[abstract] the aircraft in takeoff and landing grounding and ground motion of time, can produce larger impact load. In order to link. In the landing gear design process, researchers in addition to consider in the plane of gear static force outside, still need to consider in the take-off and landing stage dynamic performance. Landing gear in aircraft takeoff and landing grounding and ground motion should be able to withstand the big sports load and slow down this impact, so as to improve passenger comfort and safety.
Modern aircraft landing gear is by structure, institutions and various system composed of complex mechanical device, including the damping system, force the prop, the poles, wheel, brake and anti-skidding control system, ShouFangJi constitutive, electrical system, hydraulic system and some other systems and devices. Therefore landing gear design than aircraft structure design of the other components to include more engineering.
According to the basic structure of landing gear with airbus-a320 aircraft landing gear for object, analyses its A320 landing gear function principle and take or leave exercise; At the same time to its hydraulic system and the damping system have also made the correlation analysis, through which to landing gear was studied and discussed.
Keywords: gear, A320, And hoisting system; Hydraulic system; Damping system
Aircraft in takeoff and landing grounding and ground motion of time, can produce larger impact load. In order to link. In the landing gear design process, researchers in addition to consider in the plane of gear static force outside, still need to consider in the take-off and landing stage dynamic performance. Landing gear in aircraft takeoff and landing grounding and ground motion should be able to withstand the big sports load and slow down this impact, so as to improve passenger comfort and safety.
Modern aircraft landing gear is by structure, institutions and various system composed of complex mechanical device, including the damping system, force the prop, the poles, wheel, brake and anti-skidding control system, ShouFangJi constitutive, electrical system, hydraulic system and some other systems and devices. Therefore landing gear design than aircraft structure design of the other components to include more engineering.
According to the basic structure of landing gear with airbus-a320 aircraft landing gear for object, analyses its A320 landing gear function principle and take or leave exercise; At the same time to its hydraulic system and the damping system have also made the correlation analysis, through which to landing gear was studied and discussed.