The Boeing Company
Edge dams for fabrication of composite parts

Abstract:

Systems and methods are provided for composite part fabrication. One embodiment is a method that includes placing a laminate onto a base of a mandrel between side walls of the mandrel, placing edge dams between the side walls and the laminate that each abut the laminate and abut one of the side walls, each edge dam having a Coefficient of Thermal Expansion (CTE) greater than a CTE of the mandrel, the CTE of the mandrel being greater than a CTE of the laminate, heating the laminate, edge dams, and mandrel, and during the heating, thermally expanding the edge dams an amount that corresponds with a difference in thermal expansion between the laminate and the mandrel.