Unmanned aerial vehicle

Abstract

An unmanned aerial vehicle (UAV) is disclosed, including a fuselage, a wing assembly, and a heat dissipation structure. The heat dissipation structure and the wing assembly are both mounted to the fuselage. The heat dissipation structure is thermally connected to at least some electronic devices within the fuselage. The fuselage and the wing assembly together define a heat dissipation channel in communication with the external environment. At least a portion of the heat dissipation structure is exposed to the heat dissipation channel, allowing external airflow to cool the heat dissipation structure during UAV flight. Through this structure, the heat generated by the electronic devices is transferred to the heat dissipation structure and exchanged with the outside air, thereby enhancing cooling efficiency and ensuring reliable operation of the UAV.

Dependencies are inferred from the claim text.