Mirrored fabrication and assembly of aircraft wings

Systems and methods are provided for assembly line processing of aircraft wing panels. The method includes inputting wing panels into an assembly line, the assembly line having a number of work stations, the wing panels oriented such that leading edges are all on a first side of the work stations, a...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Jones, Darrell D, Smith, Daniel R
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:Systems and methods are provided for assembly line processing of aircraft wing panels. The method includes inputting wing panels into an assembly line, the assembly line having a number of work stations, the wing panels oriented such that leading edges are all on a first side of the work stations, and trailing edges are all on a second side of the work stations, and advancing the wing panels in a process direction through the number of work stations, at least a first portion of the work stations dedicated to wing panel leading edge processing, and a second portion of the work stations dedicated to wing panel trailing edge processing.