An actuator arrangement comprising a carrier element (16, 120) which is translatable and angularly moveable about a first fixed axis (20), in use, relative to a wing structure (12, 112), an actuator arm (24, 118) pivotally mounted to the carrier element (16, 120), and a support arm (30, 122) pivotally mounted, in use, to the wing structure (12, 112) about a second, fixed pivot axis (36), wherein the first and second fixed axes (20, 36) are not perpendicular to one another.


    Access

    Download


    Export, share and cite



    Title :

    Actuator arrangement


    Additional title:

    Aktuatoranordnung
    Agencement d'actionneur


    Contributors:

    Publication date :

    2018-05-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Actuator arrangement

    AMBS MARCEL / FECHLER JENS / BOETTGER FLORIAN | European Patent Office | 2017

    Free access

    ACTUATOR ARRANGEMENT

    MARCEL AMBS / DR JENS FECHLER / FLORIAN BOETTGER | European Patent Office | 2015

    Free access

    Actuator arrangement

    GERBIER DOMINIQUE / SANDLER SAMUEL / GRAND SERGE et al. | European Patent Office | 2017

    Free access

    ACTUATOR ARRANGEMENT

    AMBS MARCEL / FECHLER JENS / KARNAT BJOERN | European Patent Office | 2017

    Free access

    Actuator arrangement

    AMBS MARCEL / FECHLER JENS / KARNAT BJOERN | European Patent Office | 2019

    Free access