Fabrication of reinforced thermoplastic composite parts

Patent metadata

Field	Value
Publication number	US-9498915-B2
Application number	US-201313732624-A
Country	US
Kind code	B2
Filing date	Jan 2, 2013
Priority date	Jan 2, 2013
Publication date	Nov 22, 2016
Grant date	Nov 22, 2016

Abstract

A method of fabricating a reinforced thermoplastic composite part comprises moving a laminate of reinforcing fibers embedded in a thermoplastic matrix for sequential operations through a heating station and then a forming station. The heating station is used to soften the thermoplastic matrix in a portion of the laminate while the forming station is used to impart a geometry to a portion of the laminate whose thermoplastic matrix had just been softened. The softening and the forming are performed simultaneously on different portions of the laminate.

First claim

The invention claimed is:

1. A method of fabricating a reinforced thermoplastic composite part, the method comprising:
moving a stack of plies of reinforcing fibers impregnated with thermoplastic resin for sequential operations through separate stations including a consolidation station, a heating station downstream of the consolidation station, and a forming station downstream of the heating station;
wherein the consolidation station consolidates the stack of plies into a laminate under heat and pressure and softens the thermoplastic resin without causing the resin to flow, the heating station softens the thermoplastic resin without causing the resin to flow, and the forming station imparts a geometry to the laminate to provide the reinforced thermoplastic composite part; and
wherein the consolidation station, the heating station, and forming station simultaneously operate on different portions of the stack of plies.

2. The method of claim 1 , further comprising stacking the plies at a layup station upstream of the consolidation station as a downstream portion of the stack of plies is consolidated at the consolidation station.

3. The method of claim 1 , wherein the consolidation station includes upper and lower zones of a plurality of infrared elements that soften the resin.

4. The method of claim 1 , wherein the forming is performed with tools that are heated integrally to promote crystallization and ply slippage.

5. The method of claim 4 , wherein the forming includes using multi-stage tooling to impart different geometries to the laminate.

6. The method of claim 5 , wherein the forming is performed as a multi-shot stamping operation.

7. The method of claim 1 , further comprising adding attachment features to the formed portion of the laminate.

8. The method of claim 1 , wherein a conveyor belt is used to move the laminate through the stations.

9. The method of claim 8 , wherein a flexible polymer film is used as the conveyor belt to carry the laminate as it is moved sequentially through the stations, and wherein the film is peeled from the laminate after forming.

10. The method of claim 1 , wherein the forming is performed with a tool that is moved along with the laminate.

11. The method of claim 1 , wherein the laminate is formed into an integrally stiffened part having continuous or stretch broken fiber reinforcement.

12. A method comprising:
moving a ply stack of reinforcing fibers pre-impregnated with thermoplastic resin sequentially through separate consolidating, heating and forming stations with a conveyor belt to form a laminate, the conveyor belt including a flexible polymer film; and
peeling the polymer film from the laminate after the forming;
wherein the consolidation station, the heating station, and the forming station simultaneously operate on different portions of the ply stack.

13. The method of claim 12 , further comprising stacking plies to create an upstream portion of the ply stack while downstream portions of the ply stack are being consolidated, heated, and formed.

Assignees

• Boeing Co

Inventors

• Bartel Aaron W
• Gideon David E
• Larson Michael H

Classifications

• B29C70/50 Primary

  for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC] · CPC title

• B29C51/02 Primary

  Combined thermoforming and manufacture of the preform · CPC title

• B29D99/0003 Primary

  Producing profiled members, e.g. beams · CPC title