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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Electric actuator device


    Beteiligte:
    MIYOSHI MASATO (Autor:in) / HATAKEYAMA DAIKI (Autor:in)

    Erscheinungsdatum :

    2022-03-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    ELECTRIC ACTUATOR AND ACTUATOR DEVICE

    SAITO KAZUHIRO / HASHIMOTO SEIJI / UENO AGATO | Europäisches Patentamt | 2020

    Freier Zugriff

    ELECTRIC ACTUATOR AND ACTUATOR DEVICE

    ARITA TETSUO / KATO SHUN / SATO KEI et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    ELECTRIC ACTUATOR DEVICE

    MIYOSHI MASATO / HATAKEYAMA DAIKI | Europäisches Patentamt | 2019

    Freier Zugriff

    ELECTRIC ACTUATOR DEVICE

    MIYOSHI MASAHITO / HATAKEYAMA DAIKI | Europäisches Patentamt | 2019

    Freier Zugriff

    ELECTRIC ACTUATOR DEVICE

    MIYOSHI MASATO / HATAKEYAMA DAIKI | Europäisches Patentamt | 2020

    Freier Zugriff