A method of assembling a panelized aircraft fuselage comprises loading a keel structure on a cradle; attaching stanchions to a floor grid; positioning the floor grid and stanchions over the keel structure and attaching the stanchions to the keel structure; obtaining a full fuselage contour including locating lower panels on the floor grid while using the cradle, the floor grid, and the keel structure to support the lower panels, and locating upper panels on the lower panels; and fastening the lower panels to the keel structure and the upper panels. The fuselage is assembled upright from the keel structure without changing orientation of the fuselage.


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    Titel :

    Method of assembling panelized aircraft fuselages


    Beteiligte:
    OBEROI HARINDER S (Autor:in) / NELSON BLAIR P (Autor:in) / DRAPER ALAN S (Autor:in) / HU CHARLES Y (Autor:in) / MATTHEWSON RANDALL (Autor:in) / SARH BRANKO (Autor:in)

    Erscheinungsdatum :

    2015-07-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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