A high efficiency hydrogen fuel system for a high altitude aircraft utilizes a compressor to compress air to a sufficiently high pressure for a fuel cell. The liquid hydrogen is compressed and then used in the heat exchanger to cool the compressed air, thereby maintaining the air at a sufficiently low temperature for the fuel cell. Hydrogen is also used to cool the fuel cell as it is also depressurized before entering the fuel cell cycle. The water condensation system allows water to be removed from the gas stream to reduce the impact on the atmosphere. The hydrogen fuel system may be used with VTOL aircraft, which may enable them to fly at higher altitudes. The hydrogen fuel system may be used in other subsonic and supersonic aircraft, such as asymmetric wing aircraft.

    一种用于高空飞行器的高效氢燃料系统,其利用压缩机将空气压缩到用于燃料电池的足够高的压力。液态氢气被压缩,然后在热交换器中被用来冷却压缩空气,从而将空气保持在用于燃料电池的足够低的温度。氢气还用于冷却燃料电池,因为它在进入燃料电池循环之前也被减压。水冷凝系统允许从气流中去除水以减少对大气的影响。氢燃料系统可与VTOL飞行器一起使用,这可以使它们能够在更高的高度飞行。氢燃料系统可以用于其他亚音速和超音速飞行器,例如不对称机翼飞行器。


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    Titel :

    High-efficiency hydrogen fuel high-altitude thermal fuel cell system and aircraft using same


    Weitere Titelangaben:

    高效氢燃料高空热力燃料电池系统及使用它的飞行器


    Beteiligte:
    JOEBEN BEVELT (Autor:in) / STOLL ALEX (Autor:in) / MIKIC GREGOR WIBBLE (Autor:in) / LYNN ROBERT GULLIVER (Autor:in)

    Erscheinungsdatum :

    28.07.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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