Abstract: The landing gear system is of paramount importance during ground operations and take-off procedures, as it bears the brunt of the aircraft's weight and forces during these critical phases. It is clear that landing gear issues account for a sizable percentage of aircraft structural failures.
The landing gear must be able to endure side loads, compression loads, and drag loads during landing and takeoff. The magnitudes of drag and side loads are relatively smaller, even if compressive loads predominate. Because of this, landing gear is usually considered a one-dimensional construction. Its main purpose is to absorb the energy produced during landing and lessen the force applied to the aircraft's frame.
The oleo pneumatic landing gear strut is frequently the recommended landing gear arrangement for larger aircraft. Its capacity to efficiently absorb and release kinetic energy throughout the landing process is a crucial design requirement in addition to static strength considerations. Next, we use CATIA to build an aircraft's conventional landing gear and Auto Desk Innovator to assess its structural protection.
AUTO DESK INVENTOR tools are used to study landing gear assembly for different metal alloys and composite materials.
Estimation of aircraft landing gear linear stresses and deformation and analysis on main landing gear as well as the nose landing gear of an aircraft by linear static structural analysis are accomplished by importing the model landing gear into the AUTO DESK INVENTOR programme.
AUTO DESK INVENTOR tools are used to study landing gear assembly for different metal alloys and composite materials. Estimation of aircraft landing gear linear stresses and deformation and analysis on main landing gear as well as the nose landing gear of an aircraft by linear static structural analysis are accomplished by importing the model landing gear into the AUTO DESK INVENTOR programme
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