Ceramic matrix composites and methods for producing ceramic matrix composites

Patent metadata

Field	Value
Publication number	US-9512044-B2
Application number	US-201414204820-A
Country	US
Kind code	B2
Filing date	Mar 11, 2014
Priority date	Mar 15, 2013
Publication date	Dec 6, 2016
Grant date	Dec 6, 2016

Abstract

A ceramic matrix composite includes a plurality of fibers embedded in a matrix. The composition of the matrix is selected to achieve a desired relationship between the mechanical and thermal properties of the matrix and the fibers.

First claim

What is claimed is:

1. A method of producing a ceramic matrix composite, comprising the steps of:
forming a network of silicon carbide fibers;
depositing an interface layer on the silicon carbide fibers before depositing a matrix material; and
depositing the matrix material comprising silicon and carbon onto the silicon carbide fibers to form silicon carbide;
wherein the depositing the matrix material comprises at least one of the group consisting of (1) depositing substantial amounts of silicon in excess of silicon carbide stoichiometric amounts, (2) introducing an oxygen containing gas, (3) introducing a halogen gaseous species, (4) introducing an organometallic gaseous species, or (5) a combination thereof and
wherein the depositing the matrix material comprises depositing silicon in an amount in excess of the silicon carbide stoichiometric amount, wherein the excess amount is about 10 atomic percent to about 20 atomic percent.

2. The method of claim 1 , wherein the matrix material has approximately the same creep resistance as that of the silicon carbide fibers.

3. The method of claim 1 , wherein the interface layer includes boron nitride.

4. The method of claim 1 , wherein the matrix material is deposited by chemical vapor infiltration.

5. The method of claim 1 , further including processing the ceramic matrix composite by polymer infiltration and pyrolysis.

6. The method of claim 1 , further including processing the ceramic matrix composite by slurry infiltration.

7. The method of claim 1 , further including processing the ceramic matrix composite by melt infiltration.

8. The method of claim 1 , wherein the matrix material comprises oxygen from introducing an oxygen containing gas during deposition of the matrix material.

9. The method of claim 1 , wherein the matrix material comprises at least one element of the group consisting of aluminum, zirconium, boron, nitrogen, titanium, niobium, molybdenum, yttrium, ytterbium, or a combination thereof from introducing a halogen gaseous species during deposition of the matrix material.

10. The method of claim 1 , wherein the matrix material comprises at least one element of the group consisting of aluminum, zirconium, titanium, niobium, molybdenum, yttrium, ytterbium or a combination thereof from introducing an organometallic gaseous species during deposition of the matrix material.

11. A method of producing a ceramic matrix composite, comprising the steps of:
forming a network of silicon carbide fibers;
depositing an interface layer on the silicon carbide fibers nctwork before depositing a matrix material; and
depositing the matrix material comprising silicon and carbon onto the silicon carbide fibers to form silicon carbide,
wherein the deposited matrix material comprises at least one of the group consisting of 1) an amount of silicon or carbon in excess of silicon carbide stoichiometric amounts, 2) at least one element selected from the group consisting of aluminum, zirconium, boron, nitrogen, titanium, niobium, molybdenum, yttrium, ytterbium, oxygen or a combination thereof, or 3) a combination of (1) and (2); and
wherein the amount of silicon or carbon in excess of silicon carbide stoichiometric amounts is about 10 atomic percent to about 20 atomic percent.

12. The method of claim 11 , wherein the deposited matrix material comprises about 0.2% to about 2% of inclusions containing an element selected from the group consisting of oxygen, nitrogen or combination thereof.

13. The method of claim 11 , wherein the deposited matrix material comprises about 0.05% to about 2% of aluminum containing inclusions.

14. A method of producing a ceramic matrix composite, comprising the steps of:
forming a network of silicon carbide fibers;
depositing an interface layer on the silicon carbide fibers before depositing a matrix material; and
depositing the matrix material comprising silicon and carbon onto the silicon carbide fibers to form silicon carbide;
wherein the depositing the matrix material comprises at least one of the group consisting of (1) depositing substantial amounts of carbon in excess of silicon carbide stoichiometric amounts, (2) introducing an oxygen containing gas, (3) introducing a halogen gaseous species, (4) introducing an organometallic gaseous species, or (5) a combination thereof and
wherein the depositing the matrix material comprises depositing carbon in an amount in excess of the silicon carbide stoichiometric amount, wherein the excess amount is about 10 atomic percent to about 20 atomic percent.

15. The method of claim 14 , wherein the matrix material has approximately the same creep resistance as that of the silicon carbide fibers.

16. The method of claim 14 , wherein the interface layer includes boron nitride.

17. The method of claim 14 , wherein the matrix material is deposited by chemical vapor infiltration.

18. The method of claim 14 , further including processing the ceramic matrix composite by polymer infiltration and pyrolysis.

19. The method of claim 14 , further including processing the ceramic matrix composite by slurry infiltration.

20. The method of claim 14 , further including processing the ceramic matrix composite by melt infiltration.

21. The method of claim 14 , wherein the matrix material comprises oxygen from introducing an oxygen containing gas during deposition of the matrix material.

22. The method of claim 14 , wherein the matrix material comprises at least one element of the group consisting of aluminum, zirconium, boron, nitrogen, titanium, niobium, molybdenum, yttrium, ytterbium, or a combination thereof from introducing a halogen gaseous species during deposition of the matrix material.

23. The method of claim 14 , wherein the matrix material comprises at least one element of the group consisting of aluminum, zirconium, titanium, niobium, molybdenum, yttrium, ytterbium or a combination thereof from introducing an organometallic gaseous species during deposition of the matrix material.

Assignees

• Rolls Royce Corp

Inventors

• Lazur Andrew J
• Chamberlain Adam L

Classifications

• C04B35/62884

  by gas phase techniques · CPC title

• C04B2235/386

  Boron nitrides · CPC title

• C04B2235/6581

  Total pressure below 1 atmosphere, e.g. vacuum · CPC title

• C04B2235/9607

  Thermal properties, e.g. thermal expansion coefficient · CPC title

• C04B2235/5244

  Silicon carbide · CPC title