2. Problem 2

For the Front Landing Gear Module, it is specified that a spring is required to soften the wheel forces

transmitted to the aircraft.

The only location for this spring has been identified as indicated in green in Figure 4 with the following

restriction and conditions:

SEE DETAIL A-

Static Length (L)

Minimum Length (L_min)

80mm

30 mm

20

DETAIL A

SCALE 1:1

Figure 4: Front Landing Gear Module Spring Position

a. Design a suitable spring which is able to cater for all loading conditions.