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) overlapping the first side (1a) of the first panel (1), and the number of plies of the forward stack of plies (5) decreasing toward the opposite side of the first side (1 a) of the first panel (1).


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    Title :

    AIRCRAFT COMPOSITE PANEL ASSEMBLY AND MANUFACTURING METHOD THEREOF


    Additional title:

    ASSEMBLAGE DE PANNEAU COMPOSITE D'AERONEF ET METHODE DE FABRICATION ASSOCIEE



    Publication date :

    2018-05-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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