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 :

    AIRCRAFT CONTROL SURFACE ACTUATOR


    Additional title:

    STELLANTRIEB FÜR DIE STEUERFLÄCHE EINES FLUGZEUGES
    ACTIONNEUR DE GOUVERNE DE COMMANDE D'AÉRONEF


    Contributors:

    Publication date :

    2019-11-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16H Getriebe , GEARING



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