Systems and methods are provided for assembling a section of a fuselage of an aircraft. The method includes pulsing a half barrel section of the fuselage along a track in a process direction, utilizing an indexing feature associated with the half barrel section to determine a desired contour for a portion of the half barrel section, and enforcing the desired contour onto the half barrel section using components that enforce an inner mold line and components that enforce an outer mold line when the half barrel section is out of tolerance from the desired contour.
Contour Enforcement For Line Assembled Fuselage Segments
2024-05-23
Patent
Electronic Resource
English
IPC: | 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 / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64C AEROPLANES , Flugzeuge |
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