An aircraft control surface actuation assembly comprises a first electromechanical actuator assembly (44) driven by two independent motors (48, 50) for redundancy, with a damping assembly (46) provided to mitigate flutter.


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    Title :

    CONTROL SURFACE ACTUATION ASSEMBLY


    Additional title:

    STEUERFLÄCHENBETÄTIGUNGSANORDNUNG
    ENSEMBLE D'ACTIONNEMENT DE SURFACE DE COMMANDE


    Contributors:

    Publication date :

    2017-11-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16H Getriebe , GEARING / B64C AEROPLANES , Flugzeuge



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