A method for wing-to-fuselage integration is disclosed. The method includes attaching a fitting to a wing box assembly of an aircraft at an early stage of integration and then attaching the fitting to a stub beam attached to a fuselage panel of the aircraft at a later stage of integration. The fitting eliminates the need to attach the stub beam directly to the wing box assembly.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Methods and Components for Wing-to-Fuselage Integration


    Beteiligte:

    Erscheinungsdatum :

    2018-03-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / 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



    Methods and components for wing-to-fuselage integration

    LOCKIN CHARLES B / ERICKSON MARCUS A / ADEDEJI OLADELE A et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    Methods and components for wing-to-fuselage integration

    LOCKIN CHARLES B / ERICKSON MARCUS A / ADEDEJI OLADELE A et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    Experimental investigation of wing/fuselage integration geometries

    MAUGHMER, M. / HALLMAN, D. / RUSZKOWSKI, R. et al. | AIAA | 1989


    Method And Apparatus For Wing-To-Fuselage Integration

    LOCKIN CHARLES B / ERICKSON MARCUS A / ADEDEJI OLADELE A et al. | Europäisches Patentamt | 2016

    Freier Zugriff