A fuselage having a longitudinal window belt has a composite outer skin including upper and lower composite skin sections.The skin includes at least one window opening located at the window belt. The upper and lower skin sections are joined together by a longitudinal splice joint located at the window belt.

    Un fuselage ayant une membrure de la fenêtre longitudinale comporte un revêtement extérieur composite comprenant des sections de revêtement supérieure et inférieure composites. Le revêtement comprend au moins une ouverture de fenêtre située au niveau de la membrure de la fenêtre. Les sections de revêtement supérieure et inférieure sont réunies au moyen dun joint de raccordement longitudinal situé à la membrure de la fenêtre.


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    Title :

    JOINING COMPOSITE FUSELAGE SECTIONS ALONG WINDOW BELTS


    Additional title:

    REUNION DE SECTIONS DE FUSELAGE COMPOSITES LE LONG DE MEMBRURES DE FENETRE


    Contributors:

    Publication date :

    2020-07-07


    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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