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Column To Rafter Connection

The document describes a structural engineering project including a column to rafter connection. It provides details on the project, materials, cross sections, loads, stress calculations, and design checks for various structural components. The analyses ensure the design meets standards and requirements.

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kheang amg
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0% found this document useful (0 votes)
155 views15 pages

Column To Rafter Connection

The document describes a structural engineering project including a column to rafter connection. It provides details on the project, materials, cross sections, loads, stress calculations, and design checks for various structural components. The analyses ensure the design meets standards and requirements.

Uploaded by

kheang amg
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
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Project:

Project no:
Author:

Project data
Project name
Project number
Author
Description
Date 04-Nov-23
Design code EN

Material
Steel S 355, S 235
Concrete C25/30

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Project item Column to rafter connection

Design
Name Column to rafter connection
Description
Analysis Stress, strain/ simplified loading

Beams and columns


β– γ- α- Offset Offset Offset
Name Cross-section Direction Pitch Rotation ex ey ez Forces in
[°] [°] [°] [mm] [mm] [mm]
10 -
Main T 0.0 -30.0 0.0 0 0 0 Node
BoxFl100x(50/50)
2-
I150x75x5x7 90.0 90.0 90.0 0 0 0 Node
I150x75x5x7(I150)
10 -
ST1 90.0 27.0 -28.0 0 -100 0 Node
BoxFl100x(50/50)
10 -
ST2 -90.0 27.0 28.0 0 100 0 Node
BoxFl100x(50/50)

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Cross-sections
Name Material
10 - BoxFl100x(50/50) S 235
2 - I150x75x5x7(I150) S 235

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Cross-sections
Name Material Drawing

10 - BoxFl100x(50/50) S 235

2 - I150x75x5x7(I150) S 235

Load effects (equilibrium not required)


N Vy Vz Mx My Mz
Name Member
[kN] [kN] [kN] [kNm] [kNm] [kNm]
LE1 Main T -5.6 0.0 -2.6 0.0 0.0 0.0
Main T 0.0 0.0 0.0 0.0 1.0 0.0
ST1 -0.5 -0.5 -2.0 0.0 1.0 0.0
ST2 -0.9 -0.5 -3.8 0.0 1.0 0.0

Check

Summary
Name Value Status
Analysis 100.0% OK
Plates 0.0 < 5.0% OK
Welds 98.3 < 100% OK
Buckling Not calculated

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Plates
Thickness σEd εPl σcEd
Name Loads Status
[mm] [MPa] [%] [MPa]
Main T-tfl 1 2.5 LE1 100.3 0.0 0.0 OK
Main T-bfl 1 2.5 LE1 140.0 0.0 0.0 OK
Main T-w 1 2.5 LE1 166.9 0.0 0.0 OK
Main T-w 2 2.5 LE1 105.1 0.0 0.0 OK
I150x75x5x7-bfl 1 7.0 LE1 53.5 0.0 0.0 OK
I150x75x5x7-tfl 1 7.0 LE1 62.2 0.0 0.0 OK
I150x75x5x7-w 1 5.0 LE1 24.3 0.0 0.0 OK
ST1-tfl 1 2.5 LE1 155.5 0.0 0.0 OK
ST1-bfl 1 2.5 LE1 48.3 0.0 0.0 OK
ST1-w 1 2.5 LE1 127.5 0.0 0.0 OK
ST1-w 2 2.5 LE1 123.6 0.0 0.0 OK
ST2-tfl 1 2.5 LE1 150.2 0.0 0.0 OK
ST2-bfl 1 2.5 LE1 38.1 0.0 0.0 OK
ST2-w 1 2.5 LE1 146.2 0.0 0.0 OK
ST2-w 2 2.5 LE1 113.5 0.0 0.0 OK

Design data
fy εlim
Material
[MPa] [%]
S 235 235.0 5.0

Overall check, LE1

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Strain check, LE1

Equivalent stress, LE1

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Welds (Plastic redistribution)


Throat σ⏊ τ⏊
Length σw,Ed εPl τ|| Ut Utc
Item Edge th. Loads Status
[mm] [MPa] [%] [MPa] [MPa] [MPa] [%] [%]
[mm]
Main T-w 2 ST1-tfl 1 2.5 51 LE1 OK
Main T-w 1 ST2-tfl 1 2.5 51 LE1 OK
Main T-bfl I150x75x5x7-bfl
◢3.0◣ 50 LE1 98.9 0.0 56.1 12.2 45.4 27.5 14.8 OK
1 1
◢3.0◣ 50 LE1 171.4 0.0 47.9 27.9 -90.8 47.6 23.9 OK
Main T-bfl
I150x75x5x7-tfl 1 ◢3.0◣ 50 LE1 130.8 0.0 -66.8 17.3 -62.6 36.3 16.4 OK
1
◢3.0◣ 50 LE1 229.8 0.0 -84.7 -47.5 113.8 63.8 26.2 OK
Main T-bfl
I150x75x5x7-w 1 ◢3.0◣ 165 LE1 30.8 0.0 16.3 0.3 15.1 8.6 2.6 OK
1
◢3.0◣ 165 LE1 39.9 0.0 18.9 3.3 -20.0 11.1 3.2 OK
Main T-w 2 ST1-w 1 ◢3.0 91 LE1 353.3 0.3 -210.0 19.2 -162.9 98.1 24.7 OK
Main T-w 2 ST1-w 2 ◢3.0 90 LE1 353.9 0.8 -137.6 -27.4 186.2 98.3 26.5 OK
Main T-w 1 ST2-w 1 ◢3.0 90 LE1 353.9 0.7 -166.4 36.3 -176.6 98.3 25.3 OK
Main T-w 1 ST2-w 2 ◢3.0 91 LE1 353.4 0.4 -195.5 -26.5 167.9 98.2 23.1 OK

Design data

βw σw,Rd 0.9 σ
[-] [MPa] [MPa]
S 235 0.80 360.0 259.2

Detailed result for Main T-w 2 ST1-tfl 1

Butt welds are assumed as full penetration and are not checked. Their resistance is assumed the same as that of the welded
member -EN 1993 - 1 - 8 - 4.7.1.

Detailed result for Main T-w 1 ST2-tfl 1

Butt welds are assumed as full penetration and are not checked. Their resistance is assumed the same as that of the welded
member -EN 1993 - 1 - 8 - 4.7.1.

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Detailed result for Main T-bfl 1 I150x75x5x7-bfl 1


Weld resistance check (EN 1993-1-8 4.5.3.2)

σw,Rd = fu /(βw γM 2 ) = 2 + 3(τ 2 + τ 2 )]0.5 =


σw,Ed = [σ⊥
​ ​ ​ ​
360.0 MPa ≥ ​


∥ ​ ​
98.9 MPa

σ⊥,Rd = 0.9fu /γM 2 =


​ ​ ​
259.2 MPa ≥ ∣σ⊥ ∣ =

56.1 MPa

where:
fu = 360.0 MPa – Ultimate strength

βw = 0.80
​ – appropriate correlation factor taken from Table 4.1

γM 2 = 1.25 ​ – Safety factor

Stress utilization
∣σ⊥ ∣
Ut = max( σσw,Ed

w,Rd
; ​


σ⊥,Rd


​ )= 27.5 %

Weld resistance check (EN 1993-1-8 4.5.3.2)

σw,Rd = fu /(βw γM 2 ) = 2 + 3(τ 2 + τ 2 )]0.5 =


σw,Ed = [σ⊥
​ ​ ​ ​
360.0 MPa ≥ ​


∥ ​ ​
171.4 MPa

σ⊥,Rd = 0.9fu /γM 2 =


​ ​ ​
259.2 MPa ≥ ∣σ⊥ ∣ =

47.9 MPa

where:
fu = 360.0 MPa – Ultimate strength

βw = 0.80
​ – appropriate correlation factor taken from Table 4.1

γM 2 = 1.25 ​ – Safety factor

Stress utilization
∣σ⊥ ∣
Ut = max( σσw,Ed

w,Rd
; ​


σ⊥,Rd


​ )= 47.6 %

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Detailed result for Main T-bfl 1 I150x75x5x7-tfl 1


Weld resistance check (EN 1993-1-8 4.5.3.2)

σw,Rd = fu /(βw γM 2 ) = 2 + 3(τ 2 + τ 2 )]0.5 =


σw,Ed = [σ⊥
​ ​ ​ ​
360.0 MPa ≥ ​


∥ ​ ​
130.8 MPa

σ⊥,Rd = 0.9fu /γM 2 =


​ ​ ​
259.2 MPa ≥ ∣σ⊥ ∣ =

66.8 MPa

where:
fu = 360.0 MPa – Ultimate strength

βw = 0.80
​ – appropriate correlation factor taken from Table 4.1

γM 2 = 1.25 ​ – Safety factor

Stress utilization
∣σ⊥ ∣
Ut = max( σσw,Ed

w,Rd
; ​


σ⊥,Rd


​ )= 36.3 %

Weld resistance check (EN 1993-1-8 4.5.3.2)

σw,Rd = fu /(βw γM 2 ) = 2 + 3(τ 2 + τ 2 )]0.5 =


σw,Ed = [σ⊥
​ ​ ​ ​
360.0 MPa ≥ ​


∥ ​ ​
229.8 MPa

σ⊥,Rd = 0.9fu /γM 2 =


​ ​ ​
259.2 MPa ≥ ∣σ⊥ ∣ =

84.7 MPa

where:
fu = 360.0 MPa – Ultimate strength

βw = 0.80
​ – appropriate correlation factor taken from Table 4.1
γM 2 = 1.25 ​ – Safety factor

Stress utilization
∣σ⊥ ∣
Ut = max( σσw,Ed

w,Rd
; ​


σ⊥,Rd


​ )= 63.8 %

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Detailed result for Main T-bfl 1 I150x75x5x7-w 1


Weld resistance check (EN 1993-1-8 4.5.3.2)

σw,Rd = fu /(βw γM 2 ) = 2 + 3(τ 2 + τ 2 )]0.5 =


σw,Ed = [σ⊥
​ ​ ​ ​
360.0 MPa ≥ ​


∥ ​ ​
30.8 MPa

σ⊥,Rd = 0.9fu /γM 2 =


​ ​ ​
259.2 MPa ≥ ∣σ⊥ ∣ =

16.3 MPa

where:
fu = 360.0 MPa – Ultimate strength

βw = 0.80
​ – appropriate correlation factor taken from Table 4.1

γM 2 = 1.25 ​ – Safety factor

Stress utilization
∣σ⊥ ∣
Ut = max( σσw,Ed

w,Rd
; ​


σ⊥,Rd


​ )= 8.6 %

Weld resistance check (EN 1993-1-8 4.5.3.2)

σw,Rd = fu /(βw γM 2 ) = 2 + 3(τ 2 + τ 2 )]0.5 =


σw,Ed = [σ⊥
​ ​ ​ ​
360.0 MPa ≥ ​


∥ ​ ​
39.9 MPa

σ⊥,Rd = 0.9fu /γM 2 =


​ ​ ​
259.2 MPa ≥ ∣σ⊥ ∣ =

18.9 MPa

where:
fu = 360.0 MPa – Ultimate strength

βw = 0.80
​ – appropriate correlation factor taken from Table 4.1

γM 2 = 1.25 ​ – Safety factor

Stress utilization
∣σ⊥ ∣
Ut = max( σσw,Ed

w,Rd
; ​


σ⊥,Rd


​ )= 11.1 %

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Detailed result for Main T-w 2 ST1-w 1


Weld resistance check (EN 1993-1-8 4.5.3.2)

σw,Rd = fu /(βw γM 2 ) = 2 + 3(τ 2 + τ 2 )]0.5 =


σw,Ed = [σ⊥
​ ​ ​ ​
360.0 MPa ≥ ​ ​

⊥ ∥​ ​
353.3 MPa

σ⊥,Rd = 0.9fu /γM 2 =


​ ​ ​
259.2 MPa ≥ ∣σ⊥ ∣ =

210.0 MPa

where:
fu = 360.0 MPa – Ultimate strength

βw = 0.80
​ – appropriate correlation factor taken from Table 4.1
γM 2 = 1.25 ​ – Safety factor

Stress utilization
∣σ⊥ ∣
Ut = max( σσw,Ed

w,Rd
; ​


σ⊥,Rd


​ )= 98.1 %

Detailed result for Main T-w 2 ST1-w 2


Weld resistance check (EN 1993-1-8 4.5.3.2)

σw,Rd = fu /(βw γM 2 ) = 2 + 3(τ 2 + τ 2 )]0.5 =


σw,Ed = [σ⊥
​ ​ ​ ​
360.0 MPa ≥ ​ ​

⊥ ∥​ ​
353.9 MPa

σ⊥,Rd = 0.9fu /γM 2 =


​ ​ ​
259.2 MPa ≥ ∣σ⊥ ∣ =

137.6 MPa

where:
fu = 360.0 MPa – Ultimate strength

βw = 0.80
​ – appropriate correlation factor taken from Table 4.1

γM 2 = 1.25 ​ – Safety factor

Stress utilization
∣σ⊥ ∣
Ut = max( σσw,Ed

w,Rd
; ​


σ⊥,Rd


​ )= 98.3 %

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Detailed result for Main T-w 1 ST2-w 1


Weld resistance check (EN 1993-1-8 4.5.3.2)

σw,Rd = fu /(βw γM 2 ) = 2 + 3(τ 2 + τ 2 )]0.5 =


σw,Ed = [σ⊥
​ ​ ​ ​
360.0 MPa ≥ ​ ​

⊥ ∥​ ​
353.9 MPa

σ⊥,Rd = 0.9fu /γM 2 =


​ ​ ​
259.2 MPa ≥ ∣σ⊥ ∣ =

166.4 MPa

where:
fu = 360.0 MPa – Ultimate strength

βw = 0.80
​ – appropriate correlation factor taken from Table 4.1

γM 2 = 1.25 ​ – Safety factor

Stress utilization
∣σ⊥ ∣
Ut = max( σσw,Ed

w,Rd
; ​


σ⊥,Rd


​ )= 98.3 %

Detailed result for Main T-w 1 ST2-w 2


Weld resistance check (EN 1993-1-8 4.5.3.2)

σw,Rd = fu /(βw γM 2 ) = 2 + 3(τ 2 + τ 2 )]0.5 =


σw,Ed = [σ⊥
​ ​ ​ ​
360.0 MPa ≥ ​ ​

⊥ ∥​ ​
353.4 MPa

σ⊥,Rd = 0.9fu /γM 2 =


​ ​ ​
259.2 MPa ≥ ∣σ⊥ ∣ =

195.5 MPa

where:
fu = 360.0 MPa – Ultimate strength

βw = 0.80
​ – appropriate correlation factor taken from Table 4.1
γM 2 = 1.25 ​ – Safety factor

Stress utilization
∣σ⊥ ∣
Ut = max( σσw,Ed

w,Rd
; ​


σ⊥,Rd


​ )= 98.2 %

Buckling
Buckling analysis was not calculated.

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Bill of material

Manufacturing operations
Plates Welds Length
Name Shape Nr. Bolts Nr.
[mm] [mm] [mm]
CUT1 Double fillet: a = 3.0 265.1
Butt: a = 2.5 51.4
CUT2 Fillet: a = 3.0 90.5
Fillet: a = 3.0 89.8
Butt: a = 2.5 51.4
CUT3 Fillet: a = 3.0 89.8
Fillet: a = 3.0 90.5

Welds
Throat thickness Leg size Length
Type Material
[mm] [mm] [mm]
Double fillet S 235 3.0 4.2 265.1
Butt S 235 - - 102.8
Fillet S 235 3.0 4.2 180.3
Fillet S 235 3.0 4.2 180.3

Symbol explanation
Symbol Symbol explanation
εPl Strain
σEd Eq. stress
fy Yield strength
εlim Limit of plastic strain
σw,Ed Equivalent stress
σw,Rd Equivalent stress resistance
σ⏊ Perpendicular stress
τ|| Shear stress parallel to weld axis
τ⏊ Shear stress perpendicular to weld axis
0.9 σw,Rd Perpendicular stress resistance - 0.9*fu/γM2
βw Corelation factor EN 1993-1-8 tab. 4.1
Ut Utilization
Utc Weld capacity utilization

Code settings
Item Value Unit Reference
γM0 1.00 - EN 1993-1-1: 6.1
γM1 1.00 - EN 1993-1-1: 6.1
γM2 1.25 - EN 1993-1-1: 6.1
γM3 1.25 - EN 1993-1-8: 2.2

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Item Value Unit Reference


γC 1.50 - EN 1992-1-1: 2.4.2.4
γInst 1.20 - EN 1992-4: Table 4.1
Joint coefficient βj 0.67 - EN 1993-1-8: 6.2.5
Effective area - influence of mesh size 0.10 -
Friction coefficient - concrete 0.25 - EN 1993-1-8
Friction coefficient in slip-resistance 0.30 - EN 1993-1-8 tab 3.7
Limit plastic strain 0.05 - EN 1993-1-5
Weld stress evaluation Plastic redistribution
Detailing No
Distance between bolts [d] 2.20 - EN 1993-1-8: tab 3.3
Distance between bolts and edge [d] 1.20 - EN 1993-1-8: tab 3.3
Concrete breakout resistance check Both EN 1992-4: 7.2.1.4 and 7.2.2.5
Use calculated αb in bearing check. Yes EN 1993-1-8: tab 3.4
Cracked concrete Yes EN 1992-4
Local deformation check No CIDECT DG 1, 3 - 1.1
Local deformation limit 0.03 - CIDECT DG 1, 3 - 1.1
Geometrical nonlinearity (GMNA) Yes Analysis with large deformations for hollow section joints
Braced system No EN 1993-1-8: 5.2.2.5

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