Disclosed is a wing (5) for an aircraft (1), comprising a main wing (11), and a leading edge high lift assembly (13) comprising a high lift body (15), and a connection assembly (17) connecting the high lift body (15) to the main wing (11) in such a way that the high lift body (15) is movable relative to the main wing (11) between a stowed position and a deployed position, wherein the connection assembly (17) comprises a first connection element (19) that is mounted to the high lift body (15) and that is movably mounted to the main wing (11), wherein the connection assembly (17) comprises a second connection element (21) that is mounted to the high lift body (15) in a position spaced apart from the first connection element (19) in a span direction (23), and that is movably mounted to the main wing (11). The object to provide a wing comprising a simple, lightweight and aerodynamically optimized leading edge high lift assembly, is achieved in that the connection assembly (17) comprises an additional support device (33) arranged spaced apart from the first and second connection elements (19, 21) and configured to support the high lift body (15) at the main wing (11) against movement or deformation of the high lift body (15) relative to the main wing (11).


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    Title :

    LEADING EDGE HIGH LIFT ASSEMBLY AND WING FOR AN AIRCRAFT


    Additional title:

    ANORDNUNG FÜR EINE HOCHAUFTRIEBSVORRICHTUNG EINER TRAGFLÄCHENVORDERKANTE UND FLÜGEL FÜR EIN FLUGZEUG
    ENSEMBLE DE DISPOSITIF HYPERSUSTENTATEUR DE BORD D'ATTAQUE ET AILE D'AÉRONEF


    Contributors:

    Publication date :

    2025-04-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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