A high-lift device to be provided on a main wing body of an aircraft includes a slat and a slat moving mechanism moving the slat between a deployed position and a retracted position. The slat includes a slat front surface, a slat rear surface, and a fillet surface between the slat front surface and the slat rear surface, the slat rear surface is a curved surface recessed toward inside of the slat, the fillet surface is a curved surface projecting outward the slat, and, in a cross section taken along a plane orthogonal to a pitch axis direction of the aircraft, an inflection point between the slat rear surface and the fillet surface is positioned lower than a vertex on a front side of the main wing body when the slat is retracted.


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    Titel :

    HIGH-LIFT DEVICE AND AIRCRAFT WING


    Beteiligte:

    Erscheinungsdatum :

    19.03.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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