In accordance with at least one aspect of this disclosure, an emergency power unit for an aircraft includes, a fuel cell system (102) configured to generate power using a fuel and an oxidant. A thermal management system (124, 224, 324, 424) is in thermal communication with the fuel cell system (102) to divert heat from the fuel cell system (102) to the thermal management system (124, 224, 324, 424).


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    Title :

    SYSTEMS FOR COOLING EMERGENCY POWER UNITS


    Additional title:

    SYSTEME ZUR KÜHLUNG VON NOTANTRIEBSAGGREGATEN
    SYSTÈMES DE REFROIDISSEMENT D'UNITÉS D'ALIMENTATION DE SECOURS


    Contributors:

    Publication date :

    2025-05-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / 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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