Systems and methods are provided for installing ribs (572) and/or spars (580) to a wing panel (550) while a contour is enforced. Methods include suspending a wing panel beneath a shuttle (540) that enforces the contour, advancing the wing panel through work stations (520) via the shuttle, and installing a rib or a spar (or another wing panel) at a work station, while the contour is enforced. Other methods include locating a wing panel beneath a shuttle, coupling adjustable-length pogos (545) to the wing panel at locations distinct from those corresponding with an installation location, e.g. for a rib or a spar, and controlling the length of the pogos to enforce a contour to the wing panel. Some systems include a track (510), work stations disposed along the track, and a shuttle to advance along the track and convey a wing panel to each of the work stations while enforcing a contour onto the wing panel.


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    Titel :

    ASSEMBLY LINE FABRICATION AND ASSEMBLY OF AIRCRAFT WINGS


    Weitere Titelangaben:

    FLIESSBANDFERTIGUNG UND MONTAGE VON FLUGZEUGFLÜGELN
    FABRICATION ET ASSEMBLAGE EN LIGNE D'AILES D'AÉRONEF


    Beteiligte:
    SMITH DANIEL R (Autor:in) / JONES DARRELL D (Autor:in)

    Erscheinungsdatum :

    2022-05-25


    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



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