A heat dissipation structure includes a housing configured to accommodate a heating element of an aerial vehicle. The housing includes a first air vent configured to guide an airflow into the housing and a second air vent configured to guide the airflow out of the housing. The airflow includes a propeller-generated airflow generated by a propeller of the aerial vehicle during rotation. The housing is located at an end of an arm of the aerial vehicle, away from the propeller in a longitudinal direction of the arm. A projection of the housing on a plane on which an area of rotation of the propeller lies at least partially overlaps the area of rotation of the propeller.
HEAT DISSIPATION STRUCTURE, HEAT DISSIPATION METHOD AND DEVICE, AERIAL VEHICLE, AND READABLE STORAGE MEDIUM
2024-03-14
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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