A aircraft wing assembly comprising a wing box comprising: an upper surface 12; a lower surface 14; and a leading edge structure 16, connecting the upper surface to the lower surface and secured to the upper surface at a connection point 30, and a drive mechanism secured to the wing box; and a high lift device mounted to the drive mechanism. The drive mechanism 24, 25, is configured to move the high lift device between a retracted position and an extended position, and wherein the high lift device is configured to overlap the connection point when in the retracted position.


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    Titel :

    Aircraft wing assembly


    Beteiligte:
    PETER KELLY (Autor:in)

    Erscheinungsdatum :

    05.06.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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