A heat dissipation structure includes a housing configured to accommodate a heating element of an unmanned aerial vehicle (UAV). The housing includes a first air vent and a second air vent. The first air vent is configured to guide an airflow into the housing. The airflow includes a propeller-generated airflow generated by a propeller of the UAV during rotation. A side projection of the first air vent on a side of the housing at least partially overlaps a side projection of the propeller on the side of the housing. The second air vent is configured to guide the airflow out of the housing.


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    Titel :

    HEAT DISSIPATION STRUCTURE, HEAT DISSIPATION METHOD AND DEVICE, UNMANNED AERIAL VEHICLE, AND READABLE STORAGE MEDIUM


    Beteiligte:
    CAI ZHIWEI (Autor:in) / ZHANG YAWEN (Autor:in)

    Erscheinungsdatum :

    05.11.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge




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