An electric actuator device is provided with: an electric actuator body that has a first fulcrum connected to a rudder surface side of an aircraft and a second fulcrum connected to the aircraft body side, and is driven by an electric motor such that the first fulcrum and the second fulcrum can be brought closer together and drawn further apart; a support member for advancing/retracting between a support position at which the support member supports the first fulcrum or the second fulcrum thereunder, and a retracted position at which the support member is retracted from under the first fulcrum or the second fulcrum; and a retention member for retaining the first fulcrum or the second fulcrum when the support member is located in the retracted position.


    Access

    Download


    Export, share and cite



    Title :

    Electric actuator device


    Contributors:

    Publication date :

    2022-03-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    ELECTRIC ACTUATOR AND ACTUATOR DEVICE

    SAITO KAZUHIRO / HASHIMOTO SEIJI / UENO AGATO | European Patent Office | 2020

    Free access

    ELECTRIC ACTUATOR AND ACTUATOR DEVICE

    ARITA TETSUO / KATO SHUN / SATO KEI et al. | European Patent Office | 2020

    Free access

    ELECTRIC ACTUATOR DEVICE

    MIYOSHI MASATO / HATAKEYAMA DAIKI | European Patent Office | 2021

    Free access

    ELECTRIC ACTUATOR DEVICE

    MIYOSHI MASATO / HATAKEYAMA DAIKI | European Patent Office | 2019

    Free access

    ELECTRIC ACTUATOR DEVICE

    MIYOSHI MASAHITO / HATAKEYAMA DAIKI | European Patent Office | 2019

    Free access