An assembly is provided for an aircraft. This aircraft assembly includes an aircraft control surface and a hydraulic actuator. The hydraulic actuator includes a housing and a piston within the housing. The housing is formed integral with the aircraft control surface.


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    Titel :

    Aircraft control surface with integrated hydraulic actuator


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

    Erscheinungsdatum :

    11.03.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F15B SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL , Druckmittelbetriebene Systeme allgemein



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