A fuel cell system and a control method using the same. The fuel cell system includes a propeller wing of a flying object and connected to a rotor, a main radiator and a sub-radiator arranged so that heat of cooling water is dissipated by a downdraft generated by rotation of the propeller wing, and a controller to provide the cooling water to one or both of the main radiator and the sub-radiator based on an operation mode of the flying object.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Fuel cell system and control method using same


    Beteiligte:
    CHOI SUNG KYUNG (Autor:in) / WON JONG BO (Autor:in)

    Erscheinungsdatum :

    2024-03-26


    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 / B64C AEROPLANES , Flugzeuge / B64U



    FUEL CELL SYSTEM AND CONTROL METHOD USING SAME

    CHOI SUNG KYUNG / WON JONG BO | Europäisches Patentamt | 2023

    Freier Zugriff

    FUEL CELL SYSTEM AND CONTROL METHOD USING THE SAME

    CHOI SUNG KYUNG / WON JONG BO | Europäisches Patentamt | 2023

    Freier Zugriff

    FUEL CELL SYSTEM VEHICLE HAVING THE SAME AND CONTROL METHOD FOR FUEL CELL SYSTEM

    PARK GUN HYUNG / PARK JUN YOUNG | Europäisches Patentamt | 2017

    Freier Zugriff


    FUEL CELL SYSTEM AND VEHICLE COMPRISING THE SAME CONTROL METHOD FOR FUEL CELL SYSTEM

    RYU JUNG HWAN | Europäisches Patentamt | 2019

    Freier Zugriff