What are the major components of landing gear?
A Landing Gear system comprises of many structural and system components. The structural components include Main fitting, Shock absorber, Bogie beam/ Trailing arm, Axle, Torque links, Drag/ Side braces, Retraction actuator, Down lock mechanism, Up lock, Wheel, Tire etc. The Main Landing Gear is an aircraft’s principal landing gear system component. It is located beneath the aircraft’s wings or fuselage and is designed to support the majority of the weight of the aircraft.aircraft landing gear is the undercarriage of an aircraft, used for takeoff, landing, and taxiing. It typically includes wheels, struts, brakes, and sometimes skids or floats. There are two main types: tricycle gear, with a nose wheel and two main wheels, and tailwheel gear, with a rear wheel or skid.
What are two different configurations of landing gear?
There are two main types: tricycle gear, with a nose wheel and two main wheels, and tailwheel gear, with a rear wheel or skid. Landing gear can be fixed or retractable, enhancing aerodynamics during flight. Main gear Airbus 320 Each of the two main landing gear assemblies consists of a conventional two wheel direct type with an integral shock absorber supported in the fore and aft direction by a fixed drag strut and laterally by a folding strut mechanically locked when in the DOWN position.
What materials are used in landing gears?
Landing gear cylinders and main axles are commonly made from high-strength low alloy steels, but the cylinders are also made from high-strength aluminium alloys. M steel is widely used for high stress aircraft landing gears and structures; however, this steel is not corrosion-resistant and requires protective coatings.