The utility model relates to the technical field of
landing gear, concretely relates to a
landing gear damping mechanism. It includes stand, crossbeam, wheel frame and sets up the damping component between stand and crossbeam, and the damping component is constituted by outer tube,
piston rod,
piston head,
honeycomb aluminium energy absorption module group and disc spring bag etc.
Honeycomb aluminium energy absorption module group is at least two
layers along the axial direction and is equipped with deformation joint between
layers, and
honeycomb aluminium energy absorption module group, disc spring bag and
piston rod are arranged in outer tube from top to bottom, and the conical force transmission rod of
piston rod top inserts the central hole of
honeycomb aluminium energy absorption module group and forms the
conical surface cooperation. The
landing gear adopts the "hydraulic damping-honeycomb aluminium-disc spring" compound damping structure, and through honeycomb aluminium graded energy absorption, disc spring nonlinear elasticity and friction damping, hydraulic damping
medium energy dissipation, effectively solve the problem of traditional landing gear energy
absorption efficiency low,
high frequency vibration attenuation deficiency,
heavy load impact load concentration etc., and is suitable for
high frequency impact and concentrated load working condition, and the damping effect is good.