The Boeing Company
Hybrid non-woven composite part

Abstract:

Disclosed herein is a method of forming a composite part. The method includes heating an unconsolidated mat including a first thermoplastic, a second thermoplastic, and reinforcing fibers to a first temperature. The first thermoplastic includes a first melting temperature and the second thermoplastic includes a second melting temperature greater than the first melting temperature. The first temperature is greater than the second melting temperature. The method includes compressing the unconsolidated mat, while heated, into a composite fiber-reinforced consolidated sheet. The method includes reheating the composite fiber-reinforced consolidated sheet to a second temperature, wherein the second temperature is above the first melting temperature and below the second melting temperature and, while reheated, forming the composite fiber-reinforced consolidated sheet into a desired shape.