A wing panel actuator assembly comprising: an actuator housing (40); an actuator piston (50) arranged in the actuator housing and axially movable relative to the actuator housing; a connecting rod (60) attached, at one end (62), to an end (51) of the piston extending from the actuator housing; the actuator housing and piston arranged to be accommodated inside a movable panel (2) of an aircraft wing, the connecting rod arranged to be attached, in use, at its end (61) opposite the one end (62) attached to the piston, to a wing structure of the aircraft wing, the panel being pivotable about a pivot point P relative to the wing structure (1) by means of the actuator piston.


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    Titel :

    FLIGHT CONTROL ACTUATOR


    Weitere Titelangaben:

    ACTIONNEUR DE COMMANDE DE VOL


    Beteiligte:
    POTIER KARL (Autor:in) / DAVIS JENNIFER (Autor:in) / MEDINA RAPHAEL (Autor:in) / SOCHELEAU JEROME (Autor:in)

    Erscheinungsdatum :

    01.09.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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