You have been tasked with designing a beam to support a lifting crane. The applied load is offset from the centre of the carriage used to mount the crane to the overhead beam. Therefore, the loads applied to the two axels, P₁ and P₂, differ. The position of the crane can vary (dependent on the variable, x, shown below). Example of a lifting crane Sall Image courtesy of dzwignice.info Material Properties (Beam A-B) Value Symbol Units E 69.0 GPa 0.28 N/A 7.19 Mg/m³ 330.0 MPa 110.0 MPa V PRALEX P Gallow Tallow A O x Structural idealisation -1.5m->> 4m- P2 Loads P₁ = 4kN P₂ = 1.5kN OB

Structural Analysis
6th Edition
ISBN:9781337630931
Author:KASSIMALI, Aslam.
Publisher:KASSIMALI, Aslam.
Chapter2: Loads On Structures
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You have been tasked with designing a beam to support a lifting crane. The applied load is offset
from the centre of the carriage used to mount the crane to the overhead beam. Therefore, the loads
applied to the two axels, P₁ and P₂, differ. The position of the crane can vary (dependent on the
variable, x, shown below).
Example of a lifting crane
FRIALEX
Image courtesy of dzwignice.info
Material Properties (Beam A-B)
Value
Units
69.0
GPa
0.28
N/A
7.19
Mg/m³
330.0
MPa
110.0
MPa
Symbol
E
V
P
Jallow
Tallow
A O
x
Structural idealisation
P2
P₁
1.5m →
4m.
Loads
P₁ = 4kN
P2 = 1.5kN
OB
Determine the required section modulus, S, of the beam based on the material properties
and the maximum bending moment.
Note: the section modulus S = =-=
y
Transcribed Image Text:You have been tasked with designing a beam to support a lifting crane. The applied load is offset from the centre of the carriage used to mount the crane to the overhead beam. Therefore, the loads applied to the two axels, P₁ and P₂, differ. The position of the crane can vary (dependent on the variable, x, shown below). Example of a lifting crane FRIALEX Image courtesy of dzwignice.info Material Properties (Beam A-B) Value Units 69.0 GPa 0.28 N/A 7.19 Mg/m³ 330.0 MPa 110.0 MPa Symbol E V P Jallow Tallow A O x Structural idealisation P2 P₁ 1.5m → 4m. Loads P₁ = 4kN P2 = 1.5kN OB Determine the required section modulus, S, of the beam based on the material properties and the maximum bending moment. Note: the section modulus S = =-= y
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