Ceramic matrix composite structures with controlled microstructures fabricated using chemical vapor infiltration (CVI)

Patent metadata

Field	Value
Publication number	US-12054432-B2
Application number	US-202117234176-A
Country	US
Kind code	B2
Filing date	Apr 19, 2021
Priority date	Feb 27, 2015
Publication date	Aug 6, 2024
Grant date	Aug 6, 2024

Abstract

According to a method set forth herein a plurality of preform plies having first and second preform plies can be associated together to define a preform. The preform can be subject to chemical vapor infiltration (CVI) processing to define a ceramic matrix composite (CMC) structure.

First claim

What is claimed is:

1. A structure comprising:
a plurality of preform plies associated together to define a preform, wherein the plurality of preform plies include a binder, a carrier, a filler, and a pore former;
wherein a first preform ply and a second preform ply of the plurality of preform plies have different average pore sizes; and
wherein the preform comprises at least one of the following:
a) a solid structure, wherein the plurality of preform plies includes a center preform ply, a first set of preform plies from the center preform ply to a preform ply defining a first outer surface of the preform having increasing average pore sizes, and a second set of preform plies from the center preform ply to a preform ply defining a second outer surface of the preform having increasing average pore sizes, or
b) a hollow structure preform, wherein the plurality of preform plies of the preform define a sidewall of the hollow structure preform, wherein the plurality of preform plies includes a center preform ply, a first set of preform plies from the center preform ply to a preform ply defining an outer surface of the hollow structure preform having increasing average pore sizes, and a second set of preform plies from the center preform ply to a preform ply defining an inner surface of the hollow structure preform having decreasing average pore sizes, or
c) the preform is a hollow structure preform, wherein the plurality of preform plies of the preform define a sidewall of the hollow structure preform, wherein a certain preform ply of the plurality of preform plies that defines an inner surface of the hollow structure preform has a smallest average pore size of the plurality of preform plies, and wherein preform plies of the plurality of preform plies in a succession of locations from a location of the certain preform ply to a location of a preform ply that defines an outer surface of the hollow structure preform have increasing average pore sizes.

2. The structure of claim 1 , wherein the second preform ply has a larger average pore size than the first preform ply.

3. The structure of claim 1 , wherein the first preform ply is the center preform ply, the center preform ply has a first average pore size and the second preform ply has a second average pore size, the second average pore size being larger than the first average pore size.

4. The structure of claim 1 , wherein the plurality of preform plies includes a third preform ply, wherein the second preform ply is disposed at a first side of the first preform ply, wherein the third preform ply is disposed at a second side of the first preform ply, and wherein the second preform ply and the third preform ply each have a larger average pore size than an average pore size of the first preform ply.

5. The structure of claim 1 , wherein the center preform ply of the plurality of preform plies has a smallest average pore size of the plurality of preform plies, and wherein preform plies at successive locations from a location of the center preform ply to a location of a preform ply defining an outer surface of the preform have increasing average pore sizes.

6. The structure of claim 1 , wherein the preform has a plurality of plies, each successive ply having larger average pore size than an innermost ply.

7. The structure of claim 1 , wherein the preform is in a shape of a turbine component.

8. The structure of claim 1 , wherein the preform is in a shape of a turbine component, and wherein the center preform ply of the plurality of preform plies has a smaller average pore size than one or more end ply of the plurality of preform plies that defines an outer surface of the preform.

9. The structure of claim 1 , wherein a count of the plurality of preform plies is selected from the group consisting of more than 5 preform plies, more than 20 preform plies, more than 50 preform plies, and more than 100 preform plies.

10. The structure of claim 1 , wherein the first preform ply includes fibers.

11. The structure of claim 10 , wherein the fibers comprise silicon carbide.

12. The structure of claim 10 , wherein the fibers include unidirectional fibers.

13. The structure of claim 10 , wherein the fibers include woven fibers.

14. The structure of claim 10 , wherein the fibers include a combination of unidirectional fibers and woven fibers.

15. The structure of claim 10 , wherein a coating is formed on the fibers.

16. The structure of claim 15 , wherein the coating is a matrix coating.

17. The structure of claim 15 , wherein the coating comprises a material selected from the group consisting of SiC, BN, B 4 C, Si 3 N 4 , MoSi 2 , SiOC, SiNC and SiONC.

18. The structure of claim 15 , wherein the coating is BN.

19. A structure comprising:
a plurality of preform plies defining a preform, the plurality of preform plies including a center preform ply, a first outer surface preform ply, and a second outer surface preform ply, wherein the plurality of preform plies include a binder, a carrier, a filler, and a pore former;
wherein the first outer surface preform ply has a first outer surface average pore size, the second outer surface preform ply has a second outer surface average pore size, and the center preform ply has a center average pore size;
wherein both the first outer surface average pore size and the second outer surface average pore size are greater than the center average pore size; and
wherein the plurality of preform plies further includes
a first set of preform plies extending from the center preform ply to the first outer surface preform ply; and
a second set of preform plies extending from the center preform ply to the second outer surface preform ply;
wherein the first set of preform plies and the second set of preform plies each have increasing average pore sizes from the center preform ply.

20. The structure of claim 19 , wherein a count of the plurality of preform plies is selected from the group consisting of more than 5 preform plies, more than 20 preform plies, more than 50 preform plies, and more than 100 preform plies.

Assignees

• Gen Electric

Inventors

• Weaver Jared Hogg
• Corman Gregory Scot
• Luthra Krishan Lal

Classifications

• C23C16/045

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

• C04B2237/38

  Fiber or whisker reinforced · CPC title

• C04B2235/614

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

• C04B2235/5208

  Fibers · CPC title

• C04B37/001

  directly with other burned ceramic articles · CPC title