An actuator system having a controlled element configured for rotary movement about a first axis relative to a reference structure; a linkage system between the element and reference structure; a first actuator and a second actuator configured to power a first degree of freedom and an independent second degree of freedom of the linkage system, respectively; the linkage system having a first link configured for rotary movement about a second axis not coincident to the first axis and second link configured for rotary movement about a third axis; the linkage system configured such that a first angle of rotation may be driven independently of a second angle of rotation between said first link and said reference structure; wherein one of the first or second actuators is configured and arranged to drive rotation of the element about the first axis when the other is operatively locked.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Rotary actuator


    Beteiligte:
    KOPP JOHN (Autor:in) / SCHLEIFE MATTHEW (Autor:in)

    Erscheinungsdatum :

    2015-07-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16H Getriebe , GEARING



    ROTARY ACTUATOR

    STANDLEY JOHN A / LISENKO KIM R / ZAZYNSKI TIMOTHY PAUL | Europäisches Patentamt | 2021

    Freier Zugriff

    ROTARY ACTUATOR

    Europäisches Patentamt | 2018

    Freier Zugriff

    ROTARY ACTUATOR

    KUME MIKINE | Europäisches Patentamt | 2017

    Freier Zugriff

    ROTARY ACTUATOR

    STANDLEY JOHN A / LISENKO KIM R / ZAZYNSKI TIMOTHY PAUL | Europäisches Patentamt | 2023

    Freier Zugriff

    ROTARY ACTUATOR

    STANDLEY JOHN A / LISENKO KIM R / ZAZYNSKI TIMOTHY PAUL | Europäisches Patentamt | 2021

    Freier Zugriff