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.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT SUPPORT STRUCTURE


    Additional title:

    TRAGESTRUKTUR FÜR EIN FLUGZEUG
    STRUCTURE DE SUPPORT D'AÉRONEF


    Contributors:

    Publication date :

    2021-10-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn



    Aircraft support structure

    OTTO WILLIAM M | European Patent Office | 2015

    Free access

    SUPPORT STRUCTURE FOR AIRCRAFT

    CLARK VICTORIA A / WECKNER OLIVER / SMITH JEFFREY D et al. | European Patent Office | 2024

    Free access

    TUBE SUPPORT STRUCTURE FOR AIRCRAFT

    MINAMI KEISUKE | European Patent Office | 2016

    Free access

    TUBE SUPPORT STRUCTURE FOR AIRCRAFT

    MINAMI KEISUKE | European Patent Office | 2019

    Free access

    SUPPORT STRUCTURE FOR AN AIRCRAFT

    CLARKE VICTORIA A / WECKNER OLAF / SMITH JAY D et al. | European Patent Office | 2024

    Free access