This invention relates to the field of unmanned aerial vehicle (UAV) technology, specifically disclosing a UAV with a wing protection structure and its protection method. The UAV includes a UAV body, a first protection structure, a buffer structure, a second protection structure, and a linkage structure. The UAV body includes a
fuselage and arms. The arms consist of a first arm, a second arm, and a wing
assembly. The first arm is fixed to the side wall of the
fuselage, and the second arm is connected to the first arm via a hinge axis and can swing horizontally. The wing
assembly is located at the end of the second arm. The first protection structure is located around the wing
assembly and detachably connected to the second arm. The buffer structure is located at the
hinge point of the two arms. The second protection structure is located at both ends of the
fuselage. The linkage structure connects the first and second protection structures. The protection method includes lateral
impact protection steps and front-to-
rear impact protection steps. This invention achieves the transmission and conversion of
impact force through the linkage structure, enabling the buffer structure to effectively buffer impacts from multiple directions.