A small unmanned plane undercarriage buffer relates to the field of
aviation aircrafts and solves problems of low buffering efficiency, easy bounce, low reliability of a present flat spring type buffer. The small unmanned plane undercarriage buffer comprises an external cylinder, a first spring on the external cylinder, an internal cylinder having a damping hole, an air sac between the external cylinder and the internal cylinder; an
upper joint, a lower joint, a
piston rod extending into the internal cylinder, a
piston, a damping plate, a pressure-limiting valve, a
check valve, a guide sleeve and a locking cover, wherein the
piston rod is orderly covered with the piston, the damping plate and the pressure-limiting plate; the
piston rod is orderly covered with the
check valve, the guide sleeve and the locking cover; the
check valve, the guide sleeve and the locking cover are all disposed in the external cylinder; an internal-external cylinder annular
oil storage cavity is formed between the internal cylinder and the external cylinder; the damping plate axially moves along the
piston rod; the pressure-limiting plate limits maximum damping force to a preset valve during compression
stroke; after the locking cover is tightly screwed, the guide sleeve, the check valve and the internal cylinder are axially pressed to the lower joint; the check valve controls communication between the internal-external cylinder annular
oil storage cavity and a right cavity of the internal cylinder; and two ends of a first spring are respectively pressed against the upper and lower joints. The small unmanned plane undercarriage buffer possesses high buffering efficiency, uneasy bounce, stable performance and great reliability.