Forming a surface layer of a ceramic matrix composite article

Patent metadata

Field	Value
Publication number	US-11192829-B2
Application number	US-201916539644-A
Country	US
Kind code	B2
Filing date	Aug 13, 2019
Priority date	Jan 27, 2015
Publication date	Dec 7, 2021
Grant date	Dec 7, 2021

Abstract

The disclosure describes techniques for forming a surface layer of an article including a CMC using a cast. In some examples, the surface layer includes three-dimensional surface features, which may increase adhesion between the CMC and a coating on the CMC. In some examples, the surface layer may include excess material, with or without three-dimensional surface features, which is on the CMC. The excess material may be machined to remove some of the excess material and facilitate conforming the article to dimensional tolerances, e.g., for fitting the article to another component. The excess material may reduce a likelihood that the CMC (e.g., reinforcement material in the CMC) is damaged by the machining.

First claim

What is claimed is:

1. A method comprising:
filling a cast with a slurry;
stamping the slurry on a surface of an impregnated porous preform using the cast to form a surface layer including excess material, wherein the cast defines the shape of the surface layer including excess material, and wherein the impregnated porous preform comprises a reinforcement material and at least one ceramic matrix precursor;
drying the slurry to form a greenbody preform;
removing at least some of the green surface layer including excess material;
infiltrating the greenbody preform and the green surface layer with a molten infiltrant to form a ceramic matrix composite article including the surface layer; and
machining the ceramic matrix composite article to remove some of the surface layer including excess material to define a contact surface for contacting another component.

2. The method of claim 1 , wherein:
the slurry comprises a first slurry; and
the method further comprises:
impregnating a porous preform with a second slurry; and
drying the second slurry to form the impregnated porous preform.

3. The method of claim 2 , wherein a composition of the first slurry is different than a composition of the second slurry.

4. The method of claim 2 , wherein a composition of the first slurry is the same as a composition of the second slurry.

5. The method of claim 1 , wherein the surface layer including excess material defines a plurality of three-dimensional surface features, and wherein three-dimensional surface features of the plurality of three-dimensional surface features comprise at least one of depressions, grooves, ridges, or protrusions.

6. The method of claim 1 , wherein the surface layer including excess material extends over only a portion of the surface.

7. The method of claim 1 , wherein the surface layer including excess material extends over substantially all of the surface.

8. The method of claim 5 , further comprising:
3D printing a master mold defining the geometry of the three-dimensional surface features; and
forming the cast from as the negative of the master mold.

9. The method of claim 1 , wherein the cast is flexible.

10. The method of claim 1 , further comprising:
assembling the ceramic matrix composite article with a second component such that the surface layer including the excess material contacts the second component.

11. A method comprising:
placing a porous preform in a mold adjacent a cast, wherein the porous preform comprises a reinforcement material;
impregnating the porous preform and a space between the porous preform and the cast with a slurry comprising a ceramic matrix precursor to form an impregnated porous preform including a surface layer including excess material, wherein the shape of the surface layer including the excess material is defined by a negative of the cast;
drying the slurry to form a greenbody preform;
infiltrating the greenbody preform with a molten infiltrant to form a ceramic matrix composite article including the excess material; and
machining the ceramic matrix composite article to remove some of the surface layer including excess material to define a contact surface for contacting another component.

12. The method of claim 11 , wherein the surface layer including excess material defines a plurality of three-dimensional surface features, and wherein three-dimensional surface features of the plurality of three-dimensional surface features comprise at least one of depressions, grooves, ridges, or protrusions.

13. The method of claim 11 , wherein the surface layer including excess material extends over only a portion of the surface.

14. The method of claim 11 , wherein the surface layer including excess material extends over substantially all of the surface.

15. The method of claim 12 , further comprising:
3D printing a master mold defining the geometry of the three-dimensional surface features; and
forming the cast from as the negative of the master mold.

16. The method of claim 11 , wherein the cast is flexible.

17. The method of claim 11 , further comprising:
assembling the ceramic matrix composite article with a second component such that the surface layer including the excess material contacts the second component.

Assignees

• Rolls Royce Corp
• Rolls Royce High Temperature Composites Inc

Inventors

• Shim Sungbo
• Thibault Robert Wesley
• Shinavski Robert
• Lee Kang N

Classifications

• C04B2235/95

  Products characterised by their size, e.g. microceramics · CPC title

• C04B41/89 Primary

  for obtaining at least two superposed coatings having different compositions · CPC title

• C04B35/80

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

• C04B2237/083

  Carbide interlayers, e.g. silicon carbide interlayers · CPC title

• C04B41/5027

  Oxide ceramics in general; Specific oxide ceramics not covered by C04B41/5029 - C04B41/5051 · CPC title