Molding composite part with metal layer

Patent metadata

Field	Value
Publication number	US-11634820-B2
Application number	US-201916445102-A
Country	US
Kind code	B2
Filing date	Jun 18, 2019
Priority date	Jun 18, 2019
Publication date	Apr 25, 2023
Grant date	Apr 25, 2023

Abstract

A method of molding a metalized composite part. The method comprises: introducing particles comprising at least one metal into a gas stream; directing the gas stream toward a surface of a thermoplastic composite part, thereby depositing a metal layer on the composite part to form a metallized composite part; and molding the metallized composite part to introduce a bend without delamination of the metal layer from the metallized composite part.

First claim

What is claimed is:

1. A method of molding a metallized composite part, the method comprising:
disposing an electrochemical insulating layer comprising poly-ether-ether-ketone (PEEK), poly-ether-ketone-ketone (PEKK), or a combination thereof, onto a surface of a thermoplastic composite part;
introducing particles comprising at least one metal into a gas stream, the particles being at a temperature that is lower than the melting point of the particles;
directing the gas stream toward a surface of the thermoplastic composite part, thereby cold spraying a metal layer on the composite part to form the metallized composite part;
after forming the metallized composite part, heating the metal layer at an anneal temperature ranging from about 315° C. to about 400° C., the anneal temperature being maintained for a period of time ranging from about 30 seconds to about 30 minutes so as to increase ductility of the metal layer compared to the ductility of the metal layer prior to the heating; and
molding the metallized composite part to introduce a bend without delamination of the metal layer from the metallized composite part, wherein the heating occurs prior to the molding; and
wherein the electrochemical insulating layer is between the thermoplastic composite part and the metal layer.

2. The method of claim 1 , wherein the at least one metal is chosen from aluminum, copper, gold, and silver.

3. The method of claim 2 , further comprising coating onto the metal layer at least one additional metal layer that is different from the metal layer, wherein the at least one additional metal layer comprises at least one metal chosen from Ag, Al, Au, Co, Cr, Fe, Ni, Mo, Pd, Pt, Rh, Ru, Sn, Ti, W, Zn, and Zr.

4. The method of claim 3 , wherein an electrochemical insulating layer is disposed between the thermoplastic composite part and the metal layer.

5. The method of claim 1 , wherein the thermoplastic composite part comprises a thermoplastic and one or more filler materials.

6. The method of claim 5 , wherein the one or more filler materials are chosen from carbon nanotubes, inorganic fibers, carbon fibers, graphite fibers, woven glass fibers, unwoven glass fibers, ceramic fibers, alumina fibers, boron fibers, metal fibers, metalized fibers, metal coated glass fibers, metal coated alumina fibers, metal coated boron fibers, carbon particles, graphite particles, metal particles, glass particles, organic fibers and combinations thereof.

7. The method of claim 1 , wherein the metal layer imparts electrical EMI resistance or lightning protection, erosion protection, electromagnetic interference shielding, electromagnetic emission shielding, or lightning strike protection to the metalized composite part.

8. The method of claim 1 , further comprising heating the particles prior to the cold spraying of the metal layer at an anneal temperature ranging from about 315° C. to about 400° C. to increase ductility of the metal layer.

9. The method of claim 1 , wherein the metal layer has a thickness ranging from about 0.01 mil to about 20 mils.

10. The method of claim 1 , wherein the metal layer allows the composite to be paintable.

11. The method of claim 1 , wherein the metal layer provides UV protection to the thermoplastic composite part.

12. The method of claim 1 , further comprising cold spray coating or thermal spray coating onto the metal layer at least one additional metal layer different from the metal layer.

13. The method of claim 12 , wherein the at least one additional metal layer comprises at least one metal chosen from Ag, Al, Au, Co, Cr, Cu, Fe, Ni, Mo, Pd, Pt, Rh, Ru, Sn, Ti, W, Zn, and Zr.

14. The method of claim 1 , wherein the gas stream has a temperature and pressure adjusted to prevent significant thermal softening or significant ablation of the surface of the electrochemical insulating layer.

15. The method of claim 1 , wherein the metal layer has a thickness ranging from 4 mils to about 20 mils.

16. The method of claim 1 , wherein the metallized composite part is molded while the metallized composite part is at the anneal temperature.

17. The method of claim 1 , further comprising attaching the molded metallized composite part to an exterior of a wing of an aircraft, and wherein the metal layer isolates an electrical charge from a lightning strike from the thermoplastic composite part, thereby preventing edge glow.

18. The method of claim 1 , wherein an electrochemical insulating layer is positioned between the thermoplastic composite part and the metal layer, and further comprising attaching an additional metal layer on the metal layer, wherein the metal layer comprises aluminum, and wherein the additional metal layer comprises nickel.

19. The method of claim 1 , further comprising heating the metal layer at an anneal temperature after molding.

20. A method of imparting electrical EMI resistance or lightning protection to a thermoplastic composite part, the method comprising:
disposing an electrochemical insulating layer comprising poly-ether-ether-ketone (PEEK), poly-ether-ketone-ketone (PEKK), or a combination thereof, onto a surface of the thermoplastic composite part;
introducing particles comprising at least one metal into a gas stream, the particles being at a temperature that is lower than the melting point of the particles;
directing the gas stream toward a surface of a thermoplastic composite part, thereby cold spraying a metal layer on the composite part to form a metallized composite part;
after forming the metallized composite part, heating the metal layer at an anneal temperature ranging from about 315° C. to about 400° C., the anneal temperature being maintained for a period of time ranging from about 30 seconds to about 30 minutes so as to increase ductility of the metal layer compared to the ductility of the metal layer prior to the heating; and
molding the metallized composite part to introduce a bend without delamination of the metal layer from the metallized composite part,
wherein the electrochemical insulating layer is between the thermoplastic composite part and the metal layer,
wherein the heating of the metal layer occurs prior to the molding, and
wherein the metal layer imparts electrical EMI resistance or lightning protection to the thermoplastic composite part.

21. The method of claim 20 , wherein the metal layer comprises at least one metal chosen from aluminum, copper, gold, and silver.

22. The method of claim 21 , further comprising coating onto the metal layer at least one additional metal layer that is different from the metal layer, wherein the at least one additional metal layer comprises at least one metal chosen from Ag, Al, Au, Co, Cr, Fe, Ni, Mo, Pd, Pt, Rh, Ru, Sn, Ti, W, Zn, and Zr.

23. The method of claim 22 , wherein an electrochemical insulating layer is disposed between the thermoplastic composite part and the metal layer.

24. The method of claim 20 , further comprising heating the particles prior to the cold spraying of the metal layer at an anneal temperature ranging from about 315° C. to about 400° C. to increase ductility of the metal layer.

25. The method of claim 24 , wherein the heating of the metal layer occurs prior to the molding of the metal layer.

26. The method of claim 25 , wherein the anneal temperature is maintained for a period of time ranging from about 2 minutes to about 30 minutes.

27. The method of claim 20 , wherei

Assignees

• Boeing Co

Inventors

• Bruton Eric A
• Childers Christopher H
• Gaydos Stephen P

Classifications

• B29K2995/0011

  Electromagnetic wave shielding material · CPC title

• H05K9/0088

  comprising a plurality of shielding layers; combining different shielding material structure · CPC title

• C23C28/023

  only coatings of metal elements only · CPC title

• B29C53/04

  of plates or sheets {(B29C63/04 takes precedence; bending or folding paper B31F1/0003; folding films B65H45/00)} · CPC title

• C23C24/04 Primary

  Impact or kinetic deposition of particles · CPC title