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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ROTARY ACTUATION FOR THIN WING APPLICATIONS


    Beteiligte:

    Erscheinungsdatum :

    27.10.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Rotary actuation for thin wing applications

    DAVIES STEPHEN HARLOW | Europäisches Patentamt | 2025

    Freier Zugriff

    ROTARY ACTUATION FOR THIN WING APPLICATIONS

    DAVIES STEPHEN HARLOW | Europäisches Patentamt | 2022

    Freier Zugriff

    ROTARY ACTUATION FOR THIN WING APPLICATIONS

    DAVIES STEPHEN HARLOW | Europäisches Patentamt | 2024

    Freier Zugriff

    Beam-penetrating spline rotary actuation folding wing and aircraft

    WANG YIFAN / LI QINGQIAN / QIN JUNYANG et al. | Europäisches Patentamt | 2024

    Freier Zugriff