An autonomous propeller propulsion system for an aircraft. The autonomous system comprises a chassis with first attachment systems which engage with second attachment systems of the wing to ensure detachable attachment of the autonomous system, a fuel cell attached to the chassis, an electric motor attached to the chassis and having an output shaft, a propshaft rotated by the output shaft, a propeller attached to the propshaft, a controller converting an electric current delivered by the fuel cells into an electric current delivered to the electric motor, a hydrogen feed duct and an air feed duct, a set of auxiliary equipment, and a first connection arrangement, which connects with a second connection arrangement of the aircraft.


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    Titel :

    Autonomous propeller propulsion system for an aircraft, said autonomous propeller propulsion system comprising a fuel cell


    Beteiligte:
    THOMAS MATTHIEU (Autor:in) / ROUX ANTHONY (Autor:in) / POIRIER DIDIER (Autor:in) / VERSEUX OLIVIER (Autor:in) / ANGER ANDRÉ (Autor:in) / BAMMER BENEDIKT (Autor:in) / KLEWER GUIDO (Autor:in) / GALLANT GUILLAUME (Autor:in) / VOGEL FLORIAN (Autor:in) / WEHLE CHRISTIAN (Autor:in)

    Erscheinungsdatum :

    23.08.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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