An electrical power supply device in an aircraft, the device including an enclosure, the enclosure containing at least: a fuel cell; a dihydrogen generator; a gas feed circuit connecting the dihydrogen generator to the anode of the fuel cell; an oxygen feed device feeding the cathode of the fuel cell; and a cooling circuit of the fuel cell associated with at least one heat exchanger; wherein the enclosure is mounted on an actuator system, the actuator system being configured to move the enclosure from a first position in which the enclosure is housed inside an outer wall of the aircraft, to a second position in which the enclosure projects from the outer wall.


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    Title :

    DISPOSITIF D'ALIMENTATION EN ENERGIE DANS UN AERONEF ET PROCEDE DE REFROIDISSEMENT DE CE DISPOSITIF


    Additional title:

    DEVICE FOR SUPPLYING ENERGY IN AN AIRCRAFT AND METHOD FOR COOLING THIS DEVICE
    VORRICHTUNG ZUR ENERGIEVERSORGUNG IN EINEM FLUGZEUG UND VERFAHREN ZUR KÜHLUNG DIESER VORRICHTUNG


    Contributors:

    Publication date :

    2020-08-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

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



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