A fuselage for an airplane including a frame comprising an upper truss and a lower truss extending from a front end of the fuselage towards the rear end of the fuselage, wherein the lower truss comprises one or more forward box beams, a plurality of support rings attached to the upper truss and lower truss, a front bulkhead connected to a first end of the upper truss and lower truss, a main bulkhead connected to the upper truss and lower truss, a pressure vessel adapted to fit within the frame between the front bulkhead and main bulkhead, and a skin adapted to fit over the frame.


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    Titel :

    AIRCRAFT SUPPORT STRUCTURE


    Weitere Titelangaben:

    TRAGESTRUKTUR FÜR EIN FLUGZEUG
    STRUCTURE DE SUPPORT D'AÉRONEF


    Beteiligte:
    OTTO WILLIAM M (Autor:in)

    Erscheinungsdatum :

    2021-10-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn



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