The invention discloses a heat dissipation shell for an unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicles, and the heat dissipation shell is characterized by comprising a shell body, a heat conduction plate is fixedly connected to the interior of the shell body, and a plurality of uniformly distributed heat absorption rods are fixedly connected between the heat conduction plate and the shell body; a plurality of mounting holes and heat dissipation holes which are uniformly distributed are formed in the upper end and the lower end of the shell body in a penetrating mode correspondingly, the mounting holes and the heat dissipation holes are located between the shell body and the heat conduction plate, fans are installed in the mounting holes, and the heat conduction plate is installed in the shell body, so that the unmanned aerial vehicle running equipment is separated from the heat dissipation area, thus the problem that the unmanned aerial vehicle breaks down due to the fact that dust enters the shell body is effectively avoided, meanwhile, the heat conduction plate can transfer heat generated during operation of the unmanned aerial vehicle to the heat absorption rod, and then the heat absorption rod is cooled through cooperation of the fans and the heat dissipation holes, therefore, the heat dissipation effect is good, and impurities or dust are prevented from entering the shell body.

    本发明公开了一种无人机用散热壳体,属于无人机技术领域,其技术方案要点包括机壳本体,机壳本体的内部固定连接有导热板,导热板与机壳本体之间固定连接有多个均匀分布的吸热棒,机壳本体的上下两端分别贯穿开设有多个均匀分布的安装孔和散热孔,多个安装孔和多个散热孔均位于机壳本体与导热板之间,多个安装孔的内部均安装有风扇,通过在机壳本体的内部安装导热板,将无人机运行设备与散热区隔开,进而有效避免灰尘进入机壳本体的内部导致无人机发生故障的问题,同时导热板会将无人机运行时产生的热量传递给吸热棒,然后通过风扇与散热孔的配合对吸热棒进行降温,进而达到了散热效果好和防止杂质或灰尘会进入机壳本体内的问题。


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    Titel :

    Heat dissipation shell for unmanned aerial vehicle


    Weitere Titelangaben:

    一种无人机用散热壳体


    Beteiligte:
    WU JIANG (Autor:in) / ZHAO YAN (Autor:in) / ZHAO YUQIONG (Autor:in) / CHEN GUANG (Autor:in) / QI ZHIXIANG (Autor:in)

    Erscheinungsdatum :

    2022-01-07


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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