In a fuselage portion for an aircraft, in order to reduce the assembly clearance between the soleplate (120) of a circumferential frame and a fuselage skin (112) in composite material while limiting the mass of the fuselage portion, a ply drop-off (118) is used comprising two portions (124, 126) oriented in the circumferential direction and having different respective slopes.


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    Titel :

    Aircraft fuselage portion made of composite material


    Beteiligte:

    Erscheinungsdatum :

    2015-05-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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