Method to limit silicon in B4C particulate based CMC composites

Patent metadata

Field	Value
Publication number	US-12528745-B2
Application number	US-202217887228-A
Country	US
Kind code	B2
Filing date	Aug 12, 2022
Priority date	Aug 12, 2022
Publication date	Jan 20, 2026
Grant date	Jan 20, 2026

Abstract

A method of fabricating a composite component, includes forming a fibrous preform by forming a first ceramic particle layer over a first textile layer, the first ceramic particle layer having a first group of ceramic particles, disposing a second textile layer over the first ceramic particle layer, forming a second ceramic particle layer over the second textile layer, the second ceramic particle layer having a second group of ceramic particles, and disposing a third textile layer over the second ceramic particle layer. The method further includes densifying the fibrous preform.

First claim

What is claimed is:

1 . A method of fabricating a composite component, comprising:
forming a fibrous preform by:
forming a first ceramic particle layer over a first textile layer, the first ceramic particle layer having a first group of ceramic particles comprising a first volume of boron carbide powder;
disposing a second textile layer over the first ceramic particle layer;
forming a second ceramic particle layer over the second textile layer, the second ceramic particle layer having a second group of ceramic particles comprising a second volume of boron carbide powder;
disposing a third textile layer over the second ceramic particle layer; and
forming a third ceramic particle layer over the third textile layer, the third ceramic particle layer having a third group of ceramic particles comprising a third volume of boron carbide powder, wherein the first group of ceramic particles has a first average particle size, the second group of ceramic particles has a second average particle size, and the third group of ceramic particles has a third average particle size, the second average particle size being less than the first average particle size and the third average particle size being less than the second average particle size; and
densifying the fibrous preform.

2 . The method of fabricating a composite component of claim 1 , wherein the first, second, and third, textile layers comprise carbon fiber.

3 . The method of fabricating a composite component of claim 1 , wherein the first volume of boron carbide powder has a fourth average particle size, the second volume of boron carbide powder has a fifth average particle size, and the third volume of boron carbide powder has a sixth average particle size, the fifth average particle size being less than the fourth average particle size and the sixth average particle size being less than the fifth average particle size.

4 . The method of fabricating a composite component of claim 3 , further comprising densifying the fibrous preform for a predetermined period of time to limit silicon infiltration, the predetermined period of time being based on the third average particle size such that pores formed in the third ceramic particle layer are smaller than pores formed in the second ceramic particle layer and the pores formed in the second ceramic particle layer are smaller than the pores formed in the first ceramic particle layer.

5 . The method of fabricating a composite component of claim 1 , further comprising performing a silicon melt infiltration after densifying the fibrous preform.

6 . The method of fabricating a composite component of claim 1 , further comprising locating a carbon/carbon member through the fibrous preform.

7 . The method of fabricating a composite component of claim 6 , further comprising forming an opening through the carbon/carbon member.

8 . The method of fabricating a composite component of claim 7 , wherein a diameter of the opening is between 25% and 75% of a diameter of the carbon/carbon member.

9 . The method of fabricating a composite component of claim 1 , further comprising:
disposing the first textile layer on a first plate; locating a first shim around an outer perimeter of the first textile layer; locating a second shim around an outer perimeter of the second textile layer; disposing a second plate over the third textile layer, wherein at least one of the first plate or the second plate includes at least one of a groove or an orifice; and applying a compressive load to the third textile layer.

10 . A method of forming a fibrous preform for fabricating a composite component, comprising:
locating a first fiber layer in a mold; forming a first layer of ceramic particles and phenolic resin powder over the first fiber layer, the first layer of ceramic particles having a first group of boron carbide powder particles; locating a second fiber layer in the mold and over the first layer of ceramic particles and phenolic resin powder; forming a second layer of ceramic particles and phenolic resin powder over the second fiber layer, the second ceramic layer of ceramic particles having a second group of boron carbide powder particles; locating a third fiber layer over the second layer of ceramic particles and phenolic resin powder; forming a third layer of ceramic particles and phenolic resin powder over the third fiber layer, the third ceramic layer of ceramic particles having a third group of boron carbide powder particles, wherein the first layer of ceramic particles has a first average particle size, the second layer of ceramic particles has a second average particle size, and the third layer of ceramic particles has a third average particle size, the second average particle size being less than the first average particle size and the third average particle size being less than the second average particle size; and curing the fibrous preform.

11 . The method of forming a fibrous preform of claim 10 , further comprising wherein the first, second, and third, fiber layers comprise carbon fiber.

12 . The method of forming a fibrous preform of claim 10 , wherein the first group of boron carbide powder particles has a fourth average particle size, the second group of boron carbide powder particles has a fifth average particle size, and the sixth group of boron carbide powder particles has a sixth average particle size, the fifth average particle size being less than the fourth average particle size and the sixth average particle size being less than the fifth average particle size.

13 . The method of forming a fibrous preform of claim 12 , further comprising curing the fibrous preform for a predetermined period of time to limit silicon infiltration, the predetermined period of time being based on the third average particle size such that pores formed in the third layer of ceramic particles are smaller than pores formed in the second layer of ceramic particles and the pores formed in the second layer of ceramic particles are smaller than the pores formed in the first layer of ceramic particles.

14 . The method of claim 10 , further comprising locating a plurality of carbon/carbon members in the mold, wherein the plurality of carbon/carbon members is located through each of the first fiber layer, the second fiber layer, and the third fiber layer.

15 . The method of claim 10 , further comprising needling through the first fiber layer, the second fiber layer, and the third fiber layer to form a plurality of z-direction fibers extending between the first fiber layer and the third fiber layer.

16 . The method of claim 15 , wherein the first fiber layer, the second fiber layer, and the third fiber layer each have an open weave comprised of between 25% and 75% open area.

17 . A method of fabricating a composite component, comprising:
forming a fibrous preform by:
forming a first ceramic particle layer over a first textile layer, the first ceramic particle layer having a first group of ceramic particles;
disposing a second textile layer over the first ceramic particle layer;
forming a second ceramic particle layer over the second textile layer, the second ceramic particle layer having a second group of ceramic particles; and
disposing a third textile layer over the second ceramic particle layer;
densifying the fibrous preform locating a carbon/carbon member through the fibrous preform; and forming an opening through the carbon/carbon member.

18 . A method of forming a fibrous preform for fabricating a composite component, comprising:
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Assignees

• Goodrich Corp

Inventors

• Kirkpatrick Christopher T

Classifications

• C04B41/91

  involving the removal of part of the materials of the treated articles, e.g. etching · CPC title

• C04B2235/428

  Silicon · CPC title

• C04B2235/5248

  Carbon, e.g. graphite · CPC title

• C04B2235/3821

  Boron carbides · CPC title

• C04B2235/616

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