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ASEC for Manufacturing and Industrial Projects - ARESCO
Tebbin Plant
145-MISR BANI SUEF COMPANY
BOOSTER FAN PLATFORM
& DUCT SUPPORT
CALCULATION SHEET
Document no. : 145-MB-S-CA-9000
Prepared by : Eng. Ali Ahmed Elkashef
Checked by : Eng. Ashraf maghraby
Approved by : Eng. Mohamed Hikal
Date : 09-06-2015 Rev. 0
1. INTRODUCTION 1
2. DESIGN DATA 2
2.1 Applicable codes and standards 2
2.2 Material Characteristics 2
2.3 Design Loads 3
2.4 Technical Specifications 4
3. ANALYSIS 15
3.1 Calculation Method 15
3.2 Main Assumptions 15
3.3 Model Configration 15
3.4 Load Combinations 56
4. DESIGN 60
4.1 Allowable Stresses 60
4.2 Design of Beam Columns 61
4.3 Design of Bracing members 62
4.4 Design of Base connections 85
4.5 Design of Beam connections 91
5 - CHECK OF DEFLECTION 120
APPENDIX (1) 121
INDEX
1. INTRODUCTION
SAP 2000 V14.2.2
Reference Documents: (refer to Appendix (1)
Mechanical GAs drawings ---------------------------# 1517-110-GA-634B
Analysis has been carried out using the commercial software
This note is concerned with Fan CR1-FN02 platform Of Misr Bani Suef Company Project.
The aim of this document is to design the steel structure supporting the mechanical loads , and carry out all the
necessary checks and verifications.
#1517-110-GD-6222
#1517-110-GD-6224
1
2. DESIGN DATA
2.1 Applicable codes and standards
- Structural steel design is in accordance with the Egyptian Code of Practice for Steel
Constructions and Bridges (ASD) Code No. (205). Ministerial Decree No 279 - 2001
- Egyptian Code for Loads on Structural Elements and Buildings Code No. (201).
2.2 Material Characteristics
- Structural Steel :
Mass Density (  ) = 7.85 t/cm3
Modulus of Elasticity (E) = 2100 t/cm2
Coefficient of thermal Expansion () = 1.2x10-5
/ o
C
Structural Steel used is of Grade --- ST - 37
Nominal ultimate strength ( Fu ) = 3.60 t/cm2
(Thickness < 40 mm)
= 3.40 t/cm2
(40 mm < Thickness < 100 mm)
Nominal yield strength ( Fy ) = 2.40 t/cm2
(Thickness < 40 mm)
= 2.15 t/cm2
(40 mm < Thickness < 100 mm)
- Bolts used are (HSB) High Strength bolts of the following grades:
Grade (8.8)
Nominal ultimate strength ( Fub) = 8.00 t/cm2
Nominal yield strength ( Fyb) = 6.40 t/cm2
The bolt follows DIN 931
The nut follows DIN 555
The washer follows DIN 126
- Anchor bolts :
It is of steel grade ST - 37
Nominal ultimate strength ( Fu) = 3.60 t/cm2
(Diameters < 40 mm)
Nominal yield strength ( Fy) = 2.40 t/cm2
(Diameters < 40 mm)
- Welds :
The grade of weld material shall not be less than grade of base metal.
2
2.3 Design Loads
(DL) Dead load
The dead loads include the self-weight of steel structure, and covering material.
The unit weight of steel = 7.85 t/m3
Grating plate (30x30x3) = 40 Kg/m2
(LL) Live load
This load applied in the areas with covering material and / or surrounding the machines.
- Live load on platf.(LL) = 250 Kg/m2
- Dust load on platf. = 50 Kg/m2
Mechanical loads
Refer to mechanical loads presented in 1517-110-GD-6224 (appendix (1))
(MD) Mechanical dead loads (permanent loads)
- MD ---- cosidered as Load case (A)
(ML) Mechanical live loads
- ML ---- cosidered as Load case (D) - Load case (A) except for support (207SG)
The basic design loads given here below include the most permanent or variable loads that should
be considered in load combinations.
will be Load case (B) - Load case (A)
3
(W) Wind loads
The design wind load (P) = Ce .k .q
Where k is combined height, exposure factor.
Ce is pressure coefficient for the structure or portion of structure.
qs is wind pressure. qs = 0.078 T/m2
(Temp) Temperature load
(EQ) Seismic load
2.4 Technical Specifications
Deformations
Slenderness value for members
- Allowable slenderness ratio (  = K L / i ) should not increase than the following values:
For Tension Members:  max < 300
For Compression Members:
For Beam Columns :  max < 180
For Bracing Members :  max < 200
Ce=1.3 for columns / 1.1 for beams
- The allowable vertical deflection due to live load for beams is limited to Span / 200 and for
cantilevers is limited to Span/ 180
- The allowable lateral drift at top of columns due to combined lateral and gravity loads is limited to
Height / 150 .
This load is taken in the longitudinal and transversal directions of structure in accordance with
Egyptian Code (201).
The temperature effect will be considered by applying the change (increase or decrease) in
temperature = +30/-20 o
C
For this type of light weight structures we can neglect its effect as it doesn't govern the design if
compared with wind load.
4
SAP2000
SAP2000 v14.2.2 - File:BFP - Frame Span Loads (DL) (As Defined) - Tonf, m, C Units
6/7/15 16:04:42
5
SAP2000
SAP2000 v14.2.2 - File:BFP - Frame Span Loads (LL) (As Defined) - Tonf, m, C Units
6/7/15 16:05:29
6
SAP2000
SAP2000 v14.2.2 - File:BFP - Frame Span Loads (MD) (As Defined) - Tonf, m, C Units
6/7/15 16:11:13
7
SAP2000
SAP2000 v14.2.2 - File:BFP - Frame Span Loads (ML) (As Defined) - Tonf, m, C Units
6/7/15 16:08:00
8
SAP2000
SAP2000 v14.2.2 - File:BFP - Frame Span Loads (Wx) (As Defined) - Tonf, m, C Units
6/7/15 16:07:00
9
SAP2000
SAP2000 v14.2.2 - File:BFP - Frame Span Loads (Wy) (As Defined) - Tonf, m, C Units
6/7/15 16:07:24
10
SAP2000
SAP2000 v14.2.2 - File:BFP - Frame Span Loads (C1) (As Defined) - Tonf, m, C Units
6/7/15 16:11:41
11
SAP2000
SAP2000 v14.2.2 - File:BFP - Frame Span Loads (C2) (As Defined) - Tonf, m, C Units
6/7/15 16:12:11
12
SAP2000
SAP2000 v14.2.2 - File:BFP - Frame Span Loads (C3) (As Defined) - Tonf, m, C Units
6/7/15 16:12:52
13
SAP2000
SAP2000 v14.2.2 - File:BFP - Frame Span Loads (C4) (As Defined) - Tonf, m, C Units
6/7/15 16:13:18
14
3. ANALYSIS
3.1 Calculation Method
- The calculation will be done considering working stress design method.
- For evaluating the maximum stress in elements, the straining actions will be calculated for two cases:
Case  :
Primary stresses due to ……...dead loads + live loads
In design the stresses in members due to case  should not exceed the allowable stresses.
Case  :
Primary and additional stresses due to ………Case  loads + Secondary Loads
- Design of connection will be based on bearing type bolts.
3.2 Main Assumptions
3.3 Model Configuration
- Here below we will present the frame elements labels and profiles
In design the stresses in members due to case  should not exceed the allowable stresses
by more than 20%.
- For any moving loads where the impact effect is not considered in the given mechanical loads
then load factors have to be added to consider the impact effect by increasing LL by 25%.
15
SAP2000
SAP2000 v14.2.2 - File:BFP - Frame Releases - Tonf, m, C Units
6/7/15 15:30:17
16
SAP2000
SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=15.025 - Tonf, m, C Units
6/7/15 15:32:19
17
SAP2000
SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=20.525 - Tonf, m, C Units
6/7/15 16:00:01
18
SAP2000
SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=28.671 - Tonf, m, C Units
6/7/15 16:00:38
19
SAP2000
SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=39.871 - Tonf, m, C Units
6/7/15 16:01:10
20
SAP2000
SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=5.125 - Tonf, m, C Units
6/7/15 15:31:02
21
SAP2000
SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=9.665 - Tonf, m, C Units
6/7/15 15:31:44
22
SAP2000
SAP2000 v14.2.2 - File:BFP - Frame Releases - Tonf, m, C Units
6/7/15 15:29:53
23
SAP2000
SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=5.125 - Tonf, m, C Units
6/7/15 15:01:53
24
SAP2000
SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=9.665 - Tonf, m, C Units
6/7/15 15:02:48
25
SAP2000
SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=15.025 - Tonf, m, C Units
6/7/15 15:03:44
26
SAP2000
SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=20.525 - Tonf, m, C Units
6/7/15 15:04:20
27
SAP2000
SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=28.671 - Tonf, m, C Units
6/7/15 15:05:05
28
SAP2000
SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=39.871 - Tonf, m, C Units
6/7/15 15:05:40
29
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Z Plane @ Y=0 - Tonf, m, C Units
6/7/15 16:01:47
30
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Z Plane @ Y=0.71 - Tonf, m, C Units
6/7/15 16:02:11
31
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Z Plane @ Y=2.24 - Tonf, m, C Units
6/7/15 16:02:37
32
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Z Plane @ Y=3.785 - Tonf, m, C Units
6/7/15 16:03:06
33
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Z Plane @ Y=5.63 - Tonf, m, C Units
6/7/15 16:03:33
34
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Z Plane @ Y=0 - Tonf, m, C Units
6/7/15 15:06:36
35
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Z Plane @ Y=0.71 - Tonf, m, C Units
6/7/15 15:16:49
36
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Z Plane @ Y=2.24 - Tonf, m, C Units
6/7/15 15:17:29
37
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Z Plane @ Y=3.785 - Tonf, m, C Units
6/7/15 15:18:05
38
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Z Plane @ Y=5.63 - Tonf, m, C Units
6/7/15 15:18:37
39
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=1.97 - Tonf, m, C Units
6/7/15 15:21:03
40
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=10.33 - Tonf, m, C Units
6/7/15 15:25:55
41
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=10.33 - Tonf, m, C Units
6/7/15 15:26:46
42
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=4.06 - Tonf, m, C Units
6/7/15 15:21:43
43
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=4.28 - Tonf, m, C Units
6/7/15 15:22:41
44
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=6.15 - Tonf, m, C Units
6/7/15 15:23:15
45
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=8.3 - Tonf, m, C Units
6/7/15 15:24:05
46
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=8.56 - Tonf, m, C Units
6/7/15 15:25:11
47
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=1.97 - Tonf, m, C Units
6/7/15 14:50:12
48
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=4.06 - Tonf, m, C Units
6/7/15 14:51:14
49
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=4.28 - Tonf, m, C Units
6/7/15 14:52:13
50
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=6.15 - Tonf, m, C Units
6/7/15 14:52:54
51
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=8.3 - Tonf, m, C Units
6/7/15 14:54:31
52
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=8.56 - Tonf, m, C Units
6/7/15 14:55:11
53
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=10.33 - Tonf, m, C Units
6/7/15 14:56:55
54
SAP2000
SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=10.33 - Tonf, m, C Units
6/7/15 14:59:37
55
Self weight Dead Load Live Load
Mech. Dead
Load
Mech. Live
Load
+ wind in X - wind in X + wind in Y - wind in Y + EQ in X - EQ in X + EQ in Y - EQ in Y
SW DL LL MD ML C1 C2 C3 C4 WX+ WX- WY+ WY- EQX+ EQX- EQY+ EQY- Temp Temp
(+...) (-...)
COMB 1000 1.00 1.00 1.00 1.0 1.0
COMB 1001 0.83 0.83 0.83 0.83 1.0 1.2
COMB 1002 0.83 0.83 0.83 0.83 1.0 1.2
COMB 1100 0.83 0.83 0.83 0.83 1.0 1.2
COMB 1101 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 1102 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 1300 0.83 0.83 0.83 -0.83 1.0 1.2
COMB 1301 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB 1302 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB 1500 0.83 0.83 0.83 0.83 1.0 1.2
COMB 1501 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 1502 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 1700 0.83 0.83 0.83 -0.83 1.0 1.2
COMB 1701 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB 1702 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB 2000 1.00 1.00 1.00 1.00 1.0 1.0
COMB 2001 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 2002 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 2100 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 2101 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 2102 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 2110 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 2111 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 2112 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 2300 0.83 0.83 0.83 0.83 -0.83 1.0 1.2
COMB 2301 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB 2302 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB 2310 0.83 0.83 0.83 0.83 -0.83 1.0 1.2
COMB 2311 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB 2312 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB 2500 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 2501 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 2502 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 2510 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 2511 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 2512 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 2700 0.83 0.83 0.83 0.83 -0.83 1.0 1.2
COMB 2701 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB 2702 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB 2710 0.83 0.83 0.83 0.83 -0.83 1.0 1.2
COMB 2711 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB 2712 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB 3000 1.00 1.00 1.00 1.00 1.00 1.0 1.0
COMB 3001 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 3002 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
CRANE LOAD
Env. For
Brac. Des
Temperature
Envelope
3.4 Loads Combinations :-
56
Self weight Dead Load Live Load
Mech. Dead
Load
Mech. Live
Load
+ wind in X - wind in X + wind in Y - wind in Y + EQ in X - EQ in X + EQ in Y - EQ in Y
SW DL LL MD ML C1 C2 C3 C4 WX+ WX- WY+ WY- EQX+ EQX- EQY+ EQY- Temp Temp
(+...) (-...)
CRANE LOAD
Env. For
Brac. Des
Temperature
Envelope
COMB 3100 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 3101 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 3102 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 3110 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 3111 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 3112 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 3300 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2
COMB 3301 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB 3302 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB 3310 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2
COMB 3311 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB 3312 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB 3500 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 3501 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 3502 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 3510 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 3511 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 3512 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB 3700 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2
COMB 3701 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB 3702 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB 3710 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2
COMB 3711 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB 3712 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C1/3000 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.0
COMB C1/3001 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/3002 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/3100 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/3101 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/3102 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/3110 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/3111 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/3112 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/3300 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2
COMB C1/3301 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C1/3302 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C1/3310 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/3311 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/3312 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/3500 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/3501 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/3502 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/3510 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/3511 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/3512 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/3700 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2
COMB C1/3701 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C1/3702 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C1/3710 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2
57
Self weight Dead Load Live Load
Mech. Dead
Load
Mech. Live
Load
+ wind in X - wind in X + wind in Y - wind in Y + EQ in X - EQ in X + EQ in Y - EQ in Y
SW DL LL MD ML C1 C2 C3 C4 WX+ WX- WY+ WY- EQX+ EQX- EQY+ EQY- Temp Temp
(+...) (-...)
CRANE LOAD
Env. For
Brac. Des
Temperature
Envelope
COMB C1/3711 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C1/3712 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C2/3000 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.0
COMB C2/3001 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C2/3002 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C2/3100 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C2/3101 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C2/3102 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C2/3110 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C2/3111 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C2/3112 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C2/3300 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2
COMB C2/3301 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C2/3302 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C2/3310 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C2/3311 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C2/3312 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C2/3500 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C2/3501 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C2/3502 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C2/3510 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C2/3511 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C2/3512 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C2/3700 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2
COMB C2/3701 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C2/3702 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C2/3710 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2
COMB C2/3711 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C2/3712 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C3/3000 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.0
COMB C3/3001 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C3/3002 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C3/3100 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C3/3101 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C3/3102 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C3/3110 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C3/3111 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C3/3112 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C3/3300 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2
COMB C3/3301 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C3/3302 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C3/3310 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C3/3311 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C3/3312 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C3/3500 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C3/3501 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C3/3502 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C3/3510 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C3/3511 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
58
Self weight Dead Load Live Load
Mech. Dead
Load
Mech. Live
Load
+ wind in X - wind in X + wind in Y - wind in Y + EQ in X - EQ in X + EQ in Y - EQ in Y
SW DL LL MD ML C1 C2 C3 C4 WX+ WX- WY+ WY- EQX+ EQX- EQY+ EQY- Temp Temp
(+...) (-...)
CRANE LOAD
Env. For
Brac. Des
Temperature
Envelope
COMB C3/3512 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C3/3700 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2
COMB C3/3701 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C3/3702 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C3/3710 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2
COMB C3/3711 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C3/3712 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C4/3000 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.0
COMB C4/3001 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C4/3002 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C4/3100 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C4/3101 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C4/3102 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C4/3110 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C4/3111 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C4/3112 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C4/3300 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2
COMB C4/3301 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C4/3302 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C4/3310 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C4/3311 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C4/3312 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C4/3500 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C4/3501 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C4/3502 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C4/3510 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C4/3511 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C4/3512 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C4/3700 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2
COMB C4/3701 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C4/3702 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C4/3710 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2
COMB C4/3711 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C4/3712 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C1/1000 1.00 1.00 1.00 1.00 1.0 1.0
COMB C1/1001 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/1002 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/1100 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/1101 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/1102 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/1300 0.83 0.83 0.83 0.83 -0.83 1.0 1.2
COMB C1/1301 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C1/1302 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C1/1500 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/1501 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/1502 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2
COMB C1/1700 0.83 0.83 0.83 0.83 -0.83 1.0 1.2
COMB C1/1701 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
COMB C1/1702 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2
59
4. DESIGN
4.1 Allowable Stresses
-Tension Stresses:
Allowable stress ( Fat) = 0.58 Fy
-Compression Stresses:
Allowable stress (Fac ) = 0.58 Fy - [ (0.58Fy - 0.75 ) (KL/i)2
/ 104
] for (KL/i) < 100
7500/ (KL/i)2
for (KL/i) >100
-Compression Stresses due to Bending:
Allowable stress (Fb )
0.64 Fy ……………for compact section
0.58 Fy ……………for non-compact section
= FLTB in case where L unsuported of compression flange is > the allowable.
-Shear Stresses:
Allowable stress (qall ) = 0.35 Fy
Working Stress Method is used for the design, in accordance to the Egyptian Code of Practice for
Steel Constructions and Bridges Code No. (205).
in case where L unsuported of compression flange
is < the allowable.
=
60
STEEL GRADE: 37
Fy (Thickness ≤ 40) = 2.40 t/cm2
Fy (40>Thickness≤100) = 2.15 t/cm2
Fu (Thickness ≤ 40) = 3.60 t/cm2
Fu (40>Thickness≤100) = 3.40 t/cm2
B C D E F G H I J K L M N O P Q R S T U V W X Y Z AA AB AC AD AE AF AG AH AI AJ AK AL AM AN AO AP AQ AR AS AT AU AV AW AX AY AZ BA BB BC BD BE BF BG BH BI BJ BK BL BM
N Mx My Qy Qx Load Lbx Lby Lu Zx req Section H B Tw Tf A act. Ix act. Zx act. ix act. Iy act. Zy act. iy act. x y fca fbcx fbcy Fc Fcb Fex Fey Max comp. Flange tip Lucom Class Normal Check Of % Safety SBS-weld
ton m.ton m.ton ton ton case m m m Diam-mm Grade Con.Type cm3
type Name Size mm mm mm mm cm2 cm4 cm3 cm cm4 cm3 cm Act. Act. t/cm2
t/cm2
t/cm2
t/cm2
t/cm2
t/cm2
t/cm2 web flange web flange in flange stress m of section S.R. t/cm2
S.R. t/cm2
S.R. Section Margin N D-mm Grade S-mm L-mm mm
B-011 0.0 0.0 0.1 0.1 0.2 1 0.97 0.97 0.97 20 10.9 Friction 36 RS UPN 120 120 55 7 9 17.00 364 61 4.62 43 11 1.59 21 61 0.00 0.03 0.63 1.39 1.39 17.19 2.03 1.00 1.00 1.00 1.00 1.00 0.86 0.04 Outside In comp. 0.71 Compact 1.00 1.00 0.47 0.01 0.01 0.03 0.03 Safe 53 2 20 10.9 5 10 N/R
B-021 -0.7 0.3 0.4 0.2 0.5 1 2.46 1.04 3.66 20 10.9 Friction 228 RS HEA 160 152 160 6 9 38.80 1670 220 6.57 616 77 3.98 37 26 0.02 0.14 0.54 1.30 1.39 5.35 10.93 0.85 0.85 1.00 0.59 1.00 -0.70 0.22 Outside In comp. 2.07 Compact 1.00 1.00 0.50 0.02 0.03 0.03 0.03 Safe 50 2 20 10.9 5 11 N/R
G-03 -0.2 1.0 0.0 1.0 0.0 1 9.90 1.93 1.93 20 10.9 Friction 81 RS IPE 200 200 100 5.6 8.5 28.50 1940 194 8.26 142 29 2.24 120 86 0.01 0.51 0.07 0.52 1.39 0.52 1.02 0.85 0.85 1.00 0.51 1.00 -0.97 0.88 Outside In comp. 1.29 Compact 1.00 1.00 0.43 0.11 0.13 0.00 0.00 Safe 57 2 20 10.9 5 14 N/R
G-01 0.6 2.4 0.0 0.0 0.0 1 9.90 1.17 3.66 20 10.9 Friction 171 RS IPE 240 240 120 6.2 9.8 39.10 3890 324 9.97 284 47 2.69 99 43 0.01 0.73 0.01 1.39 1.39 0.76 4.00 1.00 1.00 1.00 0.49 1.00 -1.05 0.99 Outside In comp. 1.55 Compact 1.00 1.00 0.54 0.00 0.00 0.00 0.00 Safe 46 2 20 10.9 5 18 N/R
B-026 -0.1 3.6 0.2 1.7 0.3 1 2.56 1.05 1.05 20 10.9 Friction 357 RS IPE 270 270 135 6.6 10.2 45.90 5790 429 11.20 420 62 3.02 23 35 0.00 0.84 0.32 1.31 1.54 14.36 6.20 0.85 0.85 1.00 0.50 1.00 -1.00 0.73 Outside In comp. 1.74 Compact 1.00 1.00 0.78 0.11 0.14 0.01 0.02 Safe 22 2 20 10.9 5 21 N/R
G-04 -0.1 4.2 0.0 0.2 0.0 1 9.90 3.76 3.76 20 10.9 Friction 301 RS IPE 270 270 135 6.6 10.2 45.90 5790 429 11.20 420 62 3.02 88 125 0.00 0.98 0.00 0.48 1.39 0.96 0.48 1.00 0.85 1.00 0.50 1.00 -0.99 1.00 Outside In comp. 1.74 Compact 1.00 1.00 0.71 0.01 0.02 0.00 0.00 Safe 29 2 20 10.9 5 21 N/R
B-076 -3.6 0.0 0.0 0.0 0.0 1 1.37 0.69 1.37 20 10.9 Friction 2 RS UPN 120 120 55 7 9 17.00 364 61 4.62 43 11 1.59 30 43 0.21 0.04 0.00 1.27 1.39 8.53 4.04 1.00 0.85 1.00 1.00 1.00 0.77 1.00 Outside In comp. 0.71 Compact 1.03 1.00 0.20 0.00 N/C 0.00 N/C Safe 80 2 20 10.9 5 10 N/R
B-075 0.0 1.0 0.0 1.7 0.0 1 1.11 1.11 1.11 20 10.9 Friction 73 RS IPE 160 160 82 5 7.4 20.10 869 109 6.58 68 17 1.84 17 60 0.00 0.87 0.06 1.39 1.39 26.59 2.08 1.00 1.00 1.00 0.50 1.00 -1.01 0.94 Outside In comp. 1.06 Compact 1.00 1.00 0.67 0.25 0.30 0.00 0.00 Safe 33 2 20 10.9 5 10 N/R
B-069 2.0 1.4 0.1 1.3 0.1 1 5.13 3.76 0.80 20 10.9 Friction 128 RS HEA 160 152 160 6 9 38.80 1670 220 6.57 616 77 3.98 78 95 0.05 0.65 0.07 1.39 1.54 1.23 0.84 1.00 1.00 1.00 0.45 1.00 -1.23 0.89 Outside In comp. 2.07 Compact 1.00 1.00 0.55 0.16 0.19 0.01 0.01 Safe 45 2 20 10.9 5 11 N/R
B-077 4.3 1.5 0.0 0.9 0.0 1 2.46 1.85 1.85 20 10.9 Friction 116 RS IPE 200 200 100 5.6 8.5 28.50 1940 194 8.26 142 29 2.24 30 82 0.15 0.77 0.06 1.39 1.39 8.46 1.11 1.00 1.00 1.00 0.38 1.00 -1.62 0.91 Outside In comp. 1.29 Compact 1.00 1.00 0.71 0.09 0.11 0.00 0.00 Safe 29 2 20 10.9 5 14 N/R
B-071 0.0 3.2 0.0 1.6 0.0 1 3.78 1.76 1.76 20 10.9 Friction 236 RS IPE 240 240 120 6.2 9.8 39.10 3890 324 9.97 284 47 2.69 38 65 0.00 1.00 0.02 1.12 1.39 5.22 1.75 1.00 0.85 1.00 0.50 1.00 -1.00 0.98 Outside In comp. 1.55 Compact 1.00 1.00 0.73 0.12 0.15 0.00 0.00 Safe 27 2 20 10.9 5 18 N/R
B-109 2.0 0.1 0.0 0.1 0.1 1 1.21 0.61 0.61 20 10.9 Friction 22 RS UPN 120 120 55 7 9 17.00 364 61 4.62 43 11 1.59 26 38 0.11 0.16 0.27 1.39 1.54 10.93 5.18 1.00 1.00 1.00 0.51 1.00 -1.05 0.16 Outside In comp. 0.71 Compact 1.00 1.00 0.39 0.01 0.02 0.01 0.01 Safe 61 2 20 10.9 5 10 N/R
B-100 0.6 0.6 0.0 0.0 0.0 1 5.50 1.00 5.50 20 10.9 Friction 44 RS IPE 160 160 82 5 7.4 20.10 869 109 6.58 68 17 1.84 84 54 0.03 0.55 0.02 1.39 0.58 1.07 2.54 1.00 1.00 1.00 0.46 1.00 -1.15 0.97 Outside In comp. 1.06 Compact 1.00 1.00 0.96 0.01 0.01 0.00 0.00 Safe 4 2 20 10.9 5 10 N/R
2071SA -1.2 1.8 0.0 3.0 0.1 1 1.21 1.21 1.21 20 10.9 Friction 144 RS IPE 200 200 100 5.6 8.5 28.50 1940 194 8.26 142 29 2.24 15 54 0.04 0.93 0.11 1.20 1.54 34.95 2.57 1.00 1.00 1.00 0.53 1.00 -0.90 0.90 Outside In comp. 1.29 Compact 1.00 1.02 0.72 0.31 0.37 0.00 0.01 Safe 28 2 20 10.9 5 14 N/R
B-112 1.8 1.6 0.2 0.3 0.1 1 5.50 2.90 2.90 20 10.9 Friction 205 RS IPE 240 240 120 6.2 9.8 39.10 3890 324 9.97 284 47 2.69 55 108 0.05 0.49 0.38 1.39 1.39 2.46 0.64 1.00 1.00 1.00 0.44 1.00 -1.25 0.54 Outside In comp. 1.55 Compact 1.00 1.00 0.66 0.03 0.03 0.01 0.01 Safe 34 2 20 10.9 5 18 N/R
B-107 5.4 2.8 0.4 0.1 0.6 1 2.76 1.21 1.21 20 10.9 Friction 377 RS IPE 270 270 135 6.6 10.2 45.90 5790 429 11.20 420 62 3.02 25 40 0.12 0.66 0.57 1.39 1.54 12.31 4.67 1.00 1.00 1.00 0.39 1.00 -1.54 0.49 Outside In comp. 1.74 Compact 1.00 1.00 0.96 0.01 0.01 0.03 0.04 Safe 4 2 20 10.9 5 21 N/R
G-12 -12.9 0.6 0.5 0.2 0.7 1 1.78 3.50 3.50 20 10.9 Friction 271 RS IPE 300 300 150 7.1 10.7 53.80 8360 557 12.50 604 81 3.35 14 104 0.24 0.11 0.57 0.69 1.39 36.99 0.69 1.00 0.85 1.00 1.00 1.00 0.44 0.38 Outside In comp. 1.94 Compact 1.01 1.31 0.96 0.01 0.01 0.03 0.04 Safe 4 2 20 10.9 5 25 N/R
B-103 -2.0 1.2 0.3 0.3 0.4 1 5.50 1.00 5.00 20 10.9 Friction 229 RS HEA 160 152 160 6 9 38.80 1670 220 6.57 616 77 3.98 84 25 0.05 0.56 0.36 0.94 1.39 1.07 11.88 1.00 0.85 1.05 0.56 1.00 -0.79 0.63 Outside In comp. 2.07 Compact 1.05 1.00 0.74 0.03 0.04 0.02 0.02 Safe 26 2 20 10.9 5 11 N/R
G-09 0.5 11.2 0.2 6.8 0.5 1 4.92 1.22 1.22 20 10.9 Friction 900 RS HEA 300 290 300 8.5 14 113.00 18260 1260 12.70 6310 421 7.49 39 16 0.00 0.89 0.05 1.39 1.54 5.00 28.27 1.00 1.00 1.11 0.50 1.00 -1.01 0.95 Outside In comp. 3.87 Compact 1.00 1.00 0.68 0.33 0.39 0.01 0.01 Safe 32 3 20 10.9 5 29 N/R
B-004 2.7 1.5 0.0 0.1 0.0 1 3.46 0.33 3.46 20 10.9 Friction 109 RS UPN 200 200 75 8.5 11.5 32.20 1910 191 7.70 148 27 2.14 45 15 0.08 0.80 0.00 1.39 1.39 3.71 31.54 1.00 1.00 1.45 0.57 1.00 -1.31 0.99 Outside In comp. 0.97 Compact 1.00 1.00 0.63 0.01 0.01 0.00 0.00 Safe 37 2 20 10.9 5 20 N/R
B-054 0.9 0.1 0.2 0.2 0.2 1 1.25 0.88 0.88 20 10.9 Friction 95 RS IPE 200 200 100 5.6 8.5 28.50 1940 194 8.26 142 29 2.24 15 39 0.03 0.07 0.60 1.39 1.54 32.75 4.92 1.00 1.00 1.00 0.22 1.00 -3.63 0.06 Outside In comp. 1.29 Compact 1.00 1.00 0.50 0.02 0.03 0.01 0.02 Safe 50 2 20 10.9 5 14 N/R
B-047 -0.6 0.2 0.4 0.2 0.2 1 1.25 0.88 0.88 20 10.9 Friction 217 RS IPE 240 240 120 6.2 9.8 39.10 3890 324 9.97 284 47 2.69 13 33 0.01 0.05 0.87 1.32 1.54 47.71 7.09 0.85 0.85 1.00 0.69 1.00 -0.45 0.07 Outside In comp. 1.55 Compact 1.00 1.00 0.67 0.01 0.01 0.01 0.01 Safe 33 2 20 10.9 5 18 N/R
B-084 -0.3 0.1 0.4 0.2 1.0 1 1.25 0.88 0.88 20 10.9 Friction 230 RS IPE 270 270 135 6.6 10.2 45.90 5790 429 11.20 420 62 3.02 11 29 0.01 0.03 0.71 1.34 1.54 60.21 8.93 1.00 1.00 1.00 0.63 1.00 -0.58 0.05 Outside In comp. 1.74 Compact 1.00 1.00 0.54 0.02 0.02 0.06 0.07 Safe 46 2 20 10.9 5 21 N/R
P-03 -8.2 0.0 0.0 0.0 0.0 1 1.94 1.94 1.94 20 10.9 Friction 6 RS IPE 160 160 82 5 7.4 20.10 869 109 6.58 68 17 1.84 29 105 0.41 0.00 0.07 0.67 1.39 8.63 0.67 0.85 0.85 1.75 1.00 1.00 0.99 0.85 Outside In comp. 1.06 Compact 1.00 2.14 0.71 0.00 0.00 0.00 N/C Safe 29 2 20 10.9 5 10 N/R
2030SG -7.1 0.5 0.2 0.3 0.7 1 1.40 1.40 1.40 20 10.9 Friction 129 RS HEA 160 152 160 6 9 38.80 1670 220 6.57 616 77 3.98 21 35 0.18 0.23 0.24 1.31 1.54 16.52 6.06 1.00 1.00 1.00 1.00 1.00 0.03 0.63 Outside In comp. 2.07 Compact 1.01 1.03 0.47 0.03 0.04 0.04 0.04 Safe 53 2 20 10.9 5 11 N/R
P-02 -4.7 0.0 0.0 0.0 0.0 1 1.97 1.97 1.97 20 10.9 Friction 0 RS IPE 200 200 100 5.6 8.5 28.50 1940 194 8.26 142 29 2.24 24 88 0.17 0.00 0.00 0.90 1.39 13.19 0.97 1.00 0.85 1.00 1.00 1.00 1.00 1.00 Outside In comp. 1.29 Compact 1.01 1.03 0.19 0.00 N/C 0.00 N/C Safe 81 2 20 10.9 5 14 N/R
C-05 -17.6 1.0 0.0 0.5 0.0 1 4.28 2.56 4.28 20 10.9 Friction 83 RS IPE 270 270 135 6.6 10.2 45.90 5790 429 11.20 420 62 3.02 38 85 0.38 0.23 0.04 0.93 1.39 5.14 1.04 0.85 0.85 1.28 1.00 1.00 0.32 0.94 Outside In comp. 1.74 Compact 1.00 1.34 0.62 0.03 0.04 0.00 0.00 Safe 38 2 20 10.9 5 21 N/R
C-09 -9.9 0.0 0.0 0.0 0.0 1 10.42 2.09 10.42 20 10.9 Friction 10 RS IPE 200 200 100 5.6 8.5 28.50 1940 194 8.26 142 29 2.24 126 93 0.35 0.00 0.07 0.47 0.35 0.47 0.87 0.85 0.85 1.04 1.00 1.00 1.00 0.83 Outside In comp. 1.29 Compact 3.28 1.42 0.81 0.00 N/C 0.00 0.00 Safe 19 2 20 10.9 5 14 N/R
G-07 3.9 5.5 0.0 1.7 0.0 1 11.20 2.80 4.23 20 10.9 Friction 410 RS IPE 300 300 150 7.1 10.7 53.80 8360 557 12.50 604 81 3.35 90 84 0.07 0.99 0.04 1.39 1.39 0.93 1.07 1.00 1.00 1.53 0.46 1.00 -1.19 0.96 Outside In comp. 1.94 Compact 1.00 1.00 0.79 0.09 0.11 0.00 0.00 Safe 21 2 20 10.9 5 25 N/R
B-066 -6.5 1.2 0.3 0.4 0.1 1 4.50 4.92 4.50 20 10.9 Friction 222 RS HEA 300 290 300 8.5 14 113.00 18260 1260 12.70 6310 421 7.49 35 66 0.06 0.10 0.06 1.11 1.39 5.97 1.74 0.85 0.85 1.00 0.87 1.00 -0.14 0.70 Outside In comp. 3.87 Compact 1.00 1.00 0.17 0.02 0.02 0.00 0.00 Safe 83 3 20 10.9 5 29 N/R
CROSS SECTION
Cmx

MISR BANI SUEF CAMPANY
BOOSTER FAN PLATFORM & DUCT SUPPORT
DESIGN OF SECTIONS
Mem. No.
BOLTS
A2

Cmy Cb
Check Of [qx]
REMARKSA1
Check Of [qy] Bolted conn. Welded conn.
4.2. Design of beam columns
61
m
70 mm 7 mm cm
cm
cm
< <
< Fc
ton >
ton
2
DateDate
-
AM
Checked
-
Date
-
HK
Approved
-
Design of Bolted Connection :
Section
Single angle
70x7
t/cm2
-
10
Stress Ratio = 0.62
Check Stress Ratio :
0.234
0.375Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
SAFE
Actual Stress :
Allowable Stress :
0.251
1.392
Check Stress Ratio :
t/cm
2
Ft =
f ta =
30
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
70x7
e =
1 -
67.1
0
q r =
Iv =
Rev. Descreption Design
F tr =
p
(S.R = 0.65)
tG.P
α = 0.8 tmin =
a =
1.50
Bolted
iu = 2.67
Single angle
Properties of Section :
Section :
Area =
M12
300
Lby =
9.40
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
1.97
109.5 200
ARESCO
TEBBIN
cm4
17.6
Thickness of Gusset Plate =
Iu =
t =
cm4
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
2.20
1.80
t/cm2
1.50
Sheet No. :
1.37iv =
Case of Loading :ton Grade of Steel : I
Member ID : HB-003
Lbx =
10 mm
ton
1.50 1.0m
Type of Connection :
Length =
Bolts :
m
109.5
7.17 cm2
λv =
Kg/mWeight =
A red =
Check as Tension Member :
cm
2
1.0Ky =
7.38
SAFE
< Ft
1.61
3.78
Stress Ratio =
SAFE (S.R = 0.34)
0.18
0.4 Fy = 0.96
6.43
At =
ton
t/cm2
SAFE
2M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Shear Strength :
No. of Bolts = 1.31
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min = 2.42
1.68
cm2
cm2
2.2 tonqr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm7
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λv =
e p p e
x
4.3 Desgin of bracing members:-
62
m
60 mm 6 mm cm
cm
cm
< <
< Fc
ton >
ton
2
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λv =
qr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm6
2.07
1.68
cm2
cm2
0.1 tonShear Strength :
No. of Bolts = 0.03
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min =
SAFE
2M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Stress Ratio =
SAFE (S.R = 0)
0.00
0.4 Fy = 0.96
5.51
At =
ton
t/cm2
< Ft
1.38
3.24
SAFE
A red =
Check as Tension Member :
cm
2
1.0Ky =
5.42
Type of Connection :
Length =
Bolts :
m
120.5
5.12 cm2
λv =
Kg/mWeight =
Lbx =
10 mm
ton
1.41 1.0m
ton Grade of Steel : I
Member ID : HB-039
t/cm
2
1.41
Sheet No. :
1.17iv =
Case of Loading :
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
0.06
0.03
120.5 200
ARESCO
TEBBIN
cm4
9.4
Thickness of Gusset Plate =
Iu =
t =
cm4
300
Lby =
6.91
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
1.69a =
1.41
Bolted
iu = 2.29
Single angle
Properties of Section :
Section :
Area =
M12
Rev. Descreption Design
F tr =
p
(S.R = 0.01)
tG.P
α = 0.8 tmin =
1 -
36.1
0
q r =
Iv =
30
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
60x6
e =
SAFE
Actual Stress :
Allowable Stress :
0.005
1.392
Check Stress Ratio :
t/cm
2
Ft =
f ta =
Stress Ratio = 0.03
Check Stress Ratio :
0.008
0.310Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
Approved
-
Design of Bolted Connection :
Section
Single angle
60x6
t/cm2
-
10
DateDate
-
AM
Checked
-
Date
-
HK
e p p e
x
4.3 Desgin of bracing members:-
63
m
60 mm 6 mm cm
cm
cm
< <
< Fc
ton >
ton
2
DateDate
-
AM
Checked
-
Date
-
HK
Approved
-
Design of Bolted Connection :
Section
Single angle
60x6
t/cm2
-
10
Stress Ratio = 0.36
Check Stress Ratio :
0.191
0.524Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
SAFE
Actual Stress :
Allowable Stress :
0.045
1.392
Check Stress Ratio :
t/cm
2
Ft =
f ta =
30
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
60x6
e =
1 -
36.1
0
q r =
Iv =
Rev. Descreption Design
F tr =
p
(S.R = 0.39)
tG.P
α = 0.8 tmin =
a =
1.05
Bolted
iu = 2.29
Single angle
Properties of Section :
Section :
Area =
M12
300
Lby =
6.91
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
1.69
89.8 200
ARESCO
TEBBIN
cm4
9.4
Thickness of Gusset Plate =
Iu =
t =
cm4
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
1.32
0.23
t/cm2
1.05
Sheet No. :
1.17iv =
Case of Loading :ton Grade of Steel : I
Member ID : HB-047
Lbx =
10 mm
ton
1.05 1.0m
Type of Connection :
Length =
Bolts :
m
89.8
5.12 cm2
λv =
Kg/mWeight =
A red =
Check as Tension Member :
cm
2
1.0Ky =
5.42
SAFE
< Ft
1.38
3.24
Stress Ratio =
SAFE (S.R = 0.23)
0.03
0.4 Fy = 0.96
5.51
At =
ton
t/cm2
SAFE
2M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Shear Strength :
No. of Bolts = 0.79
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min = 2.07
1.68
cm2
cm2
1.3 tonqr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm6
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λv =
e p p e
x
4.3 Desgin of bracing members:-
64
m
70 mm 7 mm cm
cm
cm
< <
< Fc
ton >
ton
2
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λv =
qr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm7
2.42
1.68
cm2
cm2
1.8 tonShear Strength :
No. of Bolts = 1.07
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min =
SAFE
2M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Stress Ratio =
SAFE (S.R = 0.27)
0.02
0.4 Fy = 0.96
6.43
At =
ton
t/cm2
< Ft
1.61
3.78
SAFE
A red =
Check as Tension Member :
cm
2
1.0Ky =
7.38
Type of Connection :
Length =
Bolts :
m
116.4
7.17 cm2
λv =
Kg/mWeight =
Lbx =
10 mm
ton
1.59 1.0m
ton Grade of Steel : I
Member ID : HB-058
t/cm
2
1.59
Sheet No. :
1.37iv =
Case of Loading :
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
1.80
0.23
116.4 200
ARESCO
TEBBIN
cm4
17.6
Thickness of Gusset Plate =
Iu =
t =
cm4
300
Lby =
9.40
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
1.97a =
1.59
Bolted
iu = 2.67
Single angle
Properties of Section :
Section :
Area =
M12
Rev. Descreption Design
F tr =
p
(S.R = 0.53)
tG.P
α = 0.8 tmin =
1 -
67.1
0
q r =
Iv =
30
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
70x7
e =
SAFE
Actual Stress :
Allowable Stress :
0.032
1.392
Check Stress Ratio :
t/cm
2
Ft =
f ta =
Stress Ratio = 0.58
Check Stress Ratio :
0.191
0.332Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
Approved
-
Design of Bolted Connection :
Section
Single angle
70x7
t/cm2
-
10
DateDate
-
AM
Checked
-
Date
-
HK
e p p e
x
4.3 Desgin of bracing members:-
65
m
80 mm 8 mm cm
cm
cm
< <
< Fc
ton >
ton
2
DateDate
-
AM
Checked
-
Date
-
HK
Approved
-
Design of Bolted Connection :
Section
Single angle
80x8
t/cm2
-
10
Stress Ratio = 0.61
Check Stress Ratio :
0.203
0.334Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
SAFE
Actual Stress :
Allowable Stress :
0.017
1.392
Check Stress Ratio :
t/cm
2
Ft =
f ta =
35
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
80x8
e =
1 -
115.0
0
q r =
Iv =
Rev. Descreption Design
F tr =
p
(S.R = 0.74)
tG.P
α = 0.8 tmin =
a =
1.80
Bolted
iu = 3.06
Single angle
Properties of Section :
Section :
Area =
M12
300
Lby =
12.30
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
2.26
116.1 200
ARESCO
TEBBIN
cm4
29.6
Thickness of Gusset Plate =
Iu =
t =
cm4
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
2.50
0.16
t/cm2
1.80
Sheet No. :
1.55iv =
Case of Loading :ton Grade of Steel : I
Member ID : HB-120
Lbx =
10 mm
ton
1.80 1.0m
Type of Connection :
Length =
Bolts :
m
116.1
9.58 cm2
λv =
Kg/mWeight =
A red =
Check as Tension Member :
cm
2
1.0Ky =
9.66
SAFE
< Ft
2.24
4.32
Stress Ratio =
SAFE (S.R = 0.31)
0.01
0.4 Fy = 0.96
8.04
At =
ton
t/cm2
SAFE
2M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Shear Strength :
No. of Bolts = 1.49
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min = 2.76
1.68
cm2
cm2
2.5 tonqr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm8
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λv =
e p p e
x
4.3 Desgin of bracing members:-
66
m
60 mm 6 mm cm
cm
cm
< <
< Fc
ton >
ton
2
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λv =
qr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm6
2.07
1.68
cm2
cm2
2.6 tonShear Strength :
No. of Bolts = 1.53
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min =
SAFE
2M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Stress Ratio =
SAFE (S.R = 0.46)
0.07
0.4 Fy = 0.96
5.51
At =
ton
t/cm2
< Ft
1.38
3.24
SAFE
A red =
Check as Tension Member :
cm
2
1.0Ky =
5.42
Type of Connection :
Length =
Bolts :
m
105.1
5.12 cm2
λv =
Kg/mWeight =
Lbx =
10 mm
ton
1.23 1.0m
ton Grade of Steel : I
Member ID : HB-147
t/cm
2
1.23
Sheet No. :
1.17iv =
Case of Loading :
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
2.57
0.47
105.1 200
ARESCO
TEBBIN
cm4
9.4
Thickness of Gusset Plate =
Iu =
t =
cm4
300
Lby =
6.91
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
1.69a =
1.23
Bolted
iu = 2.29
Single angle
Properties of Section :
Section :
Area =
M12
Rev. Descreption Design
F tr =
p
(S.R = 0.76)
tG.P
α = 0.8 tmin =
1 -
36.1
0
q r =
Iv =
30
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
60x6
e =
SAFE
Actual Stress :
Allowable Stress :
0.092
1.392
Check Stress Ratio :
t/cm
2
Ft =
f ta =
Stress Ratio = 0.91
Check Stress Ratio :
0.371
0.407Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
Approved
-
Design of Bolted Connection :
Section
Single angle
60x6
t/cm2
-
10
DateDate
-
AM
Checked
-
Date
-
HK
e p p e
x
4.3 Desgin of bracing members:-
67
m
100 mm 10 mm cm
cm
cm
< <
< Fc
ton >
ton
2
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λu =
qr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm10
3.46
1.68
cm2
cm2
0.2 tonShear Strength :
No. of Bolts = 0.09
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min =
SAFE
2M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Stress Ratio =
SAFE (S.R = 0.01)
0.00
0.4 Fy = 0.96
11.80
At =
ton
t/cm2
< Ft
3.80
5.40
SAFE
A net =
Check as Tension Member :
cm
2
1.0Ky =
30.2
Type of Connection :
Length =
Bolts :
m
183.2
35.60 cm2
λu =
Kg/mWeight =
Lbx =
10 mm
ton
7.00 1.0m
ton Grade of Steel : I
Member ID : MRHB
t/cm
2
7.00
Sheet No. :
1.95iv =
Case of Loading :
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
0.12
0.16
183.2 200
ARESCO
TEBBIN
cm4
73.3
Thickness of Gusset Plate =
Iu =
t =
cm4
300
Lby =
38.40
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
2.82a =
7.00
Bolted
iu = 3.82
2Ls Star-Shaped
Properties of Section :
Section :
Area =
M12
Rev. Descreption Design
F tr =
p
(S.R = 0.04)
tG.P
α = 0.8 tmin =
1 -
280.0
0
q r =
Iv =
45
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
100x10
e =
SAFE
Actual Stress :
Allowable Stress :
0.004
1.392
Check Stress Ratio :
t/cm
2
Ft =
f ta =
Stress Ratio = 0.01
Check Stress Ratio :
0.003
0.223Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
Approved
-
Design of Bolted Connection :
Section
2Ls Star-Shaped
100x10
t/cm2
-
10
DateDate
-
AM
Checked
-
Date
-
HK
e p p e
x
4.3 Desgin of bracing members:-
68
m
60 mm 6 mm cm
cm
cm
< <
< <
< Fc
ton >
ton
2
DateDate
-
AM
Checked
-
Date
-
HK
Approved
-
Design of Bolted Connection :
Section
2Ls Back to Back
60x6
t/cm2
-
8
Stress Ratio = 0.51
Check Stress Ratio :
0.178
0.351Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
SAFE
Actual Stress :
Allowable Stress :
0.000
1.392
Check Stress Ratio :
t/cm
2
Ft =
96.1
f ta =
30
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
60x6
e =
1 -
22.8
96.1
0
λy =
q r =
Iy =
λy = 200
Rev. Descreption Design
F tr =
p
(S.R = 0.44)
tG.P
α = 0.8 tmin =
a =
2.66
Bolted
ix = 1.82
2Ls Back to Back
Properties of Section :
Section :
Area =
M12
300
300
Lby =
13.82
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
1.69
146.2 200
ARESCO
TEBBIN
cm4
106.0
Thickness of Gusset Plate =
Ix =
t =
cm4
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
2.46
0.00
t/cm2
2.66
Sheet No. :
2.77
SAFE
iy =
Case of Loading :ton Grade of Steel : I
Member ID : NB-03
Lbx =
8 mm
ton
2.66 1.0m
Type of Connection :
Length =
Bolts :
m
146.2
12.14 cm2
λx =
Kg/mWeight =
A net =
Check as Tension Member :
cm
2
1.0Ky =
10.84
SAFE
SAFE
< Ft
1.84
4.32
Stress Ratio =
SAFE (S.R = 0.33)
0.00
0.4 Fy = 0.96
7.35
At =
ton
t/cm2
SAFE
2M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Shear Strength :
No. of Bolts = 0.89
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min = 2.76
3.36
cm2
cm2
2.5 tonqr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm8
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λx =
e p p e
x
4.3 Desgin of bracing members:-
69
m
70 mm 7 mm cm
cm
cm
< <
< <
< Fc
ton >
ton
4
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λx =
qr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm8
2.76
3.36
cm2
cm2
8.4 tonShear Strength :
No. of Bolts = 3.04
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min =
SAFE
4M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Stress Ratio =
SAFE (S.R = 0.65)
0.00
0.4 Fy = 0.96
12.88
At =
ton
t/cm2
< Ft
1.84
10.08
SAFE
SAFE
A net =
Check as Tension Member :
cm
2
1.0Ky =
14.76
Type of Connection :
Length =
Bolts :
m
81.8
16.84 cm2
λx =
Kg/mWeight =
Lbx =
8 mm
ton
3.47 0.5m
ton Grade of Steel : I
Member ID : NB-05
t/cm
2
3.47
Sheet No. :
3.18
SAFE
iy =
Case of Loading :
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
8.40
0.00
81.8 200
ARESCO
TEBBIN
cm4
190.4
Thickness of Gusset Plate =
Ix =
t =
cm4
300
300
Lby =
18.80
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
1.97a =
1.74
Bolted
ix = 2.12
2Ls Back to Back
Properties of Section :
Section :
Area =
M12
Rev. Descreption Design
F tr =
p
(S.R = 0.75)
tG.P
α = 0.8 tmin =
1 -
42.4
109.0
0
λy =
q r =
Iy =
λy = 200
30
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
70x7
e =
SAFE
Actual Stress :
Allowable Stress :
0.000
1.392
Check Stress Ratio :
t/cm
2
Ft =
109.0
f ta =
Stress Ratio = 0.71
Check Stress Ratio :
0.447
0.631Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
Approved
-
Design of Bolted Connection :
Section
2Ls Back to Back
70x7
t/cm2
-
8
DateDate
-
AM
Checked
-
Date
-
HK
e p p e
x
4.3 Desgin of bracing members:-
70
m
60 mm 6 mm cm
cm
cm
< <
< <
< Fc
ton >
ton
3
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λx =
qr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm8
2.76
3.36
cm2
cm2
6.4 tonShear Strength :
No. of Bolts = 2.31
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min =
SAFE
3M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Stress Ratio =
SAFE (S.R = 0.63)
0.38
0.4 Fy = 0.96
10.11
At =
ton
t/cm2
< Ft
1.84
7.20
SAFE
SAFE
A net =
Check as Tension Member :
cm
2
1.0Ky =
10.84
Type of Connection :
Length =
Bolts :
m
65.2
12.14 cm2
λx =
Kg/mWeight =
Lbx =
8 mm
ton
2.37 0.5m
ton Grade of Steel : I
Member ID : SGBR-08
t/cm
2
2.37
Sheet No. :
2.77
SAFE
iy =
Case of Loading :
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
5.60
6.40
65.2 200
ARESCO
TEBBIN
cm4
106.0
Thickness of Gusset Plate =
Ix =
t =
cm4
300
300
Lby =
13.82
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
1.69a =
1.19
Bolted
ix = 1.82
2Ls Back to Back
Properties of Section :
Section :
Area =
M12
Rev. Descreption Design
F tr =
p
(S.R = 0.77)
tG.P
α = 0.8 tmin =
1 -
22.8
85.7
0
λy =
q r =
Iy =
λy = 200
30
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
60x6
e =
SAFE
Actual Stress :
Allowable Stress :
0.527
1.392
Check Stress Ratio :
t/cm
2
Ft =
85.7
f ta =
Stress Ratio = 0.44
Check Stress Ratio :
0.405
0.920Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
Approved
-
Design of Bolted Connection :
Section
2Ls Back to Back
60x6
t/cm2
-
8
DateDate
-
AM
Checked
-
Date
-
HK
e p p e
x
4.3 Desgin of bracing members:-
71
m
60 mm 6 mm cm
cm
cm
< <
< <
< Fc
ton >
ton
3
DateDate
-
AM
Checked
-
Date
-
HK
Approved
-
Design of Bolted Connection :
Section
2Ls Back to Back
60x6
t/cm2
-
8
Stress Ratio = 0.50
Check Stress Ratio :
0.504
1.012Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
SAFE
Actual Stress :
Allowable Stress :
0.387
1.392
Check Stress Ratio :
t/cm
2
Ft =
50.6
f ta =
30
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
60x6
e =
1 -
22.8
50.6
0
λy =
q r =
Iy =
λy = 200
Rev. Descreption Design
F tr =
p
(S.R = 0.84)
tG.P
α = 0.8 tmin =
a =
1.40
Bolted
ix = 1.82
2Ls Back to Back
Properties of Section :
Section :
Area =
M12
300
300
Lby =
13.82
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
1.69
76.9 200
ARESCO
TEBBIN
cm4
106.0
Thickness of Gusset Plate =
Ix =
t =
cm4
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
6.97
4.70
t/cm2
1.40
Sheet No. :
2.77
SAFE
iy =
Case of Loading :ton Grade of Steel : I
Member ID : SGBR-14
Lbx =
8 mm
ton
1.40 1.0m
Type of Connection :
Length =
Bolts :
m
76.9
12.14 cm2
λx =
Kg/mWeight =
A net =
Check as Tension Member :
cm
2
1.0Ky =
10.84
SAFE
SAFE
< Ft
1.84
7.20
Stress Ratio =
SAFE (S.R = 0.68)
0.28
0.4 Fy = 0.96
10.11
At =
ton
t/cm2
SAFE
3M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Shear Strength :
No. of Bolts = 2.52
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min = 2.76
3.36
cm2
cm2
7.0 tonqr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm8
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λx =
e p p e
x
4.3 Desgin of bracing members:-
72
m
80 mm 8 mm cm
cm
cm
< <
< Fc
ton >
ton
2
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λu =
qr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm8
2.76
1.68
cm2
cm2
0.8 tonShear Strength :
No. of Bolts = 0.49
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min =
SAFE
2M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Stress Ratio =
SAFE (S.R = 0.1)
0.02
0.4 Fy = 0.96
8.04
At =
ton
t/cm2
< Ft
2.24
4.32
SAFE
A net =
Check as Tension Member :
cm
2
1.0Ky =
19.32
Type of Connection :
Length =
Bolts :
m
179.7
22.36 cm2
λu =
Kg/mWeight =
Lbx =
10 mm
ton
5.50 1.0m
ton Grade of Steel : I
Member ID : VB-031
t/cm
2
5.50
Sheet No. :
1.55iv =
Case of Loading :
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
0.83
0.53
179.7 200
ARESCO
TEBBIN
cm4
29.6
Thickness of Gusset Plate =
Iu =
t =
cm4
300
Lby =
24.60
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
2.26a =
5.50
Bolted
iu = 3.06
2Ls Star-Shaped
Properties of Section :
Section :
Area =
M12
Rev. Descreption Design
F tr =
p
(S.R = 0.24)
tG.P
α = 0.8 tmin =
1 -
115.0
0
q r =
Iv =
35
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
80x8
e =
SAFE
Actual Stress :
Allowable Stress :
0.024
1.392
Check Stress Ratio :
t/cm
2
Ft =
f ta =
Stress Ratio = 0.15
Check Stress Ratio :
0.034
0.232Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
Approved
-
Design of Bolted Connection :
Section
2Ls Star-Shaped
80x8
t/cm2
-
10
DateDate
-
AM
Checked
-
Date
-
HK
e p p e
x
4.3 Desgin of bracing members:-
73
m
80 mm 8 mm cm
cm
cm
< <
< Fc
ton >
ton
2
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λu =
qr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm8
2.76
1.68
cm2
cm2
0.7 tonShear Strength :
No. of Bolts = 0.42
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min =
SAFE
2M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Stress Ratio =
SAFE (S.R = 0.08)
0.01
0.4 Fy = 0.96
8.04
At =
ton
t/cm2
< Ft
2.24
4.32
SAFE
A net =
Check as Tension Member :
cm
2
1.0Ky =
19.32
Type of Connection :
Length =
Bolts :
m
195.4
22.36 cm2
λu =
Kg/mWeight =
Lbx =
10 mm
ton
5.98 1.0m
ton Grade of Steel : I
Member ID : VB-036
t/cm
2
5.98
Sheet No. :
1.55iv =
Case of Loading :
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
0.71
0.31
195.4 200
ARESCO
TEBBIN
cm4
29.6
Thickness of Gusset Plate =
Iu =
t =
cm4
300
Lby =
24.60
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
2.26a =
5.98
Bolted
iu = 3.06
2Ls Star-Shaped
Properties of Section :
Section :
Area =
M12
Rev. Descreption Design
F tr =
p
(S.R = 0.21)
tG.P
α = 0.8 tmin =
1 -
115.0
0
q r =
Iv =
35
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
80x8
e =
SAFE
Actual Stress :
Allowable Stress :
0.014
1.392
Check Stress Ratio :
t/cm
2
Ft =
f ta =
Stress Ratio = 0.15
Check Stress Ratio :
0.029
0.196Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
Approved
-
Design of Bolted Connection :
Section
2Ls Star-Shaped
80x8
t/cm2
-
10
DateDate
-
AM
Checked
-
Date
-
HK
e p p e
x
4.3 Desgin of bracing members:-
74
m
60 mm 6 mm cm
cm
cm
< <
< <
< Fc
ton >
ton
2
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λx =
qr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm10
3.46
3.36
cm2
cm2
2.3 tonShear Strength :
No. of Bolts = 0.67
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min =
SAFE
2M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Stress Ratio =
SAFE (S.R = 0.24)
0.06
0.4 Fy = 0.96
9.19
At =
ton
t/cm2
< Ft
2.30
5.40
SAFE
SAFE
A net =
Check as Tension Member :
cm
2
1.0Ky =
10.84
Type of Connection :
Length =
Bolts :
m
189.8
12.14 cm2
λx =
Kg/mWeight =
Lbx =
10 mm
ton
3.45 1.0m
ton Grade of Steel : I
Member ID : VB-045
t/cm
2
3.45
Sheet No. :
2.85
SAFE
iy =
Case of Loading :
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
2.25
1.00
189.8 200
ARESCO
TEBBIN
cm4
111.9
Thickness of Gusset Plate =
Ix =
t =
cm4
300
300
Lby =
13.82
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
1.69a =
3.45
Bolted
ix = 1.82
2Ls Back to Back
Properties of Section :
Section :
Area =
M12
Rev. Descreption Design
F tr =
p
(S.R = 0.33)
tG.P
α = 0.8 tmin =
1 -
22.8
121.4
0
λy =
q r =
Iy =
λy = 200
30
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
60x6
e =
SAFE
Actual Stress :
Allowable Stress :
0.082
1.392
Check Stress Ratio :
t/cm
2
Ft =
121.4
f ta =
Stress Ratio = 0.78
Check Stress Ratio :
0.163
0.208Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
Approved
-
Design of Bolted Connection :
Section
2Ls Back to Back
60x6
t/cm2
-
10
DateDate
-
AM
Checked
-
Date
-
HK
e p p e
x
4.3 Desgin of bracing members:-
75
m
80 mm 8 mm cm
cm
cm
< <
< <
< Fc
ton >
ton
2
DateDate
-
AM
Checked
-
Date
-
HK
Approved
-
Design of Bolted Connection :
Section
2Ls Back to Back
80x8
t/cm2
-
10
Stress Ratio = 0.46
Check Stress Ratio :
0.104
0.227Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
SAFE
Actual Stress :
Allowable Stress :
0.011
1.392
Check Stress Ratio :
t/cm
2
Ft =
181.8
f ta =
35
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
80x8
e =
1 -
72.3
181.8
0
λy =
q r =
Iy =
λy = 200
Rev. Descreption Design
F tr =
p
(S.R = 0.38)
tG.P
α = 0.8 tmin =
a =
3.34
Bolted
ix = 2.42
2Ls Back to Back
Properties of Section :
Section :
Area =
M12
300
300
Lby =
24.60
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
2.26
138.0 200
ARESCO
TEBBIN
cm4
332.0
Thickness of Gusset Plate =
Ix =
t =
cm4
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
2.56
0.24
t/cm2
6.68
Sheet No. :
3.67
SAFE
iy =
Case of Loading :ton Grade of Steel : I
Member ID : VB-062
Lbx =
10 mm
ton
6.68 0.5m
Type of Connection :
Length =
Bolts :
m
138.0
22.36 cm2
λx =
Kg/mWeight =
A net =
Check as Tension Member :
cm
2
1.0Ky =
19.32
SAFE
SAFE
< Ft
2.80
5.40
Stress Ratio =
SAFE (S.R = 0.25)
0.01
0.4 Fy = 0.96
10.06
At =
ton
t/cm2
SAFE
2M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Shear Strength :
No. of Bolts = 0.76
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min = 3.46
3.36
cm2
cm2
2.6 tonqr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm10
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λx =
e p p e
x
4.3 Desgin of bracing members:-
76
m
80 mm 8 mm cm
cm
cm
< <
< <
< Fc
ton >
ton
2
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λx =
qr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm10
3.46
3.36
cm2
cm2
5.6 tonShear Strength :
No. of Bolts = 1.68
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min =
SAFE
2M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Stress Ratio =
SAFE (S.R = 0.56)
0.00
0.4 Fy = 0.96
10.06
At =
ton
t/cm2
< Ft
2.80
5.40
SAFE
SAFE
A net =
Check as Tension Member :
cm
2
1.0Ky =
19.32
Type of Connection :
Length =
Bolts :
m
146.7
22.36 cm2
λx =
Kg/mWeight =
Lbx =
10 mm
ton
3.55 1.0m
ton Grade of Steel : I
Member ID : VB-074
t/cm
2
3.55
Sheet No. :
3.67
SAFE
iy =
Case of Loading :
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
5.64
0.00
146.7 200
ARESCO
TEBBIN
cm4
332.0
Thickness of Gusset Plate =
Ix =
t =
cm4
300
300
Lby =
24.60
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
2.26a =
3.55
Bolted
ix = 2.42
2Ls Back to Back
Properties of Section :
Section :
Area =
M12
Rev. Descreption Design
F tr =
p
(S.R = 0.83)
tG.P
α = 0.8 tmin =
1 -
72.3
96.7
0
λy =
q r =
Iy =
λy = 200
35
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
80x8
e =
SAFE
Actual Stress :
Allowable Stress :
0.000
1.392
Check Stress Ratio :
t/cm
2
Ft =
96.7
f ta =
Stress Ratio = 0.66
Check Stress Ratio :
0.229
0.348Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
Approved
-
Design of Bolted Connection :
Section
2Ls Back to Back
80x8
t/cm2
-
10
DateDate
-
AM
Checked
-
Date
-
HK
e p p e
x
4.3 Desgin of bracing members:-
77
m
60 mm 6 mm cm
cm
cm
< <
< <
< Fc
ton >
ton
2
DateDate
-
AM
Checked
-
Date
-
HK
Approved
-
Design of Bolted Connection :
Section
2Ls Back to Back
60x6
t/cm2
-
8
Stress Ratio = 0.66
Check Stress Ratio :
0.246
0.373Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
SAFE
Actual Stress :
Allowable Stress :
0.030
1.392
Check Stress Ratio :
t/cm
2
Ft =
93.2
f ta =
30
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
60x6
e =
1 -
22.8
93.2
0
λy =
q r =
Iy =
λy = 200
Rev. Descreption Design
F tr =
p
(S.R = 0.61)
tG.P
α = 0.8 tmin =
a =
2.58
Bolted
ix = 1.82
2Ls Back to Back
Properties of Section :
Section :
Area =
M12
300
300
Lby =
13.82
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
1.69
141.8 200
ARESCO
TEBBIN
cm4
106.0
Thickness of Gusset Plate =
Ix =
t =
cm4
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
3.40
0.37
t/cm2
2.58
Sheet No. :
2.77
SAFE
iy =
Case of Loading :ton Grade of Steel : I
Member ID : VB-078
Lbx =
8 mm
ton
2.58 1.0m
Type of Connection :
Length =
Bolts :
m
141.8
12.14 cm2
λx =
Kg/mWeight =
A net =
Check as Tension Member :
cm
2
1.0Ky =
10.84
SAFE
SAFE
< Ft
1.84
4.32
Stress Ratio =
SAFE (S.R = 0.46)
0.02
0.4 Fy = 0.96
7.35
At =
ton
t/cm2
SAFE
2M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Shear Strength :
No. of Bolts = 1.23
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min = 2.76
3.36
cm2
cm2
3.4 tonqr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm8
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λx =
e p p e
x
4.3 Desgin of bracing members:-
78
m
60 mm 6 mm cm
cm
cm
< <
< <
< Fc
ton >
ton
2
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λx =
qr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm8
2.76
3.36
cm2
cm2
0.2 tonShear Strength :
No. of Bolts = 0.08
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min =
SAFE
2M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Stress Ratio =
SAFE (S.R = 0.03)
0.01
0.4 Fy = 0.96
7.35
At =
ton
t/cm2
< Ft
1.84
4.32
SAFE
SAFE
A net =
Check as Tension Member :
cm
2
1.0Ky =
10.84
Type of Connection :
Length =
Bolts :
m
186.3
12.14 cm2
λx =
Kg/mWeight =
Lbx =
8 mm
ton
3.39 1.0m
ton Grade of Steel : I
Member ID : VB-079
t/cm
2
3.39
Sheet No. :
2.77
SAFE
iy =
Case of Loading :
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
0.21
0.23
186.3 200
ARESCO
TEBBIN
cm4
106.0
Thickness of Gusset Plate =
Ix =
t =
cm4
300
300
Lby =
13.82
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
1.69a =
3.39
Bolted
ix = 1.82
2Ls Back to Back
Properties of Section :
Section :
Area =
M12
Rev. Descreption Design
F tr =
p
(S.R = 0.04)
tG.P
α = 0.8 tmin =
1 -
22.8
122.4
0
λy =
q r =
Iy =
λy = 200
30
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
60x6
e =
SAFE
Actual Stress :
Allowable Stress :
0.019
1.392
Check Stress Ratio :
t/cm
2
Ft =
122.4
f ta =
Stress Ratio = 0.07
Check Stress Ratio :
0.015
0.216Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
Approved
-
Design of Bolted Connection :
Section
2Ls Back to Back
60x6
t/cm2
-
8
DateDate
-
AM
Checked
-
Date
-
HK
e p p e
x
4.3 Desgin of bracing members:-
79
m
80 mm 8 mm cm
cm
cm
< <
< <
< Fc
ton >
ton
2
DateDate
-
AM
Checked
-
Date
-
HK
Approved
-
Design of Bolted Connection :
Section
2Ls Back to Back
80x8
t/cm2
-
10
Stress Ratio = 0.37
Check Stress Ratio :
0.079
0.212Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
SAFE
Actual Stress :
Allowable Stress :
0.000
1.392
Check Stress Ratio :
t/cm
2
Ft =
188.1
f ta =
35
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
80x8
e =
1 -
72.3
188.1
0
λy =
q r =
Iy =
λy = 200
Rev. Descreption Design
F tr =
p
(S.R = 0.28)
tG.P
α = 0.8 tmin =
a =
3.46
Bolted
ix = 2.42
2Ls Back to Back
Properties of Section :
Section :
Area =
M12
300
300
Lby =
24.60
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
2.26
142.8 200
ARESCO
TEBBIN
cm4
332.0
Thickness of Gusset Plate =
Ix =
t =
cm4
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
1.94
0.00
t/cm2
6.91
Sheet No. :
3.67
SAFE
iy =
Case of Loading :ton Grade of Steel : I
Member ID : VB-081
Lbx =
10 mm
ton
6.91 0.5m
Type of Connection :
Length =
Bolts :
m
142.8
22.36 cm2
λx =
Kg/mWeight =
A net =
Check as Tension Member :
cm
2
1.0Ky =
19.32
SAFE
SAFE
< Ft
2.80
5.40
Stress Ratio =
SAFE (S.R = 0.19)
0.00
0.4 Fy = 0.96
10.06
At =
ton
t/cm2
SAFE
2M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Shear Strength :
No. of Bolts = 0.58
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min = 3.46
3.36
cm2
cm2
1.9 tonqr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm10
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λx =
e p p e
x
4.3 Desgin of bracing members:-
80
m
70 mm 7 mm cm
cm
cm
< <
< <
< Fc
ton >
ton
4
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λx =
qr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm8
2.76
3.36
cm2
cm2
8.7 tonShear Strength :
No. of Bolts = 3.16
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min =
SAFE
4M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Stress Ratio =
SAFE (S.R = 0.67)
0.00
0.4 Fy = 0.96
12.88
At =
ton
t/cm2
< Ft
1.84
10.08
SAFE
SAFE
A net =
Check as Tension Member :
cm
2
1.0Ky =
14.76
Type of Connection :
Length =
Bolts :
m
109.1
16.84 cm2
λx =
Kg/mWeight =
Lbx =
8 mm
ton
2.31 1.0m
ton Grade of Steel : I
Member ID : VB-086
t/cm
2
2.31
Sheet No. :
3.18
SAFE
iy =
Case of Loading :
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
8.74
0.00
109.1 200
ARESCO
TEBBIN
cm4
190.4
Thickness of Gusset Plate =
Ix =
t =
cm4
300
300
Lby =
18.80
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
1.97a =
2.31
Bolted
ix = 2.12
2Ls Back to Back
Properties of Section :
Section :
Area =
M12
Rev. Descreption Design
F tr =
p
(S.R = 0.79)
tG.P
α = 0.8 tmin =
1 -
42.4
72.7
0
λy =
q r =
Iy =
λy = 200
30
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
70x7
e =
SAFE
Actual Stress :
Allowable Stress :
0.000
1.392
Check Stress Ratio :
t/cm
2
Ft =
72.7
f ta =
Stress Ratio = 0.74
Check Stress Ratio :
0.465
0.630Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
Approved
-
Design of Bolted Connection :
Section
2Ls Back to Back
70x7
t/cm2
-
8
DateDate
-
AM
Checked
-
Date
-
HK
e p p e
x
4.3 Desgin of bracing members:-
81
m
60 mm 6 mm cm
cm
cm
< <
< <
< Fc
ton >
ton
2
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λx =
qr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm8
2.76
3.36
cm2
cm2
3.0 tonShear Strength :
No. of Bolts = 1.10
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min =
SAFE
2M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Stress Ratio =
SAFE (S.R = 0.41)
0.03
0.4 Fy = 0.96
7.35
At =
ton
t/cm2
< Ft
1.84
4.32
SAFE
SAFE
A net =
Check as Tension Member :
cm
2
1.0Ky =
10.84
Type of Connection :
Length =
Bolts :
m
70.1
12.14 cm2
λx =
Kg/mWeight =
Lbx =
8 mm
ton
2.55 0.5m
ton Grade of Steel : I
Member ID : VB-090
t/cm
2
2.55
Sheet No. :
2.77
SAFE
iy =
Case of Loading :
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
3.04
0.52
70.1 200
ARESCO
TEBBIN
cm4
106.0
Thickness of Gusset Plate =
Ix =
t =
cm4
300
300
Lby =
13.82
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
1.69a =
1.28
Bolted
ix = 1.82
2Ls Back to Back
Properties of Section :
Section :
Area =
M12
Rev. Descreption Design
F tr =
p
(S.R = 0.54)
tG.P
α = 0.8 tmin =
1 -
22.8
92.1
0
λy =
q r =
Iy =
λy = 200
30
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
60x6
e =
SAFE
Actual Stress :
Allowable Stress :
0.043
1.392
Check Stress Ratio :
t/cm
2
Ft =
92.1
f ta =
Stress Ratio = 0.26
Check Stress Ratio :
0.220
0.848Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
Approved
-
Design of Bolted Connection :
Section
2Ls Back to Back
60x6
t/cm2
-
8
DateDate
-
AM
Checked
-
Date
-
HK
e p p e
x
4.3 Desgin of bracing members:-
82
m
70 mm 7 mm cm
cm
cm
< <
< <
< Fc
ton >
ton
2
DateDate
-
AM
Checked
-
Date
-
HK
Approved
-
Design of Bolted Connection :
Section
2Ls Back to Back
70x7
t/cm2
-
8
Stress Ratio = 0.83
Check Stress Ratio :
0.272
0.329Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
SAFE
Actual Stress :
Allowable Stress :
0.172
1.392
Check Stress Ratio :
t/cm
2
Ft =
100.6
f ta =
30
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
70x7
e =
1 -
42.4
100.6
0
λy =
q r =
Iy =
λy = 200
Rev. Descreption Design
F tr =
p
(S.R = 0.92)
tG.P
α = 0.8 tmin =
a =
3.20
Bolted
ix = 2.12
2Ls Back to Back
Properties of Section :
Section :
Area =
M12
300
300
Lby =
18.80
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
1.97
150.9 200
ARESCO
TEBBIN
cm4
190.4
Thickness of Gusset Plate =
Ix =
t =
cm4
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
5.11
2.90
t/cm2
3.20
Sheet No. :
3.18
SAFE
iy =
Case of Loading :ton Grade of Steel : I
Member ID : VB-105
Lbx =
8 mm
ton
3.20 1.0m
Type of Connection :
Length =
Bolts :
m
150.9
16.84 cm2
λx =
Kg/mWeight =
A net =
Check as Tension Member :
cm
2
1.0Ky =
14.76
SAFE
SAFE
< Ft
1.84
4.32
Stress Ratio =
SAFE (S.R = 0.69)
0.12
0.4 Fy = 0.96
7.35
At =
ton
t/cm2
SAFE
2M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Shear Strength :
No. of Bolts = 1.85
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min = 2.76
3.36
cm2
cm2
5.1 tonqr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm8
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λx =
e p p e
x
4.3 Desgin of bracing members:-
83
m
80 mm 8 mm cm
cm
cm
< <
< <
< Fc
ton >
ton
4
DateDate
-
AM
Checked
-
Date
-
HK
Approved
-
Design of Bolted Connection :
Section
2Ls Back to Back
80x8
t/cm2
-
10
Stress Ratio = 0.85
Check Stress Ratio :
0.510
0.601Allowable Stress : Fc =
Actual Stress : f ca =
SAFE
SAFE
Actual Stress :
Allowable Stress :
0.000
1.392
Check Stress Ratio :
t/cm
2
Ft =
73.6
f ta =
35
AK
50
-
MISR BANI SUEF CAMPANY
Issued for Approval
BOOSTER FAN PLATFORM & DUCT SUPPORT
80x8
e =
1 -
72.3
73.6
0
λy =
q r =
Iy =
λy = 200
Rev. Descreption Design
F tr =
p
(S.R = 0.93)
tG.P
α = 0.8 tmin =
a =
2.70
Bolted
ix = 2.42
2Ls Back to Back
Properties of Section :
Section :
Area =
M12
300
300
Lby =
24.60
Check Slenderness Ratio :
Design Calculation Sheet
Design of Angles Subjected to Axial Force
According to ECP No.(205)
Kx =
2.26
111.7 200
ARESCO
TEBBIN
cm4
332.0
Thickness of Gusset Plate =
Ix =
t =
cm4
asec
Project Tiltle :
Compression =
ST- 37Tension =
Departement :
12.54
0.00
t/cm2
2.70
Sheet No. :
3.67
SAFE
iy =
Case of Loading :ton Grade of Steel : I
Member ID : VB-117
Lbx =
10 mm
ton
2.70 1.0m
Type of Connection :
Length =
Bolts :
m
111.7
22.36 cm2
λx =
Kg/mWeight =
A net =
Check as Tension Member :
cm
2
1.0Ky =
19.32
SAFE
SAFE
< Ft
2.80
12.60
Stress Ratio =
SAFE (S.R = 0.73)
0.00
0.4 Fy = 0.96
16.97
At =
ton
t/cm2
SAFE
4M12(8.8)
e
25
Bolts
Check of Shear Rapture :
Shear Strength :
No. of Bolts = 3.73
Bearing Strength :
R sh = q b x A s x n =
Bolts
R b = F b x d x t min = 3.46
3.36
cm2
cm2
12.5 tonqr x Ash + Ftr x At =
0.725 Fy = 1.74
x
mm10
Check as Compression Member :
Grade of Bolts : 8.8 Ash =Bolts : M12
t/cm2
t/cm
2
Check Slenderness Ratio :
λx =
e p p e
x
4.3 Desgin of bracing members:-
84
Joint OutputCase CaseType StepType F1 F2 F3
Text Text Text Text Tonf Tonf Tonf
159 ENV. Combination Max 0.1301 0.4909 10.0431
159 ENV. Combination Min ‐0.1308 ‐1.9141 ‐1.326
161 ENV. Combination Min ‐0.1302 ‐0.8183 ‐2.8709
162 ENV. Combination Max 0.1304 1.9317 10.6314
Extreme output reaction for IPE200 base connection:-
4.4-Design of bases connections:-
85
0
X
C X
T
30
Qy
20
Qx
Qr
20
20 20
Bearing Plate Data :
< %
mm %
mm %
< %
< %
< %
23
mm
mm mm Cm2
< <
< 1.1 *
* * mm
Ø mm
mm mm mm
* * mm mm
* * mm mm
mm
400 mm
qr = Qr/Atotal =
400 mmUse Embebed Length = 520Anchor Bolt Total Length =
mmRequired Embebed Length =
Minimum Embebed Length ( 20 d ) =
of Tmin
6.8Flange Weld Size = Web Weld Size =
0.72
FINALLY USE :
21
30
Hole Diameter =
Hole Diameter =
GROUT THICK. =
mm
ftall-toncm
2
1.01
Embebed Length =
GRADE
Bearing Plate Area =
Bearing Plates Are Clashed
Check of Pitch Bolt Distance
1.4
100
qall-toncm
2
4.6+ 3-NUT & WASHER
21
Max. Bearing =
4.48
kg/cm2
of Bearing plate
ton
160Thread Length =
250
S2-(mm)
Please Decrease dictanse S1
140
80
60
140
Check of Edge Bolt Distance
12
8.5
5.6
Anchor Bolt Data :
Fu-toncm2
3.6
Fy-toncm2
2.4
M-(mm)
20
qact. (ton/cm2
) =
fcu-kg/cm
2
fb-kgcm2
250
fCall-kgcm2
70.00 8.18
Steel Data:
20
ton (TEN.)
0.27 Safe
21.1
ton
80
S1-(mm)
20
Approve By
(Qr/n)/(Abolt) =
SAFE0.61(fact/ftall)2
+(qact/qall)2
=
Joint Forces :-
10.01
Steel Grade
ton (COM.)
AM
0.72
Design By
300
Rev.
Steel Grade
MISR BANI SUEF COMPANY
600
D-(mm)
IPE200
mm
mm
mm
mm
mm
B-(mm)
Project
1.94
0.131
ton
ton
Tw =
Tf =
Column Size :-
200
2.88 Bf =
AK
5 140
2
Bolt (d)
20
r =
30.00
10
100
d-(mm)
Design of Base Connection (Hinged-with anchor bolts)-(N,Q)
Dept. Item BASE PLATE FOR SECTION IPE200
H =
Grout (mm)
d-(mm)t-(mm) b-(mm)
0.765
N-(mm)
fw-all-toncm
2
37
240 140
100
As/bolt(cm
2
)
2.45
t-(mm) b-(mm)
HKCheck By
240
0
Tpl-(mm)
X2 =
kg/cm2
Check of Plate Thickness due to Compresion(C):
30mm
Check of concrete due to Compresion(C):
70.0
0.13 ton.cm/cm
SAFEfcon = C / ( B * D ) = 29.8
25 mm Moment/unit width =X1 =
kg/cm2
6 * M / (0.58 * Fy * B) =
Check of Plate Thickness due to Tension(T):
Thickness required t (mm)= 6 * M / (0.72 * Fy * B) = 6.8 SAFE
ftact (ton/cm2
) = T/(n*Abolt) = 0.59 ton/cm2
Check of Anchor Bolt due to Shear(Qr) & Tension(T):
Moment = T(tension)x[(D-S1)x0.5-N] = 14.4 ton.cm
Thickness required t (mm)=
0.61
SAFE
SAFE
ton/cm2
Safe 0.25
Safety Ratio
All Tension Supported By Bearing Plate
ton/cm2
1.01
ton/cm2
Thread Length = 160
Safe0.72
Safety Ratio 0.43
Safety Ratio 0.27
0.58
160
Actual Tension / Anchor =
Required Length of Anchor Bolts :- 96.9 Cm2
37
0.05
520
400
Check of weld:
-154
Max.Tension Supported By Bearing Plate= 2.2 ton
0.40
60 10
ton/cm2
BASE PLATE
ANCHOR BOLT 2
240
BEARING PLATE 10
25 140
100
37
400
GRADE
GRADE 37
520
100
37
feq = (fca
2
+3*q2
) = ton/cm2
TEMPLATE 5 140 60
37
GRADE
Total Length =
0.80
Weld Size ( of Tmin )
TemPlate Data :
1.94
Number(n) Fu-toncm2
3.6
Base Plate Data :
Concrete Data:
0.765
Safety Ratio
Safety Ratio
fconXmax.(x1 or x2)2
/2 =
0.84
WELD RATIO 0.8
0.72
20
GRADE
NOTE:
q
all & ftall decreased by 15 % according to clause 6.7.5 in ECP 205-2001
fca = Max.(C,T)/Atotal =
1
A total cm2= 39.57
SAFE
Safety Ratio 0.52
ton/cm2
86
Joint OutputCase StepType F1 F2 F3
Text Text Text Tonf Tonf Tonf
47 ENV. Max 0.6558 1.2618 10.259
51 ENV. Min ‐0.2236 ‐1.6546 ‐15.0122
296 ENV. Max 0.3845 0.9532 25.0996
Extreme output reaction for IPE270 base connection:-
87
0
X
C X
T
30
Qy
#
Qx
Qr
#
15 15
Bearing Plate Data :
< %
mm %
mm %
< %
< %
< %
23
mm
mm mm Cm
2
< <
< 1.1 *
* * mm
Ø mm
mm mm mm
* * mm mm
* * mm mm
mm
600 mm
qr = Qr/Atotal =
600 mmUse Embebed Length = 750Anchor Bolt Total Length =
mmRequired Embebed Length =
Minimum Embebed Length ( 20 d ) =
of Tmin
8.16Flange Weld Size = Web Weld Size =
0.72
FINALLY USE :
31
30
Hole Diameter =
Hole Diameter =
GROUT THICK. =
mm
ftall-toncm
2
1.01
Embebed Length =
GRADE
Bearing Plate Area =
Bearing Plates Are Clashed
Check of Pitch Bolt Distance
3.8
100
qall-toncm
2
4.6+ 3-NUT & WASHER
31
Max. Bearing =
5.28
kg/cm2
of Bearing plate
ton
200Thread Length =
32140
S2-(mm)
Please Decrease dictanse S1
240
140
230
230
Check of Edge Bolt Distance
15
10.2
6.6
Anchor Bolt Data :
Fu-toncm
2
3.6
Fy-toncm2
2.4
M-(mm)
52.5
qact. (ton/cm2
) =
fcu-kg/cm2
fb-kgcm2
250
fCall-kgcm2
70.00 8.18
Steel Data:
15
ton (TEN.)
0.39 Safe
29.6
ton
140
S1-(mm)
20
Approve By
(Qr/n)/(Abolt) =
SAFE0.45(fact/ftall)2
+(qact/qall)2
=
Joint Forces :-
25.1
Steel Grade
ton (COM.)
AM
0.72
Design By
300
Rev.
Steel Grade
MISR BANI SUEF COMPANY
600
D-(mm)
IPE270
mm
mm
mm
mm
mm
B-(mm)
Project
1.66
0.66
ton
ton
Tw =
Tf =
Column Size :-
270
15.02 Bf =
AK
5 230
4
Bolt (d)
30
r =
30.00
10
135
d-(mm)
Design of Base Connection (Hinged-with anchor bolts)-(N,Q)
Dept. Item BASE PLATE FOR SECTION IPE270
H =
Grout (mm)
d-(mm)t-(mm) b-(mm)
0.765
N-(mm)
fw-all-toncm
2
37
300 240
100
As/bolt(cm2
)
5.61
t-(mm) b-(mm)
HKCheck By
300
140
Tpl-(mm)
X2 =
kg/cm
2
Check of Plate Thickness due to Compresion(C):
66mm
Check of concrete due to Compresion(C):
70.0
0.76 ton.cm/cm
SAFEfcon = C / ( B * D ) = 34.9
21.75 mm Moment/unit width =X1 =
kg/cm2
6 * M / (0.58 * Fy * B) =
Check of Plate Thickness due to Tension(T):
Thickness required t (mm)= 6 * M / (0.72 * Fy * B) = 16.2 SAFE
ftact (ton/cm2
) = T/(n*Abolt) = 0.67 ton/cm
2
Check of Anchor Bolt due to Shear(Qr) & Tension(T):
Moment = T(tension)x[(D-S1)x0.5-N] = 48.8 ton.cm
Thickness required t (mm)=
0.45
SAFE
SAFE
ton/cm2
Safe 0.39
Safety Ratio
ton/cm
2
1.01
ton/cm2
Thread Length = 200
Safe0.72
Safety Ratio 0.50
Safety Ratio 0.51
0.66
200
Actual Tension / Anchor =
Required Length of Anchor Bolts :- 92.9 Cm
2
37
0.03
750
600
Check of weld:
209
Max.Tension Supported By Bearing Plate= 2.1 ton
0.08
230 10
ton/cm
2
BASE PLATE
ANCHOR BOLT 4
300
BEARING PLATE 10
32 240
100
37
600
GRADE
GRADE 37
750
100
37
feq = (fca
2
+3*q
2
) = ton/cm
2
TEMPLATE 5 230 230
37
GRADE
Total Length =
0.80
Weld Size ( of Tmin )
TemPlate Data :
1.79
Number(n) Fu-toncm2
3.6
Base Plate Data :
Concrete Data:
0.765
Safety Ratio
Safety Ratio
fconXmax.(x1 or x2)
2
/2 =
0.93
WELD RATIO 0.8
0.72
30
GRADE
NOTE: q
all & ftall decreased by 15 % according to clause 6.7.5 in ECP 205-2001
fca = Max.(C,T)/Atotal =
1
A total cm2= 64.45
SAFE
Safety Ratio 0.10
ton/cm2
88
Joint OutputCase CaseType F1 F2 F3
Text Text Text Tonf Tonf Tonf
203 ENV. Combination 2.4955 0.000255 1.0418
203 ENV. Combination ‐1.912 ‐0.00042 ‐1.1233
204 ENV. Combination ‐1.7624 ‐0.00047 ‐1.0057
Extreme output reaction for UPN200 base connection:-
89
0
X
C X
T
30
Qy
#
Qx
Qr
#
20 20
Bearing Plate Data :
< %
mm %
mm %
< %
< %
< %
23
mm
mm mm Cm
2
< <
< 1.1 *
* * mm
Ø mm
mm mm mm
* * mm mm
* * mm mm
mm
NOTE:
q
all & ftall decreased by 15 % according to clause 6.7.5 in ECP 205-2001
fca = Max.(C,T)/Atotal =
1
A total cm2= 47.90
SAFE
Safety Ratio 0.67
ton/cm
2
0.765
Safety Ratio
Safety Ratio
fconXmax.(x1 or x2)
2
/2 =
0.62
WELD RATIO 0.8
0.80
Weld Size ( of Tmin )
TemPlate Data :
2.50
Number(n)
0.72
20
GRADE 37
feq = (fca
2
+3*q
2
) = ton/cm
2
TEMPLATE 5 140 60
37
GRADE
Total Length =
37
400
GRADE
GRADE 37
510
100
ton/cm
2
BASE PLATE
ANCHOR BOLT 2
240
BEARING PLATE 10
20 160
100
510
400
Check of weld:
-324
Max.Tension Supported By Bearing Plate= 2.2 ton
0.51
60 10
150
Actual Tension / Anchor =
Required Length of Anchor Bolts :- 96.9 Cm2
37
0.05
ton/cm2
Thread Length = 150
Safe0.72
Safety Ratio 0.04
Safety Ratio 0.17
0.23
0.50
SAFE
SAFE
ton/cm
2
Safe 0.02
Safety Ratio
All Tension Supported By Bearing Plate
ton/cm2
1.01ftact (ton/cm
2
) = T/(n*Abolt) = 0.23 ton/cm
2
Check of Anchor Bolt due to Shear(Qr) & Tension(T):
Moment = T(tension)x[(D-S1)x0.5-N] = 5.7 ton.cm
Thickness required t (mm)= 6 * M / (0.58 * Fy * B) =
Check of Plate Thickness due to Tension(T):
Thickness required t (mm)= 6 * M / (0.72 * Fy * B) = 3.4 SAFE
0.03 ton.cm/cm
SAFEfcon = C / ( B * D ) = 2.7
25 mm Moment/unit width =X1 =
kg/cm
2
X2 =
kg/cm
2
Check of Plate Thickness due to Compresion(C):
50mm
Check of concrete due to Compresion(C):
Fu-toncm2
3.6
100
As/bolt(cm
2
)
2.45
t-(mm) b-(mm)
HKCheck By
70.0
Base Plate Data :
Concrete Data:
Grout (mm)
d-(mm)t-(mm) b-(mm)
0.765
N-(mm)
75
d-(mm)
Design of Base Connection (Hinged-with anchor bolts)-(N,Q)
Dept. Item BASE PLATE FOR SECTION UPN200
H =
Bf =
AK
5 140
2
Bolt (d)
20
r =
30.00
10
fw-all-toncm
2
Project
0
2.5
ton
ton
Tw =
Tf =
Column Size :- 240
0200
MISR BANI SUEF COMPANY
600
D-(mm)
UPN200
mm
mm
mm
1.13
ton (COM.)
AM
0.72
Design By
300
Rev.
Steel Grade
20
Approve By
(Qr/n)/(Abolt) =
SAFE0.50(fact/ftall)
2
+(qact/qall)
2
=
Joint Forces :-
1.042
Steel Grade
37
ton (TEN.)
0.09 Safe
12.3
ton
80
S1-(mm)
qact. (ton/cm
2
) =
fcu-kg/cm
2
fb-kgcm2
250
fCall-kgcm2
70.00 8.18
Steel Data:
mm
mm
6
11.5
8.5
Anchor Bolt Data :
Fu-toncm
2
3.6
Fy-toncm2
2.4
240
B-(mm)
160
M-(mm)
42.5 20
Tpl-(mm)
200
S2-(mm)
Please Decrease dictanse S1
160
80
60
140
Check of Edge Bolt Distance
4.6+ 3-NUT & WASHER
21
Max. Bearing =
6.8
kg/cm2
of Bearing plate
ton
150Thread Length =
ftall-toncm2
1.01
Embebed Length =
GRADE
Bearing Plate Area =
Bearing Plates Are Clashed
Check of Pitch Bolt Distance
0.6
100
qall-toncm2
21
30
Hole Diameter =
Hole Diameter =
GROUT THICK. =
mm
mmRequired Embebed Length =
Minimum Embebed Length ( 20 d ) =
of Tmin
9.2Flange Weld Size = Web Weld Size =
0.72
FINALLY USE :
400 mm
qr = Qr/Atotal =
400 mmUse Embebed Length = 510Anchor Bolt Total Length =
90
Frame Station OutputCase CaseType StepType P V2 V3
Text m Text Text Text Tonf Tonf Tonf
B‐021 4.92 ENV. Combination Min ‐1.041 0.2423 ‐1.4483
B‐103 5.5 ENV. Combination Max 0.2678 2.5909 0.2414
B‐067 9.9 ENV. Combination Max 8.109 0.0482 0.0485
Extrem out put reactions for HEA160 shear connection:
4.5 Design of Beam connections:-
91
I
2
4
1
20 mm
5
< mm
t = mm
ton < 1
<
cm
<
<
<
12.91
20
SAFE
(Subjected to Shear +Torsion)
Mcan = 7.67 cm.t
cm2
4.90
ton
SAFE
6.47
0.12
ton
SAFE
18.41
Check of Combined Shear and Tension :
E= 80 mm
0.72
160
End Plate Thickness :
mm
mmNet Width = 116
SAFE
-
t/cm
2
19 cm.t
0.236
t/cm2
169.9 cm
4
Face (1-1) :
0.17
0.792
t/cm
2
0.72
Face (2-2) :
ton
Checked Date
8.0 6.0 mmaround the Flanges = mm
5.0
Point (B) :
2.03 6.47
Check of Tension :
Tensile Strength :
ton
α = 0.60
Stressed Area =
t/cm
2
t/cm
2
Sweld :
Point (A) :
0.41 t/cm
2
HK
0.792
- - - -
Check on Weld :
0.3
Sweld =
(Subjected to Shear +Tension)
around the Web = mm
DateDesign DateApproved
AM
Rev. Descreption
0
4.90
Bearing Strength :
Rleast =
Shear Strength :
Issued for Approval AK
1 - -
SAFE
Check of Bolts :
Grade of Bolts : 8.8
Number of Columns of Bolts =
tmin =
Number of Plans Subjected to Shear =
Bolt Diameter = 20
mm
St 37
Connection :
Member :
Design Calculation Sheet
Design of Bolted Shear Connection
of the Bearing Type
HEA160
asec
H = 160
Connected Beams :
Beam (1) :
mm
Qy = 2.6
H = 152
HEA 160
ARESCO
TEBBIN
Qx = 1.5 ton
ton
bf =
mm
mm
N =
tw =
tf =
mm
mm
160
6.0
Arrangement of Bolts :
A= 30
tw =
80
9.0
Rsh a =
2.45
4.90
8.64 ton
mm
0.74
ton
Check of Shear :
mm
mm
bf =
IPE 160
5.0
Beam (2) :
82 mm
mm
tf = 7.4 mm
Number of Bolts :
B = D= mm
Bp =
40
1.61t = mm
t/cm
2
t/cm2
0.38
SAFE
Project Tiltle :
Department : Booster Fan Platform & Duct Support
MISR BANI SUEF COMPANY
Case of Loading :
8.1 ton
Grade of Steel :
 nAqR sbsh
 tmindFR bb












22
n
Q
n
Q yx
 subt AF0.33R
    
2
A
2
tAeq q3ff
    
2
B
2
tBeq q3ff












22
t
ta
sh
ash
R
R
R
R

bf
M
t
all
6
X
t
M

p
t
w
y
y
I
xM
A
Q
q
.
VL
    
22
xytotal
qqq
pI

p
t
x
I
yM
q
.

n
T
Rta
y
F0.58
net
y
t
A
Q
f

bf
M
t
all
6
92
Frame Station OutputCase CaseType StepType P V2 V3
Text m Text Text Text Tonf Tonf Tonf
B‐066 0 ENV. Combination Min ‐0.5646 ‐0.4651 ‐0.1014
B‐066 4.92 ENV. Combination Max ‐0.0981 0.6676 0.0533
B‐066 4.92 ENV. Combination Min ‐7.7812 ‐0.5404 ‐0.061
Extrem out put reactions for HEA300 hanged from HEA160 connection:
93
II
4
2
1
1
2 ton <
3 t = mm
20 mm
<
ton < 1
<
Aw FL=
70.7
19.5
51.2
Aw Total =
-
--- -
SAFE
Check of Combined Shear and Tension :
mm
cm
2
mm
ton
mm
0
Qx =ton
Bolt Diameter =
Grade of Steel : St-37
Case of Loading :
Connected Beams :
H =
mmmm bf =
-
Rev. Descreption
20 mm
290
Grade of Bolts : 8.8
tmin = Allowable & Actual Stresses on Bolts :
mm
Number of Columns of Bolts =
tf =
Date
Design of Shear Plate : Shear Strength :
Tensile Strength : ton
Check of Tension :
Bp =
1.2
mm
Stressed Area = 2.45
Number of Plans Subjected to Shear =
Number of Bolts :
Arrangement of Bolts :
B =
152 mm
7.9
HEA 300
ton
Beam (2) :
Qy =
H =
MISR BANI SUEF COMPANY
BOOSTER FAN PLATFORM & DUCT SUPPORT ID :
1.5
Input Data :
Project Tiltle :
Department :
Sheet No. :
T =
Sweld :
ton5.88
4.67 ton
Bearing Strength :
Rleast =
8.5
300
14.0
Beam (1) : HEA 160
0
1
mm37D=
160 mm
α= 0.6
At Point (A) :
mm
Check on Weld :
mm
A= 180
tw =
tf = 9.0
bf = 160
tw = 6.0
HK
-
Checked Date Approved
AM
Design Date
- -
Issued for Approval AK -
cm2
cm2
0.792
Aw WEB=
SAFEt/cm2
t/cm2
0.70
0.19 SAFE
C =
mm
Properties of Weld :
7.76Take t =
Hp =
7.84
2.01
Design Calculation Sheet
Design of Shear Connection
ACCORDING TO EGYPTIAN CODE OF PRACTICE NO. (205)
0
20 mm
mm
86
7.76
ton
SAFE
mm
(LONGITUDINAL DIRECTION)
(TRANSVERSE DIRECTION)
around the Web = 8.0 mm
0.30around the Flanges = 10.0 mm
cm2
#NUM! mm Rsh a = 4.67 ton
0.456
ton4.67
180
mm
Check of Shear :
E =
 nAqR sbsh
 tmindFR bb












22
n
Q
n
Q yx
 subt AF0.33R

n
T
Rta
ys F
A
Q
q 35.0
2
3













22
t
ta
sh
ash
R
R
R
R
    
2
A
2
tAeq q3ff

bf
M
t
all
6

bf
M
t
all
6
94
Frame Station OutputCase CaseType StepType P V2 V3
Text m Text Text Text Tonf Tonf Tonf
G‐09 0 ENV. CombinatioMin ‐0.2907 ‐7.7284 ‐1.1727
G‐10 6.43197 ENV. CombinatioMax 0.7488 7.9353 0.1355
G‐06 6.43197 ENV. CombinatioMax 1.4467 2.6899 0.4802
Extrem out put reactions for HEA300 typical shear connection:
95
I
2
4
1
16 mm
5
< mm
t = mm
ton < 1
<
cm
<
<
<
6.22
16
SAFE
(Subjected to Shear +Torsion)
Mcan = 3.34 cm.t
cm
2
4.90
ton
SAFE
6.47
0.17
ton
SAFE
7.81
Check of Combined Shear and Tension :
E= 140 mm
0.72
300
End Plate Thickness :
mm
mmNet Width = 256
SAFE
-
t/cm2
74 cm.t
0.33
t/cm
2
1251.8 cm4
Face (1-1) :
0.02
0.792
t/cm
2
0.99
Face (2-2) :
ton
Checked Date
10.0 6.0 mmaround the Flanges = mm
6.0
Point (B) :
0.36 6.47
Check of Tension :
Tensile Strength :
ton
α = 0.60
Stressed Area =
t/cm
2
t/cm2
Sweld :
Point (A) :
0.50 t/cm2
HK
0.792
- - - -
Check on Weld :
0.326
Sweld =
(Subjected to Shear +Tension)
around the Web = mm
DateDesign DateApproved
AM
Rev. Descreption
0
4.90
Bearing Strength :
Rleast =
Shear Strength :
Issued for Approval AK
1 - -
SAFE
Check of Bolts :
Grade of Bolts : 8.8
Number of Columns of Bolts =
tmin =
Number of Plans Subjected to Shear =
Bolt Diameter = 20
mm
St 37
Connection :
Member :
Design Calculation Sheet
Design of Bolted Shear Connection
of the Bearing Type
HEA300
asec
H = 300
Connected Beams :
Beam (1) :
mm
Qy = 7.9
H = 290
HEA 300
ARESCO
TEBBIN
Qx = 1.2 ton
ton
bf =
mm
mm
N =
tw =
tf =
mm
mm
300
8.5
Arrangement of Bolts :
A= 69
tw =
140
14.0
Rsh a =
2.45
4.90
6.91 ton
mm
2.01
ton
Check of Shear :
mm
mm
bf =
IPE 300
7.1
Beam (2) :
150 mm
mm
tf = 10.7 mm
Number of Bolts :
B = D= mm
Bp =
80
2.23t = mm
t/cm
2
t/cm
2
0.46
SAFE
Project Tiltle :
Department : Booster Fan Platform & Duct Support
MISR BANI SUEF COMPANY
Case of Loading :
1.5 ton
Grade of Steel :
 nAqR sbsh
 tmindFR bb












22
n
Q
n
Q yx
 subt AF0.33R
    
2
A
2
tAeq q3ff
    
2
B
2
tBeq q3ff












22
t
ta
sh
ash
R
R
R
R

bf
M
t
all
6
X
tM

p
t
w
y
y
I
xM
A
Q
q
.
VL
    
22
xytotal
qqq
pI

p
t
x
I
yM
q
.

n
T
Rta
yF0.58
net
y
t
A
Q
f

bf
M
t
all
6
96
Frame Station OutputCase CaseType StepType P V2 V3
Text m Text Text Text Tonf Tonf Tonf
P‐02 0 ENV. Combination Min ‐4.6931 ‐0.0246 ‐0.0246
Extrem out put reactions for IPE200 Post connection:
97
II
4
2
1
1
2 ton <
3 t = mm
10 mm
<
ton < 1
<
0.000
ton3.53
220
mm
Check of Shear :
E =
0.000 mm Rsh a = 3.53 ton
cm
2
(LONGITUDINAL DIRECTION)
(TRANSVERSE DIRECTION)
around the Web = 5.0 mm
0.00around the Flanges = 6.0 mm
mm
72
4.97
ton
SAFE
mm0
10 mm
Design Calculation Sheet
Design of Shear Connection
ACCORDING TO EGYPTIAN CODE OF PRACTICE NO. (205)
0.00 SAFE
C =
mm
Properties of Weld :
4.97Take t =
Hp =
0.04
0.01
cm2
0.792
Aw WEB=
SAFEt/cm
2
t/cm
2
0.00
cm2
Design Date
- -
Issued for Approval AK - HK
-
Checked Date Approved
AM
tw =
tf = 8.5
bf = 100
tw = 5.6
At Point (A) :
mm
Check on Weld :
mm
A= 120
6.6
135
10.2
Beam (1) : IPE 200
0
1
mm32D=
Sweld :
ton3.77
3.53 ton
Bearing Strength :
Rleast =
MISR BANI SUEF COMPANY
BOOSTER FAN PLATFORM & DUCT SUPPORT ID :
0.0
Input Data :
Project Tiltle :
Department :
Sheet No. :
T =
0.0
IPE 270
ton
Beam (2) :
Qy =
H =
0.0
mm
Stressed Area = 1.57
Number of Plans Subjected to Shear =
Number of Bolts :
Arrangement of Bolts :
B =
200 mm
tf =
Date
Design of Shear Plate : Shear Strength :
Tensile Strength : ton
Check of Tension :
Bp = 135 mm
Grade of Bolts : 8.8
tmin = Allowable & Actual Stresses on Bolts :
mm
Number of Columns of Bolts =
α= 0.6
H =
mmmm bf =
-
Rev. Descreption
16 mm
270 mm
50
Qx =ton
Bolt Diameter =
Grade of Steel : St-37
Case of Loading :
Connected Beams :
SAFE
Check of Combined Shear and Tension :
mm
cm2
mm
ton
Aw FL=
35.2
16.0
19.2
Aw Total =
-
--- -
 nAqR sbsh
 tmindFR bb












22
n
Q
n
Q yx
 subt AF0.33R

n
T
Rta
ys F
A
Q
q 35.0
2
3













22
t
ta
sh
ash
R
R
R
R
    
2
A
2
tAeq q3ff

bf
M
t
all
6

bf
M
t
all
6
98
Frame Station OutputCase CaseType StepType P V2 V3
Text m Text Text Text Tonf Tonf Tonf
P‐03 0 ENV. Combination Min ‐8.1883 ‐0.0424 ‐0.024
P‐03 0 ENV. Combination Max 4.5779 0.042 0.024
Extrem out put reactions for IPE160 over Beam connection:
99
II
4
2
1
1
2 ton <
3 t = mm
10 mm
<
ton < 1
<
1.016
ton3.84
200
mm
Check of Shear :
E =
15.603 mm Rsh a = 2.02 ton
cm
2
(LONGITUDINAL DIRECTION)
(TRANSVERSE DIRECTION)
around the Web = 4.0 mm
1.15around the Flanges = 6.0 mm
mm
60
2.66
ton
SAFE
mm0
10 mm
Design Calculation Sheet
Design of Shear Connection
ACCORDING TO EGYPTIAN CODE OF PRACTICE NO. (205)
0.19 SAFE
C =
mm
Properties of Weld :
2.66Take t =
Hp =
0.04
0.01
cm2
0.792
Aw WEB=
SAFEt/cm
2
t/cm
2
0.14
cm2
Design Date
- -
Issued for Approval AK - HK
-
Checked Date Approved
AM
tw =
tf = 8.5
bf = 100
tw = 5.6
At Point (A) :
mm
Check on Weld :
mm
A= 100
5.0
#N/A
7.4
Beam (1) : IPE 200
0
1
mm31D=
Sweld :
ton2.02
2.02 ton
Bearing Strength :
Rleast =
MISR BANI SUEF COMPANY
BOOSTER FAN PLATFORM & DUCT SUPPORT ID :
0.0
Input Data :
Project Tiltle :
Department :
Sheet No. :
T =
0.0
IPE 160
ton
Beam (2) :
Qy =
H =
4.6
mm
Stressed Area = 0.84
Number of Plans Subjected to Shear =
Number of Bolts :
Arrangement of Bolts :
B =
200 mm
tf =
Date
Design of Shear Plate : Shear Strength :
Tensile Strength : ton
Check of Tension :
Bp = 122 mm
Grade of Bolts : 8.8
tmin = Allowable & Actual Stresses on Bolts :
mm
Number of Columns of Bolts =
α= 1.0
H =
mmmm bf =
-
Rev. Descreption
12 mm
160 mm
50
Qx =ton
Bolt Diameter =
Grade of Steel : St-37
Case of Loading :
Connected Beams :
SAFE
Check of Combined Shear and Tension :
mm
cm2
mm
ton
Aw FL=
32.0
12.8
19.2
Aw Total =
-
--- -
 nAqR sbsh
 tmindFR bb












22
n
Q
n
Q yx
 subt AF0.33R

n
T
Rta
ys F
A
Q
q 35.0
2
3













22
t
ta
sh
ash
R
R
R
R
    
2
A
2
tAeq q3ff

bf
M
t
all
6

bf
M
t
all
6
100
Frame Station OutputCase CaseType StepType P V2 V3
Text m Text Text Text Tonf Tonf Tonf
B‐074 0 ENV. Combination Min ‐0.5441 ‐2.214 ‐0.1873
B‐074 0 ENV. Combination Max 1.1071 ‐0.8711 0.0977
Extrem out put reactions for IPE160 typical shear connection connection:
101
ARESCO
TEBBIN
IPE160Sheet No. :
Conn. No. :
ton2.22Q =
ton1.11N =cm.t7.77Mweld =
IPE240GirderIPE160Beam
mm L240Hg =mm160Hb =
mm120Bg =mm82Bb =
mm6.20Twg =mm5.00Twb =
mm9.8Tfg =mm7.40Tfb =
mm15r =mm9.00r =
mm6Tplate =
mm25B =mm35A =
mm25C2 =mm20C1=
OK140Check Dim. ( L )mm25E =mm50D =
mm25Edge for N =mm25Edge for Q =
1NO.OF Sh. PLAN8.8mm Bolt Grade16BOLT DIA.(d) =2BOLT NO. (n) =
26.4Fyb =t/cm2
8Fub =cm2
1.57AS =
t/cm2
2.4Fy =t/cm2
3.6Fu =37Steel Grade
LINES2NO.OF W. L. =mm5S =Tmin.0.8Weld Size
t/cm2
0.792Feq = 1.1 * Fweld=t/cm2
0.72Fweld = 0.2 * Fu=
mm5tmin.=0.25K =0.6αN =0.6αQ =
t/bolt1.73RbN.=αN*Fu*d*tmin.=t/bolt1.73RbQ.=αQ*Fu*d*tmin.=t/bolt3.14Rsh=KxFubxAs=
ok0.75>1Long Joint F =t/bolt1.73Rleast =
Safet/bolt1.73<t/bolt1.24
t/cm2
0.96qr =0.4Fy=cm2
2.4Ash.net =
t/cm2
1.74Ftr = 0.725Fy =cm2
0.8At.net =
Safeton2.22>ton3.70Qall=qr* Ash+Ftr*At=
t/cm2
0.96qr =0.4Fy =cm2
0.8Ash.net =
t/cm2
1.74Ftr = 0.725Fy =cm2
2.4At.net =
Safeton1.11>ton4.94Qall=qr*Ash+Ftr*At=
ton3.70<ton2.48Req1 =CHECK-1
Safe1<0.41Req2 =CHECK-2
cm3
25cm2
Zsec. =12.7Asec.=
ton2.22cm.t Qsec. =7.8Msec.=ton1.11Nsec. =
Safet/cm2
0.84<t/cm2
0.32q =
Safet/cm2
1.4<t/cm2
0.39ft =
SafeSafet/cm2
1.54<t/cm2
0.71feq. =
cm4
83.83cm2
Iw =10.02Aw =cm10.02Lw =
Safet/cm2
0.72<t/cm2
0.58ft =N/A+M*Y /I =
Safet/cm2
0.72<t/cm2
0.22q = Q / A =
SafeSafet/cm2
0.792<t/cm2
0.69
0.41Rup.2 Safe Ratio=0.67Rup.1 Safe Ratio=0.72Bolt Safe Ratio=
0.87Conn. Safe Ratio=0.87Weld Safe Ratio=0.46Sec. Safe Ratio=
mm111X60X6PL.FINALLY USE :
HSBB.T.8.8GRADE16M2
mm25B =mm35A =@
mm25C2 =mm20C1 =
mm25E =mm50D =
mm5Sw =Weld Lines2Tmin.0.8Weld Size
Design of Shear Conn. Bearing Type According to ECP No.(205)
Design Calculation Sheet
asec
MISR BANI SUEF COMPANY
BOOSTER FAN PLATFORM & DUCT SUPPORTDepartment :
Project Title :
CHECK OF WELD :
CHECK OF BEAM SEC.:
BOLT DIMENSIONS:
STRAINING ACTIONS:
RUPTURE DUE TO TENSION :
RUPTURE DUE TO SHEAR :
EQUIVALENT RUPTURE :
CONNECTION PROPERTIES:
CHECK OF BOLTS:

 









 22
teq 3qff
    
22
sh nNnQR
102
Frame Station OutputCase CaseType StepType P V2 V3
Text m Text Text Text Tonf Tonf Tonf
B‐054 0 ENV. Combination Min ‐0.5361 ‐0.3766 ‐0.4469
B‐077 0 ENV. Combination Max 4.1844 ‐0.3248 0.0367
2071SA 1.21 ENV. Combination Max ‐0.011 2.9635 0
Extrem out put reactions for IPE200 shear connection :
103
ARESCO
TEBBIN
IPE200Sheet No. :
Conn. No. :
ton2.97Q =
ton4.2N =cm.t10.395Mweld =
IPE200GirderIPE200Beam
mm L200Hg =mm200Hb =
mm100Bg =mm100Bb =
mm5.60Twg =mm5.60Twb =
mm8.5Tfg =mm8.50Tfb =
mm12r =mm12.00r =
mm6Tplate =
mm25B =mm35A =
mm25C2 =mm25C1=
OK200Check Dim. ( L )mm25E =mm50D =
mm25Edge for N =mm25Edge for Q =
1NO.OF Sh. PLAN8.8mm Bolt Grade16BOLT DIA.(d) =3BOLT NO. (n) =
26.4Fyb =t/cm2
8Fub =cm2
1.57AS =
t/cm2
2.4Fy =t/cm2
3.6Fu =37Steel Grade
LINES2NO.OF W. L. =mm5S =Tmin.0.8Weld Size
t/cm2
0.792Feq = 1.1 * Fweld=t/cm2
0.72Fweld = 0.2 * Fu=
mm5.6tmin.=0.25K =0.6αN =0.6αQ =
t/bolt1.94RbN.=αN*Fu*d*tmin.=t/bolt1.94RbQ.=αQ*Fu*d*tmin.=t/bolt3.14Rsh=KxFubxAs=
ok0.75>1Long Joint F =t/bolt1.94Rleast =
Safet/bolt1.94<t/bolt1.71
t/cm2
0.96qr =0.4Fy=cm2
4.48Ash.net =
t/cm2
1.74Ftr = 0.725Fy =cm2
0.896At.net =
Safeton2.97>ton5.86Qall=qr* Ash+Ftr*At=
t/cm2
0.96qr =0.4Fy =cm2
0.896Ash.net =
t/cm2
1.74Ftr = 0.725Fy =cm2
4.48At.net =
Safeton4.2>ton8.66Qall=qr*Ash+Ftr*At=
ton5.86<ton5.14Req1 =CHECK-1
Safe1<0.49Req2 =CHECK-2
cm3
21cm2
Zsec. =8.4Asec.=
ton2.97cm.t Qsec. =10.4Msec.=ton4.2Nsec. =
Safet/cm2
0.84<t/cm2
0.35q =
Safet/cm2
1.4<t/cm2
1.00ft =
SafeSafet/cm2
1.54<t/cm2
1.02feq. =
cm4
319.42cm2
Iw =15.65Aw =cm15.65Lw =
Safet/cm2
0.72<t/cm2
0.52ft =N/A+M*Y /I =
Safet/cm2
0.72<t/cm2
0.19q = Q / A =
SafeSafet/cm2
0.792<t/cm2
0.62
0.49Rup.2 Safe Ratio=0.88Rup.1 Safe Ratio=0.89Bolt Safe Ratio=
0.89Conn. Safe Ratio=0.78Weld Safe Ratio=0.66Sec. Safe Ratio=
mm167X60X6PL.FINALLY USE :
HSBB.T.8.8GRADE16M3
mm25B =mm35A =@
mm25C2 =mm25C1 =
mm25E =mm50D =
mm5Sw =Weld Lines2Tmin.0.8Weld Size
Design of Shear Conn. Bearing Type According to ECP No.(205)
Design Calculation Sheet
asec
MISR BANI SUEF COMPANY
BOOSTER FAN PLATFORM & DUCT SUPPORTDepartment :
Project Title :
CHECK OF WELD :
CHECK OF BEAM SEC.:
BOLT DIMENSIONS:
STRAINING ACTIONS:
RUPTURE DUE TO TENSION :
RUPTURE DUE TO SHEAR :
EQUIVALENT RUPTURE :
CONNECTION PROPERTIES:
CHECK OF BOLTS:

 









 22
teq 3qff
    
22
sh nNnQR
104
Frame Station OutputCase CaseType StepType P V2 V3
Text m Text Text Text Tonf Tonf Tonf
2072SA 1.21 ENV. Combination Max 1.1188 3.9686 0.05
B‐007 2.24 ENV. Combination Min ‐0.5912 ‐0.8882 ‐1.4988
B‐007 2.24 ENV. Combination Max 2.2563 1.7524 0.7803
Extrem out put reactions for IPE240 shear connection:
105
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note
Booster fan cr1 fn02 platform & duct support calculation note

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Booster fan cr1 fn02 platform & duct support calculation note

  • 1. ASEC for Manufacturing and Industrial Projects - ARESCO Tebbin Plant 145-MISR BANI SUEF COMPANY BOOSTER FAN PLATFORM & DUCT SUPPORT CALCULATION SHEET Document no. : 145-MB-S-CA-9000 Prepared by : Eng. Ali Ahmed Elkashef Checked by : Eng. Ashraf maghraby Approved by : Eng. Mohamed Hikal Date : 09-06-2015 Rev. 0
  • 2. 1. INTRODUCTION 1 2. DESIGN DATA 2 2.1 Applicable codes and standards 2 2.2 Material Characteristics 2 2.3 Design Loads 3 2.4 Technical Specifications 4 3. ANALYSIS 15 3.1 Calculation Method 15 3.2 Main Assumptions 15 3.3 Model Configration 15 3.4 Load Combinations 56 4. DESIGN 60 4.1 Allowable Stresses 60 4.2 Design of Beam Columns 61 4.3 Design of Bracing members 62 4.4 Design of Base connections 85 4.5 Design of Beam connections 91 5 - CHECK OF DEFLECTION 120 APPENDIX (1) 121 INDEX
  • 3. 1. INTRODUCTION SAP 2000 V14.2.2 Reference Documents: (refer to Appendix (1) Mechanical GAs drawings ---------------------------# 1517-110-GA-634B Analysis has been carried out using the commercial software This note is concerned with Fan CR1-FN02 platform Of Misr Bani Suef Company Project. The aim of this document is to design the steel structure supporting the mechanical loads , and carry out all the necessary checks and verifications. #1517-110-GD-6222 #1517-110-GD-6224 1
  • 4. 2. DESIGN DATA 2.1 Applicable codes and standards - Structural steel design is in accordance with the Egyptian Code of Practice for Steel Constructions and Bridges (ASD) Code No. (205). Ministerial Decree No 279 - 2001 - Egyptian Code for Loads on Structural Elements and Buildings Code No. (201). 2.2 Material Characteristics - Structural Steel : Mass Density (  ) = 7.85 t/cm3 Modulus of Elasticity (E) = 2100 t/cm2 Coefficient of thermal Expansion () = 1.2x10-5 / o C Structural Steel used is of Grade --- ST - 37 Nominal ultimate strength ( Fu ) = 3.60 t/cm2 (Thickness < 40 mm) = 3.40 t/cm2 (40 mm < Thickness < 100 mm) Nominal yield strength ( Fy ) = 2.40 t/cm2 (Thickness < 40 mm) = 2.15 t/cm2 (40 mm < Thickness < 100 mm) - Bolts used are (HSB) High Strength bolts of the following grades: Grade (8.8) Nominal ultimate strength ( Fub) = 8.00 t/cm2 Nominal yield strength ( Fyb) = 6.40 t/cm2 The bolt follows DIN 931 The nut follows DIN 555 The washer follows DIN 126 - Anchor bolts : It is of steel grade ST - 37 Nominal ultimate strength ( Fu) = 3.60 t/cm2 (Diameters < 40 mm) Nominal yield strength ( Fy) = 2.40 t/cm2 (Diameters < 40 mm) - Welds : The grade of weld material shall not be less than grade of base metal. 2
  • 5. 2.3 Design Loads (DL) Dead load The dead loads include the self-weight of steel structure, and covering material. The unit weight of steel = 7.85 t/m3 Grating plate (30x30x3) = 40 Kg/m2 (LL) Live load This load applied in the areas with covering material and / or surrounding the machines. - Live load on platf.(LL) = 250 Kg/m2 - Dust load on platf. = 50 Kg/m2 Mechanical loads Refer to mechanical loads presented in 1517-110-GD-6224 (appendix (1)) (MD) Mechanical dead loads (permanent loads) - MD ---- cosidered as Load case (A) (ML) Mechanical live loads - ML ---- cosidered as Load case (D) - Load case (A) except for support (207SG) The basic design loads given here below include the most permanent or variable loads that should be considered in load combinations. will be Load case (B) - Load case (A) 3
  • 6. (W) Wind loads The design wind load (P) = Ce .k .q Where k is combined height, exposure factor. Ce is pressure coefficient for the structure or portion of structure. qs is wind pressure. qs = 0.078 T/m2 (Temp) Temperature load (EQ) Seismic load 2.4 Technical Specifications Deformations Slenderness value for members - Allowable slenderness ratio (  = K L / i ) should not increase than the following values: For Tension Members:  max < 300 For Compression Members: For Beam Columns :  max < 180 For Bracing Members :  max < 200 Ce=1.3 for columns / 1.1 for beams - The allowable vertical deflection due to live load for beams is limited to Span / 200 and for cantilevers is limited to Span/ 180 - The allowable lateral drift at top of columns due to combined lateral and gravity loads is limited to Height / 150 . This load is taken in the longitudinal and transversal directions of structure in accordance with Egyptian Code (201). The temperature effect will be considered by applying the change (increase or decrease) in temperature = +30/-20 o C For this type of light weight structures we can neglect its effect as it doesn't govern the design if compared with wind load. 4
  • 7. SAP2000 SAP2000 v14.2.2 - File:BFP - Frame Span Loads (DL) (As Defined) - Tonf, m, C Units 6/7/15 16:04:42 5
  • 8. SAP2000 SAP2000 v14.2.2 - File:BFP - Frame Span Loads (LL) (As Defined) - Tonf, m, C Units 6/7/15 16:05:29 6
  • 9. SAP2000 SAP2000 v14.2.2 - File:BFP - Frame Span Loads (MD) (As Defined) - Tonf, m, C Units 6/7/15 16:11:13 7
  • 10. SAP2000 SAP2000 v14.2.2 - File:BFP - Frame Span Loads (ML) (As Defined) - Tonf, m, C Units 6/7/15 16:08:00 8
  • 11. SAP2000 SAP2000 v14.2.2 - File:BFP - Frame Span Loads (Wx) (As Defined) - Tonf, m, C Units 6/7/15 16:07:00 9
  • 12. SAP2000 SAP2000 v14.2.2 - File:BFP - Frame Span Loads (Wy) (As Defined) - Tonf, m, C Units 6/7/15 16:07:24 10
  • 13. SAP2000 SAP2000 v14.2.2 - File:BFP - Frame Span Loads (C1) (As Defined) - Tonf, m, C Units 6/7/15 16:11:41 11
  • 14. SAP2000 SAP2000 v14.2.2 - File:BFP - Frame Span Loads (C2) (As Defined) - Tonf, m, C Units 6/7/15 16:12:11 12
  • 15. SAP2000 SAP2000 v14.2.2 - File:BFP - Frame Span Loads (C3) (As Defined) - Tonf, m, C Units 6/7/15 16:12:52 13
  • 16. SAP2000 SAP2000 v14.2.2 - File:BFP - Frame Span Loads (C4) (As Defined) - Tonf, m, C Units 6/7/15 16:13:18 14
  • 17. 3. ANALYSIS 3.1 Calculation Method - The calculation will be done considering working stress design method. - For evaluating the maximum stress in elements, the straining actions will be calculated for two cases: Case  : Primary stresses due to ……...dead loads + live loads In design the stresses in members due to case  should not exceed the allowable stresses. Case  : Primary and additional stresses due to ………Case  loads + Secondary Loads - Design of connection will be based on bearing type bolts. 3.2 Main Assumptions 3.3 Model Configuration - Here below we will present the frame elements labels and profiles In design the stresses in members due to case  should not exceed the allowable stresses by more than 20%. - For any moving loads where the impact effect is not considered in the given mechanical loads then load factors have to be added to consider the impact effect by increasing LL by 25%. 15
  • 18. SAP2000 SAP2000 v14.2.2 - File:BFP - Frame Releases - Tonf, m, C Units 6/7/15 15:30:17 16
  • 19. SAP2000 SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=15.025 - Tonf, m, C Units 6/7/15 15:32:19 17
  • 20. SAP2000 SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=20.525 - Tonf, m, C Units 6/7/15 16:00:01 18
  • 21. SAP2000 SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=28.671 - Tonf, m, C Units 6/7/15 16:00:38 19
  • 22. SAP2000 SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=39.871 - Tonf, m, C Units 6/7/15 16:01:10 20
  • 23. SAP2000 SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=5.125 - Tonf, m, C Units 6/7/15 15:31:02 21
  • 24. SAP2000 SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=9.665 - Tonf, m, C Units 6/7/15 15:31:44 22
  • 25. SAP2000 SAP2000 v14.2.2 - File:BFP - Frame Releases - Tonf, m, C Units 6/7/15 15:29:53 23
  • 26. SAP2000 SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=5.125 - Tonf, m, C Units 6/7/15 15:01:53 24
  • 27. SAP2000 SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=9.665 - Tonf, m, C Units 6/7/15 15:02:48 25
  • 28. SAP2000 SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=15.025 - Tonf, m, C Units 6/7/15 15:03:44 26
  • 29. SAP2000 SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=20.525 - Tonf, m, C Units 6/7/15 15:04:20 27
  • 30. SAP2000 SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=28.671 - Tonf, m, C Units 6/7/15 15:05:05 28
  • 31. SAP2000 SAP2000 v14.2.2 - File:BFP - Y-Z Plane @ X=39.871 - Tonf, m, C Units 6/7/15 15:05:40 29
  • 32. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Z Plane @ Y=0 - Tonf, m, C Units 6/7/15 16:01:47 30
  • 33. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Z Plane @ Y=0.71 - Tonf, m, C Units 6/7/15 16:02:11 31
  • 34. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Z Plane @ Y=2.24 - Tonf, m, C Units 6/7/15 16:02:37 32
  • 35. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Z Plane @ Y=3.785 - Tonf, m, C Units 6/7/15 16:03:06 33
  • 36. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Z Plane @ Y=5.63 - Tonf, m, C Units 6/7/15 16:03:33 34
  • 37. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Z Plane @ Y=0 - Tonf, m, C Units 6/7/15 15:06:36 35
  • 38. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Z Plane @ Y=0.71 - Tonf, m, C Units 6/7/15 15:16:49 36
  • 39. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Z Plane @ Y=2.24 - Tonf, m, C Units 6/7/15 15:17:29 37
  • 40. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Z Plane @ Y=3.785 - Tonf, m, C Units 6/7/15 15:18:05 38
  • 41. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Z Plane @ Y=5.63 - Tonf, m, C Units 6/7/15 15:18:37 39
  • 42. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=1.97 - Tonf, m, C Units 6/7/15 15:21:03 40
  • 43. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=10.33 - Tonf, m, C Units 6/7/15 15:25:55 41
  • 44. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=10.33 - Tonf, m, C Units 6/7/15 15:26:46 42
  • 45. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=4.06 - Tonf, m, C Units 6/7/15 15:21:43 43
  • 46. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=4.28 - Tonf, m, C Units 6/7/15 15:22:41 44
  • 47. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=6.15 - Tonf, m, C Units 6/7/15 15:23:15 45
  • 48. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=8.3 - Tonf, m, C Units 6/7/15 15:24:05 46
  • 49. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=8.56 - Tonf, m, C Units 6/7/15 15:25:11 47
  • 50. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=1.97 - Tonf, m, C Units 6/7/15 14:50:12 48
  • 51. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=4.06 - Tonf, m, C Units 6/7/15 14:51:14 49
  • 52. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=4.28 - Tonf, m, C Units 6/7/15 14:52:13 50
  • 53. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=6.15 - Tonf, m, C Units 6/7/15 14:52:54 51
  • 54. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=8.3 - Tonf, m, C Units 6/7/15 14:54:31 52
  • 55. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=8.56 - Tonf, m, C Units 6/7/15 14:55:11 53
  • 56. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=10.33 - Tonf, m, C Units 6/7/15 14:56:55 54
  • 57. SAP2000 SAP2000 v14.2.2 - File:BFP - X-Y Plane @ Z=10.33 - Tonf, m, C Units 6/7/15 14:59:37 55
  • 58. Self weight Dead Load Live Load Mech. Dead Load Mech. Live Load + wind in X - wind in X + wind in Y - wind in Y + EQ in X - EQ in X + EQ in Y - EQ in Y SW DL LL MD ML C1 C2 C3 C4 WX+ WX- WY+ WY- EQX+ EQX- EQY+ EQY- Temp Temp (+...) (-...) COMB 1000 1.00 1.00 1.00 1.0 1.0 COMB 1001 0.83 0.83 0.83 0.83 1.0 1.2 COMB 1002 0.83 0.83 0.83 0.83 1.0 1.2 COMB 1100 0.83 0.83 0.83 0.83 1.0 1.2 COMB 1101 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 1102 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 1300 0.83 0.83 0.83 -0.83 1.0 1.2 COMB 1301 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB 1302 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB 1500 0.83 0.83 0.83 0.83 1.0 1.2 COMB 1501 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 1502 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 1700 0.83 0.83 0.83 -0.83 1.0 1.2 COMB 1701 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB 1702 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB 2000 1.00 1.00 1.00 1.00 1.0 1.0 COMB 2001 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 2002 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 2100 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 2101 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 2102 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 2110 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 2111 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 2112 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 2300 0.83 0.83 0.83 0.83 -0.83 1.0 1.2 COMB 2301 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB 2302 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB 2310 0.83 0.83 0.83 0.83 -0.83 1.0 1.2 COMB 2311 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB 2312 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB 2500 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 2501 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 2502 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 2510 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 2511 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 2512 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 2700 0.83 0.83 0.83 0.83 -0.83 1.0 1.2 COMB 2701 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB 2702 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB 2710 0.83 0.83 0.83 0.83 -0.83 1.0 1.2 COMB 2711 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB 2712 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB 3000 1.00 1.00 1.00 1.00 1.00 1.0 1.0 COMB 3001 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 3002 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 CRANE LOAD Env. For Brac. Des Temperature Envelope 3.4 Loads Combinations :- 56
  • 59. Self weight Dead Load Live Load Mech. Dead Load Mech. Live Load + wind in X - wind in X + wind in Y - wind in Y + EQ in X - EQ in X + EQ in Y - EQ in Y SW DL LL MD ML C1 C2 C3 C4 WX+ WX- WY+ WY- EQX+ EQX- EQY+ EQY- Temp Temp (+...) (-...) CRANE LOAD Env. For Brac. Des Temperature Envelope COMB 3100 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 3101 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 3102 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 3110 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 3111 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 3112 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 3300 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2 COMB 3301 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB 3302 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB 3310 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2 COMB 3311 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB 3312 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB 3500 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 3501 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 3502 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 3510 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 3511 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 3512 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB 3700 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2 COMB 3701 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB 3702 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB 3710 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2 COMB 3711 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB 3712 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C1/3000 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.0 COMB C1/3001 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/3002 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/3100 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/3101 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/3102 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/3110 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/3111 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/3112 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/3300 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2 COMB C1/3301 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C1/3302 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C1/3310 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/3311 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/3312 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/3500 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/3501 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/3502 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/3510 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/3511 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/3512 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/3700 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2 COMB C1/3701 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C1/3702 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C1/3710 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2 57
  • 60. Self weight Dead Load Live Load Mech. Dead Load Mech. Live Load + wind in X - wind in X + wind in Y - wind in Y + EQ in X - EQ in X + EQ in Y - EQ in Y SW DL LL MD ML C1 C2 C3 C4 WX+ WX- WY+ WY- EQX+ EQX- EQY+ EQY- Temp Temp (+...) (-...) CRANE LOAD Env. For Brac. Des Temperature Envelope COMB C1/3711 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C1/3712 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C2/3000 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.0 COMB C2/3001 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C2/3002 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C2/3100 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C2/3101 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C2/3102 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C2/3110 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C2/3111 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C2/3112 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C2/3300 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2 COMB C2/3301 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C2/3302 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C2/3310 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C2/3311 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C2/3312 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C2/3500 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C2/3501 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C2/3502 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C2/3510 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C2/3511 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C2/3512 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C2/3700 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2 COMB C2/3701 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C2/3702 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C2/3710 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2 COMB C2/3711 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C2/3712 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C3/3000 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.0 COMB C3/3001 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C3/3002 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C3/3100 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C3/3101 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C3/3102 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C3/3110 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C3/3111 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C3/3112 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C3/3300 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2 COMB C3/3301 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C3/3302 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C3/3310 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C3/3311 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C3/3312 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C3/3500 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C3/3501 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C3/3502 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C3/3510 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C3/3511 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 58
  • 61. Self weight Dead Load Live Load Mech. Dead Load Mech. Live Load + wind in X - wind in X + wind in Y - wind in Y + EQ in X - EQ in X + EQ in Y - EQ in Y SW DL LL MD ML C1 C2 C3 C4 WX+ WX- WY+ WY- EQX+ EQX- EQY+ EQY- Temp Temp (+...) (-...) CRANE LOAD Env. For Brac. Des Temperature Envelope COMB C3/3512 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C3/3700 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2 COMB C3/3701 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C3/3702 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C3/3710 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2 COMB C3/3711 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C3/3712 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C4/3000 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.0 COMB C4/3001 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C4/3002 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C4/3100 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C4/3101 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C4/3102 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C4/3110 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C4/3111 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C4/3112 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C4/3300 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2 COMB C4/3301 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C4/3302 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C4/3310 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C4/3311 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C4/3312 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C4/3500 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C4/3501 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C4/3502 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C4/3510 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C4/3511 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C4/3512 0.83 0.83 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C4/3700 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2 COMB C4/3701 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C4/3702 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C4/3710 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 1.0 1.2 COMB C4/3711 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C4/3712 0.83 0.83 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C1/1000 1.00 1.00 1.00 1.00 1.0 1.0 COMB C1/1001 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/1002 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/1100 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/1101 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/1102 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/1300 0.83 0.83 0.83 0.83 -0.83 1.0 1.2 COMB C1/1301 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C1/1302 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C1/1500 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/1501 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/1502 0.83 0.83 0.83 0.83 0.83 0.83 1.0 1.2 COMB C1/1700 0.83 0.83 0.83 0.83 -0.83 1.0 1.2 COMB C1/1701 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 COMB C1/1702 0.83 0.83 0.83 0.83 -0.83 0.83 1.0 1.2 59
  • 62. 4. DESIGN 4.1 Allowable Stresses -Tension Stresses: Allowable stress ( Fat) = 0.58 Fy -Compression Stresses: Allowable stress (Fac ) = 0.58 Fy - [ (0.58Fy - 0.75 ) (KL/i)2 / 104 ] for (KL/i) < 100 7500/ (KL/i)2 for (KL/i) >100 -Compression Stresses due to Bending: Allowable stress (Fb ) 0.64 Fy ……………for compact section 0.58 Fy ……………for non-compact section = FLTB in case where L unsuported of compression flange is > the allowable. -Shear Stresses: Allowable stress (qall ) = 0.35 Fy Working Stress Method is used for the design, in accordance to the Egyptian Code of Practice for Steel Constructions and Bridges Code No. (205). in case where L unsuported of compression flange is < the allowable. = 60
  • 63. STEEL GRADE: 37 Fy (Thickness ≤ 40) = 2.40 t/cm2 Fy (40>Thickness≤100) = 2.15 t/cm2 Fu (Thickness ≤ 40) = 3.60 t/cm2 Fu (40>Thickness≤100) = 3.40 t/cm2 B C D E F G H I J K L M N O P Q R S T U V W X Y Z AA AB AC AD AE AF AG AH AI AJ AK AL AM AN AO AP AQ AR AS AT AU AV AW AX AY AZ BA BB BC BD BE BF BG BH BI BJ BK BL BM N Mx My Qy Qx Load Lbx Lby Lu Zx req Section H B Tw Tf A act. Ix act. Zx act. ix act. Iy act. Zy act. iy act. x y fca fbcx fbcy Fc Fcb Fex Fey Max comp. Flange tip Lucom Class Normal Check Of % Safety SBS-weld ton m.ton m.ton ton ton case m m m Diam-mm Grade Con.Type cm3 type Name Size mm mm mm mm cm2 cm4 cm3 cm cm4 cm3 cm Act. Act. t/cm2 t/cm2 t/cm2 t/cm2 t/cm2 t/cm2 t/cm2 web flange web flange in flange stress m of section S.R. t/cm2 S.R. t/cm2 S.R. Section Margin N D-mm Grade S-mm L-mm mm B-011 0.0 0.0 0.1 0.1 0.2 1 0.97 0.97 0.97 20 10.9 Friction 36 RS UPN 120 120 55 7 9 17.00 364 61 4.62 43 11 1.59 21 61 0.00 0.03 0.63 1.39 1.39 17.19 2.03 1.00 1.00 1.00 1.00 1.00 0.86 0.04 Outside In comp. 0.71 Compact 1.00 1.00 0.47 0.01 0.01 0.03 0.03 Safe 53 2 20 10.9 5 10 N/R B-021 -0.7 0.3 0.4 0.2 0.5 1 2.46 1.04 3.66 20 10.9 Friction 228 RS HEA 160 152 160 6 9 38.80 1670 220 6.57 616 77 3.98 37 26 0.02 0.14 0.54 1.30 1.39 5.35 10.93 0.85 0.85 1.00 0.59 1.00 -0.70 0.22 Outside In comp. 2.07 Compact 1.00 1.00 0.50 0.02 0.03 0.03 0.03 Safe 50 2 20 10.9 5 11 N/R G-03 -0.2 1.0 0.0 1.0 0.0 1 9.90 1.93 1.93 20 10.9 Friction 81 RS IPE 200 200 100 5.6 8.5 28.50 1940 194 8.26 142 29 2.24 120 86 0.01 0.51 0.07 0.52 1.39 0.52 1.02 0.85 0.85 1.00 0.51 1.00 -0.97 0.88 Outside In comp. 1.29 Compact 1.00 1.00 0.43 0.11 0.13 0.00 0.00 Safe 57 2 20 10.9 5 14 N/R G-01 0.6 2.4 0.0 0.0 0.0 1 9.90 1.17 3.66 20 10.9 Friction 171 RS IPE 240 240 120 6.2 9.8 39.10 3890 324 9.97 284 47 2.69 99 43 0.01 0.73 0.01 1.39 1.39 0.76 4.00 1.00 1.00 1.00 0.49 1.00 -1.05 0.99 Outside In comp. 1.55 Compact 1.00 1.00 0.54 0.00 0.00 0.00 0.00 Safe 46 2 20 10.9 5 18 N/R B-026 -0.1 3.6 0.2 1.7 0.3 1 2.56 1.05 1.05 20 10.9 Friction 357 RS IPE 270 270 135 6.6 10.2 45.90 5790 429 11.20 420 62 3.02 23 35 0.00 0.84 0.32 1.31 1.54 14.36 6.20 0.85 0.85 1.00 0.50 1.00 -1.00 0.73 Outside In comp. 1.74 Compact 1.00 1.00 0.78 0.11 0.14 0.01 0.02 Safe 22 2 20 10.9 5 21 N/R G-04 -0.1 4.2 0.0 0.2 0.0 1 9.90 3.76 3.76 20 10.9 Friction 301 RS IPE 270 270 135 6.6 10.2 45.90 5790 429 11.20 420 62 3.02 88 125 0.00 0.98 0.00 0.48 1.39 0.96 0.48 1.00 0.85 1.00 0.50 1.00 -0.99 1.00 Outside In comp. 1.74 Compact 1.00 1.00 0.71 0.01 0.02 0.00 0.00 Safe 29 2 20 10.9 5 21 N/R B-076 -3.6 0.0 0.0 0.0 0.0 1 1.37 0.69 1.37 20 10.9 Friction 2 RS UPN 120 120 55 7 9 17.00 364 61 4.62 43 11 1.59 30 43 0.21 0.04 0.00 1.27 1.39 8.53 4.04 1.00 0.85 1.00 1.00 1.00 0.77 1.00 Outside In comp. 0.71 Compact 1.03 1.00 0.20 0.00 N/C 0.00 N/C Safe 80 2 20 10.9 5 10 N/R B-075 0.0 1.0 0.0 1.7 0.0 1 1.11 1.11 1.11 20 10.9 Friction 73 RS IPE 160 160 82 5 7.4 20.10 869 109 6.58 68 17 1.84 17 60 0.00 0.87 0.06 1.39 1.39 26.59 2.08 1.00 1.00 1.00 0.50 1.00 -1.01 0.94 Outside In comp. 1.06 Compact 1.00 1.00 0.67 0.25 0.30 0.00 0.00 Safe 33 2 20 10.9 5 10 N/R B-069 2.0 1.4 0.1 1.3 0.1 1 5.13 3.76 0.80 20 10.9 Friction 128 RS HEA 160 152 160 6 9 38.80 1670 220 6.57 616 77 3.98 78 95 0.05 0.65 0.07 1.39 1.54 1.23 0.84 1.00 1.00 1.00 0.45 1.00 -1.23 0.89 Outside In comp. 2.07 Compact 1.00 1.00 0.55 0.16 0.19 0.01 0.01 Safe 45 2 20 10.9 5 11 N/R B-077 4.3 1.5 0.0 0.9 0.0 1 2.46 1.85 1.85 20 10.9 Friction 116 RS IPE 200 200 100 5.6 8.5 28.50 1940 194 8.26 142 29 2.24 30 82 0.15 0.77 0.06 1.39 1.39 8.46 1.11 1.00 1.00 1.00 0.38 1.00 -1.62 0.91 Outside In comp. 1.29 Compact 1.00 1.00 0.71 0.09 0.11 0.00 0.00 Safe 29 2 20 10.9 5 14 N/R B-071 0.0 3.2 0.0 1.6 0.0 1 3.78 1.76 1.76 20 10.9 Friction 236 RS IPE 240 240 120 6.2 9.8 39.10 3890 324 9.97 284 47 2.69 38 65 0.00 1.00 0.02 1.12 1.39 5.22 1.75 1.00 0.85 1.00 0.50 1.00 -1.00 0.98 Outside In comp. 1.55 Compact 1.00 1.00 0.73 0.12 0.15 0.00 0.00 Safe 27 2 20 10.9 5 18 N/R B-109 2.0 0.1 0.0 0.1 0.1 1 1.21 0.61 0.61 20 10.9 Friction 22 RS UPN 120 120 55 7 9 17.00 364 61 4.62 43 11 1.59 26 38 0.11 0.16 0.27 1.39 1.54 10.93 5.18 1.00 1.00 1.00 0.51 1.00 -1.05 0.16 Outside In comp. 0.71 Compact 1.00 1.00 0.39 0.01 0.02 0.01 0.01 Safe 61 2 20 10.9 5 10 N/R B-100 0.6 0.6 0.0 0.0 0.0 1 5.50 1.00 5.50 20 10.9 Friction 44 RS IPE 160 160 82 5 7.4 20.10 869 109 6.58 68 17 1.84 84 54 0.03 0.55 0.02 1.39 0.58 1.07 2.54 1.00 1.00 1.00 0.46 1.00 -1.15 0.97 Outside In comp. 1.06 Compact 1.00 1.00 0.96 0.01 0.01 0.00 0.00 Safe 4 2 20 10.9 5 10 N/R 2071SA -1.2 1.8 0.0 3.0 0.1 1 1.21 1.21 1.21 20 10.9 Friction 144 RS IPE 200 200 100 5.6 8.5 28.50 1940 194 8.26 142 29 2.24 15 54 0.04 0.93 0.11 1.20 1.54 34.95 2.57 1.00 1.00 1.00 0.53 1.00 -0.90 0.90 Outside In comp. 1.29 Compact 1.00 1.02 0.72 0.31 0.37 0.00 0.01 Safe 28 2 20 10.9 5 14 N/R B-112 1.8 1.6 0.2 0.3 0.1 1 5.50 2.90 2.90 20 10.9 Friction 205 RS IPE 240 240 120 6.2 9.8 39.10 3890 324 9.97 284 47 2.69 55 108 0.05 0.49 0.38 1.39 1.39 2.46 0.64 1.00 1.00 1.00 0.44 1.00 -1.25 0.54 Outside In comp. 1.55 Compact 1.00 1.00 0.66 0.03 0.03 0.01 0.01 Safe 34 2 20 10.9 5 18 N/R B-107 5.4 2.8 0.4 0.1 0.6 1 2.76 1.21 1.21 20 10.9 Friction 377 RS IPE 270 270 135 6.6 10.2 45.90 5790 429 11.20 420 62 3.02 25 40 0.12 0.66 0.57 1.39 1.54 12.31 4.67 1.00 1.00 1.00 0.39 1.00 -1.54 0.49 Outside In comp. 1.74 Compact 1.00 1.00 0.96 0.01 0.01 0.03 0.04 Safe 4 2 20 10.9 5 21 N/R G-12 -12.9 0.6 0.5 0.2 0.7 1 1.78 3.50 3.50 20 10.9 Friction 271 RS IPE 300 300 150 7.1 10.7 53.80 8360 557 12.50 604 81 3.35 14 104 0.24 0.11 0.57 0.69 1.39 36.99 0.69 1.00 0.85 1.00 1.00 1.00 0.44 0.38 Outside In comp. 1.94 Compact 1.01 1.31 0.96 0.01 0.01 0.03 0.04 Safe 4 2 20 10.9 5 25 N/R B-103 -2.0 1.2 0.3 0.3 0.4 1 5.50 1.00 5.00 20 10.9 Friction 229 RS HEA 160 152 160 6 9 38.80 1670 220 6.57 616 77 3.98 84 25 0.05 0.56 0.36 0.94 1.39 1.07 11.88 1.00 0.85 1.05 0.56 1.00 -0.79 0.63 Outside In comp. 2.07 Compact 1.05 1.00 0.74 0.03 0.04 0.02 0.02 Safe 26 2 20 10.9 5 11 N/R G-09 0.5 11.2 0.2 6.8 0.5 1 4.92 1.22 1.22 20 10.9 Friction 900 RS HEA 300 290 300 8.5 14 113.00 18260 1260 12.70 6310 421 7.49 39 16 0.00 0.89 0.05 1.39 1.54 5.00 28.27 1.00 1.00 1.11 0.50 1.00 -1.01 0.95 Outside In comp. 3.87 Compact 1.00 1.00 0.68 0.33 0.39 0.01 0.01 Safe 32 3 20 10.9 5 29 N/R B-004 2.7 1.5 0.0 0.1 0.0 1 3.46 0.33 3.46 20 10.9 Friction 109 RS UPN 200 200 75 8.5 11.5 32.20 1910 191 7.70 148 27 2.14 45 15 0.08 0.80 0.00 1.39 1.39 3.71 31.54 1.00 1.00 1.45 0.57 1.00 -1.31 0.99 Outside In comp. 0.97 Compact 1.00 1.00 0.63 0.01 0.01 0.00 0.00 Safe 37 2 20 10.9 5 20 N/R B-054 0.9 0.1 0.2 0.2 0.2 1 1.25 0.88 0.88 20 10.9 Friction 95 RS IPE 200 200 100 5.6 8.5 28.50 1940 194 8.26 142 29 2.24 15 39 0.03 0.07 0.60 1.39 1.54 32.75 4.92 1.00 1.00 1.00 0.22 1.00 -3.63 0.06 Outside In comp. 1.29 Compact 1.00 1.00 0.50 0.02 0.03 0.01 0.02 Safe 50 2 20 10.9 5 14 N/R B-047 -0.6 0.2 0.4 0.2 0.2 1 1.25 0.88 0.88 20 10.9 Friction 217 RS IPE 240 240 120 6.2 9.8 39.10 3890 324 9.97 284 47 2.69 13 33 0.01 0.05 0.87 1.32 1.54 47.71 7.09 0.85 0.85 1.00 0.69 1.00 -0.45 0.07 Outside In comp. 1.55 Compact 1.00 1.00 0.67 0.01 0.01 0.01 0.01 Safe 33 2 20 10.9 5 18 N/R B-084 -0.3 0.1 0.4 0.2 1.0 1 1.25 0.88 0.88 20 10.9 Friction 230 RS IPE 270 270 135 6.6 10.2 45.90 5790 429 11.20 420 62 3.02 11 29 0.01 0.03 0.71 1.34 1.54 60.21 8.93 1.00 1.00 1.00 0.63 1.00 -0.58 0.05 Outside In comp. 1.74 Compact 1.00 1.00 0.54 0.02 0.02 0.06 0.07 Safe 46 2 20 10.9 5 21 N/R P-03 -8.2 0.0 0.0 0.0 0.0 1 1.94 1.94 1.94 20 10.9 Friction 6 RS IPE 160 160 82 5 7.4 20.10 869 109 6.58 68 17 1.84 29 105 0.41 0.00 0.07 0.67 1.39 8.63 0.67 0.85 0.85 1.75 1.00 1.00 0.99 0.85 Outside In comp. 1.06 Compact 1.00 2.14 0.71 0.00 0.00 0.00 N/C Safe 29 2 20 10.9 5 10 N/R 2030SG -7.1 0.5 0.2 0.3 0.7 1 1.40 1.40 1.40 20 10.9 Friction 129 RS HEA 160 152 160 6 9 38.80 1670 220 6.57 616 77 3.98 21 35 0.18 0.23 0.24 1.31 1.54 16.52 6.06 1.00 1.00 1.00 1.00 1.00 0.03 0.63 Outside In comp. 2.07 Compact 1.01 1.03 0.47 0.03 0.04 0.04 0.04 Safe 53 2 20 10.9 5 11 N/R P-02 -4.7 0.0 0.0 0.0 0.0 1 1.97 1.97 1.97 20 10.9 Friction 0 RS IPE 200 200 100 5.6 8.5 28.50 1940 194 8.26 142 29 2.24 24 88 0.17 0.00 0.00 0.90 1.39 13.19 0.97 1.00 0.85 1.00 1.00 1.00 1.00 1.00 Outside In comp. 1.29 Compact 1.01 1.03 0.19 0.00 N/C 0.00 N/C Safe 81 2 20 10.9 5 14 N/R C-05 -17.6 1.0 0.0 0.5 0.0 1 4.28 2.56 4.28 20 10.9 Friction 83 RS IPE 270 270 135 6.6 10.2 45.90 5790 429 11.20 420 62 3.02 38 85 0.38 0.23 0.04 0.93 1.39 5.14 1.04 0.85 0.85 1.28 1.00 1.00 0.32 0.94 Outside In comp. 1.74 Compact 1.00 1.34 0.62 0.03 0.04 0.00 0.00 Safe 38 2 20 10.9 5 21 N/R C-09 -9.9 0.0 0.0 0.0 0.0 1 10.42 2.09 10.42 20 10.9 Friction 10 RS IPE 200 200 100 5.6 8.5 28.50 1940 194 8.26 142 29 2.24 126 93 0.35 0.00 0.07 0.47 0.35 0.47 0.87 0.85 0.85 1.04 1.00 1.00 1.00 0.83 Outside In comp. 1.29 Compact 3.28 1.42 0.81 0.00 N/C 0.00 0.00 Safe 19 2 20 10.9 5 14 N/R G-07 3.9 5.5 0.0 1.7 0.0 1 11.20 2.80 4.23 20 10.9 Friction 410 RS IPE 300 300 150 7.1 10.7 53.80 8360 557 12.50 604 81 3.35 90 84 0.07 0.99 0.04 1.39 1.39 0.93 1.07 1.00 1.00 1.53 0.46 1.00 -1.19 0.96 Outside In comp. 1.94 Compact 1.00 1.00 0.79 0.09 0.11 0.00 0.00 Safe 21 2 20 10.9 5 25 N/R B-066 -6.5 1.2 0.3 0.4 0.1 1 4.50 4.92 4.50 20 10.9 Friction 222 RS HEA 300 290 300 8.5 14 113.00 18260 1260 12.70 6310 421 7.49 35 66 0.06 0.10 0.06 1.11 1.39 5.97 1.74 0.85 0.85 1.00 0.87 1.00 -0.14 0.70 Outside In comp. 3.87 Compact 1.00 1.00 0.17 0.02 0.02 0.00 0.00 Safe 83 3 20 10.9 5 29 N/R CROSS SECTION Cmx  MISR BANI SUEF CAMPANY BOOSTER FAN PLATFORM & DUCT SUPPORT DESIGN OF SECTIONS Mem. No. BOLTS A2  Cmy Cb Check Of [qx] REMARKSA1 Check Of [qy] Bolted conn. Welded conn. 4.2. Design of beam columns 61
  • 64. m 70 mm 7 mm cm cm cm < < < Fc ton > ton 2 DateDate - AM Checked - Date - HK Approved - Design of Bolted Connection : Section Single angle 70x7 t/cm2 - 10 Stress Ratio = 0.62 Check Stress Ratio : 0.234 0.375Allowable Stress : Fc = Actual Stress : f ca = SAFE SAFE Actual Stress : Allowable Stress : 0.251 1.392 Check Stress Ratio : t/cm 2 Ft = f ta = 30 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 70x7 e = 1 - 67.1 0 q r = Iv = Rev. Descreption Design F tr = p (S.R = 0.65) tG.P α = 0.8 tmin = a = 1.50 Bolted iu = 2.67 Single angle Properties of Section : Section : Area = M12 300 Lby = 9.40 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 1.97 109.5 200 ARESCO TEBBIN cm4 17.6 Thickness of Gusset Plate = Iu = t = cm4 asec Project Tiltle : Compression = ST- 37Tension = Departement : 2.20 1.80 t/cm2 1.50 Sheet No. : 1.37iv = Case of Loading :ton Grade of Steel : I Member ID : HB-003 Lbx = 10 mm ton 1.50 1.0m Type of Connection : Length = Bolts : m 109.5 7.17 cm2 λv = Kg/mWeight = A red = Check as Tension Member : cm 2 1.0Ky = 7.38 SAFE < Ft 1.61 3.78 Stress Ratio = SAFE (S.R = 0.34) 0.18 0.4 Fy = 0.96 6.43 At = ton t/cm2 SAFE 2M12(8.8) e 25 Bolts Check of Shear Rapture : Shear Strength : No. of Bolts = 1.31 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = 2.42 1.68 cm2 cm2 2.2 tonqr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm7 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λv = e p p e x 4.3 Desgin of bracing members:- 62
  • 65. m 60 mm 6 mm cm cm cm < < < Fc ton > ton 2 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λv = qr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm6 2.07 1.68 cm2 cm2 0.1 tonShear Strength : No. of Bolts = 0.03 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = SAFE 2M12(8.8) e 25 Bolts Check of Shear Rapture : Stress Ratio = SAFE (S.R = 0) 0.00 0.4 Fy = 0.96 5.51 At = ton t/cm2 < Ft 1.38 3.24 SAFE A red = Check as Tension Member : cm 2 1.0Ky = 5.42 Type of Connection : Length = Bolts : m 120.5 5.12 cm2 λv = Kg/mWeight = Lbx = 10 mm ton 1.41 1.0m ton Grade of Steel : I Member ID : HB-039 t/cm 2 1.41 Sheet No. : 1.17iv = Case of Loading : asec Project Tiltle : Compression = ST- 37Tension = Departement : 0.06 0.03 120.5 200 ARESCO TEBBIN cm4 9.4 Thickness of Gusset Plate = Iu = t = cm4 300 Lby = 6.91 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 1.69a = 1.41 Bolted iu = 2.29 Single angle Properties of Section : Section : Area = M12 Rev. Descreption Design F tr = p (S.R = 0.01) tG.P α = 0.8 tmin = 1 - 36.1 0 q r = Iv = 30 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 60x6 e = SAFE Actual Stress : Allowable Stress : 0.005 1.392 Check Stress Ratio : t/cm 2 Ft = f ta = Stress Ratio = 0.03 Check Stress Ratio : 0.008 0.310Allowable Stress : Fc = Actual Stress : f ca = SAFE Approved - Design of Bolted Connection : Section Single angle 60x6 t/cm2 - 10 DateDate - AM Checked - Date - HK e p p e x 4.3 Desgin of bracing members:- 63
  • 66. m 60 mm 6 mm cm cm cm < < < Fc ton > ton 2 DateDate - AM Checked - Date - HK Approved - Design of Bolted Connection : Section Single angle 60x6 t/cm2 - 10 Stress Ratio = 0.36 Check Stress Ratio : 0.191 0.524Allowable Stress : Fc = Actual Stress : f ca = SAFE SAFE Actual Stress : Allowable Stress : 0.045 1.392 Check Stress Ratio : t/cm 2 Ft = f ta = 30 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 60x6 e = 1 - 36.1 0 q r = Iv = Rev. Descreption Design F tr = p (S.R = 0.39) tG.P α = 0.8 tmin = a = 1.05 Bolted iu = 2.29 Single angle Properties of Section : Section : Area = M12 300 Lby = 6.91 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 1.69 89.8 200 ARESCO TEBBIN cm4 9.4 Thickness of Gusset Plate = Iu = t = cm4 asec Project Tiltle : Compression = ST- 37Tension = Departement : 1.32 0.23 t/cm2 1.05 Sheet No. : 1.17iv = Case of Loading :ton Grade of Steel : I Member ID : HB-047 Lbx = 10 mm ton 1.05 1.0m Type of Connection : Length = Bolts : m 89.8 5.12 cm2 λv = Kg/mWeight = A red = Check as Tension Member : cm 2 1.0Ky = 5.42 SAFE < Ft 1.38 3.24 Stress Ratio = SAFE (S.R = 0.23) 0.03 0.4 Fy = 0.96 5.51 At = ton t/cm2 SAFE 2M12(8.8) e 25 Bolts Check of Shear Rapture : Shear Strength : No. of Bolts = 0.79 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = 2.07 1.68 cm2 cm2 1.3 tonqr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm6 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λv = e p p e x 4.3 Desgin of bracing members:- 64
  • 67. m 70 mm 7 mm cm cm cm < < < Fc ton > ton 2 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λv = qr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm7 2.42 1.68 cm2 cm2 1.8 tonShear Strength : No. of Bolts = 1.07 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = SAFE 2M12(8.8) e 25 Bolts Check of Shear Rapture : Stress Ratio = SAFE (S.R = 0.27) 0.02 0.4 Fy = 0.96 6.43 At = ton t/cm2 < Ft 1.61 3.78 SAFE A red = Check as Tension Member : cm 2 1.0Ky = 7.38 Type of Connection : Length = Bolts : m 116.4 7.17 cm2 λv = Kg/mWeight = Lbx = 10 mm ton 1.59 1.0m ton Grade of Steel : I Member ID : HB-058 t/cm 2 1.59 Sheet No. : 1.37iv = Case of Loading : asec Project Tiltle : Compression = ST- 37Tension = Departement : 1.80 0.23 116.4 200 ARESCO TEBBIN cm4 17.6 Thickness of Gusset Plate = Iu = t = cm4 300 Lby = 9.40 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 1.97a = 1.59 Bolted iu = 2.67 Single angle Properties of Section : Section : Area = M12 Rev. Descreption Design F tr = p (S.R = 0.53) tG.P α = 0.8 tmin = 1 - 67.1 0 q r = Iv = 30 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 70x7 e = SAFE Actual Stress : Allowable Stress : 0.032 1.392 Check Stress Ratio : t/cm 2 Ft = f ta = Stress Ratio = 0.58 Check Stress Ratio : 0.191 0.332Allowable Stress : Fc = Actual Stress : f ca = SAFE Approved - Design of Bolted Connection : Section Single angle 70x7 t/cm2 - 10 DateDate - AM Checked - Date - HK e p p e x 4.3 Desgin of bracing members:- 65
  • 68. m 80 mm 8 mm cm cm cm < < < Fc ton > ton 2 DateDate - AM Checked - Date - HK Approved - Design of Bolted Connection : Section Single angle 80x8 t/cm2 - 10 Stress Ratio = 0.61 Check Stress Ratio : 0.203 0.334Allowable Stress : Fc = Actual Stress : f ca = SAFE SAFE Actual Stress : Allowable Stress : 0.017 1.392 Check Stress Ratio : t/cm 2 Ft = f ta = 35 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 80x8 e = 1 - 115.0 0 q r = Iv = Rev. Descreption Design F tr = p (S.R = 0.74) tG.P α = 0.8 tmin = a = 1.80 Bolted iu = 3.06 Single angle Properties of Section : Section : Area = M12 300 Lby = 12.30 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 2.26 116.1 200 ARESCO TEBBIN cm4 29.6 Thickness of Gusset Plate = Iu = t = cm4 asec Project Tiltle : Compression = ST- 37Tension = Departement : 2.50 0.16 t/cm2 1.80 Sheet No. : 1.55iv = Case of Loading :ton Grade of Steel : I Member ID : HB-120 Lbx = 10 mm ton 1.80 1.0m Type of Connection : Length = Bolts : m 116.1 9.58 cm2 λv = Kg/mWeight = A red = Check as Tension Member : cm 2 1.0Ky = 9.66 SAFE < Ft 2.24 4.32 Stress Ratio = SAFE (S.R = 0.31) 0.01 0.4 Fy = 0.96 8.04 At = ton t/cm2 SAFE 2M12(8.8) e 25 Bolts Check of Shear Rapture : Shear Strength : No. of Bolts = 1.49 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = 2.76 1.68 cm2 cm2 2.5 tonqr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm8 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λv = e p p e x 4.3 Desgin of bracing members:- 66
  • 69. m 60 mm 6 mm cm cm cm < < < Fc ton > ton 2 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λv = qr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm6 2.07 1.68 cm2 cm2 2.6 tonShear Strength : No. of Bolts = 1.53 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = SAFE 2M12(8.8) e 25 Bolts Check of Shear Rapture : Stress Ratio = SAFE (S.R = 0.46) 0.07 0.4 Fy = 0.96 5.51 At = ton t/cm2 < Ft 1.38 3.24 SAFE A red = Check as Tension Member : cm 2 1.0Ky = 5.42 Type of Connection : Length = Bolts : m 105.1 5.12 cm2 λv = Kg/mWeight = Lbx = 10 mm ton 1.23 1.0m ton Grade of Steel : I Member ID : HB-147 t/cm 2 1.23 Sheet No. : 1.17iv = Case of Loading : asec Project Tiltle : Compression = ST- 37Tension = Departement : 2.57 0.47 105.1 200 ARESCO TEBBIN cm4 9.4 Thickness of Gusset Plate = Iu = t = cm4 300 Lby = 6.91 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 1.69a = 1.23 Bolted iu = 2.29 Single angle Properties of Section : Section : Area = M12 Rev. Descreption Design F tr = p (S.R = 0.76) tG.P α = 0.8 tmin = 1 - 36.1 0 q r = Iv = 30 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 60x6 e = SAFE Actual Stress : Allowable Stress : 0.092 1.392 Check Stress Ratio : t/cm 2 Ft = f ta = Stress Ratio = 0.91 Check Stress Ratio : 0.371 0.407Allowable Stress : Fc = Actual Stress : f ca = SAFE Approved - Design of Bolted Connection : Section Single angle 60x6 t/cm2 - 10 DateDate - AM Checked - Date - HK e p p e x 4.3 Desgin of bracing members:- 67
  • 70. m 100 mm 10 mm cm cm cm < < < Fc ton > ton 2 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λu = qr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm10 3.46 1.68 cm2 cm2 0.2 tonShear Strength : No. of Bolts = 0.09 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = SAFE 2M12(8.8) e 25 Bolts Check of Shear Rapture : Stress Ratio = SAFE (S.R = 0.01) 0.00 0.4 Fy = 0.96 11.80 At = ton t/cm2 < Ft 3.80 5.40 SAFE A net = Check as Tension Member : cm 2 1.0Ky = 30.2 Type of Connection : Length = Bolts : m 183.2 35.60 cm2 λu = Kg/mWeight = Lbx = 10 mm ton 7.00 1.0m ton Grade of Steel : I Member ID : MRHB t/cm 2 7.00 Sheet No. : 1.95iv = Case of Loading : asec Project Tiltle : Compression = ST- 37Tension = Departement : 0.12 0.16 183.2 200 ARESCO TEBBIN cm4 73.3 Thickness of Gusset Plate = Iu = t = cm4 300 Lby = 38.40 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 2.82a = 7.00 Bolted iu = 3.82 2Ls Star-Shaped Properties of Section : Section : Area = M12 Rev. Descreption Design F tr = p (S.R = 0.04) tG.P α = 0.8 tmin = 1 - 280.0 0 q r = Iv = 45 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 100x10 e = SAFE Actual Stress : Allowable Stress : 0.004 1.392 Check Stress Ratio : t/cm 2 Ft = f ta = Stress Ratio = 0.01 Check Stress Ratio : 0.003 0.223Allowable Stress : Fc = Actual Stress : f ca = SAFE Approved - Design of Bolted Connection : Section 2Ls Star-Shaped 100x10 t/cm2 - 10 DateDate - AM Checked - Date - HK e p p e x 4.3 Desgin of bracing members:- 68
  • 71. m 60 mm 6 mm cm cm cm < < < < < Fc ton > ton 2 DateDate - AM Checked - Date - HK Approved - Design of Bolted Connection : Section 2Ls Back to Back 60x6 t/cm2 - 8 Stress Ratio = 0.51 Check Stress Ratio : 0.178 0.351Allowable Stress : Fc = Actual Stress : f ca = SAFE SAFE Actual Stress : Allowable Stress : 0.000 1.392 Check Stress Ratio : t/cm 2 Ft = 96.1 f ta = 30 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 60x6 e = 1 - 22.8 96.1 0 λy = q r = Iy = λy = 200 Rev. Descreption Design F tr = p (S.R = 0.44) tG.P α = 0.8 tmin = a = 2.66 Bolted ix = 1.82 2Ls Back to Back Properties of Section : Section : Area = M12 300 300 Lby = 13.82 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 1.69 146.2 200 ARESCO TEBBIN cm4 106.0 Thickness of Gusset Plate = Ix = t = cm4 asec Project Tiltle : Compression = ST- 37Tension = Departement : 2.46 0.00 t/cm2 2.66 Sheet No. : 2.77 SAFE iy = Case of Loading :ton Grade of Steel : I Member ID : NB-03 Lbx = 8 mm ton 2.66 1.0m Type of Connection : Length = Bolts : m 146.2 12.14 cm2 λx = Kg/mWeight = A net = Check as Tension Member : cm 2 1.0Ky = 10.84 SAFE SAFE < Ft 1.84 4.32 Stress Ratio = SAFE (S.R = 0.33) 0.00 0.4 Fy = 0.96 7.35 At = ton t/cm2 SAFE 2M12(8.8) e 25 Bolts Check of Shear Rapture : Shear Strength : No. of Bolts = 0.89 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = 2.76 3.36 cm2 cm2 2.5 tonqr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm8 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λx = e p p e x 4.3 Desgin of bracing members:- 69
  • 72. m 70 mm 7 mm cm cm cm < < < < < Fc ton > ton 4 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λx = qr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm8 2.76 3.36 cm2 cm2 8.4 tonShear Strength : No. of Bolts = 3.04 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = SAFE 4M12(8.8) e 25 Bolts Check of Shear Rapture : Stress Ratio = SAFE (S.R = 0.65) 0.00 0.4 Fy = 0.96 12.88 At = ton t/cm2 < Ft 1.84 10.08 SAFE SAFE A net = Check as Tension Member : cm 2 1.0Ky = 14.76 Type of Connection : Length = Bolts : m 81.8 16.84 cm2 λx = Kg/mWeight = Lbx = 8 mm ton 3.47 0.5m ton Grade of Steel : I Member ID : NB-05 t/cm 2 3.47 Sheet No. : 3.18 SAFE iy = Case of Loading : asec Project Tiltle : Compression = ST- 37Tension = Departement : 8.40 0.00 81.8 200 ARESCO TEBBIN cm4 190.4 Thickness of Gusset Plate = Ix = t = cm4 300 300 Lby = 18.80 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 1.97a = 1.74 Bolted ix = 2.12 2Ls Back to Back Properties of Section : Section : Area = M12 Rev. Descreption Design F tr = p (S.R = 0.75) tG.P α = 0.8 tmin = 1 - 42.4 109.0 0 λy = q r = Iy = λy = 200 30 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 70x7 e = SAFE Actual Stress : Allowable Stress : 0.000 1.392 Check Stress Ratio : t/cm 2 Ft = 109.0 f ta = Stress Ratio = 0.71 Check Stress Ratio : 0.447 0.631Allowable Stress : Fc = Actual Stress : f ca = SAFE Approved - Design of Bolted Connection : Section 2Ls Back to Back 70x7 t/cm2 - 8 DateDate - AM Checked - Date - HK e p p e x 4.3 Desgin of bracing members:- 70
  • 73. m 60 mm 6 mm cm cm cm < < < < < Fc ton > ton 3 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λx = qr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm8 2.76 3.36 cm2 cm2 6.4 tonShear Strength : No. of Bolts = 2.31 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = SAFE 3M12(8.8) e 25 Bolts Check of Shear Rapture : Stress Ratio = SAFE (S.R = 0.63) 0.38 0.4 Fy = 0.96 10.11 At = ton t/cm2 < Ft 1.84 7.20 SAFE SAFE A net = Check as Tension Member : cm 2 1.0Ky = 10.84 Type of Connection : Length = Bolts : m 65.2 12.14 cm2 λx = Kg/mWeight = Lbx = 8 mm ton 2.37 0.5m ton Grade of Steel : I Member ID : SGBR-08 t/cm 2 2.37 Sheet No. : 2.77 SAFE iy = Case of Loading : asec Project Tiltle : Compression = ST- 37Tension = Departement : 5.60 6.40 65.2 200 ARESCO TEBBIN cm4 106.0 Thickness of Gusset Plate = Ix = t = cm4 300 300 Lby = 13.82 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 1.69a = 1.19 Bolted ix = 1.82 2Ls Back to Back Properties of Section : Section : Area = M12 Rev. Descreption Design F tr = p (S.R = 0.77) tG.P α = 0.8 tmin = 1 - 22.8 85.7 0 λy = q r = Iy = λy = 200 30 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 60x6 e = SAFE Actual Stress : Allowable Stress : 0.527 1.392 Check Stress Ratio : t/cm 2 Ft = 85.7 f ta = Stress Ratio = 0.44 Check Stress Ratio : 0.405 0.920Allowable Stress : Fc = Actual Stress : f ca = SAFE Approved - Design of Bolted Connection : Section 2Ls Back to Back 60x6 t/cm2 - 8 DateDate - AM Checked - Date - HK e p p e x 4.3 Desgin of bracing members:- 71
  • 74. m 60 mm 6 mm cm cm cm < < < < < Fc ton > ton 3 DateDate - AM Checked - Date - HK Approved - Design of Bolted Connection : Section 2Ls Back to Back 60x6 t/cm2 - 8 Stress Ratio = 0.50 Check Stress Ratio : 0.504 1.012Allowable Stress : Fc = Actual Stress : f ca = SAFE SAFE Actual Stress : Allowable Stress : 0.387 1.392 Check Stress Ratio : t/cm 2 Ft = 50.6 f ta = 30 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 60x6 e = 1 - 22.8 50.6 0 λy = q r = Iy = λy = 200 Rev. Descreption Design F tr = p (S.R = 0.84) tG.P α = 0.8 tmin = a = 1.40 Bolted ix = 1.82 2Ls Back to Back Properties of Section : Section : Area = M12 300 300 Lby = 13.82 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 1.69 76.9 200 ARESCO TEBBIN cm4 106.0 Thickness of Gusset Plate = Ix = t = cm4 asec Project Tiltle : Compression = ST- 37Tension = Departement : 6.97 4.70 t/cm2 1.40 Sheet No. : 2.77 SAFE iy = Case of Loading :ton Grade of Steel : I Member ID : SGBR-14 Lbx = 8 mm ton 1.40 1.0m Type of Connection : Length = Bolts : m 76.9 12.14 cm2 λx = Kg/mWeight = A net = Check as Tension Member : cm 2 1.0Ky = 10.84 SAFE SAFE < Ft 1.84 7.20 Stress Ratio = SAFE (S.R = 0.68) 0.28 0.4 Fy = 0.96 10.11 At = ton t/cm2 SAFE 3M12(8.8) e 25 Bolts Check of Shear Rapture : Shear Strength : No. of Bolts = 2.52 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = 2.76 3.36 cm2 cm2 7.0 tonqr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm8 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λx = e p p e x 4.3 Desgin of bracing members:- 72
  • 75. m 80 mm 8 mm cm cm cm < < < Fc ton > ton 2 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λu = qr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm8 2.76 1.68 cm2 cm2 0.8 tonShear Strength : No. of Bolts = 0.49 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = SAFE 2M12(8.8) e 25 Bolts Check of Shear Rapture : Stress Ratio = SAFE (S.R = 0.1) 0.02 0.4 Fy = 0.96 8.04 At = ton t/cm2 < Ft 2.24 4.32 SAFE A net = Check as Tension Member : cm 2 1.0Ky = 19.32 Type of Connection : Length = Bolts : m 179.7 22.36 cm2 λu = Kg/mWeight = Lbx = 10 mm ton 5.50 1.0m ton Grade of Steel : I Member ID : VB-031 t/cm 2 5.50 Sheet No. : 1.55iv = Case of Loading : asec Project Tiltle : Compression = ST- 37Tension = Departement : 0.83 0.53 179.7 200 ARESCO TEBBIN cm4 29.6 Thickness of Gusset Plate = Iu = t = cm4 300 Lby = 24.60 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 2.26a = 5.50 Bolted iu = 3.06 2Ls Star-Shaped Properties of Section : Section : Area = M12 Rev. Descreption Design F tr = p (S.R = 0.24) tG.P α = 0.8 tmin = 1 - 115.0 0 q r = Iv = 35 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 80x8 e = SAFE Actual Stress : Allowable Stress : 0.024 1.392 Check Stress Ratio : t/cm 2 Ft = f ta = Stress Ratio = 0.15 Check Stress Ratio : 0.034 0.232Allowable Stress : Fc = Actual Stress : f ca = SAFE Approved - Design of Bolted Connection : Section 2Ls Star-Shaped 80x8 t/cm2 - 10 DateDate - AM Checked - Date - HK e p p e x 4.3 Desgin of bracing members:- 73
  • 76. m 80 mm 8 mm cm cm cm < < < Fc ton > ton 2 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λu = qr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm8 2.76 1.68 cm2 cm2 0.7 tonShear Strength : No. of Bolts = 0.42 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = SAFE 2M12(8.8) e 25 Bolts Check of Shear Rapture : Stress Ratio = SAFE (S.R = 0.08) 0.01 0.4 Fy = 0.96 8.04 At = ton t/cm2 < Ft 2.24 4.32 SAFE A net = Check as Tension Member : cm 2 1.0Ky = 19.32 Type of Connection : Length = Bolts : m 195.4 22.36 cm2 λu = Kg/mWeight = Lbx = 10 mm ton 5.98 1.0m ton Grade of Steel : I Member ID : VB-036 t/cm 2 5.98 Sheet No. : 1.55iv = Case of Loading : asec Project Tiltle : Compression = ST- 37Tension = Departement : 0.71 0.31 195.4 200 ARESCO TEBBIN cm4 29.6 Thickness of Gusset Plate = Iu = t = cm4 300 Lby = 24.60 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 2.26a = 5.98 Bolted iu = 3.06 2Ls Star-Shaped Properties of Section : Section : Area = M12 Rev. Descreption Design F tr = p (S.R = 0.21) tG.P α = 0.8 tmin = 1 - 115.0 0 q r = Iv = 35 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 80x8 e = SAFE Actual Stress : Allowable Stress : 0.014 1.392 Check Stress Ratio : t/cm 2 Ft = f ta = Stress Ratio = 0.15 Check Stress Ratio : 0.029 0.196Allowable Stress : Fc = Actual Stress : f ca = SAFE Approved - Design of Bolted Connection : Section 2Ls Star-Shaped 80x8 t/cm2 - 10 DateDate - AM Checked - Date - HK e p p e x 4.3 Desgin of bracing members:- 74
  • 77. m 60 mm 6 mm cm cm cm < < < < < Fc ton > ton 2 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λx = qr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm10 3.46 3.36 cm2 cm2 2.3 tonShear Strength : No. of Bolts = 0.67 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = SAFE 2M12(8.8) e 25 Bolts Check of Shear Rapture : Stress Ratio = SAFE (S.R = 0.24) 0.06 0.4 Fy = 0.96 9.19 At = ton t/cm2 < Ft 2.30 5.40 SAFE SAFE A net = Check as Tension Member : cm 2 1.0Ky = 10.84 Type of Connection : Length = Bolts : m 189.8 12.14 cm2 λx = Kg/mWeight = Lbx = 10 mm ton 3.45 1.0m ton Grade of Steel : I Member ID : VB-045 t/cm 2 3.45 Sheet No. : 2.85 SAFE iy = Case of Loading : asec Project Tiltle : Compression = ST- 37Tension = Departement : 2.25 1.00 189.8 200 ARESCO TEBBIN cm4 111.9 Thickness of Gusset Plate = Ix = t = cm4 300 300 Lby = 13.82 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 1.69a = 3.45 Bolted ix = 1.82 2Ls Back to Back Properties of Section : Section : Area = M12 Rev. Descreption Design F tr = p (S.R = 0.33) tG.P α = 0.8 tmin = 1 - 22.8 121.4 0 λy = q r = Iy = λy = 200 30 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 60x6 e = SAFE Actual Stress : Allowable Stress : 0.082 1.392 Check Stress Ratio : t/cm 2 Ft = 121.4 f ta = Stress Ratio = 0.78 Check Stress Ratio : 0.163 0.208Allowable Stress : Fc = Actual Stress : f ca = SAFE Approved - Design of Bolted Connection : Section 2Ls Back to Back 60x6 t/cm2 - 10 DateDate - AM Checked - Date - HK e p p e x 4.3 Desgin of bracing members:- 75
  • 78. m 80 mm 8 mm cm cm cm < < < < < Fc ton > ton 2 DateDate - AM Checked - Date - HK Approved - Design of Bolted Connection : Section 2Ls Back to Back 80x8 t/cm2 - 10 Stress Ratio = 0.46 Check Stress Ratio : 0.104 0.227Allowable Stress : Fc = Actual Stress : f ca = SAFE SAFE Actual Stress : Allowable Stress : 0.011 1.392 Check Stress Ratio : t/cm 2 Ft = 181.8 f ta = 35 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 80x8 e = 1 - 72.3 181.8 0 λy = q r = Iy = λy = 200 Rev. Descreption Design F tr = p (S.R = 0.38) tG.P α = 0.8 tmin = a = 3.34 Bolted ix = 2.42 2Ls Back to Back Properties of Section : Section : Area = M12 300 300 Lby = 24.60 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 2.26 138.0 200 ARESCO TEBBIN cm4 332.0 Thickness of Gusset Plate = Ix = t = cm4 asec Project Tiltle : Compression = ST- 37Tension = Departement : 2.56 0.24 t/cm2 6.68 Sheet No. : 3.67 SAFE iy = Case of Loading :ton Grade of Steel : I Member ID : VB-062 Lbx = 10 mm ton 6.68 0.5m Type of Connection : Length = Bolts : m 138.0 22.36 cm2 λx = Kg/mWeight = A net = Check as Tension Member : cm 2 1.0Ky = 19.32 SAFE SAFE < Ft 2.80 5.40 Stress Ratio = SAFE (S.R = 0.25) 0.01 0.4 Fy = 0.96 10.06 At = ton t/cm2 SAFE 2M12(8.8) e 25 Bolts Check of Shear Rapture : Shear Strength : No. of Bolts = 0.76 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = 3.46 3.36 cm2 cm2 2.6 tonqr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm10 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λx = e p p e x 4.3 Desgin of bracing members:- 76
  • 79. m 80 mm 8 mm cm cm cm < < < < < Fc ton > ton 2 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λx = qr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm10 3.46 3.36 cm2 cm2 5.6 tonShear Strength : No. of Bolts = 1.68 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = SAFE 2M12(8.8) e 25 Bolts Check of Shear Rapture : Stress Ratio = SAFE (S.R = 0.56) 0.00 0.4 Fy = 0.96 10.06 At = ton t/cm2 < Ft 2.80 5.40 SAFE SAFE A net = Check as Tension Member : cm 2 1.0Ky = 19.32 Type of Connection : Length = Bolts : m 146.7 22.36 cm2 λx = Kg/mWeight = Lbx = 10 mm ton 3.55 1.0m ton Grade of Steel : I Member ID : VB-074 t/cm 2 3.55 Sheet No. : 3.67 SAFE iy = Case of Loading : asec Project Tiltle : Compression = ST- 37Tension = Departement : 5.64 0.00 146.7 200 ARESCO TEBBIN cm4 332.0 Thickness of Gusset Plate = Ix = t = cm4 300 300 Lby = 24.60 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 2.26a = 3.55 Bolted ix = 2.42 2Ls Back to Back Properties of Section : Section : Area = M12 Rev. Descreption Design F tr = p (S.R = 0.83) tG.P α = 0.8 tmin = 1 - 72.3 96.7 0 λy = q r = Iy = λy = 200 35 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 80x8 e = SAFE Actual Stress : Allowable Stress : 0.000 1.392 Check Stress Ratio : t/cm 2 Ft = 96.7 f ta = Stress Ratio = 0.66 Check Stress Ratio : 0.229 0.348Allowable Stress : Fc = Actual Stress : f ca = SAFE Approved - Design of Bolted Connection : Section 2Ls Back to Back 80x8 t/cm2 - 10 DateDate - AM Checked - Date - HK e p p e x 4.3 Desgin of bracing members:- 77
  • 80. m 60 mm 6 mm cm cm cm < < < < < Fc ton > ton 2 DateDate - AM Checked - Date - HK Approved - Design of Bolted Connection : Section 2Ls Back to Back 60x6 t/cm2 - 8 Stress Ratio = 0.66 Check Stress Ratio : 0.246 0.373Allowable Stress : Fc = Actual Stress : f ca = SAFE SAFE Actual Stress : Allowable Stress : 0.030 1.392 Check Stress Ratio : t/cm 2 Ft = 93.2 f ta = 30 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 60x6 e = 1 - 22.8 93.2 0 λy = q r = Iy = λy = 200 Rev. Descreption Design F tr = p (S.R = 0.61) tG.P α = 0.8 tmin = a = 2.58 Bolted ix = 1.82 2Ls Back to Back Properties of Section : Section : Area = M12 300 300 Lby = 13.82 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 1.69 141.8 200 ARESCO TEBBIN cm4 106.0 Thickness of Gusset Plate = Ix = t = cm4 asec Project Tiltle : Compression = ST- 37Tension = Departement : 3.40 0.37 t/cm2 2.58 Sheet No. : 2.77 SAFE iy = Case of Loading :ton Grade of Steel : I Member ID : VB-078 Lbx = 8 mm ton 2.58 1.0m Type of Connection : Length = Bolts : m 141.8 12.14 cm2 λx = Kg/mWeight = A net = Check as Tension Member : cm 2 1.0Ky = 10.84 SAFE SAFE < Ft 1.84 4.32 Stress Ratio = SAFE (S.R = 0.46) 0.02 0.4 Fy = 0.96 7.35 At = ton t/cm2 SAFE 2M12(8.8) e 25 Bolts Check of Shear Rapture : Shear Strength : No. of Bolts = 1.23 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = 2.76 3.36 cm2 cm2 3.4 tonqr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm8 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λx = e p p e x 4.3 Desgin of bracing members:- 78
  • 81. m 60 mm 6 mm cm cm cm < < < < < Fc ton > ton 2 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λx = qr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm8 2.76 3.36 cm2 cm2 0.2 tonShear Strength : No. of Bolts = 0.08 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = SAFE 2M12(8.8) e 25 Bolts Check of Shear Rapture : Stress Ratio = SAFE (S.R = 0.03) 0.01 0.4 Fy = 0.96 7.35 At = ton t/cm2 < Ft 1.84 4.32 SAFE SAFE A net = Check as Tension Member : cm 2 1.0Ky = 10.84 Type of Connection : Length = Bolts : m 186.3 12.14 cm2 λx = Kg/mWeight = Lbx = 8 mm ton 3.39 1.0m ton Grade of Steel : I Member ID : VB-079 t/cm 2 3.39 Sheet No. : 2.77 SAFE iy = Case of Loading : asec Project Tiltle : Compression = ST- 37Tension = Departement : 0.21 0.23 186.3 200 ARESCO TEBBIN cm4 106.0 Thickness of Gusset Plate = Ix = t = cm4 300 300 Lby = 13.82 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 1.69a = 3.39 Bolted ix = 1.82 2Ls Back to Back Properties of Section : Section : Area = M12 Rev. Descreption Design F tr = p (S.R = 0.04) tG.P α = 0.8 tmin = 1 - 22.8 122.4 0 λy = q r = Iy = λy = 200 30 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 60x6 e = SAFE Actual Stress : Allowable Stress : 0.019 1.392 Check Stress Ratio : t/cm 2 Ft = 122.4 f ta = Stress Ratio = 0.07 Check Stress Ratio : 0.015 0.216Allowable Stress : Fc = Actual Stress : f ca = SAFE Approved - Design of Bolted Connection : Section 2Ls Back to Back 60x6 t/cm2 - 8 DateDate - AM Checked - Date - HK e p p e x 4.3 Desgin of bracing members:- 79
  • 82. m 80 mm 8 mm cm cm cm < < < < < Fc ton > ton 2 DateDate - AM Checked - Date - HK Approved - Design of Bolted Connection : Section 2Ls Back to Back 80x8 t/cm2 - 10 Stress Ratio = 0.37 Check Stress Ratio : 0.079 0.212Allowable Stress : Fc = Actual Stress : f ca = SAFE SAFE Actual Stress : Allowable Stress : 0.000 1.392 Check Stress Ratio : t/cm 2 Ft = 188.1 f ta = 35 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 80x8 e = 1 - 72.3 188.1 0 λy = q r = Iy = λy = 200 Rev. Descreption Design F tr = p (S.R = 0.28) tG.P α = 0.8 tmin = a = 3.46 Bolted ix = 2.42 2Ls Back to Back Properties of Section : Section : Area = M12 300 300 Lby = 24.60 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 2.26 142.8 200 ARESCO TEBBIN cm4 332.0 Thickness of Gusset Plate = Ix = t = cm4 asec Project Tiltle : Compression = ST- 37Tension = Departement : 1.94 0.00 t/cm2 6.91 Sheet No. : 3.67 SAFE iy = Case of Loading :ton Grade of Steel : I Member ID : VB-081 Lbx = 10 mm ton 6.91 0.5m Type of Connection : Length = Bolts : m 142.8 22.36 cm2 λx = Kg/mWeight = A net = Check as Tension Member : cm 2 1.0Ky = 19.32 SAFE SAFE < Ft 2.80 5.40 Stress Ratio = SAFE (S.R = 0.19) 0.00 0.4 Fy = 0.96 10.06 At = ton t/cm2 SAFE 2M12(8.8) e 25 Bolts Check of Shear Rapture : Shear Strength : No. of Bolts = 0.58 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = 3.46 3.36 cm2 cm2 1.9 tonqr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm10 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λx = e p p e x 4.3 Desgin of bracing members:- 80
  • 83. m 70 mm 7 mm cm cm cm < < < < < Fc ton > ton 4 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λx = qr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm8 2.76 3.36 cm2 cm2 8.7 tonShear Strength : No. of Bolts = 3.16 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = SAFE 4M12(8.8) e 25 Bolts Check of Shear Rapture : Stress Ratio = SAFE (S.R = 0.67) 0.00 0.4 Fy = 0.96 12.88 At = ton t/cm2 < Ft 1.84 10.08 SAFE SAFE A net = Check as Tension Member : cm 2 1.0Ky = 14.76 Type of Connection : Length = Bolts : m 109.1 16.84 cm2 λx = Kg/mWeight = Lbx = 8 mm ton 2.31 1.0m ton Grade of Steel : I Member ID : VB-086 t/cm 2 2.31 Sheet No. : 3.18 SAFE iy = Case of Loading : asec Project Tiltle : Compression = ST- 37Tension = Departement : 8.74 0.00 109.1 200 ARESCO TEBBIN cm4 190.4 Thickness of Gusset Plate = Ix = t = cm4 300 300 Lby = 18.80 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 1.97a = 2.31 Bolted ix = 2.12 2Ls Back to Back Properties of Section : Section : Area = M12 Rev. Descreption Design F tr = p (S.R = 0.79) tG.P α = 0.8 tmin = 1 - 42.4 72.7 0 λy = q r = Iy = λy = 200 30 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 70x7 e = SAFE Actual Stress : Allowable Stress : 0.000 1.392 Check Stress Ratio : t/cm 2 Ft = 72.7 f ta = Stress Ratio = 0.74 Check Stress Ratio : 0.465 0.630Allowable Stress : Fc = Actual Stress : f ca = SAFE Approved - Design of Bolted Connection : Section 2Ls Back to Back 70x7 t/cm2 - 8 DateDate - AM Checked - Date - HK e p p e x 4.3 Desgin of bracing members:- 81
  • 84. m 60 mm 6 mm cm cm cm < < < < < Fc ton > ton 2 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λx = qr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm8 2.76 3.36 cm2 cm2 3.0 tonShear Strength : No. of Bolts = 1.10 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = SAFE 2M12(8.8) e 25 Bolts Check of Shear Rapture : Stress Ratio = SAFE (S.R = 0.41) 0.03 0.4 Fy = 0.96 7.35 At = ton t/cm2 < Ft 1.84 4.32 SAFE SAFE A net = Check as Tension Member : cm 2 1.0Ky = 10.84 Type of Connection : Length = Bolts : m 70.1 12.14 cm2 λx = Kg/mWeight = Lbx = 8 mm ton 2.55 0.5m ton Grade of Steel : I Member ID : VB-090 t/cm 2 2.55 Sheet No. : 2.77 SAFE iy = Case of Loading : asec Project Tiltle : Compression = ST- 37Tension = Departement : 3.04 0.52 70.1 200 ARESCO TEBBIN cm4 106.0 Thickness of Gusset Plate = Ix = t = cm4 300 300 Lby = 13.82 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 1.69a = 1.28 Bolted ix = 1.82 2Ls Back to Back Properties of Section : Section : Area = M12 Rev. Descreption Design F tr = p (S.R = 0.54) tG.P α = 0.8 tmin = 1 - 22.8 92.1 0 λy = q r = Iy = λy = 200 30 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 60x6 e = SAFE Actual Stress : Allowable Stress : 0.043 1.392 Check Stress Ratio : t/cm 2 Ft = 92.1 f ta = Stress Ratio = 0.26 Check Stress Ratio : 0.220 0.848Allowable Stress : Fc = Actual Stress : f ca = SAFE Approved - Design of Bolted Connection : Section 2Ls Back to Back 60x6 t/cm2 - 8 DateDate - AM Checked - Date - HK e p p e x 4.3 Desgin of bracing members:- 82
  • 85. m 70 mm 7 mm cm cm cm < < < < < Fc ton > ton 2 DateDate - AM Checked - Date - HK Approved - Design of Bolted Connection : Section 2Ls Back to Back 70x7 t/cm2 - 8 Stress Ratio = 0.83 Check Stress Ratio : 0.272 0.329Allowable Stress : Fc = Actual Stress : f ca = SAFE SAFE Actual Stress : Allowable Stress : 0.172 1.392 Check Stress Ratio : t/cm 2 Ft = 100.6 f ta = 30 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 70x7 e = 1 - 42.4 100.6 0 λy = q r = Iy = λy = 200 Rev. Descreption Design F tr = p (S.R = 0.92) tG.P α = 0.8 tmin = a = 3.20 Bolted ix = 2.12 2Ls Back to Back Properties of Section : Section : Area = M12 300 300 Lby = 18.80 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 1.97 150.9 200 ARESCO TEBBIN cm4 190.4 Thickness of Gusset Plate = Ix = t = cm4 asec Project Tiltle : Compression = ST- 37Tension = Departement : 5.11 2.90 t/cm2 3.20 Sheet No. : 3.18 SAFE iy = Case of Loading :ton Grade of Steel : I Member ID : VB-105 Lbx = 8 mm ton 3.20 1.0m Type of Connection : Length = Bolts : m 150.9 16.84 cm2 λx = Kg/mWeight = A net = Check as Tension Member : cm 2 1.0Ky = 14.76 SAFE SAFE < Ft 1.84 4.32 Stress Ratio = SAFE (S.R = 0.69) 0.12 0.4 Fy = 0.96 7.35 At = ton t/cm2 SAFE 2M12(8.8) e 25 Bolts Check of Shear Rapture : Shear Strength : No. of Bolts = 1.85 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = 2.76 3.36 cm2 cm2 5.1 tonqr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm8 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λx = e p p e x 4.3 Desgin of bracing members:- 83
  • 86. m 80 mm 8 mm cm cm cm < < < < < Fc ton > ton 4 DateDate - AM Checked - Date - HK Approved - Design of Bolted Connection : Section 2Ls Back to Back 80x8 t/cm2 - 10 Stress Ratio = 0.85 Check Stress Ratio : 0.510 0.601Allowable Stress : Fc = Actual Stress : f ca = SAFE SAFE Actual Stress : Allowable Stress : 0.000 1.392 Check Stress Ratio : t/cm 2 Ft = 73.6 f ta = 35 AK 50 - MISR BANI SUEF CAMPANY Issued for Approval BOOSTER FAN PLATFORM & DUCT SUPPORT 80x8 e = 1 - 72.3 73.6 0 λy = q r = Iy = λy = 200 Rev. Descreption Design F tr = p (S.R = 0.93) tG.P α = 0.8 tmin = a = 2.70 Bolted ix = 2.42 2Ls Back to Back Properties of Section : Section : Area = M12 300 300 Lby = 24.60 Check Slenderness Ratio : Design Calculation Sheet Design of Angles Subjected to Axial Force According to ECP No.(205) Kx = 2.26 111.7 200 ARESCO TEBBIN cm4 332.0 Thickness of Gusset Plate = Ix = t = cm4 asec Project Tiltle : Compression = ST- 37Tension = Departement : 12.54 0.00 t/cm2 2.70 Sheet No. : 3.67 SAFE iy = Case of Loading :ton Grade of Steel : I Member ID : VB-117 Lbx = 10 mm ton 2.70 1.0m Type of Connection : Length = Bolts : m 111.7 22.36 cm2 λx = Kg/mWeight = A net = Check as Tension Member : cm 2 1.0Ky = 19.32 SAFE SAFE < Ft 2.80 12.60 Stress Ratio = SAFE (S.R = 0.73) 0.00 0.4 Fy = 0.96 16.97 At = ton t/cm2 SAFE 4M12(8.8) e 25 Bolts Check of Shear Rapture : Shear Strength : No. of Bolts = 3.73 Bearing Strength : R sh = q b x A s x n = Bolts R b = F b x d x t min = 3.46 3.36 cm2 cm2 12.5 tonqr x Ash + Ftr x At = 0.725 Fy = 1.74 x mm10 Check as Compression Member : Grade of Bolts : 8.8 Ash =Bolts : M12 t/cm2 t/cm 2 Check Slenderness Ratio : λx = e p p e x 4.3 Desgin of bracing members:- 84
  • 87. Joint OutputCase CaseType StepType F1 F2 F3 Text Text Text Text Tonf Tonf Tonf 159 ENV. Combination Max 0.1301 0.4909 10.0431 159 ENV. Combination Min ‐0.1308 ‐1.9141 ‐1.326 161 ENV. Combination Min ‐0.1302 ‐0.8183 ‐2.8709 162 ENV. Combination Max 0.1304 1.9317 10.6314 Extreme output reaction for IPE200 base connection:- 4.4-Design of bases connections:- 85
  • 88. 0 X C X T 30 Qy 20 Qx Qr 20 20 20 Bearing Plate Data : < % mm % mm % < % < % < % 23 mm mm mm Cm2 < < < 1.1 * * * mm Ø mm mm mm mm * * mm mm * * mm mm mm 400 mm qr = Qr/Atotal = 400 mmUse Embebed Length = 520Anchor Bolt Total Length = mmRequired Embebed Length = Minimum Embebed Length ( 20 d ) = of Tmin 6.8Flange Weld Size = Web Weld Size = 0.72 FINALLY USE : 21 30 Hole Diameter = Hole Diameter = GROUT THICK. = mm ftall-toncm 2 1.01 Embebed Length = GRADE Bearing Plate Area = Bearing Plates Are Clashed Check of Pitch Bolt Distance 1.4 100 qall-toncm 2 4.6+ 3-NUT & WASHER 21 Max. Bearing = 4.48 kg/cm2 of Bearing plate ton 160Thread Length = 250 S2-(mm) Please Decrease dictanse S1 140 80 60 140 Check of Edge Bolt Distance 12 8.5 5.6 Anchor Bolt Data : Fu-toncm2 3.6 Fy-toncm2 2.4 M-(mm) 20 qact. (ton/cm2 ) = fcu-kg/cm 2 fb-kgcm2 250 fCall-kgcm2 70.00 8.18 Steel Data: 20 ton (TEN.) 0.27 Safe 21.1 ton 80 S1-(mm) 20 Approve By (Qr/n)/(Abolt) = SAFE0.61(fact/ftall)2 +(qact/qall)2 = Joint Forces :- 10.01 Steel Grade ton (COM.) AM 0.72 Design By 300 Rev. Steel Grade MISR BANI SUEF COMPANY 600 D-(mm) IPE200 mm mm mm mm mm B-(mm) Project 1.94 0.131 ton ton Tw = Tf = Column Size :- 200 2.88 Bf = AK 5 140 2 Bolt (d) 20 r = 30.00 10 100 d-(mm) Design of Base Connection (Hinged-with anchor bolts)-(N,Q) Dept. Item BASE PLATE FOR SECTION IPE200 H = Grout (mm) d-(mm)t-(mm) b-(mm) 0.765 N-(mm) fw-all-toncm 2 37 240 140 100 As/bolt(cm 2 ) 2.45 t-(mm) b-(mm) HKCheck By 240 0 Tpl-(mm) X2 = kg/cm2 Check of Plate Thickness due to Compresion(C): 30mm Check of concrete due to Compresion(C): 70.0 0.13 ton.cm/cm SAFEfcon = C / ( B * D ) = 29.8 25 mm Moment/unit width =X1 = kg/cm2 6 * M / (0.58 * Fy * B) = Check of Plate Thickness due to Tension(T): Thickness required t (mm)= 6 * M / (0.72 * Fy * B) = 6.8 SAFE ftact (ton/cm2 ) = T/(n*Abolt) = 0.59 ton/cm2 Check of Anchor Bolt due to Shear(Qr) & Tension(T): Moment = T(tension)x[(D-S1)x0.5-N] = 14.4 ton.cm Thickness required t (mm)= 0.61 SAFE SAFE ton/cm2 Safe 0.25 Safety Ratio All Tension Supported By Bearing Plate ton/cm2 1.01 ton/cm2 Thread Length = 160 Safe0.72 Safety Ratio 0.43 Safety Ratio 0.27 0.58 160 Actual Tension / Anchor = Required Length of Anchor Bolts :- 96.9 Cm2 37 0.05 520 400 Check of weld: -154 Max.Tension Supported By Bearing Plate= 2.2 ton 0.40 60 10 ton/cm2 BASE PLATE ANCHOR BOLT 2 240 BEARING PLATE 10 25 140 100 37 400 GRADE GRADE 37 520 100 37 feq = (fca 2 +3*q2 ) = ton/cm2 TEMPLATE 5 140 60 37 GRADE Total Length = 0.80 Weld Size ( of Tmin ) TemPlate Data : 1.94 Number(n) Fu-toncm2 3.6 Base Plate Data : Concrete Data: 0.765 Safety Ratio Safety Ratio fconXmax.(x1 or x2)2 /2 = 0.84 WELD RATIO 0.8 0.72 20 GRADE NOTE: q all & ftall decreased by 15 % according to clause 6.7.5 in ECP 205-2001 fca = Max.(C,T)/Atotal = 1 A total cm2= 39.57 SAFE Safety Ratio 0.52 ton/cm2 86
  • 89. Joint OutputCase StepType F1 F2 F3 Text Text Text Tonf Tonf Tonf 47 ENV. Max 0.6558 1.2618 10.259 51 ENV. Min ‐0.2236 ‐1.6546 ‐15.0122 296 ENV. Max 0.3845 0.9532 25.0996 Extreme output reaction for IPE270 base connection:- 87
  • 90. 0 X C X T 30 Qy # Qx Qr # 15 15 Bearing Plate Data : < % mm % mm % < % < % < % 23 mm mm mm Cm 2 < < < 1.1 * * * mm Ø mm mm mm mm * * mm mm * * mm mm mm 600 mm qr = Qr/Atotal = 600 mmUse Embebed Length = 750Anchor Bolt Total Length = mmRequired Embebed Length = Minimum Embebed Length ( 20 d ) = of Tmin 8.16Flange Weld Size = Web Weld Size = 0.72 FINALLY USE : 31 30 Hole Diameter = Hole Diameter = GROUT THICK. = mm ftall-toncm 2 1.01 Embebed Length = GRADE Bearing Plate Area = Bearing Plates Are Clashed Check of Pitch Bolt Distance 3.8 100 qall-toncm 2 4.6+ 3-NUT & WASHER 31 Max. Bearing = 5.28 kg/cm2 of Bearing plate ton 200Thread Length = 32140 S2-(mm) Please Decrease dictanse S1 240 140 230 230 Check of Edge Bolt Distance 15 10.2 6.6 Anchor Bolt Data : Fu-toncm 2 3.6 Fy-toncm2 2.4 M-(mm) 52.5 qact. (ton/cm2 ) = fcu-kg/cm2 fb-kgcm2 250 fCall-kgcm2 70.00 8.18 Steel Data: 15 ton (TEN.) 0.39 Safe 29.6 ton 140 S1-(mm) 20 Approve By (Qr/n)/(Abolt) = SAFE0.45(fact/ftall)2 +(qact/qall)2 = Joint Forces :- 25.1 Steel Grade ton (COM.) AM 0.72 Design By 300 Rev. Steel Grade MISR BANI SUEF COMPANY 600 D-(mm) IPE270 mm mm mm mm mm B-(mm) Project 1.66 0.66 ton ton Tw = Tf = Column Size :- 270 15.02 Bf = AK 5 230 4 Bolt (d) 30 r = 30.00 10 135 d-(mm) Design of Base Connection (Hinged-with anchor bolts)-(N,Q) Dept. Item BASE PLATE FOR SECTION IPE270 H = Grout (mm) d-(mm)t-(mm) b-(mm) 0.765 N-(mm) fw-all-toncm 2 37 300 240 100 As/bolt(cm2 ) 5.61 t-(mm) b-(mm) HKCheck By 300 140 Tpl-(mm) X2 = kg/cm 2 Check of Plate Thickness due to Compresion(C): 66mm Check of concrete due to Compresion(C): 70.0 0.76 ton.cm/cm SAFEfcon = C / ( B * D ) = 34.9 21.75 mm Moment/unit width =X1 = kg/cm2 6 * M / (0.58 * Fy * B) = Check of Plate Thickness due to Tension(T): Thickness required t (mm)= 6 * M / (0.72 * Fy * B) = 16.2 SAFE ftact (ton/cm2 ) = T/(n*Abolt) = 0.67 ton/cm 2 Check of Anchor Bolt due to Shear(Qr) & Tension(T): Moment = T(tension)x[(D-S1)x0.5-N] = 48.8 ton.cm Thickness required t (mm)= 0.45 SAFE SAFE ton/cm2 Safe 0.39 Safety Ratio ton/cm 2 1.01 ton/cm2 Thread Length = 200 Safe0.72 Safety Ratio 0.50 Safety Ratio 0.51 0.66 200 Actual Tension / Anchor = Required Length of Anchor Bolts :- 92.9 Cm 2 37 0.03 750 600 Check of weld: 209 Max.Tension Supported By Bearing Plate= 2.1 ton 0.08 230 10 ton/cm 2 BASE PLATE ANCHOR BOLT 4 300 BEARING PLATE 10 32 240 100 37 600 GRADE GRADE 37 750 100 37 feq = (fca 2 +3*q 2 ) = ton/cm 2 TEMPLATE 5 230 230 37 GRADE Total Length = 0.80 Weld Size ( of Tmin ) TemPlate Data : 1.79 Number(n) Fu-toncm2 3.6 Base Plate Data : Concrete Data: 0.765 Safety Ratio Safety Ratio fconXmax.(x1 or x2) 2 /2 = 0.93 WELD RATIO 0.8 0.72 30 GRADE NOTE: q all & ftall decreased by 15 % according to clause 6.7.5 in ECP 205-2001 fca = Max.(C,T)/Atotal = 1 A total cm2= 64.45 SAFE Safety Ratio 0.10 ton/cm2 88
  • 91. Joint OutputCase CaseType F1 F2 F3 Text Text Text Tonf Tonf Tonf 203 ENV. Combination 2.4955 0.000255 1.0418 203 ENV. Combination ‐1.912 ‐0.00042 ‐1.1233 204 ENV. Combination ‐1.7624 ‐0.00047 ‐1.0057 Extreme output reaction for UPN200 base connection:- 89
  • 92. 0 X C X T 30 Qy # Qx Qr # 20 20 Bearing Plate Data : < % mm % mm % < % < % < % 23 mm mm mm Cm 2 < < < 1.1 * * * mm Ø mm mm mm mm * * mm mm * * mm mm mm NOTE: q all & ftall decreased by 15 % according to clause 6.7.5 in ECP 205-2001 fca = Max.(C,T)/Atotal = 1 A total cm2= 47.90 SAFE Safety Ratio 0.67 ton/cm 2 0.765 Safety Ratio Safety Ratio fconXmax.(x1 or x2) 2 /2 = 0.62 WELD RATIO 0.8 0.80 Weld Size ( of Tmin ) TemPlate Data : 2.50 Number(n) 0.72 20 GRADE 37 feq = (fca 2 +3*q 2 ) = ton/cm 2 TEMPLATE 5 140 60 37 GRADE Total Length = 37 400 GRADE GRADE 37 510 100 ton/cm 2 BASE PLATE ANCHOR BOLT 2 240 BEARING PLATE 10 20 160 100 510 400 Check of weld: -324 Max.Tension Supported By Bearing Plate= 2.2 ton 0.51 60 10 150 Actual Tension / Anchor = Required Length of Anchor Bolts :- 96.9 Cm2 37 0.05 ton/cm2 Thread Length = 150 Safe0.72 Safety Ratio 0.04 Safety Ratio 0.17 0.23 0.50 SAFE SAFE ton/cm 2 Safe 0.02 Safety Ratio All Tension Supported By Bearing Plate ton/cm2 1.01ftact (ton/cm 2 ) = T/(n*Abolt) = 0.23 ton/cm 2 Check of Anchor Bolt due to Shear(Qr) & Tension(T): Moment = T(tension)x[(D-S1)x0.5-N] = 5.7 ton.cm Thickness required t (mm)= 6 * M / (0.58 * Fy * B) = Check of Plate Thickness due to Tension(T): Thickness required t (mm)= 6 * M / (0.72 * Fy * B) = 3.4 SAFE 0.03 ton.cm/cm SAFEfcon = C / ( B * D ) = 2.7 25 mm Moment/unit width =X1 = kg/cm 2 X2 = kg/cm 2 Check of Plate Thickness due to Compresion(C): 50mm Check of concrete due to Compresion(C): Fu-toncm2 3.6 100 As/bolt(cm 2 ) 2.45 t-(mm) b-(mm) HKCheck By 70.0 Base Plate Data : Concrete Data: Grout (mm) d-(mm)t-(mm) b-(mm) 0.765 N-(mm) 75 d-(mm) Design of Base Connection (Hinged-with anchor bolts)-(N,Q) Dept. Item BASE PLATE FOR SECTION UPN200 H = Bf = AK 5 140 2 Bolt (d) 20 r = 30.00 10 fw-all-toncm 2 Project 0 2.5 ton ton Tw = Tf = Column Size :- 240 0200 MISR BANI SUEF COMPANY 600 D-(mm) UPN200 mm mm mm 1.13 ton (COM.) AM 0.72 Design By 300 Rev. Steel Grade 20 Approve By (Qr/n)/(Abolt) = SAFE0.50(fact/ftall) 2 +(qact/qall) 2 = Joint Forces :- 1.042 Steel Grade 37 ton (TEN.) 0.09 Safe 12.3 ton 80 S1-(mm) qact. (ton/cm 2 ) = fcu-kg/cm 2 fb-kgcm2 250 fCall-kgcm2 70.00 8.18 Steel Data: mm mm 6 11.5 8.5 Anchor Bolt Data : Fu-toncm 2 3.6 Fy-toncm2 2.4 240 B-(mm) 160 M-(mm) 42.5 20 Tpl-(mm) 200 S2-(mm) Please Decrease dictanse S1 160 80 60 140 Check of Edge Bolt Distance 4.6+ 3-NUT & WASHER 21 Max. Bearing = 6.8 kg/cm2 of Bearing plate ton 150Thread Length = ftall-toncm2 1.01 Embebed Length = GRADE Bearing Plate Area = Bearing Plates Are Clashed Check of Pitch Bolt Distance 0.6 100 qall-toncm2 21 30 Hole Diameter = Hole Diameter = GROUT THICK. = mm mmRequired Embebed Length = Minimum Embebed Length ( 20 d ) = of Tmin 9.2Flange Weld Size = Web Weld Size = 0.72 FINALLY USE : 400 mm qr = Qr/Atotal = 400 mmUse Embebed Length = 510Anchor Bolt Total Length = 90
  • 93. Frame Station OutputCase CaseType StepType P V2 V3 Text m Text Text Text Tonf Tonf Tonf B‐021 4.92 ENV. Combination Min ‐1.041 0.2423 ‐1.4483 B‐103 5.5 ENV. Combination Max 0.2678 2.5909 0.2414 B‐067 9.9 ENV. Combination Max 8.109 0.0482 0.0485 Extrem out put reactions for HEA160 shear connection: 4.5 Design of Beam connections:- 91
  • 94. I 2 4 1 20 mm 5 < mm t = mm ton < 1 < cm < < < 12.91 20 SAFE (Subjected to Shear +Torsion) Mcan = 7.67 cm.t cm2 4.90 ton SAFE 6.47 0.12 ton SAFE 18.41 Check of Combined Shear and Tension : E= 80 mm 0.72 160 End Plate Thickness : mm mmNet Width = 116 SAFE - t/cm 2 19 cm.t 0.236 t/cm2 169.9 cm 4 Face (1-1) : 0.17 0.792 t/cm 2 0.72 Face (2-2) : ton Checked Date 8.0 6.0 mmaround the Flanges = mm 5.0 Point (B) : 2.03 6.47 Check of Tension : Tensile Strength : ton α = 0.60 Stressed Area = t/cm 2 t/cm 2 Sweld : Point (A) : 0.41 t/cm 2 HK 0.792 - - - - Check on Weld : 0.3 Sweld = (Subjected to Shear +Tension) around the Web = mm DateDesign DateApproved AM Rev. Descreption 0 4.90 Bearing Strength : Rleast = Shear Strength : Issued for Approval AK 1 - - SAFE Check of Bolts : Grade of Bolts : 8.8 Number of Columns of Bolts = tmin = Number of Plans Subjected to Shear = Bolt Diameter = 20 mm St 37 Connection : Member : Design Calculation Sheet Design of Bolted Shear Connection of the Bearing Type HEA160 asec H = 160 Connected Beams : Beam (1) : mm Qy = 2.6 H = 152 HEA 160 ARESCO TEBBIN Qx = 1.5 ton ton bf = mm mm N = tw = tf = mm mm 160 6.0 Arrangement of Bolts : A= 30 tw = 80 9.0 Rsh a = 2.45 4.90 8.64 ton mm 0.74 ton Check of Shear : mm mm bf = IPE 160 5.0 Beam (2) : 82 mm mm tf = 7.4 mm Number of Bolts : B = D= mm Bp = 40 1.61t = mm t/cm 2 t/cm2 0.38 SAFE Project Tiltle : Department : Booster Fan Platform & Duct Support MISR BANI SUEF COMPANY Case of Loading : 8.1 ton Grade of Steel :  nAqR sbsh  tmindFR bb             22 n Q n Q yx  subt AF0.33R      2 A 2 tAeq q3ff      2 B 2 tBeq q3ff             22 t ta sh ash R R R R  bf M t all 6 X t M  p t w y y I xM A Q q . VL      22 xytotal qqq pI  p t x I yM q .  n T Rta y F0.58 net y t A Q f  bf M t all 6 92
  • 95. Frame Station OutputCase CaseType StepType P V2 V3 Text m Text Text Text Tonf Tonf Tonf B‐066 0 ENV. Combination Min ‐0.5646 ‐0.4651 ‐0.1014 B‐066 4.92 ENV. Combination Max ‐0.0981 0.6676 0.0533 B‐066 4.92 ENV. Combination Min ‐7.7812 ‐0.5404 ‐0.061 Extrem out put reactions for HEA300 hanged from HEA160 connection: 93
  • 96. II 4 2 1 1 2 ton < 3 t = mm 20 mm < ton < 1 < Aw FL= 70.7 19.5 51.2 Aw Total = - --- - SAFE Check of Combined Shear and Tension : mm cm 2 mm ton mm 0 Qx =ton Bolt Diameter = Grade of Steel : St-37 Case of Loading : Connected Beams : H = mmmm bf = - Rev. Descreption 20 mm 290 Grade of Bolts : 8.8 tmin = Allowable & Actual Stresses on Bolts : mm Number of Columns of Bolts = tf = Date Design of Shear Plate : Shear Strength : Tensile Strength : ton Check of Tension : Bp = 1.2 mm Stressed Area = 2.45 Number of Plans Subjected to Shear = Number of Bolts : Arrangement of Bolts : B = 152 mm 7.9 HEA 300 ton Beam (2) : Qy = H = MISR BANI SUEF COMPANY BOOSTER FAN PLATFORM & DUCT SUPPORT ID : 1.5 Input Data : Project Tiltle : Department : Sheet No. : T = Sweld : ton5.88 4.67 ton Bearing Strength : Rleast = 8.5 300 14.0 Beam (1) : HEA 160 0 1 mm37D= 160 mm α= 0.6 At Point (A) : mm Check on Weld : mm A= 180 tw = tf = 9.0 bf = 160 tw = 6.0 HK - Checked Date Approved AM Design Date - - Issued for Approval AK - cm2 cm2 0.792 Aw WEB= SAFEt/cm2 t/cm2 0.70 0.19 SAFE C = mm Properties of Weld : 7.76Take t = Hp = 7.84 2.01 Design Calculation Sheet Design of Shear Connection ACCORDING TO EGYPTIAN CODE OF PRACTICE NO. (205) 0 20 mm mm 86 7.76 ton SAFE mm (LONGITUDINAL DIRECTION) (TRANSVERSE DIRECTION) around the Web = 8.0 mm 0.30around the Flanges = 10.0 mm cm2 #NUM! mm Rsh a = 4.67 ton 0.456 ton4.67 180 mm Check of Shear : E =  nAqR sbsh  tmindFR bb             22 n Q n Q yx  subt AF0.33R  n T Rta ys F A Q q 35.0 2 3              22 t ta sh ash R R R R      2 A 2 tAeq q3ff  bf M t all 6  bf M t all 6 94
  • 97. Frame Station OutputCase CaseType StepType P V2 V3 Text m Text Text Text Tonf Tonf Tonf G‐09 0 ENV. CombinatioMin ‐0.2907 ‐7.7284 ‐1.1727 G‐10 6.43197 ENV. CombinatioMax 0.7488 7.9353 0.1355 G‐06 6.43197 ENV. CombinatioMax 1.4467 2.6899 0.4802 Extrem out put reactions for HEA300 typical shear connection: 95
  • 98. I 2 4 1 16 mm 5 < mm t = mm ton < 1 < cm < < < 6.22 16 SAFE (Subjected to Shear +Torsion) Mcan = 3.34 cm.t cm 2 4.90 ton SAFE 6.47 0.17 ton SAFE 7.81 Check of Combined Shear and Tension : E= 140 mm 0.72 300 End Plate Thickness : mm mmNet Width = 256 SAFE - t/cm2 74 cm.t 0.33 t/cm 2 1251.8 cm4 Face (1-1) : 0.02 0.792 t/cm 2 0.99 Face (2-2) : ton Checked Date 10.0 6.0 mmaround the Flanges = mm 6.0 Point (B) : 0.36 6.47 Check of Tension : Tensile Strength : ton α = 0.60 Stressed Area = t/cm 2 t/cm2 Sweld : Point (A) : 0.50 t/cm2 HK 0.792 - - - - Check on Weld : 0.326 Sweld = (Subjected to Shear +Tension) around the Web = mm DateDesign DateApproved AM Rev. Descreption 0 4.90 Bearing Strength : Rleast = Shear Strength : Issued for Approval AK 1 - - SAFE Check of Bolts : Grade of Bolts : 8.8 Number of Columns of Bolts = tmin = Number of Plans Subjected to Shear = Bolt Diameter = 20 mm St 37 Connection : Member : Design Calculation Sheet Design of Bolted Shear Connection of the Bearing Type HEA300 asec H = 300 Connected Beams : Beam (1) : mm Qy = 7.9 H = 290 HEA 300 ARESCO TEBBIN Qx = 1.2 ton ton bf = mm mm N = tw = tf = mm mm 300 8.5 Arrangement of Bolts : A= 69 tw = 140 14.0 Rsh a = 2.45 4.90 6.91 ton mm 2.01 ton Check of Shear : mm mm bf = IPE 300 7.1 Beam (2) : 150 mm mm tf = 10.7 mm Number of Bolts : B = D= mm Bp = 80 2.23t = mm t/cm 2 t/cm 2 0.46 SAFE Project Tiltle : Department : Booster Fan Platform & Duct Support MISR BANI SUEF COMPANY Case of Loading : 1.5 ton Grade of Steel :  nAqR sbsh  tmindFR bb             22 n Q n Q yx  subt AF0.33R      2 A 2 tAeq q3ff      2 B 2 tBeq q3ff             22 t ta sh ash R R R R  bf M t all 6 X tM  p t w y y I xM A Q q . VL      22 xytotal qqq pI  p t x I yM q .  n T Rta yF0.58 net y t A Q f  bf M t all 6 96
  • 99. Frame Station OutputCase CaseType StepType P V2 V3 Text m Text Text Text Tonf Tonf Tonf P‐02 0 ENV. Combination Min ‐4.6931 ‐0.0246 ‐0.0246 Extrem out put reactions for IPE200 Post connection: 97
  • 100. II 4 2 1 1 2 ton < 3 t = mm 10 mm < ton < 1 < 0.000 ton3.53 220 mm Check of Shear : E = 0.000 mm Rsh a = 3.53 ton cm 2 (LONGITUDINAL DIRECTION) (TRANSVERSE DIRECTION) around the Web = 5.0 mm 0.00around the Flanges = 6.0 mm mm 72 4.97 ton SAFE mm0 10 mm Design Calculation Sheet Design of Shear Connection ACCORDING TO EGYPTIAN CODE OF PRACTICE NO. (205) 0.00 SAFE C = mm Properties of Weld : 4.97Take t = Hp = 0.04 0.01 cm2 0.792 Aw WEB= SAFEt/cm 2 t/cm 2 0.00 cm2 Design Date - - Issued for Approval AK - HK - Checked Date Approved AM tw = tf = 8.5 bf = 100 tw = 5.6 At Point (A) : mm Check on Weld : mm A= 120 6.6 135 10.2 Beam (1) : IPE 200 0 1 mm32D= Sweld : ton3.77 3.53 ton Bearing Strength : Rleast = MISR BANI SUEF COMPANY BOOSTER FAN PLATFORM & DUCT SUPPORT ID : 0.0 Input Data : Project Tiltle : Department : Sheet No. : T = 0.0 IPE 270 ton Beam (2) : Qy = H = 0.0 mm Stressed Area = 1.57 Number of Plans Subjected to Shear = Number of Bolts : Arrangement of Bolts : B = 200 mm tf = Date Design of Shear Plate : Shear Strength : Tensile Strength : ton Check of Tension : Bp = 135 mm Grade of Bolts : 8.8 tmin = Allowable & Actual Stresses on Bolts : mm Number of Columns of Bolts = α= 0.6 H = mmmm bf = - Rev. Descreption 16 mm 270 mm 50 Qx =ton Bolt Diameter = Grade of Steel : St-37 Case of Loading : Connected Beams : SAFE Check of Combined Shear and Tension : mm cm2 mm ton Aw FL= 35.2 16.0 19.2 Aw Total = - --- -  nAqR sbsh  tmindFR bb             22 n Q n Q yx  subt AF0.33R  n T Rta ys F A Q q 35.0 2 3              22 t ta sh ash R R R R      2 A 2 tAeq q3ff  bf M t all 6  bf M t all 6 98
  • 101. Frame Station OutputCase CaseType StepType P V2 V3 Text m Text Text Text Tonf Tonf Tonf P‐03 0 ENV. Combination Min ‐8.1883 ‐0.0424 ‐0.024 P‐03 0 ENV. Combination Max 4.5779 0.042 0.024 Extrem out put reactions for IPE160 over Beam connection: 99
  • 102. II 4 2 1 1 2 ton < 3 t = mm 10 mm < ton < 1 < 1.016 ton3.84 200 mm Check of Shear : E = 15.603 mm Rsh a = 2.02 ton cm 2 (LONGITUDINAL DIRECTION) (TRANSVERSE DIRECTION) around the Web = 4.0 mm 1.15around the Flanges = 6.0 mm mm 60 2.66 ton SAFE mm0 10 mm Design Calculation Sheet Design of Shear Connection ACCORDING TO EGYPTIAN CODE OF PRACTICE NO. (205) 0.19 SAFE C = mm Properties of Weld : 2.66Take t = Hp = 0.04 0.01 cm2 0.792 Aw WEB= SAFEt/cm 2 t/cm 2 0.14 cm2 Design Date - - Issued for Approval AK - HK - Checked Date Approved AM tw = tf = 8.5 bf = 100 tw = 5.6 At Point (A) : mm Check on Weld : mm A= 100 5.0 #N/A 7.4 Beam (1) : IPE 200 0 1 mm31D= Sweld : ton2.02 2.02 ton Bearing Strength : Rleast = MISR BANI SUEF COMPANY BOOSTER FAN PLATFORM & DUCT SUPPORT ID : 0.0 Input Data : Project Tiltle : Department : Sheet No. : T = 0.0 IPE 160 ton Beam (2) : Qy = H = 4.6 mm Stressed Area = 0.84 Number of Plans Subjected to Shear = Number of Bolts : Arrangement of Bolts : B = 200 mm tf = Date Design of Shear Plate : Shear Strength : Tensile Strength : ton Check of Tension : Bp = 122 mm Grade of Bolts : 8.8 tmin = Allowable & Actual Stresses on Bolts : mm Number of Columns of Bolts = α= 1.0 H = mmmm bf = - Rev. Descreption 12 mm 160 mm 50 Qx =ton Bolt Diameter = Grade of Steel : St-37 Case of Loading : Connected Beams : SAFE Check of Combined Shear and Tension : mm cm2 mm ton Aw FL= 32.0 12.8 19.2 Aw Total = - --- -  nAqR sbsh  tmindFR bb             22 n Q n Q yx  subt AF0.33R  n T Rta ys F A Q q 35.0 2 3              22 t ta sh ash R R R R      2 A 2 tAeq q3ff  bf M t all 6  bf M t all 6 100
  • 103. Frame Station OutputCase CaseType StepType P V2 V3 Text m Text Text Text Tonf Tonf Tonf B‐074 0 ENV. Combination Min ‐0.5441 ‐2.214 ‐0.1873 B‐074 0 ENV. Combination Max 1.1071 ‐0.8711 0.0977 Extrem out put reactions for IPE160 typical shear connection connection: 101
  • 104. ARESCO TEBBIN IPE160Sheet No. : Conn. No. : ton2.22Q = ton1.11N =cm.t7.77Mweld = IPE240GirderIPE160Beam mm L240Hg =mm160Hb = mm120Bg =mm82Bb = mm6.20Twg =mm5.00Twb = mm9.8Tfg =mm7.40Tfb = mm15r =mm9.00r = mm6Tplate = mm25B =mm35A = mm25C2 =mm20C1= OK140Check Dim. ( L )mm25E =mm50D = mm25Edge for N =mm25Edge for Q = 1NO.OF Sh. PLAN8.8mm Bolt Grade16BOLT DIA.(d) =2BOLT NO. (n) = 26.4Fyb =t/cm2 8Fub =cm2 1.57AS = t/cm2 2.4Fy =t/cm2 3.6Fu =37Steel Grade LINES2NO.OF W. L. =mm5S =Tmin.0.8Weld Size t/cm2 0.792Feq = 1.1 * Fweld=t/cm2 0.72Fweld = 0.2 * Fu= mm5tmin.=0.25K =0.6αN =0.6αQ = t/bolt1.73RbN.=αN*Fu*d*tmin.=t/bolt1.73RbQ.=αQ*Fu*d*tmin.=t/bolt3.14Rsh=KxFubxAs= ok0.75>1Long Joint F =t/bolt1.73Rleast = Safet/bolt1.73<t/bolt1.24 t/cm2 0.96qr =0.4Fy=cm2 2.4Ash.net = t/cm2 1.74Ftr = 0.725Fy =cm2 0.8At.net = Safeton2.22>ton3.70Qall=qr* Ash+Ftr*At= t/cm2 0.96qr =0.4Fy =cm2 0.8Ash.net = t/cm2 1.74Ftr = 0.725Fy =cm2 2.4At.net = Safeton1.11>ton4.94Qall=qr*Ash+Ftr*At= ton3.70<ton2.48Req1 =CHECK-1 Safe1<0.41Req2 =CHECK-2 cm3 25cm2 Zsec. =12.7Asec.= ton2.22cm.t Qsec. =7.8Msec.=ton1.11Nsec. = Safet/cm2 0.84<t/cm2 0.32q = Safet/cm2 1.4<t/cm2 0.39ft = SafeSafet/cm2 1.54<t/cm2 0.71feq. = cm4 83.83cm2 Iw =10.02Aw =cm10.02Lw = Safet/cm2 0.72<t/cm2 0.58ft =N/A+M*Y /I = Safet/cm2 0.72<t/cm2 0.22q = Q / A = SafeSafet/cm2 0.792<t/cm2 0.69 0.41Rup.2 Safe Ratio=0.67Rup.1 Safe Ratio=0.72Bolt Safe Ratio= 0.87Conn. Safe Ratio=0.87Weld Safe Ratio=0.46Sec. Safe Ratio= mm111X60X6PL.FINALLY USE : HSBB.T.8.8GRADE16M2 mm25B =mm35A =@ mm25C2 =mm20C1 = mm25E =mm50D = mm5Sw =Weld Lines2Tmin.0.8Weld Size Design of Shear Conn. Bearing Type According to ECP No.(205) Design Calculation Sheet asec MISR BANI SUEF COMPANY BOOSTER FAN PLATFORM & DUCT SUPPORTDepartment : Project Title : CHECK OF WELD : CHECK OF BEAM SEC.: BOLT DIMENSIONS: STRAINING ACTIONS: RUPTURE DUE TO TENSION : RUPTURE DUE TO SHEAR : EQUIVALENT RUPTURE : CONNECTION PROPERTIES: CHECK OF BOLTS:              22 teq 3qff      22 sh nNnQR 102
  • 105. Frame Station OutputCase CaseType StepType P V2 V3 Text m Text Text Text Tonf Tonf Tonf B‐054 0 ENV. Combination Min ‐0.5361 ‐0.3766 ‐0.4469 B‐077 0 ENV. Combination Max 4.1844 ‐0.3248 0.0367 2071SA 1.21 ENV. Combination Max ‐0.011 2.9635 0 Extrem out put reactions for IPE200 shear connection : 103
  • 106. ARESCO TEBBIN IPE200Sheet No. : Conn. No. : ton2.97Q = ton4.2N =cm.t10.395Mweld = IPE200GirderIPE200Beam mm L200Hg =mm200Hb = mm100Bg =mm100Bb = mm5.60Twg =mm5.60Twb = mm8.5Tfg =mm8.50Tfb = mm12r =mm12.00r = mm6Tplate = mm25B =mm35A = mm25C2 =mm25C1= OK200Check Dim. ( L )mm25E =mm50D = mm25Edge for N =mm25Edge for Q = 1NO.OF Sh. PLAN8.8mm Bolt Grade16BOLT DIA.(d) =3BOLT NO. (n) = 26.4Fyb =t/cm2 8Fub =cm2 1.57AS = t/cm2 2.4Fy =t/cm2 3.6Fu =37Steel Grade LINES2NO.OF W. L. =mm5S =Tmin.0.8Weld Size t/cm2 0.792Feq = 1.1 * Fweld=t/cm2 0.72Fweld = 0.2 * Fu= mm5.6tmin.=0.25K =0.6αN =0.6αQ = t/bolt1.94RbN.=αN*Fu*d*tmin.=t/bolt1.94RbQ.=αQ*Fu*d*tmin.=t/bolt3.14Rsh=KxFubxAs= ok0.75>1Long Joint F =t/bolt1.94Rleast = Safet/bolt1.94<t/bolt1.71 t/cm2 0.96qr =0.4Fy=cm2 4.48Ash.net = t/cm2 1.74Ftr = 0.725Fy =cm2 0.896At.net = Safeton2.97>ton5.86Qall=qr* Ash+Ftr*At= t/cm2 0.96qr =0.4Fy =cm2 0.896Ash.net = t/cm2 1.74Ftr = 0.725Fy =cm2 4.48At.net = Safeton4.2>ton8.66Qall=qr*Ash+Ftr*At= ton5.86<ton5.14Req1 =CHECK-1 Safe1<0.49Req2 =CHECK-2 cm3 21cm2 Zsec. =8.4Asec.= ton2.97cm.t Qsec. =10.4Msec.=ton4.2Nsec. = Safet/cm2 0.84<t/cm2 0.35q = Safet/cm2 1.4<t/cm2 1.00ft = SafeSafet/cm2 1.54<t/cm2 1.02feq. = cm4 319.42cm2 Iw =15.65Aw =cm15.65Lw = Safet/cm2 0.72<t/cm2 0.52ft =N/A+M*Y /I = Safet/cm2 0.72<t/cm2 0.19q = Q / A = SafeSafet/cm2 0.792<t/cm2 0.62 0.49Rup.2 Safe Ratio=0.88Rup.1 Safe Ratio=0.89Bolt Safe Ratio= 0.89Conn. Safe Ratio=0.78Weld Safe Ratio=0.66Sec. Safe Ratio= mm167X60X6PL.FINALLY USE : HSBB.T.8.8GRADE16M3 mm25B =mm35A =@ mm25C2 =mm25C1 = mm25E =mm50D = mm5Sw =Weld Lines2Tmin.0.8Weld Size Design of Shear Conn. Bearing Type According to ECP No.(205) Design Calculation Sheet asec MISR BANI SUEF COMPANY BOOSTER FAN PLATFORM & DUCT SUPPORTDepartment : Project Title : CHECK OF WELD : CHECK OF BEAM SEC.: BOLT DIMENSIONS: STRAINING ACTIONS: RUPTURE DUE TO TENSION : RUPTURE DUE TO SHEAR : EQUIVALENT RUPTURE : CONNECTION PROPERTIES: CHECK OF BOLTS:              22 teq 3qff      22 sh nNnQR 104
  • 107. Frame Station OutputCase CaseType StepType P V2 V3 Text m Text Text Text Tonf Tonf Tonf 2072SA 1.21 ENV. Combination Max 1.1188 3.9686 0.05 B‐007 2.24 ENV. Combination Min ‐0.5912 ‐0.8882 ‐1.4988 B‐007 2.24 ENV. Combination Max 2.2563 1.7524 0.7803 Extrem out put reactions for IPE240 shear connection: 105