in house assessment mechanica figure 1 ac 101 aircraft design the ac 1
In House Assessment- Mechanica
Figure 1: AC-101 Aircraft Design
The AC-101 aircraft has been developed as a multi-purpose aircraft with the following specifications:
Maximum Take-Off Weight
Maximum Take-off Roll
Maximum Deceleration under Braking
Minimum Landing Roll
Maximum Structural Loading
i. Wheel locations
ii. Wheel installation and fixation arrangement
iii. Suitable bearing arrangement
1. Problem 1
aircraft consists of a standard tricycle landing gear arrangement for which the front landing gear
needs to be detailed.
on the layout given in Figure 2, determine:
a. The maximum load on the front landing gear module.
b. A suitable diameter and material for the Front Landing Gear Axle.
Given the Wheels specified in Figure 3, propose a suitable design for the axle. Include at
least the following:
Figure 2: AC-101 Landing Gear Arrangement
Aluminium hub rubber wheels
New Aluminium hub rubber wheel
5.00 - AL
CNC Aluminium hub rubber wheels
Figure 3: Front Wheel Specification
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