Ceramic matrix composite components having a deltoid region and methods for fabricating the same

Patent metadata

Field	Value
Publication number	US-10995040-B2
Application number	US-201715456628-A
Country	US
Kind code	B2
Filing date	Mar 13, 2017
Priority date	Mar 14, 2016
Publication date	May 4, 2021
Grant date	May 4, 2021

Abstract

A method for fabricating a ceramic matrix composite component having a deltoid region is provided. The method includes providing a porous ceramic preform. The porous ceramic preform includes a layer-to-layer weave of ceramic fibers that forms a modified layer-to-layer woven core and at least one 2-dimensional layer of ceramic fibers that is disposed adjacent to the modified layer-to-layer woven core. The porous ceramic preform is formed into a ceramic matrix composite body having the deltoid region such that the modified layer-to-layer woven core extends through the deltoid region.

First claim

What is claimed is:

1. A method for fabricating comprising:
providing a porous ceramic preform comprising a layer-to-layer weave of ceramic fibers that forms a modified layer-to-layer woven core and at least one 2-dimensional layer of ceramic fibers disposed adjacent to the modified layer-to-layer woven core; and
forming the porous ceramic preform into a ceramic matrix composite body that comprises: a base wall generally in an X-Y plane; a first wall and a second wall that each extend from the base wall and are generally transverse to the X-Y plane, the first wall generally extending in afirst Z plane and the second wall generally extending in a second Z plane; a first deltoid region disposed at or proximate an intersection of the X-Y plane and the first Z plane; a second deltoid region disposed at or proximate an intersection of the X-Y plane and the second Z-plane,
wherein the porous ceramic preform is formed into the ceramic matrix composite body such that the modified layer-to-layer woven core extends through the first deltoid region, through the second deltoid region, and into an interior mid-section of the base wall from the first deltoid region to the second deltoid region.

2. The method of claim 1 , wherein providing the porous ceramic preform comprises providing the modified layer-to-layer woven core comprising a 2.5-dimensional weave of ceramic fibers.

3. The method of claim 1 , wherein providing the porous ceramic preform comprises providing the modified layer-to-layer woven core comprising a 3-dimensional weave of ceramic fibers.

4. The method of claim 1 , wherein providing the porous ceramic preform comprises providing the at least one 2-dimensional layer of ceramic fibers comprising a layer of 2-dimensional weave of ceramic fibers.

5. The method of claim 4 , wherein providing the porous ceramic preform comprises providing the at least one 2-dimensional layer of ceramic fibers comprising a layup that includes a plurality of layers of the 2-dimensional weave of ceramic fibers.

6. The method of claim 1 , wherein providing the porous ceramic preform comprises providing the at least one 2-dimensional layer of ceramic fibers comprising a layer of unidirectional ceramic fibers.

7. The method of claim 6 , wherein providing the porous ceramic preform comprises providing the at least one 2-dimensional layer of ceramic fibers comprising a layup that includes a plurality of layers of the unidirectional ceramic fibers, wherein the unidirectional ceramic fibers in each layer are oriented independent of or substantially parallel to the unidirectional ceramic fibers in an adjacent layer.

8. The method of claim 1 , wherein providing and forming the porous ceramic preform into the ceramic matrix composite body comprises providing the modified layer-to-layer woven core having from about 15 to about 50 vol. % of the ceramic fibers in the deltoid region based on a total volume of the deltoid region.

9. The method of claim 1 , wherein the porous ceramic preform is formed into the ceramic matrix composite further such that the modified layer-to-layer extends into interior mid-sections of the first wall and the second wall.

10. The method of claim 9 , wherein providing and forming the porous ceramic preform into the ceramic matrix composite body comprises providing the modified layer-to-layer woven core having from about 15 to about 20 vol. % of the ceramic fibers extending longitudinally in the deltoid region generally in the Z plane, based on a total volume of ceramic fibers in the deltoid region, and from about 80 to about 85 vol. % of the ceramic fibers extending longitudinally in the deltoid region generally in the X-Y plane, based on the total volume of ceramic fibers in the deltoid region.

11. The method of claim 9 , wherein forming the ceramic matrix composite body comprises forming the base wall and, independently, the generally transverse wall having an overall thickness of from about 0.175 to about 0.225 inches, and wherein providing and forming the porous ceramic preform into the ceramic matrix composite body comprises providing the modified layer-to-layer woven core having a thickness of from about 0.030 to about 0.050 inches in the base wall and, independently, in the generally transverse wall.

12. The method of claim 9 , wherein the at least one 2-dimensional layer of ceramic fibers comprises a first 2-dimensional layer and a second 2-dimensional layer of ceramic fibers, wherein providing the porous ceramic preform comprises arranging the modified layer-to-layer woven core between the first and second 2-dimensional layers of ceramic fibers, and wherein forming the ceramic matrix composite body comprises forming the ceramic matrix composite body such that the first 2-dimensional layer of ceramic fibers extends over the deltoid region from the base wall to the generally transverse wall and the second 2-dimensional layer of ceramic fibers extends under the deltoid region along the base wall.

13. The method of claim 9 , wherein providing the porous ceramic preform comprises arranging the at least one 2-dimensional layers of ceramic fibers overlying the modified layer-to-layer woven core, and wherein forming the ceramic matrix composite body comprises forming the ceramic matrix composite body such that the at least one 2-dimensional layer of ceramic fibers extends generally over the deltoid region from the base wall to the generally transverse wall and the modified layer-to-layer woven core extends through and under the deltoid region to an outer base wall surface under the deltoid region.

14. The method of claim 1 , wherein the ceramic fibers of the modified layer-to-layer woven core and/or the at least one 2-dimensional layer comprise fibers of alumina, mullite, silicon carbide, zirconia or carbon.

15. The method of claim 1 , wherein the ceramic matrix composite body is a component of a gas turbine engine.

16. The method of claim 1 , wherein the ceramic matrix composite body is at least a portion of a seal segment of a gas turbine engine.

17. A method for fabricating a ceramic matrix composite component, the method comprising:
providing a porous ceramic preform comprising a layer-to-layer weave of ceramic fibers that forms a modified layer-to-layer woven core and at least one 2-dimensional layer of ceramic fibers disposed adjacent to the modified layer-to-layer woven core; and
forming the porous ceramic preform into a ceramic matrix composite body comprising a base wall that extends generally in an X-Y plane, a generally transverse wall that extends from the base wall generally in a Z plane that is substantially transverse to the X-Y plane, and a deltoid region disposed at or proximate an intersection of the X-Y plane and the Z plane,
wherein the porous ceramic preform is formed into the ceramic matrix composite body such that:
the modified layer-to-layer woven core extends through the deltoid region, through the intersection of the X-Y plane and the Z plane, and into interior mid-sections of the base wall and the generally transverse wall; and
the modified layer-to-layer woven core having from about 15 to about 20 vol. % of the ceramic fibers extending longitudinally in the deltoid region generally in the Z plane, based on a total volume of ceramic fibers in the deltoid region, and from about 80 to about 85 vol. % of the ceramic fibers extending longitudinally in the deltoid region generally in the X-Y plane, based on the total volume of ceramic fibers in the deltoid region.

18. A method for fabricating a ceramic matrix composite component, the method comprising:
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Assignees

• Rolls Royce High Temperature Composites Inc

Inventors

• Lamusga Joseph
• Barrett Christopher

Classifications

• C04B41/515 Primary

  Other specific metals · CPC title

• C04B35/80 Primary

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

• C04B2235/5224

  Alumina or aluminates · CPC title

• F05D2250/23

  prismatic · CPC title

• F05D2300/6034

  Orientation of fibres, weaving, ply angle · CPC title