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Beam Splice Conecction

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Project data
Project name
NLAREDO
Project number
Author EC
Description
Date 3/8/2023
Design code AISC 360-16

Material
Steel A36, A572 Gr.50

Project item CON2


Design
Name CON2
Description
Analysis Stress, strain/ simplified loading
Design code AISC - LRFD

Beams and columns

β– γ- α- Offset Offset Offset


Forces
Name Cross-section Direction Pitch Rotation ex ey ez
in
[°] [°] [°] [mm] [mm] [mm]
B1 5 - IR 800X250(I800) 0.0 0.0 0.0 0 0 0 Node
6 - IR
B2 180.0 0.0 0.0 0 0 0 Node
800X2502(I800)
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Cross-sections

Name Material
5 - IR 800X250(I800) A572 Gr.50
6 - IR 800X2502(I800) A572 Gr.50

Bolts

Diameter fu Gross area


Name Bolt assembly
[mm] [MPa] [mm2]
1 A325 1 A325 25 825.0 507

Load effects (equilibrium not required)

N Vy Vz Mx My Mz
Name Member
[kN] [kN] [kN] [kNm] [kNm] [kNm]
LE1 B1 8.9 0.0 -118.0 0.0 -549.0 0.0

Check
Summary

Name Value Check status


Analysis 100.0% OK
Plates 0.0 < 5.0% OK
Bolts 77.9 < 100% OK
Welds 75.1 < 100% OK
Buckling Not calculated

Plates

Fy Thickness σEd εPl σcEd


Name Loads Check status
[MPa] [mm] [MPa] [%] [MPa]
B1-bfl 1 344.7 8.0 LE1 310.3 0.0 0.0 OK
B1-tfl 1 344.7 8.0 LE1 308.0 0.0 0.0 OK
B1-w 1 344.7 6.3 LE1 289.8 0.0 0.0 OK
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B2-bfl 1 344.7 8.0 LE1 310.3 0.0 0.0 OK
B2-tfl 1 344.7 8.0 LE1 256.3 0.0 0.0 OK
B2-w 1 344.7 6.3 LE1 239.8 0.0 0.0 OK
PP1a 344.7 19.1 LE1 310.3 0.0 28.0 OK
PP1b 344.7 19.1 LE1 310.3 0.0 28.0 OK

Design data

fy εlim
Material
[MPa] [%]
A572 Gr.50 344.7 5.0

Symbol explanation

εPl Plastic strain


σcEd Contact stress
σEd Eq. stress
fy Yield strength
εlim Limit of plastic strain

Overall check, LE1


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Strain check, LE1

Equivalent stress, LE1

Bolts

Shape Item Grade Loads Ft V ϕRn,bearing Utt Uts Utts Status


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[kN] [kN] [kN] [%] [%] [%]
B1 1 A325 - 1 LE1 0.0 8.8 390.3 0.0 6.2 - OK
B2 1 A325 - 1 LE1 0.0 8.8 390.3 0.0 6.2 - OK
B3 1 A325 - 1 LE1 1.1 7.2 275.5 0.5 5.1 - OK
B4 1 A325 - 1 LE1 1.1 7.2 275.4 0.5 5.1 - OK
B5 1 A325 - 1 LE1 0.3 9.8 390.3 0.1 6.9 - OK
B6 1 A325 - 1 LE1 0.3 9.8 390.3 0.1 6.9 - OK
B7 1 A325 - 1 LE1 183.6 8.4 390.3 77.9 6.0 - OK
B8 1 A325 - 1 LE1 183.6 8.4 390.3 77.9 6.0 - OK
B9 1 A325 - 1 LE1 148.9 7.3 274.6 63.2 5.1 - OK
B10 1 A325 - 1 LE1 148.8 7.3 274.5 63.2 5.1 - OK
B11 1 A325 - 1 LE1 94.4 10.2 390.3 40.1 7.2 - OK
B12 1 A325 - 1 LE1 94.5 10.2 390.3 40.1 7.2 - OK
B13 1 A325 - 1 LE1 1.3 7.4 274.4 0.5 5.2 - OK
B14 1 A325 - 1 LE1 142.6 7.2 274.4 60.5 5.1 - OK

Design data

ϕRn,tension ϕRn,shear
Grade
[kN] [kN]
1 A325 - 1 235.6 141.4

Symbol explanation

Ft Tension force
V Resultant of shear forces Vy, Vz in bolt
ϕRn,bearing Bolt bearing resistance
Utt Utilization in tension
Uts Utilization in shear
Utts Utilization in tension and shear
ϕRn,tension Bolt tension resistance AISC 360-16 J3.6
ϕRn,shear Bolt shear resistance AISC 360-16 – J3.8

Welds

Th Ls L Lc Fn ϕRn Ut
Item Edge Xu Loads Status
[mm] [mm] [mm] [mm] [kN] [kN] [%]
PP1a B1-bfl 1 E70xx - - 250 - - - - - OK
PP1a B1-tfl 1 E70xx - - 250 - - - - - OK
PP1a B1-w 1 E70xx ◢5.6◣ ◢7.9◣ 790 49 LE1 67.6 90.1 75.1 OK
E70xx ◢5.6◣ ◢7.9◣ 790 49 LE1 67.6 90.1 75.1 OK
PP1b B2-bfl 1 E70xx - - 250 - - - - - OK
PP1b B2-tfl 1 E70xx - - 250 - - - - - OK
PP1b B2-w 1 E70xx ◢5.6◣ ◢7.9◣ 790 49 LE1 67.8 90.3 75.1 OK
E70xx ◢5.6◣ ◢7.9◣ 790 49 LE1 67.8 90.3 75.1 OK

Symbol explanation

Th Throat thickness of weld


Ls Leg size of weld
L Length of weld
Lc Length of weld critical element
Fn Force in weld critical element
ϕRn Weld resistance AISC 360-16 J2.4
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Ut Utilization

Buckling

Buckling analysis was not calculated.

Code settings
Item Value Unit Reference
Friction coefficient - concrete 0.40 - ACI 349 – B.6.1.4
Friction coefficient in slip-resistance 0.30 - AISC 360-16 J3.8
Limit plastic strain 0.05 -
Plastic
Weld stress evaluation
redistribution
Detailing No
Distance between bolts [d] 2.66 - AISC 360-16 – J3.3
Distance between bolts and edge [d] 1.25 - AISC 360-16 – J.3.4
Concrete breakout resistance check Both
Base metal capacity check at weld
No AISC 360-16: J2-2
fusion face
Cracked concrete Yes ACI 318-14 – Chapter 17
Local deformation check No
Local deformation limit 0.03 - CIDECT DG 1, 3 - 1.1
Analysis with large deformations for hollow
Geometrical nonlinearity (GMNA) Yes
section joints

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