The invention relates to a fuel cell aircraft which comprises an aircraft body and wings, the wings are arranged at the top end of the middle of the aircraft body, a movable enclosure is arranged on the aircraft body in an openable mode, a fuel cell and a fuel tank are arranged in the aircraft body, and fuel in the fuel tank is connected to the fuel cell through a pipeline. The fuel tank is detachably arranged in the machine body through the opening of the movable machine shell. A rear hatch for dismounting/mounting the fuel tank is formed in the rear end of the machine body, the movable machine shell is hinged to the rear hatch, and the fuel cell is arranged in the middle of the machine body. The mounting and fixing mode of the fuel tank is simplified, mounting can be completed by arranging the fuel tank in the machine body and covering the opening cover, and mounting steps are reduced. The fuel tank is limited and supported through the machine body, and the safety of the fuel tank is improved.

    本发明涉及一种燃料电池飞行器,包括机体和机翼,机体中部的顶端供机翼设置,所述机体上可开合地设置一活动机壳,所述机体内部设置燃料电池和燃料罐,燃料罐内部燃料通过管道连接至燃料电池,燃料罐通过活动机壳的开口处可拆卸地设置在机体内。所述机体后端开设供燃料罐拆卸/安装的后舱口,该后舱口上铰接设置所述的活动机壳,所述机体中部供所述的燃料电池设置。燃料罐安装固定方式简化,将燃料罐设置在机体内并盖上口盖即可完成安装,减少安装步骤。燃料罐通过机体限位及支撑,提高燃料罐的安全性。


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    Title :

    Fuel cell aircraft


    Additional title:

    一种燃料电池飞行器


    Contributors:
    LIN WEICHAO (author) / ZHOU JUN (author) / WU LIAONI (author)

    Publication date :

    2023-05-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY



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