An actuator system for actuating movement of a control surface of an aircraft wing includes a common input rail connectable to a means for providing movement to said input rail. The system also includes: a plurality of rotary geared actuators “RGAs”; a common output rail connectable to said control surface; wherein each of said plurality of RGAs is connected to said input rail by an individual input clutch and also connected to said output rail by an individual output clutch, and wherein the input clutch functions independently of the output clutch.


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    Title :

    ROTARY ACTUATION FOR THIN WING APPLICATIONS


    Contributors:

    Publication date :

    2022-10-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    ROTARY ACTUATION FOR THIN WING APPLICATIONS

    DAVIES STEPHEN HARLOW | European Patent Office | 2022

    Free access

    ROTARY ACTUATION FOR THIN WING APPLICATIONS

    DAVIES STEPHEN HARLOW | European Patent Office | 2022

    Free access



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