A power supply for an aircraft having an engine, the power supply comprising: a fuel cell assembly configured to be integrated into the engine, the fuel cell assembly comprising: a first fuel cell stack; during a first operating condition of the power supply, the fuel cell assembly is configured to provide a first power output from the first fuel cell stack and the second fuel cell stack, and during a second operating condition, the fuel cell assembly is further configured to provide a second power output from the first fuel cell stack, the second power output is different than the first power output.

    一种用于具有发动机的飞行器的电源,该电源包括:燃料电池组件,燃料电池组件被构造成集成到发动机中,燃料电池组件包括:第一燃料电池组;和第二燃料电池组,其中在电源的第一操作条件期间,燃料电池组件被构造成提供来自第一燃料电池组和第二燃料电池组的第一电力输出,并且在第二操作条件期间,进一步被构造成提供来自第一燃料电池组的第二电力输出,第二电力输出不同于第一电力输出。


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    Titel :

    POWER SUPPLY FOR AIRCRAFT


    Weitere Titelangaben:

    用于飞行器的电源


    Beteiligte:
    WANG HONGGANG (Autor:in) / PAN DI (Autor:in) / HUH KUM-KANG (Autor:in)

    Erscheinungsdatum :

    11.07.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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