Continuous skin leading edge slats are disclosed. A disclosed example leading edge slat (400) for use with an aircraft includes a single-piece nose skin (402) defining upper (412) and lower (414) external surfaces of the leading edge slat, where the single-piece nose skin is to extend between a fore end and an aft end of the leading edge slat, and a box spar (508) coupled to an inner surface of the single-piece nose skin. The box spar (508) includes lateral walls (520) extending away from the inner surface of the single-piece nose skin. The lateral walls define at least one compartment (528) of the box spar.


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    Titel :

    CONTINUOUS SKIN LEADING EDGE SLATS


    Weitere Titelangaben:

    VORDERKANTENLEISTEN MIT KONTINUIERLICHER HAUT
    BECS DE BORD D'ATTAQUE À REVÊTEMENT EN CONTINU


    Beteiligte:
    BARR MARK A (Autor:in) / AMOROSI STEPHEN R (Autor:in) / ANDERSON MATTHEW L (Autor:in) / BURIN RAMON A (Autor:in) / SEVERANCE MICHAEL R (Autor:in)

    Erscheinungsdatum :

    03.04.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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