An aircraft includes a fuselage, a generator configured to power the aircraft, and at least one fuel tank for storing fuel for the generator, and a fuel delivery assembly. A fuel tank is positioned in the fuselage and configured to store hydrogen fuel in a liquid phase. The fuel tank has a chamber for storing hydrogen fuel and a fuel extraction line fluidly coupled to the chamber. A fuel extraction line extends from the fuel tank in a forward direction of the fuselage and extends at a downward angle relative to a centerline of the fuselage. A fuel delivery assembly is fluidly coupled with the fuel extraction line and fluidly connects the fuel tank to the generator. The fuel delivery assembly is configured to provide hydrogen fuel from the fuel tank to the generator.

    一种飞行器,包括机身、被构造成向飞行器提供动力的发电机、和用于存放用于发电机的燃料的至少一个燃料箱、和燃料输送组件。燃料箱被定位在机身中,并且被构造成存放处于液相的氢燃料。燃料箱具有用于存放氢燃料的室和流体联接到室的燃料提取管线。燃料提取管线在机身的前向方向上从燃料箱延伸并且相对于机身的中心线以向下角度延伸。燃料输送组件与燃料提取管线流体联接,并且将燃料箱流体连接到发电机。燃料输送组件被构造成将来自燃料箱的氢燃料提供给发电机。


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    Titel :

    On-board liquid hydrogen storage for hydrogen aircraft


    Weitere Titelangaben:

    用于氢飞行器的机载液态氢存储器


    Beteiligte:

    Erscheinungsdatum :

    2023-04-07


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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