A fuselage having a longitudinal window belt (58) has a composite outer skin including upper and lower composite skin sections (52, 54). The skin includes at least one window opening (70) located at the window belt (58). The upper and lower skin sections are joined together by a longitudinal splice joint (56) located at the window belt (58).


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    Title :

    Joining composite fuselage sections along window belts


    Additional title:

    Verbinden von Verbundwerkstoffrumpfabschnitten entlang von Fensterbändern
    Fixation des sections de fuselage composite le long des bandes de fenêtre


    Contributors:

    Publication date :

    2021-12-08


    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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