Electromechanical drive system (1) to control a transmission shaft (2) connected to the mechanical operating systems of an aircraft, comprising an electric machine (3), a two-way transmission rotation (8) and a clutch assembly (9) wherein the two-way transmission rotation (8) is configured, in any direction of rotation of the transmission shaft (2), to selectively allow the passage of torque either only between the electric machine (3) and the transmission shaft (2) when the torque is supplied by the electric machine (3) to the transmission shaft (2) or between the transmission shaft (2), the clutch assembly (9) and the electric machine ( 3 ) when the torque is supplied by the transmission shaft (2) to the electric machine (3).


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    Title :

    ELECTROMECHANICAL DRIVE SYSTEM FOR AN AIRCRAFT


    Additional title:

    ELEKTROMECHANISCHES ANTRIEBSSYSTEM FÜR EIN FLUGZEUG
    SYSTÈME D'ENTRAÎNEMENT ÉLECTROMÉCANIQUE POUR AÉRONEF


    Contributors:

    Publication date :

    2024-09-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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