In the present invention, a fuselage is easily manufactured. The method of the present invention includes: scooping a trunk section (6) using a strong back (8-i), the trunk section (6) being supported by a dolly; disposing the trunk section (6) at a predetermined location by moving the strong back (8-i) using a positioner; and joining the trunk section (6) to a standard fuselage when the trunk body (6) is disposed at the predetermined location. This method for bonding a fuselage is capable of supporting the trunk section (6) by the positioner without using a crane. Therefore, according to this method for bonding a fuselage, it is possible to avoid having to provide to the trunk section (6) an outside fitting (101) used when the crane is used, and to more easily manufacture the fuselage.


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    Titel :

    METHOD FOR BONDING FUSELAGE AND STRONG BACK


    Weitere Titelangaben:

    VERFAHREN ZUM VERBINDEN EINES RUMPFES UND STARKEN HECKTEILS
    PROCÉDÉ DE COLLAGE D'UN FUSELAGE ET D'UNE PIÈCE DE RENFORT


    Beteiligte:

    Erscheinungsdatum :

    22.07.2020


    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 / B64C AEROPLANES , Flugzeuge



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