A winglet system for a wing of an aircraft is provided. The winglet system comprises an attachment end for attachment to a main wing of the aircraft, an upper winglet and a lower winglet. The upper and lower winglets are staggered and also overlap one another along the chord of the attachment end. A spanwise profile of the lower winglet has a midpoint where a slope of the spanwise profile at a point outboard of the midpoint is inclined more upwardly than a slope of the spanwise profile at the midpoint. The configuration of the winglet system may provide benefits such as a reduced bending moment and reduced negative interference between the winglets while also managing ground clearance.


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    Titel :

    WINGLET SYSTEMS FOR AIRCRAFT


    Weitere Titelangaben:

    WINGLET-SYSTEME FÜR FLUGZEUGE
    SYSTÈMES D'AILETTE POUR AÉRONEF


    Beteiligte:
    BOCHUD PASCAL (Autor:in) / LEBLOND DAVID (Autor:in) / PEPIN FRANÇOIS (Autor:in)

    Erscheinungsdatum :

    2023-08-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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