The utility model relates to the technical field of
aircraft landing gears, in particular to a damping mechanism for a main
landing gear of a light aircraft, which comprises a
landing gear, aircraft wheels, a connecting rod, a vertical
damper and the like. The undercarriage is composed of two supporting frames in
bilateral symmetry, the left supporting frame and the right supporting frame are in transverse sliding connection through a middle sliding rail, vertical shock absorbers are symmetrically arranged in the rear side of the undercarriage, and each vertical
shock absorber is composed of a fixed end, a movable end and a spring. After the
airplane wheels are in contact with the ground, pressure is applied to the vertical shock absorbers through the connecting rods, springs of the vertical shock absorbers deform, meanwhile, the connecting rods rotate, accordingly, the oblique shock absorbers are driven to move downwards through the
kidney-shaped grooves, springs of the oblique shock absorbers deform, and therefore the
airplane wheels are driven to move downwards. Through cooperation of the vertical shock absorbers and the inclined shock absorbers,
vertical force and inclined force generated when an aircraft slides can be effectively decomposed and absorbed, the shock
absorption effect is optimized, the stability of the undercarriage is improved, and the stable posture of the aircraft on the ground is ensured.