A fuel cell system configured to provide electrical power to an electrical motor producing propulsive thrust for an aircraft includes a plurality of fuel cell stacks radially arranged about a central cavity. Fuel cell plates within each of the fuel cell stacks are oriented such that major surfaces of the fuel cell plates are parallel to an airflow created by the aircraft as it moves through the air. The fuel cell system further includes a plurality of cooling devices disposed in radial cavities located between at least two fuel cell stacks in the plurality of fuel cell stacks.


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    Titel :

    AEROSPACE FUEL CELL SYSTEM INTEGRATION


    Weitere Titelangaben:

    INTEGRATION EINES LUFT- UND RAUMFAHRT-BRENNSTOFFZELLENSYSTEMS
    INTÉGRATION DE SYSTÈME DE PILE À COMBUSTIBLE AÉROSPATIALE


    Beteiligte:

    Erscheinungsdatum :

    23.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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    AEROSPACE FUEL CELL SYSTEM INTEGRATION

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    NASA Fuel Cell Development for Aerospace Applications

    Liang, A. / Hoberecht, M. | British Library Conference Proceedings | 2004


    NASA Fuel Cell Development for Aerospace Applications

    Liang, A. / Hoberecht, M. | British Library Conference Proceedings | 2004