Aircraft lifting surface (2) having a span direction, the lifting surface (2) comprising:- a stationary part (3),- a movable part (1), movable with respect to the stationary part (3) and comprising an end (4) in the span direction,- an actuation system configured to actuate the movable part (1) with respect to the stationary part (3).The actuation system comprising a sliding system joined to:- the end (4) of the movable part (1), and- configured to be joined to a stationary structure (6) of the aircraft, said stationary structure (6) being:• located adjacent in the span direction to the end (4) of the movable part (1), and• connected with the stationary part (3) of the lifting surface,so that the sliding system allows the movable part (1) to slide with respect to the stationary structure (6).


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    Title :

    AIRCRAFT LIFTING SURFACE


    Additional title:

    FLUGZEUGAUFTRIEBSFLÄCHE
    SURFACE DE SUSTENTATION D'AÉRONEF



    Publication date :

    2024-11-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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