In a fuel cell system intended for a pressure-independent operation, in which at least one fuel cell having an open cathode is provided, a first fluid chamber adjoins an inflow cross section and a second fluid chamber adjoins an outflow cross section. In the fluid chambers can be set an overpressure which is adapted to the operation of the at least one fuel cell.


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    Title :

    FUEL CELL SYSTEM FOR AN AIRCRAFT


    Contributors:

    Publication date :

    2020-02-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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



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