The Boeing Company
SYSTEM, METHOD, AND APPARATUS FOR USE IN PLY COMPACTION IN FORMING A COMPOSITE STRUCTURE

Abstract:

A method for use in ply compaction in forming a composite structure. The method includes positioning a ply of material on a forming tool having a web surface and at least one flange surface extending from the web surface, positioning a flange forming device at the ply of material on the forming tool, the flange forming device including an inflatable contact element pressurized to define a deformable contact surface, applying, by the deformable contact surface, the ply of material onto the forming tool with a predetermined pressure, wherein the deformable contact surface is moved across the forming tool, and wherein the inflatable contact element is configured to maintain the predetermined pressure as the deformable contact surface transitions from the web surface to the at least one flange surface.