The present invention discloses an engine cooling device of an unmanned aerial vehicle. The device comprises an unmanned aerial vehicle main frame, a synchronous transmission mechanism is arranged atthe upper end of the unmanned aerial vehicle main frame, an air outlet linkage mechanism is arranged on the side surface of the unmanned aerial vehicle main frame, an air inlet adjusting mechanism isarranged on the upper surface of the unmanned aerial vehicle main frame, and an active heat dissipation mechanism is arranged on the inner surface of the unmanned aerial vehicle main frame. The enginecooling device has the beneficial effects that the unmanned aerial vehicle can be cooled according to the actual working condition, the energy-saving effect is achieved while the unmanned aerial vehicle rapidly enters the normal working state, a plurality of electric appliances can be saved in a linkage mode, and the purpose of reducing the manufacturing cost is achieved.

    本发明公开了一种无人机的发动机散热装置,包括无人机主架,所述无人机主架上端设有同步传动机构,所述侧表面设有出气联动机构,所述无人机主架上表面设有进气调节机构,所述无人机主架内表面设有主动散热机构。本发明的有益效果是,可以根据实际工况对无人机进行散热,使无人机迅速进入正常的工作状态的同时达到节能的效果,通过联动的方式可以节省多个用电器,达到降低制作成本的目的。


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    Titel :

    Engine cooling device of unmanned aerial vehicle


    Weitere Titelangaben:

    一种无人机的发动机散热装置


    Beteiligte:
    LI JIE (Autor:in) / GAO SHIBIN (Autor:in) / ZHANG HAN (Autor:in)

    Erscheinungsdatum :

    08.05.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    F01P Kühlung von Kraft- und Arbeitsmaschinen oder Kraftmaschinen allgemein , COOLING OF MACHINES OR ENGINES IN GENERAL / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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