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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    Titel :

    ELECTROMECHANICAL DRIVE SYSTEM FOR AN AIRCRAFT


    Weitere Titelangaben:

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


    Beteiligte:
    ROSATA PIETRO (Autor:in) / ROSSANO MARIO (Autor:in) / LIGNAROLO VITTORIO (Autor:in)

    Erscheinungsdatum :

    04.09.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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