Metal-coated fabrics for fiber-metal laminates

Patent metadata

Field	Value
Publication number	US-11407199-B2
Application number	US-42402109-A
Country	US
Kind code	B2
Filing date	Apr 15, 2009
Priority date	Apr 15, 2009
Publication date	Aug 9, 2022
Grant date	Aug 9, 2022

Abstract

Disclosed herein are laminates that include a layer containing a metal-coated fabric. The laminate may also include a layer or layers of an organic polymeric matrix composite. In accordance with certain embodiments, the matrix composite includes a thermosetting or thermoplastic resin matrix with parallel-oriented reinforcing fibers embedded therein, interposed between the metal-coated fabric layers.

First claim

What is claimed is:

1. A composite structure comprising:
a laminate, wherein the laminate comprises:
a first non-reinforced layer comprising a polymeric fiber that is coated with a metal coating to create a metal-coated fabric;
a second fiber-reinforced layer of polymeric composite comprising a polymeric resin and a first set of parallel reinforcing fibers embedded in the polymeric resin, wherein the reinforcing fibers are not metal-coated; and
a third fiber-reinforced layer of polymeric composite comprising the polymeric resin and a second set of parallel reinforcing fibers embedded in the polymeric resin that are not metal-coated, wherein the first non-reinforced layer is bonded to the second fiber-reinforced layer and the third fiber-reinforced layer by an adhesive.

2. The composite structure of claim 1 , wherein the material of the reinforcing fibers is selected from the group consisting of aramids, polyolefins, glass, carbon, boron and ceramics.

3. The composite structure of claim 1 , wherein the metal is selected from the group consisting of titanium, aluminum, alloys of titanium, alloys of aluminum, and alloys of iron.

4. The composite structure of claim 3 , wherein the metal comprises titanium or an alloy of titanium.

5. The composite structure of claim 1 , wherein the polymeric resin is selected from the group consisting of epoxies, bismaleimides, cyanate esters, phenolics, polybenzoxazoles, polyaryletherketones, polyetheretherketones, polyimides, polyarylethersulfones, oxydiphthalic dianhydride 3, 4′ oxydianiline, and functional derivatives thereof.

6. The composite structure of claim 1 , wherein the thickness of the metal coating is from about 1 μm to about 25 μm.

7. The composite structure of claim 1 , wherein the polymeric fabric comprises a first metal coating of a first metal and a second metal coating of a second metal.

8. An aircraft skin panel comprising the composite structure of claim 1 .

9. The composite structure of claim 1 , wherein the reinforcing fibers of the layer of polymeric composite are selected from the group consisting of carbon, boron, and combinations thereof.

10. The composite structure of claim 1 , wherein the polymeric fabric, without the metal coating, has a weight of about 2 to about 20 gsm.

11. The composite structure of claim 1 , wherein the polymeric fabric, without the metal coating, has a weight of less than 1 gsm.

12. The composite structure of claim 1 , further comprising a core layer having at least one layer of the metal-coated fabric and at least one layer of polymeric composite on both sides thereof in a symmetrical arrangement of layers.

13. The composite structure of claim 1 , wherein the reinforcing fibers of the second fiber-reinforced layer of polymeric composite and the third fiber-reinforced layer of polymeric composite include a cross-sectional diameter of about 5 μm to about 50 μm.

14. The composite structure of claim 1 , wherein the metal coating completely covers the polymeric fiber of the metal-coated fabric.

15. The composite structure of claim 1 , wherein the metal coating partially covers the polymeric fiber of the metal-coated fabric.

16. A composite structure, the structure comprising;
a laminate, the laminate comprising:
a layup comprising laminated layers of metal-coated fabric layers, wherein the metal-coated fabric layers are non-reinforced and constructed of a polymeric fiber that is coated with a metal coating; and
an organic polymeric composite layer between adjacent metal-coated fabric layers, the composite layer being a reinforced layer comprising at least two plies, wherein the at least two plies comprise a polymeric matrix having commonly aligned reinforcing fibers embedded therein, wherein the reinforcing fibers are not metal, and wherein at least one of the metal-coated fabric layers are bonded to either the first ply or the second ply by an adhesive.

17. The composite structure of claim 16 , wherein the layup further comprises an outer layer of metal-coated fabric, the outer layer bonded to an adjacent composite ply.

18. The composite structure of claim 16 , wherein the polymeric matrix is selected from the group consisting of epoxies, bismaleimides, cyanate esters, phenolics, polybenzoxazoles, polyaryletherketones, polyetheretherketones, polyimides, polyarylethersulfones, oxydiphthalic dianhydride 3, 4′ oxydianiline, and functional derivatives thereof.

19. The composite structure of claim 16 , wherein the reinforcing fibers are selected from the group consisting of graphite and boron fibers.

20. The composite structure of claim 16 , wherein the metal coating completely covers the polymeric fiber of the metal-coated fabric.

Assignees

• Tsotsis Thomas K
• Boeing Co

Inventors

• Tsotsis Thomas K

Classifications

• B32B2307/306

  Resistant to heat · CPC title

• B32B2262/0276

  Polyester fibres · CPC title

• B32B27/28

  comprising synthetic resins not wholly covered by any one of the sub-groups {B32B27/30 - B32B27/42} · CPC title

• B32B2309/02

  Temperature · CPC title

• B32B2307/718

  Weight, e.g. weight per square meter · CPC title