This document provides structural calculations for the main canopy of a building located in Mumbai. It includes STAAD analysis of the steel structure, material properties, load assumptions, and results of the analysis. Key sections analyzed include the outer MS frame, inner MS frame, supporting MS pipes and tubes. Loads considered are self-weight, wind load, and live load. The analysis checks the steel structure for deflection under these loads.
Tower design using Dynamic analysis method is now became easier than ever with this simple and effective PDF manual. Starting from modeling, defining till computing results based on Dynamic Analysis you can build the tower of your dream.
Engineering is fun and so does this PDF !
Tower design using Dynamic analysis method is now became easier than ever with this simple and effective PDF manual. Starting from modeling, defining till computing results based on Dynamic Analysis you can build the tower of your dream.
Engineering is fun and so does this PDF !
The Manual explains the concept of transferring the load from the super structure up to the soil throughout Piles, which has a capacity of (End bearing, and Skin friction). It illustrates the steps needed to produce a full and safe foundation for your Super Structure.
The Manual explains the concept of transferring the load from the super structure up to the soil throughout Piles, which has a capacity of (End bearing, and Skin friction). It illustrates the steps needed to produce a full and safe foundation for your Super Structure.
Предпосылки для внедрения архитектуры ЦОД на основе парадигмы программно-определяемых сетей (SDN). Введение в архитектуру Cisco ACI (Cisco Application Centric Infrastructure)
This is a Final Portfolio for Communications 130 Visual Media. It contains all of the projects that I have done through out the semester as I learned the different Adobe CC Programs.
Las Vegas has a become a mecca for food lovers in recent years. It all started when Wolfgang Puck opened a branch of his Spago restaurant in Vegas in 1992, and since that time, celebrity chefs have flocked to the desert city in hordes and opened fantastic - and expensive, world-class restaurants. Everything's not so high end though - there's also a good selection of family-run local restaurants, small chain outposts that are really good, and out-of-the-way ethnic places.
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Final Year Project Report on Structural Analysis and Design of Multistorey RCC Building for Earthquake Resistant Design as per IS Codes. - Khwopa College of Engineering - IOE, Tribhuvan university - Civil Engineering Final Report - Bachelor Level Project
5. 01) IS : 875 ( Part 2 ) ‐ 1987
CODE OF PRACTICE FOR DESIGN LOADS FOR BUILDINGS & STRUCTURES- IMPOSED LOADS
02) IS:875 (Part 3) ‐ 1987 150
CODE OF PRACTICE FOR DESIGN LOADS FOR BUILDINGS & STRUCTURES- WIND LOADS 1.5
03) IS 1893 ( Part 1 ) :2002
01) IS: 800:2007
GENERAL CONSTRUCTION IN STEEL - CODE OF PRACTICE
IS : 801 ‐ 1876
e 200 X 20 CODE OF PRACTICE FOR USE OFCOLD-FORMED LIGHT GAUGE STEEL
STRUCTURAL MEM’BERS IN GENERALBUILDING CONSTRUCTION
03) IS:802 (1995)
Aluminium
01) IS:8147 : 1976
Code of Practice for Use of Aluminium Alloys in Structures
02) AS 1664.2:1997
Aluminium Structures - Part-2 : Allowable Stress Design
EN 13474 : Part 2 : 2000
Glass in Building - Design of Glass Panes - Part 2: Design for Uniformly Distributed Loads
Glass
ASTM E‐1300 : 2004
EN 13474 : Part 1 : 1999
Glass in Building - Design of Glass Panes - Part 1: General Basis of Design
EN 13474 : Part 2 : 2000
Glass in Building - Design of Glass Panes - Part 2: Design for Uniformly Distributed Loads
ASTM E‐1300 : 2004
EN 13474 : Part 1 : 1999
Glass in Building - Design of Glass Panes - Part 1: General Basis of Design
EN 13474 : Part 2 : 2000
Glass in Building - Design of Glass Panes - Part 2: Design for Uniformly Distributed Loads
Glass
ASTM E‐1300 : 2004
EN 13474 : Part 1 : 1999
Glass in Building - Design of Glass Panes - Part 1: General Basis of Design
EN 13474 : Part 2 : 2000
Glass in Building - Design of Glass Panes - Part 2: Design for Uniformly Distributed Loads
01) STAAD Pro
Anchors
01) Compufix : 8.4 - Fischer Anchor
02) Profis : 2.6.3 - Hilti Anchor
03) Mungo FixCalc - Fastening Design Ver:01
Glass
01) Window Glass Design - 2004
STANDARDS & SOFTWARES
STANDARD REFERENCES
Loadings (Wind, Dead & Live)
CRITERIA FOR EARTHQUAKE RESISTANT
DESIGN OF STRUCTURES - GENERAL PROVISIONS & BUILDINGS
Mild Steel
7. MS SUPPORTING STRUCTURE DESIGN FOR INCLINED SPIDER GLZ
Max Wind Pressure
W = 150 Kg/m2
= 1.5 Kn/m
2
For Steel
Density = 78.5 Kn/m2
Elasticity (E) = 200000 N/mm
2
Mass Properties of Section used
OUTER MS FRAME
MS Tube 400 X 200 X 10mm thk
Major Moment of inertia (Ixx) = 8198.6 cm
4
x = 20 cm
Minor Moment of inertia (Iyy) = 24358.6 cm
4
y = 10 cm
Major Section Modulus (Zxx) = 819.86 cm3
Major Section Modulus (Zyy) = 1217.93 cm3
Crossectional Area (A) = 116 cm2
SelfWeight = 91.06 kg/m
2
INNER MS
MS Tube 200 X 200 X 5mm thk
Major Moment of inertia (Ixx) = 2473.25 cm4
x = 10 cm
Minor Moment of inertia (Iyy) = 2473.25 cm4
y = 10 cm
Major Section Modulus (Zxx) = 247.325 cm3
Major Section Modulus (Zyy) = 247.325 cm3
Crossectional Area (A) = 39 cm2
SelfWeight = 30.62 kg/m2
SUPPORTING MS PIPE
MS PIPE DIA 193 12 mm thk
Major Moment of inertia (Ixx) = 2806.6 cm4
x = 9.6 cm
Minor Moment of inertia (Iyy) = 2806.6 cm4
y = 9.6 cm
Major Section Modulus (Zxx) = 292.3542 cm3
Major Section Modulus (Zyy) = 292.3542 cm3
Crossectional Area (A) = 68.23 cm2
SelfWeight = 53.56 kg/m2
8. SUPPORTING MS PIPE
MS PIPE DIA 508 X 10mm thk
Major Moment of inertia (Ixx) = 48520.24 cm4
x = 25 cm
Minor Moment of inertia (Iyy) = 48520.24 cm4
y = 25 cm
Major Section Modulus (Zxx) = 1910.246 cm3
Major Section Modulus (Zyy) = 1910.246 cm3
Crossectional Area (A) = 156.45 cm2
SelfWeight = 122.81 kg/m
2
SUPPORTING MS TUBE
MS TUBE DIA 150 X 1000 X 10mm thk
Major Moment of inertia (Ixx) = 695.33 cm4
x = 7.5 cm
Minor Moment of inertia (Iyy) = 1347.83 cm4
y = 5 cm
Major Section Modulus (Zxx) = 139.066 cm3
Major Section Modulus (Zyy) = 179.7107 cm3
Crossectional Area (A) = 46 cm2
SelfWeight = 36.11 kg/m
2
Loading of Canopy
1) Self Weight of MS (Y) = (Refre Staad Output)
2) Wind Load (WL) = 1.5 Kn/m
2
3) Live load (L) = 0.75 Kn/m2
Member loading
Load on Member(UDL)
= 500 mm (For Outer Frame)
= 100 mm (For Inner Frame )
= 200 mm (For Circular Section)
= 500 mm (For Big Circular Section )
Live load (UDL) = 0.375 Kn/m (For Outer Frame)
= 0.075 Kn/m (For Inner Frame )
= 0.15 Kn/m (For Circular Section)
= 0.375 Kn/m (For Big Circular Section )
Wind load (UDL) = 0.75 Kn/m (For Outer Frame)
= 0.15 Kn/m (For Inner Frame )
= 0.3 Kn/m (For Circular Section)
= 0.75 Kn/m (For Big Circular Section )
Height Member (H)
(Exposed to load )
9. Job Information
Engineer Checked Approved
Name:
Date: 20-Sep-16
Structure Type SPACE FRAME
Number of Nodes 59 Highest Node 62
Number of Elements 79 Highest Beam 86
Number of Basic Load Cases 4
Number of Combination Load Cases 14
Included in this printout are data for:
All The Whole Structure
Included in this printout are results for load cases:
Type L/C Name
Primary 1 DEAD LOAD
Primary 2 LIVE LOAD
Primary 3 WIND LOAD -VE
Primary 4 WIND LOAD +VE
Combination 5 GENERATED INDIAN CODE GENRAL_ST
Combination 6 GENERATED INDIAN CODE GENRAL_ST
Combination 7 GENERATED INDIAN CODE GENRAL_ST
Combination 8 GENERATED INDIAN CODE GENRAL_ST
Combination 9 GENERATED INDIAN CODE GENRAL_ST
Combination 10 GENERATED INDIAN CODE GENRAL_ST
Combination 11 GENERATED INDIAN CODE GENRAL_ST
Combination 12 GENERATED INDIAN CODE GENRAL_ST
Combination 13 GENERATED INDIAN CODE GENRAL_ST
Combination 14 GENERATED INDIAN CODE GENRAL_ST
Combination 15 GENERATED INDIAN CODE GENRAL_ST
Combination 16 GENERATED INDIAN CODE GENRAL_ST
Combination 17 COMBINATION LOAD CASE 17
Combination 18 COMBINATION LOAD CASE 18
14. MEMBER SPECIFICATION
Load 4
X
Y
Z
Whole Structure (Input data was modified after picture taken)
MEMBER SPECIFICATION
Load 4
X
Y
Z
Whole Structure (Input data was modified after picture taken)
36. STAAD SPACE -- PAGE NO. 23
LENGTH UNITS - METE
MEMBER TABLE RESULT ACTUAL DEFL. DEFL.LEN/ LOAD/
DEFL. LIMIT DFF LOCATION
=======================================================================
1 ST TUB40020010.0 PASS 0.000 0.003 0.695 14
240.000 0.29
2 ST TUB40020010.0 PASS 0.000 0.003 0.695 11
240.000 0.35
3 ST TUB40020010.0 PASS 0.001 0.015 3.529 11
240.000 2.65
4 ST TUB40020010.0 PASS 0.013 0.042 10.104 14
240.000 5.05
5 ST TUB40020010.0 PASS 0.000 0.002 0.450 11
240.000 0.26
6 ST TUB40020010.0 PASS 0.000 0.002 0.450 11
240.000 0.22
7 ST TUB2002005.0 PASS 0.012 0.042 10.104 14
240.000 5.05
8 ST TUB40020010.0 PASS 0.000 0.002 0.450 11
240.000 0.23
9 ST TUB40020010.0 PASS 0.000 0.002 0.450 11
240.000 0.19
10 ST TUB2002005.0 PASS 0.011 0.042 10.104 14
240.000 5.05
11 ST TUB40020010.0 PASS 0.000 0.002 0.450 11
240.000 0.22
12 ST TUB40020010.0 PASS 0.000 0.002 0.450 12
240.000 0.22
13 ST TUB2002005.0 PASS 0.010 0.042 10.104 14
240.000 5.05
14 ST TUB40020010.0 PASS 0.000 0.002 0.450 11
240.000 0.23
15 ST TUB40020010.0 PASS 0.000 0.002 0.450 14
240.000 0.26
16 ST TUB2002005.0 PASS 0.008 0.042 10.104 14
240.000 5.05
17 ST TUB40020010.0 PASS 0.000 0.002 0.450 11
240.000 0.23
37. STAAD SPACE -- PAGE NO. 24
18 ST TUB40020010.0 PASS 0.000 0.002 0.450 14
240.000 0.23
19 ST TUB2002005.0 PASS 0.006 0.042 10.104 14
240.000 4.21
20 ST TUB40020010.0 PASS 0.000 0.002 0.450 11
240.000 0.23
21 ST TUB40020010.0 PASS 0.000 0.002 0.450 14
240.000 0.23
22 ST TUB2002005.0 PASS 0.002 0.029 6.894 14
240.000 1.72
23 ST TUB40020010.0 PASS 0.000 0.002 0.450 11
240.000 0.22
24 ST TUB40020010.0 PASS 0.000 0.002 0.450 14
240.000 0.22
25 ST TUB2002005.0 PASS 0.002 0.029 6.894 14
240.000 1.72
26 ST TUB40020010.0 PASS 0.000 0.002 0.450 11
240.000 0.23
27 ST TUB40020010.0 PASS 0.000 0.002 0.450 14
240.000 0.23
28 ST TUB2002005.0 PASS 0.002 0.029 6.894 14
240.000 1.72
29 ST TUB40020010.0 PASS 0.000 0.002 0.450 11
240.000 0.23
31 ST TUB2002005.0 PASS 0.001 0.029 6.894 11
240.000 5.74
32 ST TUB40020010.0 PASS 0.000 0.002 0.450 11
240.000 0.23
33 ST TUB40020010.0 PASS 0.000 0.002 0.450 14
240.000 0.23
34 ST TUB2002005.0 PASS 0.002 0.029 6.894 11
240.000 5.74
35 ST TUB40020010.0 PASS 0.000 0.002 0.450 11
240.000 0.23
36 ST TUB40020010.0 PASS 0.000 0.002 0.450 14
240.000 0.23
37 ST TUB2002005.0 PASS 0.002 0.029 6.894 11
240.000 5.17
38 ST TUB40020010.0 PASS 0.000 0.002 0.450 11
240.000 0.22
39 ST TUB40020010.0 PASS 0.000 0.002 0.450 14
240.000 0.19
40 ST TUB2002005.0 PASS 0.002 0.042 10.104 14
240.000 4.21
41 ST TUB40020010.0 PASS 0.000 0.002 0.450 11
240.000 0.23
42 ST TUB40020010.0 PASS 0.000 0.002 0.450 12
240.000 0.23
43 ST TUB2002005.0 PASS 0.003 0.042 10.104 14
240.000 4.21
44 ST TUB40020010.0 PASS 0.000 0.002 0.450 11
240.000 0.23
45 ST TUB40020010.0 PASS 0.000 0.002 0.450 11
240.000 0.23
46 ST TUB2002005.0 PASS 0.002 0.042 10.104 14
240.000 4.21
38. STAAD SPACE -- PAGE NO. 25
47 ST TUB40020010.0 PASS 0.000 0.002 0.450 14
240.000 0.22
48 ST TUB40020010.0 PASS 0.000 0.002 0.450 11
240.000 0.22
49 ST TUB2002005.0 PASS 0.002 0.042 10.104 14
240.000 5.05
50 ST TUB40020010.0 PASS 0.000 0.002 0.450 14
240.000 0.22
51 ST TUB40020010.0 PASS 0.000 0.002 0.450 11
240.000 0.22
52 ST TUB2002005.0 PASS 0.001 0.042 10.104 14
240.000 5.05
53 ST TUB40020010.0 PASS 0.000 0.003 0.806 14
240.000 0.34
54 ST TUB40020010.0 PASS 0.000 0.003 0.806 14
240.000 0.40
55 ST TUB2002005.0 PASS 0.002 0.042 10.104 11
240.000 1.68
56 ST PIP19312.0 PASS 0.000 0.003 0.600 6
240.000 0.35
57 ST PIP50810.0 PASS 0.006 0.054 13.000 6
240.000 6.50
58 ST TUB40020010.0 PASS 0.000 0.002 0.450 14
240.000 0.23
59 ST TUB2002005.0 PASS 0.001 0.013 3.210 11
240.000 1.07
66 ST TUB40020010.0 PASS 0.004 0.023 5.506 11
240.000 1.84
67 ST TUB40020010.0 PASS 0.000 0.004 1.069 11
240.000 0.53
68 ST TUB15010010.0 PASS 0.000 0.001 0.210 6
240.000 0.12
69 ST TUB15010010.0 PASS 0.000 0.001 0.210 11
240.000 0.14
70 ST TUB15010010.0 PASS 0.000 0.001 0.352 14
240.000 0.21
71 ST TUB15010010.0 PASS 0.000 0.001 0.352 11
240.000 0.18
72 ST TUB2002005.0 PASS 0.001 0.013 3.210 11
240.000 1.07
73 ST TUB2002005.0 PASS 0.001 0.013 3.210 11
240.000 0.80
74 ST TUB2002005.0 PASS 0.000 0.013 3.210 14
240.000 2.41
75 ST TUB2002005.0 PASS 0.001 0.013 3.210 11
240.000 1.07
76 ST TUB2002005.0 PASS 0.001 0.013 3.210 11
240.000 0.80
77 ST TUB15010010.0 PASS 0.000 0.001 0.200 9
240.000 0.17
78 ST TUB15010010.0 PASS 0.000 0.001 0.200 6
240.000 0.13
79 ST TUB15010010.0 PASS 0.000 0.001 0.200 6
240.000 0.12
80 ST TUB15010010.0 PASS 0.000 0.001 0.200 13
240.000 0.13
39. STAAD SPACE -- PAGE NO. 26
81 ST TUB15010010.0 PASS 0.000 0.001 0.200 13
240.000 0.12
82 ST TUB15010010.0 PASS 0.000 0.001 0.200 5
240.000 0.18
83 ST TUB15010010.0 PASS 0.000 0.002 0.450 14
240.000 0.19
84 ST TUB15010010.0 PASS 0.000 0.002 0.450 14
240.000 0.22
85 ST TUB15010010.0 PASS 0.000 0.002 0.450 11
240.000 0.26
************** END OF TABULATED RESULT OF DESIGN **************
182. UNIT METER KG
183. STEEL MEMBER TAKE OFF LIST 1 TO 29 31 TO 59 66 TO 85
40. STAAD SPACE -- PAGE NO. 27
STEEL TAKE-OFF
--------------
PROFILE LENGTH(METE) WEIGHT(KG )
ST TUB40020010.0 37.61 3388.067
ST TUB2002005.0 171.77 5207.198
ST PIP19312.0 0.60 32.195
ST PIP50810.0 13.00 1588.615
ST TUB15010010.0 3.67 129.215
----------------
TOTAL = 10345.291
MEMBER PROFILE LENGTH WEIGHT
(METE) (KG )
1 ST TUB40020010.0 0.70 62.636
2 ST TUB40020010.0 0.70 62.636
3 ST TUB40020010.0 3.53 317.907
4 ST TUB40020010.0 10.10 910.211
5 ST TUB40020010.0 0.45 40.538
6 ST TUB40020010.0 0.45 40.538
7 ST TUB2002005.0 10.10 306.306
8 ST TUB40020010.0 0.45 40.538
9 ST TUB40020010.0 0.45 40.538
10 ST TUB2002005.0 10.10 306.306
11 ST TUB40020010.0 0.45 40.538
12 ST TUB40020010.0 0.45 40.538
13 ST TUB2002005.0 10.10 306.306
14 ST TUB40020010.0 0.45 40.538
15 ST TUB40020010.0 0.45 40.538
16 ST TUB2002005.0 10.10 306.306
17 ST TUB40020010.0 0.45 40.538
18 ST TUB40020010.0 0.45 40.538
19 ST TUB2002005.0 10.10 306.306
20 ST TUB40020010.0 0.45 40.538
21 ST TUB40020010.0 0.45 40.538
22 ST TUB2002005.0 6.89 208.994
23 ST TUB40020010.0 0.45 40.538
24 ST TUB40020010.0 0.45 40.538
25 ST TUB2002005.0 6.89 208.994
26 ST TUB40020010.0 0.45 40.538
27 ST TUB40020010.0 0.45 40.538
28 ST TUB2002005.0 6.89 208.994
29 ST TUB40020010.0 0.45 40.538
31 ST TUB2002005.0 6.89 208.994
32 ST TUB40020010.0 0.45 40.538
33 ST TUB40020010.0 0.45 40.538
34 ST TUB2002005.0 6.89 208.994
35 ST TUB40020010.0 0.45 40.538
36 ST TUB40020010.0 0.45 40.538
37 ST TUB2002005.0 6.89 208.994
41. STAAD SPACE -- PAGE NO. 28
38 ST TUB40020010.0 0.45 40.538
39 ST TUB40020010.0 0.45 40.538
40 ST TUB2002005.0 10.10 306.306
41 ST TUB40020010.0 0.45 40.538
42 ST TUB40020010.0 0.45 40.538
43 ST TUB2002005.0 10.10 306.306
44 ST TUB40020010.0 0.45 40.538
45 ST TUB40020010.0 0.45 40.538
46 ST TUB2002005.0 10.10 306.306
47 ST TUB40020010.0 0.45 40.538
48 ST TUB40020010.0 0.45 40.538
49 ST TUB2002005.0 10.10 306.306
50 ST TUB40020010.0 0.45 40.538
51 ST TUB40020010.0 0.45 40.538
52 ST TUB2002005.0 10.10 306.306
53 ST TUB40020010.0 0.81 72.581
54 ST TUB40020010.0 0.81 72.581
55 ST TUB2002005.0 10.10 306.306
56 ST PIP19312.0 0.60 32.195
57 ST PIP50810.0 13.00 1588.615
58 ST TUB40020010.0 0.45 40.538
59 ST TUB2002005.0 3.21 97.312
66 ST TUB40020010.0 5.51 496.004
67 ST TUB40020010.0 1.07 96.300
68 ST TUB15010010.0 0.21 7.386
69 ST TUB15010010.0 0.21 7.386
70 ST TUB15010010.0 0.35 12.377
71 ST TUB15010010.0 0.35 12.377
72 ST TUB2002005.0 3.21 97.312
73 ST TUB2002005.0 3.21 97.312
74 ST TUB2002005.0 3.21 97.312
75 ST TUB2002005.0 3.21 97.312
76 ST TUB2002005.0 3.21 97.312
77 ST TUB15010010.0 0.20 7.034
78 ST TUB15010010.0 0.20 7.034
79 ST TUB15010010.0 0.20 7.034
80 ST TUB15010010.0 0.20 7.034
81 ST TUB15010010.0 0.20 7.034
82 ST TUB15010010.0 0.20 7.034
83 ST TUB15010010.0 0.45 15.827
84 ST TUB15010010.0 0.45 15.827
85 ST TUB15010010.0 0.45 15.827
----------------
TOTAL = 10345.291
************ END OF DATA FROM INTERNAL STORAGE ************
184. FINISH
49. BASEPLATE (1) BASEPLATE (2)TOP VIEW OF CANOPY
BASEPLATE (3)
BASEPLATE (4)
BASEPLATE (5)
BASEPLATE (6)
Load 4
XY
Z
Whole Structure (Input data was modified after picture taken)
BASE PLATE (7)
ISOMETRIC VIEW
Load 4
X
Y
Z
Whole Structure (Input data was modified after picture taken)
51. 1 Design forces
Factored Axial load Pu = KN
Nature of axial load =
Factored Shear force Fy = KN
Dia of anchor bolts (HT bolts) = M mm
No of Anchor = Nos
Factored lateral load Fx = KN
Ultimate Tensile strength of bolt fu = Mpa
Ultimate Tesile strength of plate fcu = Mpa
Yield stress of plate fy = Mpa
Cube compressive strength of concrete fck = Mpa
2 Geometric properties
Column section =
Depth of section = mm
Width of flange = mm
Clearence of holes = mm
Dia of holes = Nominal dia of bolt + clearence = mm
Minimum Edge distance = mm Clause 10.2.4
Maximum edge distance = 12tε IS:800:2007
= mm
ε = (250/fy)1/2
=
Edge distance provided = mm
O.K
4
Design of base plate As per IS 800:2007
BASEPLATE 1 & 2 MAXIMUM REACTION FROM NODE 49 & 50
9.87 From Staad
analysisCompression
50.634
10
28
-3.2
100
250
250
20
RHS
150
100
20
30
30
50
300
1
80
75 75
25
800
30 240 30
140
100
200
150
30
300
52. Minimum spacing of bolts (2.5 d) = mm Clause 10.2.2 &
Maximum spacing of bolts (lesser of 32t or 300) = mm 10.2.3
Spacing of bolt provided = mm IS:800:2007
Taking Non- Factored Reaction For Base Plate & divided by no of nodes (48)
FX (Kn)
Fy (KN-
m)
Fz (Kn)
MX
(Kn.m)
My (KN.m) My (KN.m)
-1.504 1.238 -6.281 -1.73 -0.47 0.316
-0.269 0.503 -1.744 -0.519 -0.095 0.056
FX (Kn)
Fy (KN-
m)
Fz (Kn)
MX
(Kn.m)
My (KN.m) My (KN.m)
-2.667 42.195 8.225 -13.096 -0.079 0.56
-0.489 16.927 1.865 -5.54 -0.028 0.103
No of nodes = 48
FX (Kn)
Fy (KN-
m)
Fz (Kn)
MX
(Kn.m)
My (KN.m) My (KN.m)
-0.056 0.87906 0.17135 -0.27283 -0.001646 0.0116667
Considering Maximum Reaction From the Node 49 For Baseplate check
25
240
300
17 COMBINATION LOAD CASE 17
18 COMBINATION LOAD CASE 18
Reaction from Node 50
Reaction from Node 49
17 COMBINATION LOAD CASE 17
Loading
18 COMBINATION LOAD CASE 18
Section RHS 150 x 100 x10 mm thk
Thickness 25 mm MS Stifneer 40 x 10 mm thk
53. Staa Pro Base pLate Stress Result
Conclusion
Induce Stress = 207 N/mm2
Permissible Stress = 250 N/mm2
Hence Plate Is Safe in Stress
FX (Kn)
Fy (KN-
Fz (Kn)
MX
My (KN m) My (KN m)
Reaction From Support
FX (Kn)
y (
m)
Fz (Kn)
(Kn.m)
My (KN.m) My (KN.m)
-0.004 0.039 -0.001 0 0 0
0.264 -8.948 0.13 0 0 0
0.26 -8.909 0.129 0 0 0
-0.268 8.987 -0.131 0 0 0
0.004 0.039 -0.001 0 0 0
2.821 -9.038 0.147 0 0 0
2.825 -8.999 0.147 0 0 0
-2.818 9.077 -0.148 0 0 0
0.004 0.04 0 0 0 0
-2.692 -10.774 -43.735 0 0 0
-2.688 -10.733 -43.735 0 0 0
2.696 10.814 43.735 0 0 0
-0.004 0.04 0 0 0 0
2.22 -12.556 -44.529 0 0 0
2.216 -12.515 -44.529 0 0 0
-2.224 12.596 44.529 0 0 0
573 1 LOAD CASE 1
2 DL+ LL+(-VE) WL (NON-FACTORED)
3 COMBINATION LOAD CASE 3
4 COMBINATION LOAD CASE 4
3 COMBINATION LOAD CASE 3
4 COMBINATION LOAD CASE 4
587
69
83
2 DL+ LL+(-VE) WL (NON-FACTORED)
3 COMBINATION LOAD CASE 3
4 COMBINATION LOAD CASE 4
1 LOAD CASE 1
2 DL+ LL+(-VE) WL (NON-FACTORED)
1 LOAD CASE 1
2 DL+ LL+(-VE) WL (NON-FACTORED)
3 COMBINATION LOAD CASE 3
4 COMBINATION LOAD CASE 4
1 LOAD CASE 1
54. Anchor Fastner Design
No. of Anchors (N) = 4
Spacing (dh) = 140 mm
Spacing (dv) = 240 mm
edge dist. ( ex ) = 50 mm
edge dist. ( ey1 ) = 75 mm
edge dist. ( ey2 ) = 75 mm
Min Edge distance to RCC = 245 mm
Min Concrete Thickness = 230 mm
Min Concrete Grade = M20
F.O.S assumed = 1.5
Combined Reaction x Fos
Fx (Lateral Direction) = 12.0195 Kn
Fy (Verticle Direction) = 62.211 Kn
Fz (Axial Direction) = 132.815 Kn
Mx = 0 Kn-m
My = 0 Kn-m
Mz = 0 Kn-m
Anchor Fasteners is designed using HILTI software
Provide 4#s, HILTI "
55. Checking For Welding - Between Veticle Plate to Base Plate (As per IS :816-1969)
Maximum Axial Force Ft = 9.87 Kn
Maximum Shear Force in Major Axis Vx = 50.63 Kn
Maximum Shear Force in Minor Axis Vy = 3.20 Kn
Maximum Moment in Major Axis Mx = 0.09 kN-m
Maximum Moment in minor Axis My = 0.672 kN-m
Maximum Torsional Moment Mz = 15.72 kN-m
Thickness of Weld (tw) tw = 6 mm
Section Properties for 2 verticle Side Weld
Deiamention of Weld b = 100 mm b = 100 mm
d = 150 mm d = 150 mm
Weld Length (Lw) Lw:= 2 x(d+b) Lw:= 500 mm
Section Modulus of Weld Swx := (d2
/3) Swx := 7500 mm2
Section Modlus of Weld Swy:= (b x d) Swy:= 15000 mm2
Polar Moment Of inerti of weld Jw:= (b2
+ 3 b x d 2
) + (3 d x b2
+ d 3
) Jw:= 2447500 mm4
6 6
r:= ((b/2)2
+ ( d/2)2
)^0.5) r:= 90.13878 mm
Resltant Shear Force on Weld (factored) Rw:= ((Vx)2
+ (Vy)2
)^0.5) Rw:= 50.7 Kn
Shear Force From Resulatnat Force Pr:= Rw Pr:= 101 N
Lw mm
Moment on Weld (factored) Mwx := Mx Mwx := 90000 N.mm
Moment on Weld (factored) Mwy := My Mwy := 672000 N.mm
Tensile Stress from Moment Pm := Mwx + Mwy + Ft Pm:= 56.81974 N.mm
Swx Swy Lw
Torsional Moment in Weld (Factored) Mwt := Mt Mt:= 0 N.mm
Stress from Torsional Moment Pt := Mwt x r Pt := 0 N/mm
Jw
Resultant Stress on Weld Pw := ((Pr + Pt )2
+ Pm2
)^0.5) Pw := 116.2955 N/mm
Resultat Stress on Weld pw:= Pw pw:= 27.68941 N/mm
0.7 x tw
factored Ultimate Weld Strength þƜ:= 220 N
mm2
Weld capacity Wc:= (0.7*þƜ*tw) Wc:= 924 N
mm
% utilization U:= Pw U:= 0.12586 Pw := 116.2955 N
Wc mm
% utilization U:= pw U:= 0.12586 Hence ok
þƜ:=
Reaction Considered from Factored load node 49
56. Weld Check
Weld Check - Fillet weld
Forces
Fx = 50.63 Kn
Fy = 3.20 Kn
Fz = 9.87 Kn
Moments
Mx = 0.0900 Kn-m
My = 0.6720 Kn-m
Mz = 15.72 Kn-m
Minimum Weld thickness (tw) = 6 mm
Throat thickness = 4.2 mm (Refer Weld calc. Sheet)
Actual Width Length = 400 (2 x 200 )mm
Hence Safe
Refer Output of Weld calculatio sheet
Design Strength Check
Induced Max Stress σi = 0.0277 Kn/mm2
Permissible Stress σp = 0.22 Kn/mm2
(Allowable Stress)
Hence Safe in Welding
utilization Ratio = 0.1259 < 1
Hence Weld is safe with 6mm Fillet weld
58. 1 Design forces
Factored Axial load Pu = KN
Nature of axial load =
Factored Shear force Fy = KN
Dia of anchor bolts (HT bolts) = M mm
No of Anchor = Nos
Factored lateral load Fx = KN
Ultimate Tensile strength of bolt fu = Mpa
Ultimate Tesile strength of plate fcu = Mpa
Yield stress of plate fy = Mpa
Cube compressive strength of concrete fck = Mpa
2 Geometric properties
Column section =
Depth of section = mm
Width of flange = mm
Clearence of holes = mm
Dia of holes = Nominal dia of bolt + clearence = mm
Minimum Edge distance = mm Clause 10.2.4
Maximum edge distance = 12tε IS:800:2007
= mm
ε = (250/fy)1/2
=
Edge distance provided = mm
O.K
800
30 240 30
0
50
300
1
80
0 75
25
RHS
150
100
20
30
28
-3.2
100
250
250
20
9.87 From Staad
analysisCompression
50.634
10
4
Design of base plate As per IS 800:2007
BASEPLATE 1 & 2 MAXIMUM REACTION FROM NODE 49 & 50
200
150
30
300
30
50
140
100
59. Minimum spacing of bolts (2.5 d) = mm Clause 10.2.2 &
Maximum spacing of bolts (lesser of 32t or 300) = mm 10.2.3
Spacing of bolt provided = mm IS:800:2007
Taking Non- Factored Reaction For Base Plate & divided by no of nodes (64)
FX (Kn)
Fy (KN-
m)
Fz (Kn)
MX
(Kn.m)
My (KN.m) My (KN.m)
1.923 19.997 0.012 4.665 0.339 -0.385
1.019 9.494 -0.095 2.198 0.037 -0.204
FX (Kn)
Fy (KN-
m)
Fz (Kn)
MX
(Kn.m)
My (KN.m) My (KN.m)
2.001 32.812 1.56 -15.303 0.504 -0.4
0.773 14.426 0.45 -6.603 0.087 -0.155
No of nodes = 64
FX (Kn)
Fy (KN-
m)
Fz (Kn)
MX
(Kn.m)
My (KN.m) My (KN.m)
0.0313 0.51269 0.02438 -0.23911 0.007875 -0.00625
Considering Maximum Reaction From the Node 57 For Baseplate check
17 COMBINATION LOAD CASE 17
18 COMBINATION LOAD CASE 18
Loading
240
Reaction from Node 60
17 COMBINATION LOAD CASE 17
18 COMBINATION LOAD CASE 18
Reaction from Node 57
25
300
Section RHS 150 x 100 x10 mm thk
Thickness 20 mm
60. Staa Pro Base pLate Stress Result
Conclusion
Induce Stress = 220 N/mm2
Permissible Stress = 250 N/mm2
Hence Plate Is Safe in Stress
R ti F S t
FX (Kn) Fy (KN-
)
Fz (Kn) MX
(K )
My (KN.m) My (KN.m)
-0.004 0.045 -0.015 0 0 0
2.007 -10.771 0.674 0 0 0
2.002 -10.725 0.659 0 0 0
-2.011 10.816 -0.688 0 0 0
0.004 0.045 -0.014 0 0 0
-1.609 -8.638 0.824 0 0 0
-1.605 -8.592 0.81 0 0 0
1.613 8.683 -0.838 0 0 0
0.004 0.041 0 0 0 0
-2.937 -6.863 -60.286 0 0 0
-2.932 -6.821 -60.286 0 0 0
2.941 6.904 60.286 0 0 0
-0.004 0.041 0 0 0 0
4.543 -6.497 -58.572 0 0 0
4.538 -6.456 -58.572 0 0 0
-4.547 6.538 58.572 0 0 0
83 1 LOAD CASE 1
2 DL+ LL+(-VE) WL (NON-FACTORED)
3 COMBINATION LOAD CASE 3
4 COMBINATION LOAD CASE 4
587 1 LOAD CASE 1
2 DL+ LL+(-VE) WL (NON-FACTORED)
3 COMBINATION LOAD CASE 3
4 COMBINATION LOAD CASE 4
69 1 LOAD CASE 1
2 DL+ LL+(-VE) WL (NON-FACTORED)
3 COMBINATION LOAD CASE 3
4 COMBINATION LOAD CASE 4
Reaction From Support
573 1 LOAD CASE 1
2 DL+ LL+(-VE) WL (NON-FACTORED)
3 COMBINATION LOAD CASE 3
4 COMBINATION LOAD CASE 4
61. Anchor Fastner Design
No. of Anchors (N) = 4
Spacing (dh) = 140 mm
Spacing (dv) = 240 mm
edge dist. ( ex ) = 50 mm
edge dist. ( ey1 ) = 75 mm
edge dist. ( ey2 ) = 75 mm
Min Edge distance to RCC = 245 mm
Min Concrete Thickness = 230 mm
Min Concrete Grade = M20
F.O.S assumed = 1.5
Combined Reaction x Fos
Fx (Lateral Direction) = 16.668 Kn
Fy (Verticle Direction) = 49.4115 Kn
Fz (Axial Direction) = 180.576 Kn
Mx = 0 Kn-m
My = 0 Kn-m
Mz = 0 Kn-m
Anchor Fasteners is designed using HILTI software
Provide 4#s, HILTI "
62. Checking For Welding - Between Veticle Plate to Base Plate (As per IS :816-1969)
Maximum Axial Force Ft = 0.548 Kn
Maximum Shear Force in Major Axis Vx = 0.09 Kn
Maximum Shear Force in Minor Axis Vy = 43.10 Kn
Maximum Torsional Moment Mx = 20.459 kN-m
Maximum Moment in minor Axis My = 0.073 kN-m
Maximum Moment in Major Axis Mz = 0.018 kN-m
Thickness of Weld (tw) tw = 6 mm
Section Properties for 2 verticle Side Weld
Deiamention of Weld b = 225 mm b = 225 mm
d = 100 mm d = 100 mm
Weld Length (Lw) Lw:= 2d + b Lw:= 425 mm
Section Modulus of Weld Swx := (d2
/3) Swx := 3333.3333 mm2
Section Modlus of Weld Swy:= (b x d) Swy:= 22500 mm2
Polar Moment Of inerti of weld Jw:= in X Axis Jw:= 6653872 mm4
r:= ((b/2)2
+ ( d/2)2
)^0.5) r:= 123.1107 mm
Resltant Shear Force on Weld (factored) Rw:= ((Vx)2
+ (Vy)2
)^0.5) Rw:= 43.1 Kn
Shear Force From Resulatnat Force Pr:= Rw Pr:= 101 N
Lw mm
Moment on Weld (factored) Mwx := Mx Mwx := 18000 N.mm
Moment on Weld (factored) Mwy := My Mwy := 73000 N.mm
Tensile Stress from Moment Pm := Mwx + Mwy + Ft Pm:= 8.645734 N.mm
Swx Swy Lw
Torsional Moment in Weld (Factored) Mwt := Mt Mt:= 20.459 N.mm
Stress from Torsional Moment Pt := Mwt x r Pt := 0.000379 N/mm
Jw
Resultant Stress on Weld Pw := ((Pr + Pt )2
+ Pm2
)^0.5) Pw := 101.7896 N/mm
Resultat Stress on Weld pw:= Pw pw:= 24.23562 N/mm
0.7 x tw
factored Ultimate Weld Strength þƜ:= 220 N
mm2
Weld capacity Wc:= (0.7*þƜ*tw) Wc:= 924 N
mm
% utilization U:= Pw U:= 0.11016 Pw := 101.7896 N
Wc mm
% utilization U:= pw U:= 0.11016 Hence ok
þƜ:=
Reaction Considered from Factored load node 57
63. Weld Check
Weld Check - Fillet weld
Forces
Fx = 0.09 Kn
Fy = 43.10 Kn
Fz = 0.55 Kn
Moments
Mx = 20.4590 Kn-m
My = 0.0730 Kn-m
Mz = 0.018 Kn-m
Minimum Weld thickness (tw) = 6 mm
Throat thickness = 4.2 mm (Refer Weld calc. Sheet)
Actual Width Length = 425 mm
Hence Safe
Refer Output of Weld calculatio sheet
Design Strength Check
Induced Max Stress σi = 0.0242 Kn/mm2
Permissible Stress σp = 0.22 Kn/mm2
(Allowable Stress)
Hence Safe in Welding
utilization Ratio = 0.1102 < 1
Hence Weld is safe with 6mm Fillet weld
65. BASEPLATE (3 & 5)for Terrace level on RCC Column
Taking Maximum reaction From Node 56
Max. Reactions from Node 56
Fx (Lateral Load ) = 1.008 KN
Fy (Axial Load ) = 12.131 KN
Fz (Horizontal Load ) = -0.012 KN
Mx = 0.002 Kn-m
My = 0.366 Kn-m
Mz = 0.218 Kn-mMz 0.218 Kn m
Design of base plate
Material Used Mild Steel
Min Yeild Strength (Fyld1) = 250 N/mm2
Width of Plate (B) = 300 mm
Depth of Plate (D) = 200 mm
Thickness of Plate (T) = 20 mm
Eccentricity (e) = 0 mm
Mzt = 0.218 Kn-m (Mz + Fx x e)
Mxt = 0.002 Kn-m (Mx + Fz x e)
Max Pressure at Base (P) = 0.27585 N/mm2
(Fy/BD + 6Mxt/BD2 + 6Mzt/DB2)
Max Plate Projection (a) = 200 mm
Max Bending Moment in Base Plate (M) = 5517 N-mm (P x a2
/ 2)
Max Plate Stress = 82.755 N/mm2
(6M / t2)
<
187.5 N/mm2
(0.75fyld1)
Hence OK
66. Anchor Fastner Design
No. of Anchors (N) =
Spacing (dh) = 640 mm
Spacing (dv) = 640 mm
edge dist. ( ex ) = 80 mm
edge dist. ( ey1 ) = 80 mmedge dist. ( ey1 ) 80 mm
edge dist. ( ey2 ) = 80 mm
Min Edge distance to RCC = 125 mm
Min Concrete Thickness = 500 mm
Min Concrete Grade = M20
F.O.S assumed = 1.5
Fx (Axial Load or Verticle Load ) = 1.008 KN
Fy = 12.131 KN
Fz = -0.012 KN
Mx = 0.002 Kn-m
My = 0.366 Kn-m
Mz = 0.218 Kn-m
Anchor Fasteners is designed using HILTI software
Provide 4#s HILTI "Provide 4#s, HILTI
67. Checking For Welding - Between Veticle Plate to Base Plate (As per IS :816-1969)
Maximum Axial Force Ft = 12.13 Kn
Maximum Shear Force in Major Axis Vx = 1.09 Kn
Maximum Shear Force in Minor Axis Vz = 0.01 Kn
Maximum Moment in Major Axis Mz = 0.22 kN-m
Maximum Moment in minor Axis My = 0.37 kN-m
Maximum Torsional Moment Mz = 0 kN-m
Thickness of Weld (tw) tw = 6 mm
Section Properties
Deiamention of Weld b = 100 mm b = 100 mm
d = 150 mm d = 150 mm
Weld Length (Lw) Lw:= 2 x(d+b) Lw:= 500 mm
Section Modulus of Weld Swx := (d2
/3) Swx := 7500 mm2
Section Modlus of Weld Swy:= (b x d) Swy:= 15000 mm2
Polar Moment Of inerti of weld Jw:= (b2
+ 3 b x d 2
) + (3 d x b2
+ d 3
) Jw:= 2447500 mm4
6 6
r:= ((b/2)2
+ ( d/2)2
)^0.5) r:= 90.13878 mm
Resltant Shear Force on Weld (factored) Rw:= ((Vx)2
+ (Vy)2
)^0.5) Rw:= 1.09 Kn
Shear Force From Resulatnat Force Pr:= Rw Pr:= 2.18 N
Lw mm
Moment on Weld (factored) Mwx := Mx Mwx := 220000 N.mm
Moment on Weld (factored) Mwy := My Mwy := 370000 N.mm
Tensile Stress from Moment Pm := Mwx + Mwy + Ft Pm:= 54.02426 N.mm
Swx Swy Lw
Torsional Moment in Weld (Factored) Mwt := Mt Mt:= 0 N.mm
Stress from Torsional Moment Pt := Mwt x r Pt := 0 N/mm
Jw
Resultant Stress on Weld Pw := ((Pr + Pt )2
+ Pm2
)^0.5) Pw := 54.06807 N/mm
Resultat Stress on Weld pw:= Pw pw:= 12.87335 N/mm
0.7 x tw
factored Ultimate Weld Strength þƜ:= 220 N
mm
Weld capacity Wc:= (0.7*þƜ*tw) Wc:= 924 N
mm
% utilization U:= Pw U:= 0.05852 Pw := 54.06807 N
Wc mm
% utilization U:= pw U:= 0.05852 Hence ok
þƜ:=
Reaction Considered from Factored load node 49
68. Weld Check
Weld Check - Fillet weld
Forces
Fx = 1.09 Kn
Fy = 0.01 Kn
Fz = 12.13 Kn
Moments
Mx = 0.2200 Kn-m
My = 0.3700 Kn-m
Mz = 0 Kn-m
Minimum Weld thickness (tw) = 6 mm
Throat thickness = 4.2 mm (Refer Weld calc. Sheet)
Actual Width Length = 400 (2 x 200 )mm
Hence Safe
Refer Output of Weld calculatio sheet
Design Strength Check
Induced Max Stress σi = 0.0129 Kn/mm2
Permissible Stress σp = 0.22 Kn/mm2
(Allowable Stress)
Hence Safe in Welding
utilization Ratio = 0.0585 < 1
Hence Weld is safe with 6mm Fillet weld
70. BASEPLATE : Ground floor base plate
Max. Reactions for node 40
Fx = 0 KN
Fy = 78.337 KN
Fz = 1.526 KN
Mx = 0 Kn-m
My = 0 Kn-m
Mz = 0 Kn-mMz 0 Kn m
Design of base plate
Material Used Mild Steel
Min Yeild Strength (Fyld1) = 250 N/mm2
Width of Plate (B) = 800 mm
Depth of Plate (D) = 800 mm
Thickness of Plate (T) = 25 mm
Eccentricity (e) = 0 mm
Mzt = 0 Kn-m (Mz + Fx x e)
Mxt = 0 Kn-m (Mx + Fz x e)
Max Pressure at Base (P) = 0.122402 N/mm2
(Fy/BD + 6Mxt/BD2 + 6Mzt/DB2)
Max Plate Projection (a) = 200 mm
Max Bending Moment in Base Plate (M) = 2448.031 N-mm (P x a2
/ 2)
Max Plate Stress = 23.5011 N/mm2
(6M / t2)
187.5 N/mm2
(0.75fyld1)
Hence OK
71. No. of Anchors (N) =
Spacing (dh) = 640 mm
Spacing (dv) = 640 mm
edge dist. ( ex ) = 80 mm
edge dist. ( ey1 ) = 80 mmedge dist. ( ey1 ) 80 mm
edge dist. ( ey2 ) = 80 mm
Min Edge distance to RCC = 125 mm
Min Concrete Thickness = 500 mm
Min Concrete Grade = M20
F.O.S assumed = 1.5
Anchor Fasteners is designed using HILTI software
Provide 4#s, HILTI "HSA-M12" ANCHORS, (hef = 65mm)
Check for Side Stiffeners
Material Used =
Min Yeild Strength (Fyld2) = 250 N/mm2
Combined Width of Member (B) = 500 mmCombined Width of Member (B) = 500 mm
Depth of Member (D) = 500 mm
Min. thickness of member (t) = 10 mm (Web thickness)
No. of Faces for main memb. (n) = 4
Depth of Side Stiffeners (ds) = 100 mm
Thickness of Side Stiffeners (ts) = 4 mm
No. of Side Stiffeners (ns) = 4
Bending Stress induced
Vertical (sv) = 0 N/mm2
(6Mxt / ntDB)
Lateral (sh) = 0 N/mm2
(6Myt / nstsds2
)
Permissible Bending Stress (sp) = 165 N/mm2
(0.66fyld2)Permissible Bending Stress (sp) = 165 N/mm (0.66fyld2)
Interaction eq:-
(sv + sh) / (sp) = 0
< 1
Hence Plates are OK
72. Check For Weld (Vert. Main Memb. to Horz. Base Plate)
Fillet Weld Thickness (tw) = 6 mm
Throat Thickness (twt) = 4.242 mm (0.707 x tw)
Permissible Stress (σw) = 220 N/mm2
Permissible Stress (σw) 220 N/mm
Strength of Weld/mm run (Sw) = 933.24 (twt x σw)
Refer Detailed Calculation Sheets (weld3.pdf)
Provide Minimum 6mm FW All Around
73. Checking For Welding - Between Cylindrical section to Base Plate (As per IS :816 :1969)
Maximum Axial Force Ft = 73.541 Kn
Maximum Shear Force in Major Axis Vy = 1.48 Kn
Maximum Shear Force in Minor Axis Vz = 8.26 Kn
Maximum Moment in Major Axis My = 6.595 kN-m
Maximum Moment in minor Axis Mz = 10.966 kN-m
Maximum Torsional Moment Mx = 0.538 kN-m
Thickness of Weld (tw) tw = 8 mm
Section Properties for 2 verticle Side Weld
Diamention of Weld cr = 1571 mm cr = 1571 mm
Diamention of Circle (Diameter) d = 500 mm d = 500 mm
Inner diamter if circle di = 480 mm di = 480 mm
Weld Length (Lw) Lw:= 1571 Lw:= 1571 mm
Section Modulus of Weld Sw := (Π x d3
)/32 Sw := 12265625 mm3
Polar Moment Of inerti of weld Jw:= (Π x( r4
‐ri4
)/2 Jw:= 7693 mm4
r:= 10 mm2
Resltant Shear Force on Weld (factored) Rw:= ((VZ)2
+ (Vy)2
)^0.5) Rw:= 8.394 Kn
Shear Force From Resulatnat Force Pr:= Rw Pr:= 5.343 N
Lw mm
Moment on Weld (factored) Mwx := Mx Mwx := 6595000 N.mm
Moment on Weld (factored) Mwy := My Mwy := 10966000 N.mm
Tensile Stress from Moment Pm := Mwx + Mwy + Ft Pm:= 1.478536426 N/mm2
Sw Sw Lw
Torsional Moment in Weld (Factored) Mwt := Mt Mt:= 538000 N.mm
Stress from Torsional Moment Pt := Mwt x r Pt := 699.3370597 N/mm2
Jw
Resultant Stress on Weld Pw := ((Pr + Pt )2
+ Pm2
)^0.5) Pw := 704.6820203 N/mm
Resultat Stress on Weld pw:= Pw pw:= 125.8360751 N/mm
0.7 x tw
Ultimate Weld Strength þƜ:= 220 N
mm
Weld capacity Wc:= (0.7*þƜ*tw) Wc:= 1232 N
mm2
% utilization U:= Pw U:= 0.57198 Pw := 704.6820203 N
Wc mm2
% utilization U:= pw U:= 0.57198 Hence ok
þƜ:=
74. Weld Check
Weld Check - Fillet weld
Forces
Fx = 1.48 Kn
Fy = 73.54 Kn
Fz = 8.26 Kn
Moments
Mx = 0.5380 Kn-m
My = 6.5950 Kn-m
Mz = 10.966 Kn-m
Minimum Weld thickness (tw) = 8 mm
Throat thickness = 5.656 mm (Refer Weld calc. Sheet)
Actual Width Length = 1571 mm
Hence Safe
Refer Output of Weld calculatio sheet
Design Strength Check
Induced Max Stress σi = 0.1258 Kn/mm2
Permissible Stress σp = 0.22 Kn/mm2
(Allowable Stress)
Hence Safe in Welding
utilization Ratio = 0.572 < 1
Hence Weld is safe with 10 mm Fillet weld