An assembly (20) is provided for an aircraft. This aircraft assembly (20) includes an aircraft control surface (24) and a hydraulic actuator (26). The hydraulic actuator (26) includes a housing (70) and a piston (74) within the housing (70). The housing (70) is formed integral with the aircraft control surface (24).


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    Title :

    AIRCRAFT CONTROL SURFACE WITH INTEGRATED HYDRAULIC ACTUATOR


    Additional title:

    FLUGZEUGSTEUERFLÄCHE MIT INTEGRIERTEM HYDRAULISCHEN AKTUATOR
    GOUVERNE D'AÉRONEF À ACTIONNEUR HYDRAULIQUE INTÉGRÉ


    Contributors:

    Publication date :

    2023-07-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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