The Boeing Company
Interlayer-toughened filament-wound composite structure

Abstract:

Disclosed herein is a method for filament winding. The method includes bonding a veil material to the unidirectional fabric to veil-stabilize the unidirectional fabric. The method also includes slitting the veil-stabilized unidirectional fabric to separate a veil-stabilized fabric portion. The method also includes directing the veil-stabilized fabric portion to an application head. The method also includes winding the veil-stabilized fabric portion on a winding mandrel.