Unmanned aerial vehicle landing buffer system

The utility model provides an unmanned aerial vehicle landing buffer system, sets up at the same left landing buffer gear and right landing buffer gear of organism both sides structure including the symmetry, and among the right landing buffer gear, fixing support fixes respectively on the organism, is favorable to the ground load of diffuse transmission to fuselage, oil gas formula buffer and vaulting pole pass through universal joint to be connected with fixing support, and the rotation of release junction retrains, avoids the skid to produce the jamming at the slip in -process, during aircraft landing, the skid slides towards aircraft wing point direction, and compression oil gas formula buffer absorbs the landing shock energy, reduces aircraft landing and transships, ground load is passed through skid, vaulting pole and oil gas formula buffer and is transmitted for the fuselage, adopts threaded connection simultaneously between skid and sleeve, can make convenient change of sleeve of easy wearing and tear