An open composite panel for an aircraft includes a composite skin having an inner face and an outer face, and a plurality of stiffening ribs, each rib extending over the inner face of the skin in a respective direction of extension and projecting from the inner face to a top that is opposite said inner face. The plurality of ribs includes at least one reinforced rib, each reinforced rib having at least one elongate stiffening portion extending along the top of the reinforced rib, said stiffening portion including fibers extending substantially in the direction of extension of the reinforced rib.


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    Titel :

    PANNEAU COMPOSITE OUVERT RIGIDE


    Weitere Titelangaben:

    RIGID OPEN COMPOSITE PANEL
    STARRE OFFENE VERBUNDPLATTE



    Erscheinungsdatum :

    25.09.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse



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