The invention refers to an aircraft composite panel assembly (10) comprising a first panel (1) having upper and lower faces, the lower face having a recess (7) on a first side (1a) of the panel (1); a second panel (2) having upper and lower faces, the lower face having an outward projection (8) at a first side (2a) of the panel (2), the outward projection (8) received on the recess (7) forming a lower continuous face; and a forward stack of plies (5) of composite material bonded to the upper face of the first panel (1), the forward stack of plies (5) having an edge (5a) aligned with the first side (1 a) of the first panel (1), and the number of plies of the forward stack of plies (5) decreasing away from the first side (1a) of the first panel (1).


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    Titel :

    AIRCRAFT COMPOSITE PANEL ASSEMBLY AND MANUFACTURING METHOD THEREOF


    Weitere Titelangaben:

    FLUGZEUGVERBUNDPLATTENANORDNUNG UND HERSTELLUNGSVERFAHREN DAFÜR
    ENSEMBLE PANNEAU COMPOSITE D'AÉRONEF ET SON PROCÉDÉ DE FABRICATION



    Erscheinungsdatum :

    03.07.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    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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