An aircraft steering system (10A) includes: a first actuator (21) attached to a wing main body (11); a horn arm (13) configured to transmit an output of the first actuator (21) to a flight control surface (12); and a second actuator (22) that is a rotary actuator and attached to the flight control surface (12). At least one of the first actuator (21) and the second actuator (22) is an electromechanical actuator (EMA). A first end of the horn arm (13) is coupled to an output terminal (21a) of the first actuator (21), and a second end of the horn arm (13) is fixed to an output terminal (22a) of the second actuator (22). The second actuator (22) is attached to the flight control surface (12) such that a turning axis of the output terminal (22a) is parallel to or coincides with a fulcrum axis (hinge line) of the flight control surface (12).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT STEERING SYSTEM INCLUDING ELECTROMECHANICAL ACTUATOR


    Weitere Titelangaben:

    FLUGZEUG-LENKSYSTEM MIT ELEKTROMECHANISCHEM STELLANTRIEB
    SYSTÈME DE DIRECTION D'AÉRONEF COMPRENANT UN ACTIONNEUR ÉLECTROMÉCANIQUE


    Beteiligte:
    MIYAZONO KOHEI (Autor:in) / NISHIYAMA YOJI (Autor:in) / SUGIURA HIDEYUKI (Autor:in)

    Erscheinungsdatum :

    23.03.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16H Getriebe , GEARING



    AIRCRAFT STEERING SYSTEM INCLUDING ELECTROMECHANICAL ACTUATOR

    MIYAZONO KOHEI / NISHIYAMA YOJI / SUGIURA HIDEYUKI | Europäisches Patentamt | 2022

    Freier Zugriff

    AIRCRAFT STEERING SYSTEM WITH ELECTROMECHANICAL ACTUATOR

    MIYAZONO KOHEI / NISHIYAMA YOJI / SUGIURA HIDEYUKI | Europäisches Patentamt | 2019

    Freier Zugriff

    AIRCRAFT STEERING SYSTEM PROVIDED WITH ELECTROMECHANICAL ACTUATOR

    MIYAZONO KOHEI / NISHIYAMA YOJI / SUGIURA HIDEYUKI | Europäisches Patentamt | 2019

    Freier Zugriff

    Aircraft flight control system including electromechanical actuator

    MIYAZONO KOHEI / NISHIYAMA YOJI / SUGIURA HIDEYUKI | Europäisches Patentamt | 2022

    Freier Zugriff

    AIRCRAFT FLIGHT CONTROL SYSTEM INCLUDING ELECTROMECHANICAL ACTUATOR

    MIYAZONO KOHEI / NISHIYAMA YOJI / SUGIURA HIDEYUKI | Europäisches Patentamt | 2020

    Freier Zugriff