Systems and methods are provided for assembly line (100) processing of aircraft wing panels (150). The method includes inputting wing panels (150) into an assembly line (100), the assembly line (100) having a number of work stations (120), the wing panels (150) oriented such that leading edges (155) are all on a first side (166) of the work stations (120), and trailing edges (157) are all on a second side (165) of the work stations (120), and advancing the wing panels (150) in a process direction (181) through the number of work stations (120), at least a first portion of the work stations (120) dedicated to wing panel leading edge (155) processing, and a second portion of the work stations (120) dedicated to wing panel trailing edge (157) processing.


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    Titel :

    MIRRORED FABRICATION AND ASSEMBLY OF AIRCRAFT WINGS


    Weitere Titelangaben:

    GESPIEGELTE HERSTELLUNG UND MONTAGE VON FLUGZEUGTRAGFLÄCHEN
    FABRICATION REFLÉTÉE ET ENSEMBLE D'AILES D'AÉRONEF


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

    Erscheinungsdatum :

    2022-05-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B21J FORGING , Schmieden / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / 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 / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL



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