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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    Title :

    CONTINUOUS SKIN LEADING EDGE SLATS


    Additional title:

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


    Contributors:

    Publication date :

    2024-04-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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