An unmanned aerial vehicle flight anti-collision device

Abstract

The utility model relates to an unmanned plane technical field, concretely is an unmanned plane flight anti -collision device, including fuselage and located on the fuselage a plurality of arms, be equipped with flight wing on the arm, the arm bottom is connected with mobile wheel subassembly, be equipped with damping mechanism on mobile wheel subassembly, flight wing side edge outward one side is equipped with anti -collision device, the anti -collision device includes the semicircle arc structure located in flight wing side edge, the semicircle arc structure bottom is equipped with a plurality of support frame, the support frame includes the arm rod connected with arm and the connecting rod connected with semicircle arc structure, the obtuse angle is formed between arm rod and connecting rod, the utility model discloses the damping mechanism is set up on the mobile wheel subassembly with anti -collision device and is arranged to make the reasonable anti -collision and shock attenuation to unmanned plane, the side edge of the flight wing of unmanned plane is passed through setting semicircle arc structure simultaneously, effectively prevent the problem that the flight wing is damaged due to the impact, and the protection device is too heavy, and the influence to unmanned plane is caused simultaneously.

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