Products comprising reinforcing fibres and shape memory alloy wires and methods of making thereof

Patent metadata

Field	Value
Publication number	US-11358308-B2
Application number	US-201816623341-A
Country	US
Kind code	B2
Filing date	Jun 26, 2018
Priority date	Jun 28, 2017
Publication date	Jun 14, 2022
Grant date	Jun 14, 2022

Abstract

Some embodiments are directed to a three-dimensional (3D) preform including reinforcing fibres and shape memory alloys (SMA) wires and a composite material including a polymer matrix with a 3D-preform embedded therein, wherein the 3D-preform includes reinforcing fibres and shape memory alloy (SMA) wires.

First claim

The invention claimed is:

1. A composite material, comprising:
a polymer matrix with a three-dimensional (3D) preform embedded therein,
wherein the 3D-preform includes reinforcing fibres and shape memory alloy (SMA) wires.

2. The composite material of claim 1 , wherein the 3D-preform includes at least two layers, each independently including reinforcing fibres, SMA wires or a combination thereof, wherein the layers are stacked on top of each other and are held together by at least one filament transversing at least two of the layers.

3. The composite material of claim 1 , wherein the 3D-preform includes combination tows of reinforcing fibre and SMA wire.

4. The composite material of claim 2 , wherein the at least one filament transversing the at least two of the layers is reinforcing fibre, SMA wire or a combination thereof.

5. The composite material of claim 2 , wherein each of the layers is independently non-interlaced (e.g. non-crimp fabric or non-crimp woven fabric), woven, braided or knitted.

6. The composite material of claim 2 , wherein the at least one filament transversing the at least two of the layers is woven, stitched, tufted or z-pinned.

7. The composite material of claim 1 , wherein the 3D-preform is an orthogonal three-dimensional woven preform, an angle-interlock three-dimensional woven preform or a layer-to-layer three-dimensional woven preform.

8. The composite material of claim 1 , wherein the 3D-preform is a fully interlaced woven preform, a fully braided preform or a fully knitted preform.

9. The composite material of claim 1 , wherein the SMA wires are each independently of a composition and in a proportion to substantially enhance the impact performance or penetration resistance of the structure at a predetermined operating temperature or range thereof.

10. The composite material of claim 1 , wherein each SMA is independently selected from the group comprising Ti—Ni, Ti—Ni—Cu, Ti—Ni—Nb, Ti—Ni—Hf, Cu—Zn—Al, Cu—Al—Ni, Cu—Al—Zn—Mn, Cu—Al—Ni—Mn, Cu—Al—Mn—Ni, Fe—Mn—Si, Fe—Cr—Ni—Mn—Si—Co, Fe—Ni—Mn, Fe—Ni—C and Fe—Ni—Co—Ti alloys.

11. The composite material of claim 1 , wherein the volume fraction of the SMA wires in the composite material ranges from about 2% to about 25%.

12. The composite material of claim 2 , wherein the SMA wires each independently have a cross-section that is substantially longer in a first dimension than in a second dimension perpendicular to the first and are positioned in the 3D preform such that the longer dimension is generally parallel to the plane of the layers.

13. The composite material of claim 1 , wherein the reinforcing fibres each independently have a tensile modulus in excess of 50 GPa, for example in excess of 200 GPa.

14. The composite material of claim 1 , wherein the reinforcing fibres are each independently selected from carbon fibres, glass fibres, aramid fibres, polyethylene fibres and boron fibres.

15. A three-dimensional (3D) preform, comprising:
reinforcing fibres and
shape memory alloy (SMA) wires.

16. The 3D-preform of claim 15 , wherein the 3D-preform includes at least two layers, each independently including reinforcing fibres, SMA wires or a combination thereof, and wherein the layers are stacked on top of each other and are held together by at least one filament transversing at least two of the layers.

17. The 3D-preform of claim 15 , wherein the 3D-preform includes combination tows of reinforcing fibres and SMA wire.

18. The 3D-preform of claim 16 , wherein the at least one filament transversing the at least two of the layers is reinforcing fibre, SMA wire or a combination thereof.

19. The 3D-preform of claim 16 , wherein each of the layers is independently non-interlaced (e.g. non-crimp fabric or non-crimp woven fabric), woven, braided or knitted.

20. The 3D-preform of claim 16 , wherein the at least one filament transversing the at least two of the layers is/are woven, stitched, tufted, z-pinned or a combination thereof.

21. The 3D-preform of claim 16 , wherein the 3D-preform is an orthogonal three-dimensional woven preform, an angle-interlock three-dimensional woven preform or a layer-to-layer three-dimensional woven preform.

22. The 3D-preform of claim 15 , wherein the 3D-preform is a fully interlaced woven preform, a fully braided preform or a fully knitted preform.

23. The 3D-preform of claim 15 , wherein the SMA wires are each independently of a composition and in a proportion to substantially enhance the impact performance or penetration resistance of the structure at a predetermined operating temperature or range thereof.

24. The 3D-preform of claim 15 , wherein the SMA is selected from the group comprising Ti—Ni, Ti—Ni—Cu, Ti—Ni—Nb, Ti—Ni—Hf, Cu—Zn—Al, Cu—Al—Ni, Cu—Al—Zn—Mn, Cu—Al—Ni—Mn, Cu—Al—Mn—Ni, Fe—Mn—Si, Fe—Cr—Ni—Mn—Si—Co, Fe—Ni—Mn, Fe—Ni—C and Fe—Ni—Co—Ti alloys.

25. The 3D-preform of claim 15 , wherein the volume fraction of the SMA wires in the composite material ranges from about 2% to about 25%.

26. The 3D-preform any one of claim 15 wherein the SMA wires each independently have a cross-section that is substantially longer in a first dimension than in a second dimension perpendicular to the first and are positioned in the 3D preform such that the longer dimension is generally parallel to the plane of the layers.

27. The 3D-preform of claim 15 , wherein the reinforcing fibres each independently have a tensile modulus in excess of 50 GPa, for example in excess of 200 GPa.

28. The 3D-preform of claim 15 , wherein the reinforcing fibres are each independently selected from carbon fibres, glass fibres, aramid fibres, polyethylene fibres and boron fibres.

29. A method of making the composite material according to claim 1 , the method comprising:
forming a 3D-preform, applying a polymer matrix to the 3D-preform, and
curing the polymer matrix with the 3D-preform embedded therein.

30. A method of making a 3D-preform according to claim 15 , the method comprising:
providing the reinforcing fibres and SMA wires, and
making a 3D-preform by one or more of weaving, braiding, knitting, stitching, tufting and z-pinning.

Assignees

• Qinetiq Ltd

Inventors

• Foreman Andrew David
• Meeks Charlotte Bree
• West Robert

Classifications

• B32B5/06

  characterised by a fibrous {or filamentary} layer {mechanically connected, e.g. by needling} to another layer, e.g. of fibres, of paper · CPC title

• B32B2307/54

  Yield strength; Tensile strength · CPC title

• B32B2260/023

  Two or more layers · CPC title

• B29K2995/0091

  Damping, energy absorption · CPC title

• B32B7/09

  by stitching, needling or sewing (by {mechanically connecting} fibrous layers {to another layer} B32B5/06) · CPC title