Ceramic seal component for gas turbine engine and process of making the same

Patent metadata

Field	Value
Publication number	US-10794205-B2
Application number	US-201715443715-A
Country	US
Kind code	B2
Filing date	Feb 27, 2017
Priority date	Feb 27, 2017
Publication date	Oct 6, 2020
Grant date	Oct 6, 2020

Abstract

A ceramic brush seal for a gas turbine engine, and a process for manufacturing the seal are provided. In one example, the process includes deinfiltrating an edge of a plurality of plies having a preimpregnated configuration. The edge is defined by a plurality of ceramic fibers extending away from a portion edge of a matrix infiltrated portion of each of the plies. In another example, the process includes masking an edge of a plurality of plies, the edge being defined by a plurality of ceramic fibers extending away from a portion edge of a body portion of each of the plies, and infiltrating the body portion of the plurality of plies with a ceramic matrix slurry. The plies are stacked, formed into a green body and then fired to form the component. The plies may include oxide/oxide woven ceramic fiber plies.

First claim

What is claimed is:

1. A process of manufacturing a ceramic seal component, comprising:
deinfiltrating an edge of respective preimpregnated plies such that the deinfiltrated edge is defined by a plurality of ceramic fibers extending away from a portion edge of a matrix infiltrated portion of each of the plies, the plurality of ceramic fibers defining a less infiltrated portion than the matrix infiltrated portion;
placing the plies with the deinfiltrated edge in a stacked relationship, and orienting the edge of each of the plies in alignment with each other to define a stacked structure;
curing the stacked structure into a rigid green body having a pre-ceramic polymer matrix material structure with the deinfiltrated edge being an exposed free ceramic fiber edge of the rigid green body;
further deinfiltrating the exposed free ceramic fiber edge of the rigid green body before firing; and
firing the stacked structure to form a ceramic seal component having a flexible seal edge formed by the plurality of ceramic fibers projecting from a rigid body formed by the matrix infiltrated portion of each of the plies.

2. The process of claim 1 , wherein the deinfiltrating comprises flushing at least a portion of the edge of each of the plies with deinfiltration fluid.

3. The process of claim 1 , further comprising removing at least a portion of extraneous fibers from the deinfiltrated edge to free the ceramic fibers.

4. The process of claim 3 , wherein the removing further comprises freeing the ceramic fibers of the deinfiltrated edge to a predetermined length along the edge.

5. The process of claim 1 , further comprising threading the edge with a thread member to define a drape end.

6. The process of claim 1 , wherein the plies include a woven oxide ceramic fiber fabric, the ceramic fibers include oxide ceramic fibers, and the matrix infiltrated portion of each of the plies includes an oxide ceramic matrix.

7. The process of manufacturing a ceramic seal component of claim 1 , wherein the plurality of ceramic fibers defining a less infiltrated portion than the matrix infiltrated portion are woven to include weft fibers and warp fibers, each of the weft fibers and the warp fibers being unidirectional ceramic fibers; and placing the plies with the deinfiltrated edge in a stacked relationship further comprises orienting the unidirectional ceramic fibers in adjacent plies in the stacked structure at opposite predetermined angles relative to a radial axis of the stacked structure.

8. A process of manufacturing a ceramic seal component, comprising:
deinfiltrating an edge of respective preimpregnated plies such that the deinfiltrated edge is defined by a plurality of ceramic fibers extending away from a portion edge of a matrix infiltrated portion of each of the preimpregnated plies, the plurality of ceramic fibers defining a less infiltrated portion than the matrix infiltrated portion;
placing the preimpregnated plies with the deinfiltrated edge in a stacked relationship with an uninfiltrated ply of dry ceramic fabric such that a layer of the stacked structure includes the uninfiltrated ply adjacent an infiltrated ply, and orienting the deinfiltrated edge of each of the preimpregnated plies in alignment with each other and an edge of the uninfiltrated ply to define a stacked structure; and
firing the stacked structure to form a ceramic seal component having a flexible seal edge formed by the plurality of ceramic fibers projecting from a rigid body formed by the matrix infiltrated portion of each of the preimpregnated plies and the uninfilterated ply.

9. A process of manufacturing a ceramic seal component, comprising:
deinfiltrating an edge of respective preimpregnated plies such that a plurality of ceramic fibers extend away from a portion edge of a matrix infiltrated portion of each of the preimpregnated plies, the plurality of ceramic fibers defining a less infiltrated portion than the matrix infiltrated portion and woven to include weft fibers and warp fibers, each of the weft fibers and the warp fibers being unidirectional ceramic fibers;
placing the plies in a stacked relationship by orienting the unidirectional ceramic fibers to define a stacked structure, the unidirectional ceramic fibers in adjacent preimpregnated plies in the stacked structure oriented at opposite predetermined angles relative to a radial axis of the stacked structure; and
firing the stacked structure to form a ceramic seal component having a flexible seal edge formed by the plurality of ceramic fibers projecting from a rigid body formed by the matrix infiltrated portion of each of the plies.

10. The process of manufacturing a ceramic seal component of claim 9 , further comprising
curing the stacked structure into a rigid green body having a pre-ceramic polymer matrix material structure with the deinfiltrated edge being an exposed free ceramic fiber edge of the rigid green body; and
further deinfiltrating the exposed free ceramic fiber edge of the rigid green body before firing.

11. The process of manufacturing a ceramic seal component of claim 9 , wherein the unidirectional ceramic fibers in adjacent preimpregnated plies in the stacked structure are oriented at opposite predetermined angles of plus and minus forty-five degrees relative to the radial axis of the stacked structure.

Assignees

• Rolls Royce Nam Tech Inc

Inventors

• Overholser Ronald Walter

Classifications

• C04B2235/5268

  Orientation of the fibers · CPC title

• B32B18/00

  Layered products essentially comprising ceramics, e.g. refractory products · CPC title

• F05D2230/31

  Layer deposition · CPC title

• C04B2235/38

  Non-oxide ceramic constituents or additives · CPC title

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title