MLG SHOCK ABSORBER
The main landing gear shock absorber is a component of an aircraft's landing gear system that is designed to absorb the impact of landing and cushion the aircraft as it touches down on the runway. The shock absorber is typically located at the point where the landing gear strut attaches to the aircraft's fuselage.
The shock absorber is typically composed of a piston and cylinder filled with hydraulic fluid. When the aircraft lands, the weight of the aircraft compresses the piston, causing the hydraulic fluid to flow through small orifices and slow the movement of the piston. This action dissipates the kinetic energy of the landing, allowing the aircraft to touch down safely and smoothly.
The design of the main landing gear shock absorber is critical to the safe operation of an aircraft, as it must be able to withstand the stresses of landing and takeoff, as well as various loads and shocks that can occur during ground operations.
The shock absorber is typically located between the wheel and the aircraft structure, and it can be designed using a variety of mechanisms such as hydraulic or pneumatic systems, as well as springs or other materials that can absorb energy.
The main landing gear shock absorber is an important safety feature in aviation because it helps to ensure that the aircraft is able to land smoothly and safely, even when faced with a bumpy or uneven runway surface. Proper maintenance and replacement of the shock absorber is essential to maintain the safety and performance of an aircraft's landing gear system.
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