Systems and methods are provided for enforcing contours onto parts of an aircraft. One embodiment is a method for enforcing a contour onto aircraft parts. The method includes removaby attaching segmented ring details 852-856 to aircraft skin details 210, attaching stringers 320 to skin details to create skin assemblies, positioning skin assemblies at a support structure defining a contour, and fastening frames 310 to the skin assemblies to create a panel. The method also includes removably installing a spreader section 800 onto the panel to complete assembly of a brace prior to removal of the panel, transporting the panel while the brace enforces the contour, attaching the brace to braces for other panels to form a barrel section of a fuselage for an aircraft while the brace enforces the contour, and removing the brace from the barrel section after the barrel section has been formed.
CONTOUR RETENTION IN SEGMENTED FUSELAGE ASSEMBLIES
KONTURRETENTION IN SEGMENTIERTEN RUMPFANORDNUNGEN
RÉTENTION DE CONTOUR DANS DES ENSEMBLES DE FUSELAGE SEGMENTÉS
2020-07-01
Patent
Electronic Resource
English