An aircraft wing tip device (107) includes a unitized, monolithic leading edge torque box that is formed of polymer matrix fiber-reinforced material. The leading edge torque box includes a skin (160) that defines a continuous, uninterrupted outer mold line surface extending aftwardly from a winglet leading edge by a distance of at least approximately 60 percent of a local chord length. The leading edge torque box (172) further includes at least one internal component (162) extending between opposing inner surfaces of the skin and being integrally formed therewith.


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    Titel :

    Natural laminar flow wingtip


    Beteiligte:

    Erscheinungsdatum :

    24.06.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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