A system and method are provided to automate the assembly of a wing panel, such as utilized by commercial aircraft. In the context of a system, a tacking cell is provided that is configured to tack one or more stringers to a skin plank. The system also includes a riveting cell configured to receive a tacked plank from the tacking cell and to rivet the one or more stringers to the skin plank. The system also includes a splicing cell configured to receive a plurality of riveted planks from the riveting cell and to attach one or more splice stringers to the plurality of riveted planks. Further, the system includes a side of body cell configured to receive a spliced panel from the splicing cell and to attach a side of body chord thereto to produce a wing panel.


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    Titel :

    System and method for manufacturing a wing panel


    Beteiligte:
    SISCO FARAHNAZ TANNI (Autor:in) / SMITH DANIEL R (Autor:in) / AQUINO JAYSON J (Autor:in) / BATT EDWARD JOHN (Autor:in) / BUTTRICK JAMES N (Autor:in) / MICALE ANTONIO C (Autor:in) / JONES DARRELL D (Autor:in) / MUNK CLAYTON L (Autor:in) / COUEVAS CHRIS G (Autor:in) / NAMDARAN AZITA N (Autor:in)

    Erscheinungsdatum :

    2018-04-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B23P Sonstige Metallbearbeitung , OTHER WORKING OF METAL / B21J FORGING , Schmieden / 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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