The Boeing Company
Wrinkle reduction in formed composite laminates
Last updated:
Abstract:
Wrinkling of a contoured composite laminate part during forming to contour is reduced by using laminate plies having off-angle reinforcing fibers that provide the part with primary axial strength along a major axis of loading.
Status:
Grant
Type:
Utility
Filling date:
28 Jun 2016
Issue date:
22 Oct 2019