Frame (1) for fuselage shells of an aircraft, the fuselage comprising a skin (3) and stringers (4), the frame (1) comprising:- a plurality of sections (5), the sections (5) being separated by intermediate gaps corresponding to the position of the stringers (4) in the fuselage, each section (5) having a multi-cell configuration constituted by several modular elements (6) of composite material arranged in longitudinal direction, and- a continuous inner cap (7) on top of the sections (5) and the intermediate gaps.


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    Title :

    FRAME FOR FUSELAGE SHELLS OF AN AIRCRAFT AND FUSELAGE SHELL


    Additional title:

    RAHMEN FÜR RUMPFSCHALEN EINES FLUGZEUGS UND RUMPFSCHALE
    CADRE POUR COQUES DE FUSELAGE D'UN AÉRONEF ET COQUE DE FUSELAGE



    Publication date :

    2021-06-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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