
30.000
1.200
43
1.200
30.000
-1.200
44
-1.200
30.000
-1.200
45
4.200
27.000
1.200
46
7.200
27.000
1.200
47
4.200
30.000
1.200
48
4.200
27.000
-1.200
49
7.200
27.000
-1.200
50
4.200
30.000
-1.200
51
-4.200
27.000
1.200
52
-7.200
27.000
1.200
16
53
-4.200
30.000
1.200
54
-4.200
27.000
-1.200
55
-7.200
27.000
-1.200
56
-4.200
30.000
-1.200
57
1.200
33.000
1.200
58
-1.200
33.000
1.200
59
1.200
33.000
-1.200
60
-1.200
33.000
-1.200
61
0.000
35.000
0.000
MEMBER INCIDENCES 1
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17
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27
12
2
28
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3
29
1
30
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31
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13 4 14
19
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33
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59
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60
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61
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62
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63
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64
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65
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66
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68
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25
69
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70
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71
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30
3 24 4
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72
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80
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22
81
2
82
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90
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32
91
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96
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97
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24
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30 99
40 22
32
100
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102
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34
103
33
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104
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35
105
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106
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107
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108
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109
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110
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111
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114
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118
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120
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26
121
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122
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125
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126
32
12
127
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128
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129
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240
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MEMBER PROPERTY INDIAN
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1 TO 18 46 TO 54 82 TO 90 145 TO 148 215 TO 218 TABLE LD ISA200X150X18 SP 0.01 19 TO 26 28 TO 45 55 TO 62 64 TO 81 91 TO 98 100 TO 125 TABLE ST ISA150X150X10 127 TO 144 155 156 159 160 223 224 229 230 235 TO 250 TABLE ST ISA150X150X10 27 63 99 126 149 TO 154 157 158 161 TO 214 219 TO 222 TABLE ST ISA80X50X6
225 TO 228 231 232 251 TO 258 TABLE ST ISA80X50X6
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UNIT MMS NEWTON DEFINE MATERIAL START ISOTROPIC STEEL E 205000 POISSON 0.3
DENSITY 7.68195e-005 ALPHA 1.2e-005
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DAMP 0.03 END DEFINE MATERIAL UNIT METER KN CONSTANTS MATERIAL STEEL MEMB 1 TO 232 235 TO 258 SUPPORTS 1 11 21 31 FIXED UNIT METER KG LOAD 1 VERT
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SELFWEIGHT Y -1 JOINT LOAD
61 FX 732 46 49 52 55 FX 153
61 FX 1280 FY -1016 FZ 160
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46 49 52 55 FX 9006 FY -7844 FZ 1968 2 12 22 32 FX 4503 FY -3937 FZ 1968 LOAD 2 GWBC SELFWEIGHT Y -1 JOINT LOAD 61 FX 549 46 49 52 55 FX 1148 61 FX 515 FY -762 FZ 2342
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46 49 52 55 FX 6755 FY -5906 2 12 22 32 FX 3378 FY -2953 LOAD 3 LEFT PCBC SELFWEIGHT Y -1
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JOINT LOAD 61 FX 549 46 49 52 55 FX 1148 61 FX 960 FY -762 46 49 FX 6755 FY -5906 52 55 FX 4211 FY -4551 FZ 13293 2 12 22 32 FX 3378 FY -2953 LOAD 4 RIGHT PCBC SELFWEIGHT Y -1 JOINT LOAD 61 FX 549 46 49 52 55 FX 1148 61 FX 960 FY -762 52 55 FX 6755 FY -5906 46 49 FX 4211 FY -4551 FZ 13293
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2 12 22 32 FX 3378 FY -2953
PERFORM ANALYSIS UNIT MMS NEWTON PARAMETER
CODE IS802 LY 2800 MEMB 28
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LZ 2800 MEMB 28 MAIN 1 MEMB 1 ELA 4 ALL CNSF 1 ALL DBL 16 ALL GUSSET 8 ALL TRACK 9 ALL CHECK CODE ALL PERFORM ANALYSIS
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PRINT SUPPORT REACTION FINISH ************************************************************************ *Atul Saxena *
[email protected] *Size of Bolts is calculated. This file may be exported to Tekla Structures and detailed in Tekla.
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NOTES::
*First copy and paste this input file in your staad input file browser. Run analysis and get out put file Note that file to be imported shoud be in .std format. Genarally in staad all members of same group are separated by hyphens. We have to replace *Will size of bolts and nos will automatically reflected in Tekla Structures??
*Basically in the staad input there is a concept of grouping the members with similar characteristics such as member property, constants or loads in one go. So at the end of that particular group the member property is defined whereas at the end of each line in that group definition a hyphen *can be seen which indicates the continuation of that particular group.
*So this hyphen has to be replaced by the member property at the end of each and every line for all groups before importing the same into Tekla *Structures and if there is any user defined c/s given as an input in staad then the same needs to be taken care in Tekla Structures by defining a *conversion file or revising the profile catalog.
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PTO
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Thanks For Your Attention And
[email protected]
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