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.
MIRRORED FABRICATION AND ASSEMBLY OF AIRCRAFT WINGS
2022-05-19
Patent
Elektronische Ressource
Englisch
ASSEMBLY LINE FABRICATION AND ASSEMBLY OF AIRCRAFT WINGS
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