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