The invention relates to an electric propulsion unit for an aircraft comprising at least one first propulsion member, a second propulsion member and a single electric motor configured to drive the first propulsion member and the second propulsion member in a counter-rotating manner, the electric motor comprising a peripheral stator element comprising a first peripheral stage and a second peripheral stage which are offset along an axis, the first peripheral stage comprising at least a first phase, a second phase and a third phase which are alternated according to a first sequence in such a way as to allow a rotation of the first rotor element in the first direction of rotation, the second peripheral stage comprising phases which are alternated according to a second sequence in such a way as to allow a counter-rotating rotation of the second rotor element.


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    Title :

    PROPULSEUR ÉLECTRIQUE POUR AÉRONEF ET PROCÉDÉ D'UTILISATION D'UN TEL PROPULSEUR


    Additional title:

    ELECTRIC PROPULSION UNIT FOR AN AIRCRAFT AND METHOD FOR USING SUCH A PROPULSION UNIT
    ELEKTRISCHE ANTRIEBSEINHEIT FÜR EIN FLUGZEUG UND VERFAHREN ZUR VERWENDUNG EINER SOLCHEN ANTRIEBSEINHEIT


    Contributors:

    Publication date :

    2023-07-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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