Method for integral joining infiltrated ceramic matrix composites

Patent metadata

Field	Value
Publication number	US-2016368827-A1
Application number	US-201615188159-A
Country	US
Kind code	A1
Filing date	Jun 21, 2016
Priority date	Jun 22, 2015
Publication date	Dec 22, 2016
Grant date	—

Abstract

Integrated ceramic matrix composite components for use in gas turbine engines are disclosed along with methods for making the same. The methods include coinfiltrating a greenbody assembly with ceramic matrix to produce an integrated component.

First claim

What is claimed is:

1 . A method of making an integrated ceramic matrix composite component for use in a gas turbine engine, the method comprising the steps of
manufacturing a first green body subpart formed to include a first slot, manufacturing a second green body subpart formed to include a second slot, inserting a green body biscuit into the first slot of the first green body subpart and the second slot of the second green body subpart to create a green assembly with a joint between the first green body subpart and the second green body subpart, and slurry infiltrating the green assembly with ceramic-containing matrix to integrally join the green assembly and produce an integrated ceramic matrix composite component.

2 . The method of claim 1 , further comprising vapor infiltrating the first green body subpart, the second green body subpart, and the green body biscuit with ceramic-containing matrix to at least partially rigidify the first green body subpart, the second green body subpart, and the green body biscuit.

3 . The method of claim 2 , wherein the step of vapor infiltrating is performed before the step of inserting the green body biscuit into the first slot of the first green body subpart and the second slot of the second green body subpart to create a green assembly.

4 . The method of claim 1 , wherein manufacturing the first green body subpart includes laying up a plurality of reinforcement sheets.

5 . The method of claim 4 , further comprising chemical vapor infiltrating the first green body subpart with ceramic-containing matrix to at least partially rigidify the first green body subpart after laying up the plurality of reinforcement sheets.

6 . The method of claim 5 , wherein at least some of the plurality of reinforcement sheets are formed to include cutouts that cooperate to define the first slot before the step of vapor infiltrating the first green body subpart with ceramic-containing matrix.

7 . The method of claim 5 , further comprising machining at least some of the plurality of reinforcement sheets to define the first slot after the step of chemical vapor infiltrating the first green body subpart with ceramic-containing matrix.

8 . The method of claim 4 , wherein each of the plurality of reinforcement sheets included in the first green body subpart comprises a ceramic-containing fiber.

9 . The method of claim 8 , wherein the ceramic-containing fiber comprises silicon-carbide and the ceramic-containing matrix comprises silicon-carbide.

10 . The method of claim 1 , further comprising melt infiltrating the first green body subpart, the second green body subpart, and the green body biscuit with ceramic-containing matrix to integrally join the green assembly.

11 . The method of claim 10 , wherein the step of melt infiltrating is performed after the step of slurry infiltrating the green assembly with ceramic-containing matrix.

12 . A method of making an integrated ceramic matrix composite component for use in a gas turbine engine, the method comprising the steps of
chemical vapor infiltrating a first green body subpart, a second green body subpart, and a green body biscuit to at least partially rigidify the first green body subpart, the second green body subpart, and the green body biscuit, inserting the green body biscuit into a first slot formed in the first green body subpart and a second slot formed in the second green body subpart, and slurry infiltrating the first green body subpart, the second green body subpart, and the green body biscuit to produce an integrated ceramic matrix composite component.

13 . The method of claim 12 , wherein the step of slurry infiltrating the first green body subpart, the second green body subpart, and the green body biscuit is performed after inserting the green body biscuit into the first slot formed in the first green body subpart and the second slot formed in the second green body subpart.

14 . The method of claim 13 , wherein the step of chemical vapor infiltrating is performed before the step of inserting the green body biscuit into the first slot of the first green body subpart and the second slot of the second green body subpart.

15 . The method of claim 12 , wherein the first green body subpart includes a plurality of reinforcement sheets adapted to be suspended in ceramic-containing matrix.

16 . The method of claim 15 , wherein at least some of the plurality of reinforcement sheets are formed to include cutouts that cooperate to define the first slot before the step of vapor infiltrating the first green body subpart with ceramic-containing matrix.

17 . The method of claim 15 , further comprising machining at least some of the plurality of reinforcement sheets to define the first slot after the step of chemically infiltrating the first green body subpart with ceramic-containing matrix.

18 . The method of claim 15 , wherein each of the plurality of reinforcement sheets included in the first green body subpart comprises a ceramic-containing fiber.

19 . The method of claim 12 , further comprising melt infiltrating the first green body subpart, the second green body subpart, and the green body biscuit with ceramic-containing matrix.

20 . An integrated ceramic-matrix composite component for use in a gas turbine engine, the component comprising
a first subpart formed to include a first blind slot, a second subpart formed to include a second blind slot, and a biscuit that extends into the first blind slot and the second blind slot to form a joint between the first subpart and the second subpart, wherein the joint is coinfiltrated with ceramic-containing matrix material to integrally join the first subpart, the second subpart, and the biscuit.

Assignees

• Rolls Royce Corp
• Rolls Royce Nam Tech Inc
• Rolls-Royce High Temperature Composites Inc

Inventors

• Landwehr Sean E
• Vetters Daniel K
• Freeman Ted J
• Shinavski Robert J

Classifications

• C04B2235/614

  Gas infiltration of green bodies or pre-forms · CPC title

• C04B2235/5244

  Silicon carbide · CPC title

• C04B35/565

  based on silicon carbide · CPC title

• F05D2300/20

  Oxide or non-oxide ceramics · CPC title

• C04B41/87

  Ceramics · CPC title