Continuous fiber-reinforced silicon carbide member, manufacturing method thereof, and nuclear reactor structural member

Patent metadata

Field	Value
Publication number	US-12304176-B2
Application number	US-201815968885-A
Country	US
Kind code	B2
Filing date	May 2, 2018
Priority date	May 15, 2017
Publication date	May 20, 2025
Grant date	May 20, 2025

Abstract

There are provided a continuous fiber-reinforced silicon carbide member and the like which allow sufficient improvement in a mechanical property and environmental resistance. The continuous fiber-reinforced silicon carbide member of an embodiment is a tubular shape and has a first composite material layer and a second composite material layer. In the first composite material layer, continuous fibers of silicon carbide are combined with a matrix of silicon carbide. In the second composite material layer, continuous fibers of carbon are combined with a matrix of silicon carbide. Then, the first composite material layer and the second composite material layer are stacked.

First claim

What is claimed is:

1. A continuous fiber-reinforced silicon carbide member which is a tube-shaped continuous fiber-reinforced silicon carbide member, the member comprising:
a first composite material layer in which fiber bundles including bundled long fibers which are continuous fibers of silicon carbide are combined with a matrix of silicon carbide;
a second composite material layer in which fiber bundles including bundled long fibers which are continuous fibers consisting of carbon are combined with a matrix of silicon carbide, wherein the second composite material layer does not include other fibers other than the continuous fibers of carbon; and
an intermediate layer interposed between, and directly contacting, the first composite material layer and the second composite material layer,
wherein the first composite material layer and the second composite material layer are stacked by the first composite material layer being formed on an outer peripheral surface of the second composite material layer,
wherein the intermediate layer is formed of a single body of a material selected from the group consisting of titanium aluminum carbide, vanadium aluminum carbide, chromium aluminum carbide, niobium aluminum carbide, tantalum aluminum carbide, and titanium silicon carbide,
wherein the fiber bundles of the first composite material layer comprise 500 to 3000 pieces of the continuous fibers of silicon carbide, each having a diameter of 12 μm, and
wherein the long fibers of the fiber bundles of the second composite material layer each have a diameter of 10 μm.

2. The member of claim 1 , wherein the first composite material layer has a thickness of not less than 0.2 mm nor more than 5 mm.

3. The member of claim 1 , wherein the second composite material layer has a thickness of not less than 0.2 mm nor more than 2 mm.

4. The member of claim 1 , wherein the intermediate layer has hexagonal crystal in crystal form.

5. The member of claim 1 , wherein the intermediate layer has a thickness of not less than 0.01 mm nor more than 0.2 mm.

6. The member of claim 1 , wherein the intermediate layer is a monoclinic crystal which exhibits a hexagonal or pseudohexagonal crystalline form.

7. The member of claim 1 , wherein the intermediate layer is the titanium aluminum carbide.

8. The member of claim 1 , wherein the intermediate layer is the vanadium aluminum carbide.

9. The member of claim 1 , wherein the intermediate layer is the chromium aluminum carbide.

10. The member of claim 1 , wherein the intermediate layer is the niobium aluminum carbide.

11. The member of claim 1 , wherein the intermediate layer is the tantalum aluminum carbide.

12. The member of claim 1 , wherein the intermediate layer is the titanium silicon carbide.

13. The member of claim 1 , wherein the intermediate layer consists of titanium aluminum carbide.

14. The continuous fiber-reinforced silicon carbide member of claim 1 , wherein the fiber bundles of the second composite material layer comprise 300 pieces of the continuous fibers of carbon.

15. A continuous fiber-reinforced silicon carbide member which is a tube-shaped continuous fiber-reinforced silicon carbide member, the member comprising:
a first composite material layer in which fiber bundles including bundled long fibers which are continuous fibers of silicon carbide are combined with a matrix of silicon carbide;
a second composite material layer in which fiber bundles including bundled long fibers which are continuous fibers consisting of carbon are combined with a matrix of silicon carbide, wherein the second composite material layer does not include other fibers other than the continuous fibers of carbon; and
an intermediate layer interposed between, and directly contacting, the first composite material layer and the second composite material layer,
wherein the first composite material layer and the second composite material layer are stacked by the second composite material layer being formed on an outer peripheral surface of the first composite material layer,
wherein the intermediate layer is formed of a single body of a material selected from the group consisting of titanium aluminum carbide, vanadium aluminum carbide, chromium aluminum carbide, niobium aluminum carbide, tantalum aluminum carbide, and titanium silicon carbide,
wherein the fiber bundles of the first composite material layer comprise 500 to 3000 pieces of the continuous fibers of silicon carbide, each fiber having a diameter of 12 μm, and
wherein the long fibers of the fiber bundles of the second composite material layer each have a diameter of 10 μm.

16. The continuous fiber-reinforced silicon carbide member of claim 15 , wherein the fiber bundles of the second composite material layer comprise 300 pieces of the continuous fibers of carbon.

Assignees

• Toshiba Kk
• Toshiba Energy Systems & Solutions Corp

Inventors

• Suyama Shoko
• Ukai Masaru
• Uchihashi Masayuki
• Kakiuchi Kazuo
• Heki Hideaki

Classifications

• Y02E30/30

  Nuclear fission reactors · CPC title

• C04B35/80

  Fibres, filaments, whiskers, platelets, or the like · CPC title

• C23C16/045

  Coating cavities or hollow spaces, e.g. interior of tubes; Infiltration of porous substrates · CPC title

• C23C16/32

  Carbides · CPC title

• C04B41/87

  Ceramics · CPC title