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
14.03.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2025
|Europäisches Patentamt | 2023
|Europäisches Patentamt | 2020
|HEAT DISSIPATION ASSEMBLY, HEAT DISSIPATION DEVICE, AND UNMANNED AERIAL VEHICLE
Europäisches Patentamt | 2021
|Multi-rotor unmanned aerial vehicle heat dissipation device and heat dissipation method
Europäisches Patentamt | 2023
|