The present application relates to a fuselage assembly for an aircraft. The fuselage assembly has a stringer extending longitudinally along the fuselage. The stringer defines a fluid channel. The fluid channel is configured to form at least part of a distribution duct of a cabin air distribution system. The present application also relates to a cabin air distribution system, a frame for an aircraft fuselage, and an aircraft. The frame can also comprise a fluid duct and a skin mounting section configured to mount to a skin of the aircraft fuselage, wherein the fluid duct is spaced from the skin mounting section.


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    Title :

    FUSELAGE ASSEMBLY FOR AN AIRCRAFT


    Additional title:

    RUMPFANORDNUNG FÜR EIN FLUGZEUG
    ENSEMBLE FUSELAGE POUR AÉRONEF



    Publication date :

    2024-05-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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