Quick locking structure for wings of unmanned aerial vehicle

The utility model discloses an unmanned aerial vehicle wing quick locking structure, which relates to the technical field of unmanned aerial vehicles and comprises a vehicle body, wings are lapped at the left end and the right end of the vehicle body, one end of each wing is fixedly connected with a guide rod, the outer wall of each guide rod is inserted into the inner wall of the vehicle body, and a limiting mechanism is inserted into the inner wall of each wing. Locking mechanisms are fixedly connected to the left end and the right end of the aircraft body, each limiting mechanism comprises a mounting plate, and the outer wall of each mounting plate is connected with the inner wall of the corresponding wing in an inserted mode. According to the quick locking structure for the wings of the unmanned aerial vehicle, the outer walls of the guide rods are connected with the inner wall of the vehicle body in an inserted mode, so that the wings are preliminarily positioned, then the vehicle body and the wings are