Methods of forming fiber-reinforced composite parts and fiber-reinforced composite parts formed thereby

Patent metadata

Field	Value
Publication number	US-11229934-B2
Application number	US-201916250156-A
Country	US
Kind code	B2
Filing date	Jan 17, 2019
Priority date	Jan 17, 2019
Publication date	Jan 25, 2022
Grant date	Jan 25, 2022

Abstract

A method of forming a fiber-reinforced composite part includes forming a composite preform by extruding a hollow metal shape onto a fiber-reinforced preform at an extrusion temperature and cooling the hollow metal shape from the extrusion temperature to a temperature less than the extrusion temperature. Heat from the hollow metal shape cooling from the extrusion temperature is conducted into the fiber-reinforced preform for curing thereof. Also, thermal contraction of the hollow metal shape onto the fiber-reinforced preform applies a consolidation pressure on the fiber-reinforced preform for curing thereof. The fiber-reinforced preform may be a hollow fiber-reinforced preform and a die can be moved through the hollow fiber-reinforced preform such that consolidation pressure is applied thereto by a combination of the thermal contraction of the hollow metal shape onto the hollow fiber-reinforced preform and the die moving through the hollow fiber-reinforced preform.

First claim

What is claimed is:

1. A method of forming a fiber-reinforced composite part comprising:
extruding a hollow metal shape at an extrusion temperature, wherein the hollow metal shape is extruded with an extrusion force;
forming and positioning a fiber-reinforced preform within the hollow metal shape, wherein the fiber-reinforced preform is rigidly held in position with a counter-force to the extrusion force;
extruding the hollow metal shape onto the fiber-reinforced preform while the fiber-reinforced preform is rigidly held in position; and
cooling the hollow metal shape from the extrusion temperature to a temperature less than the extrusion temperature, wherein heat from the hollow metal shape is conducted into the fiber-reinforced preform.

2. The method of claim 1 , wherein the fiber-reinforced preform is a solid fiber-reinforced preform.

3. The method of claim 2 further comprising applying a consolidation pressure onto the fiber-reinforced preform via thermal contraction of the hollow metal shape cooling from the extrusion temperature to the temperature less than the extrusion temperature.

4. The method of claim 1 , wherein the fiber-reinforced preform is a hollow fiber-reinforced preform.

5. The method of claim 4 further comprising applying a consolidation pressure to the hollow fiber-reinforced preform by moving a die through the hollow fiber-reinforced preform.

6. The method of claim 5 , wherein the die comprises an expandable mandrel.

7. The method of claim 5 , wherein the die is drawn through the hollow fiber-reinforced preform.

8. The method of claim 5 , wherein the hollow fiber-reinforced preform is extruded over the die.

9. The method of claim 1 , wherein the hollow metal shape is extruded from an aluminum alloy, a copper alloy, a titanium alloy, a nickel alloy, or a magnesium alloy.

10. The method of claim 1 , wherein the fiber-reinforced preform comprises carbon fibers and a polymer matrix.

11. The method of claim 10 , wherein the polymer matrix is a thermoplastic polymer matrix.

12. The method of claim 11 , wherein the thermoplastic polymer matrix comprises at least one of polyethylene (PE), polyethylene terephthalate (PET), polybutylene terephthalate (PBT), polycarbonate (PC), acrylonitrile butadiene styrene (ABS), polyamide (PA or nylon) and polypropylene (PP).

13. The method of claim 10 , wherein the polymer matrix is a thermosetting polymer matrix.

14. The method of claim 13 , wherein the thermosetting polymer matrix comprises at least one of an epoxy resin, a phenolic resin, a cyanate ester resin, a bismaleimide resin, a benzoxazine resin and a polyimide resin.

15. The method of claim 1 , wherein a barrier layer is positioned between the hollow metal shape and the fiber-reinforced preform.

16. A method of forming a fiber-reinforced composite part comprising:
extruding a hollow metal shape at an extrusion temperature and an extrusion force;
forming and positioning a hollow fiber-reinforced preform within the hollow metal shape, wherein the fiber-reinforced preform is rigidly held in position with a counter-force to the extrusion force;
extruding the hollow metal shape onto the fiber-reinforced preform while the fiber-reinforced preform is rigidly held in place; and
applying consolidation pressure and heat to the hollow fiber-reinforced preform and curing the hollow fiber-reinforced preform, wherein the consolidation pressure and heat is applied to the hollow fiber-reinforced preform by thermal contraction of and heat from the hollow metal shape, respectively, cooling from the extrusion temperature to a temperature less than the extrusion temperature.

17. The method of claim 16 further comprising moving a die through the hollow fiber-reinforced preform, wherein the thermal contraction of the hollow metal shape cooling from the extrusion temperature to a temperature less than the extrusion temperature and the die moving through the hollow fiber-reinforced preform apply the consolidation pressure to the hollow fiber-reinforced preform.

18. The method of claim 16 , wherein the hollow fiber-reinforced preform comprises carbon fibers and a polymer matrix.

19. A method of forming a fiber-reinforced composite part comprising:
extruding a hollow metal shape at an extrusion temperature and an extrusion force;
forming and positioning a fiber-reinforced preform within the hollow metal shape, wherein the fiber-reinforced preform is rigidly held in position with a counter-force to the extrusion force;
extruding the hollow metal shape onto the fiber-reinforced preform while the fiber-reinforced preform is rigidly held in position; and
cooling the hollow metal shape extruded onto the fiber-reinforced preform from the extrusion temperature to a temperature less than the extrusion temperature, wherein the hollow metal shape thermally contracts and provides a consolidation pressure onto the fiber-reinforced preform during the cooling of the hollow metal shape from the extrusion temperature to the temperature less than the extrusion temperature, heat from the cooling of the hollow metal shape is conducted into the fiber-reinforced preform, and the thermal contraction and heat from the cooling hollow metal shape cure the fiber-reinforced preform.

20. The method of claim 19 , wherein the fiber-reinforced preform is a hollow fiber-reinforced preform and further comprising moving a die through the hollow fiber-reinforced preform such that the thermal contraction of the hollow metal shape onto the fiber-reinforced preform and the die moving through the hollow fiber-reinforced preform provide the consolidation pressure onto the hollow fiber-reinforced preform.

Assignees

• Ford Global Tech Llc

Inventors

• Kowal Stephen

Classifications

• B21C35/023

  Work treatment directly following extrusion, e.g. further deformation or surface treatment  (B21C35/03 takes precedence; gas treatment B21C23/009) · CPC title

• B32B15/09

  comprising polyesters · CPC title

• B32B2262/106

  Carbon fibres, e.g. graphite fibres · CPC title

• B32B2262/101

  Glass fibres · CPC title

• B21C23/085

  Making tubes (B21C23/10 take precedence) · CPC title