The invention is applicable to the technical field of aircrafts, and provides an enhanced fuselage device applicable to a hydrogen-powered unmanned aerial vehicle. The aircraft shell is of a thin-wall shell structure with the top closed and provided with a first reinforcing structure. An assembly opening and a plurality of heat dissipation holes are formed in the bottom of the aircraft shell, the heat dissipation holes are located in the two sides of the aircraft shell, and installation pipes used for installing all arms of the unmanned aerial vehicle are arranged in the circumferential direction of the aircraft shell. The structural strength of the aircraft body, especially the upper structure, can be greatly improved, and load-bearing external hanging such as a parachute can be conveniently added to the top; and meanwhile, the top integrated structure of the machine body also has better sealing performance, so that the waterproof and dustproof performance is greatly improved, and internal electronic components are protected.

    本发明适用于飞行器技术领域,提供了一种适用氢动力无人机的强化机身装置,包括飞机壳体;所述飞机壳体为顶部封闭,且设有第一加强结构的薄壁壳体结构;飞机壳体底部布设有装配口和多个散热孔,多个散热孔位于飞机壳体两侧,在所述飞机壳体周向开设有用于安装无人机各个机臂的安装管;本发明能够极大提升飞机机体尤其上部结构强度,便于顶部加装负重外挂,比如降落伞等;同时机身顶部一体化结构也具有更好的密封性,大大提升防水防尘,保护内部电子元器件。


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    Title :

    Enhanced fuselage device suitable for hydrogen-powered unmanned aerial vehicle


    Additional title:

    一种适用氢动力无人机的强化机身装置


    Contributors:
    XU WEIQIANG (author) / GAO DING (author) / SHI QING (author) / ZENG ZHIGANG (author)

    Publication date :

    2023-05-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U



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