An auxiliary power system for an airplane includes at least one fuel cell unit each with at least one fuel cell, a voltage output, a fuel intake and an outlet for reaction products, a fuel tank that is couplable with the fuel intake of the fuel cell unit, at least one compressor unit with an air intake and air outlet and an electric motor, which is couplable with a voltage output of the at least one fuel cell unit and, by way of a shaft, with the at least one compressor unit. At least the at least one fuel cell unit, the compressor unit and the electric motor are interconnected to yield a coherent unit, which continuously provides electrical power and pressurized air.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Auxiliary power system for an airplane and an airplane with such an auxiliary power system


    Beteiligte:
    HOFFJANN CLAUS (Autor:in) / ENGEL WOLFGANG (Autor:in)

    Erscheinungsdatum :

    2021-10-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    AUXILIARY POWER SYSTEM FOR AN AIRPLANE AND AN AIRPLANE WITH SUCH AN AUXILIARY POWER SYSTEM

    HOFFJANN CLAUS / ENGEL WOLFGANG | Europäisches Patentamt | 2018

    Freier Zugriff

    Auxiliary power system for an airplane and an airplane with such an auxiliary power system

    HOFFJANN CLAUS / ENGEL WOLFGANG | Europäisches Patentamt | 2019

    Freier Zugriff

    Ejector, auxiliary power device for airplane and airplane

    WU XIYUN / PAN SHANGNENG / ZHU WEIJUN | Europäisches Patentamt | 2023

    Freier Zugriff

    Auxiliary lifting assembly, airplane hatch adopting auxiliary lifting assembly, and airplane

    ZHENG XIANGWEI / YAO XIONGHUA / HAN YONGZHI et al. | Europäisches Patentamt | 2015

    Freier Zugriff

    Aircraft auxiliary balancing system and airplane

    YUAN JIANG / ZHANG JIE | Europäisches Patentamt | 2021

    Freier Zugriff