The invention designs a novel hydrogen fuel aircraft by taking normal flight of the hydrogen fuel aircraft as a main target. The front end and the rear end of a fuselage of the novel hydrogen fuel aircraft are connected with a nose cover and a rectification cover through hinges respectively, opening and closing are convenient, and a hydrogen tank and a reactor can be put in and taken out. The hydrogen tank is fixed in the front fuselage through a ribbon, and the reactor is fixed in the rear fuselage through a bolt, so that the two devices can be stably mounted in the fuselage. An air inlet cover is designed at the top of the rear fuselage, a drainage and exhaust port is designed at the bottom, and a drainage pipe is arranged in the rear fuselage to be connected with the reactor, so that air intake, drainage and exhaust can be realized, and the reactor can continuously and normally work.

    本发明以实现氢燃料飞机的正常飞行为主要目标,设计了一种新型氢燃料飞机。新型氢燃料飞机的机身前后端分别与机头罩、整流盖通过铰链相接,方便打开关闭,以实现氢气罐和反应堆的放入取出。氢气罐通过扎带固定在前机身中,反应堆通过螺栓固定在后机身中,可实现两个设备在机身内部的稳定安装。后机身顶部设计了进气口盖,底部设计了排水排气口,内部有排水管与反应堆连接,可实现进气、排水排气,从而使反应堆能持续正常的工作。


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    Titel :

    Novel hydrogen fuel aircraft


    Weitere Titelangaben:

    一种新型氢燃料飞机


    Beteiligte:
    WANG YAOKUN (Autor:in) / SUN YIQI (Autor:in) / ZHAO CHENFEI (Autor:in) / YAN SHIYU (Autor:in) / LIN ZHAORU (Autor:in) / WEI JIANING (Autor:in)

    Erscheinungsdatum :

    2023-06-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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