An aircraft component has an ultimate load of 5.28 kN and a limit load of 1.32 kN. What is its safety factor?
The safety factor is calculated by dividing the ultimate load by the limit load:
Safety Factor = Ultimate Load / Limit Load
Safety Factor = 5.28 kN / 1.32 kN = 4
Therefore, the safety factor of the aircraft component is 4.
An aircraft component has an ultimate load of 5.28 kN and a limit load of 1.32 kN. What is its safety factor?
Based on this safety factor, do you think it was designed using a fail-safe philosophy or a safe-life philosophy?
To calculate the safety factor of an aircraft component, we need to divide the ultimate load by the limit load.
Safety Factor = Ultimate Load / Limit Load
Given:
Ultimate Load = 5.28 kN
Limit Load = 1.32 kN
Safety Factor = 5.28 kN / 1.32 kN
Now, let's perform the calculation:
Safety Factor = 4
Therefore, the safety factor of the aircraft component is 4.
To find the safety factor of an aircraft component, you need to divide the ultimate load by the limit load. In this case, the ultimate load is 5.28 kN and the limit load is 1.32 kN.
Safety Factor = Ultimate Load / Limit Load
Substituting the given values:
Safety Factor = 5.28 kN / 1.32 kN
Now perform the division:
Safety Factor = 4
Therefore, the safety factor of the aircraft component is 4.