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

Patent metadata

Field	Value
Publication number	US-11255206-B2
Application number	US-202016827428-A
Country	US
Kind code	B2
Filing date	Mar 23, 2020
Priority date	Feb 27, 2017
Publication date	Feb 22, 2022
Grant date	Feb 22, 2022

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:
masking an edge of each 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;
infiltrating the body portion of the plurality of plies having the masked edge with a ceramic matrix slurry, the masked edge of the plurality of ceramic fibers defining a less infiltrated portion than the body portion, the plurality of ceramic fibers defining a less infiltrated portion than the body portion are woven to include weft fibers and warp fibers, each of the weft fibers and the warp fibers being unidirectional ceramic fibers;
placing the plurality of plies with the infiltrated body portion and masked edge in a stacked relationship, and orienting the masked edge of each of the plies in alignment with each other to define a stacked structure such that the unidirectional ceramic fibers in adjacent plies in the stacked structure are oriented at opposite predetermined angles relative to a radial axis of the stacked structure; and
firing the stacked structure to form a seal component having a flexible seal edge formed by the plurality of ceramic fibers projecting from a rigid body formed by the infiltrated body portion of each of the plies.

2. The process of claim 1 , wherein the masking step comprises mechanically masking.

3. The process of claim 2 , wherein the mechanically masking includes inserting the plurality of ceramic fibers extending away from the edge into pores of a mesh screen prior to the infiltrating, and removing the mesh screen from the plurality of ceramic fibers before firing the stacked structure.

4. The process of claim 2 , wherein the mechanically masking includes clamping the plurality of ceramic fibers extending away from the edge within a clamping device prior to the infiltrating, and removing the clamping device from the plurality of ceramic fibers before firing the stacked structure.

5. The process of claim 2 , wherein the mechanically masking includes positioning the edge upright relative to the body portion.

6. The process of claim 1 , wherein the masking step comprises chemical masking with a chemical substance configured to burn off during the firing.

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

8. A process of manufacturing a ceramic seal component, comprising:
preparing a plurality of dry uninfiltrated woven ceramic fabric plies having a uniform predetermined shape and thickness and configured to receive a ceramic matrix, each of the plurality of plies comprising a ply body and a plurality of fibers extending away from the respective ply body in one or more directions to define an edge of each of the respective plies;
applying a mask to the fibers extending away from each respective ply body to create a masked edge, the mask applied to a predetermined depth toward the respective ply body to inhibit flow of a ceramic matrix slurry and define an edge seal length of the fibers;
infiltrating the plurality of plies having the mask applied to the fibers with the ceramic matrix slurry to create infiltrated plies where the ply body defines a more infiltrated portion of the plies relative to the masked edge of the plurality of fibers defining a less infiltrated portion;
placing the infiltrated plies in a stacked relationship, and orienting the masked 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 mask applied to the fibers along one or more edges of the rigid green body; and
firing the stacked structure to form a ceramic seal component having a flexible seal edge formed by the edge seal length of the fibers projecting from a rigid body formed by the ply body of each of the plies.

9. The process of claim 8 , wherein the mask comprises a chemical mask, applying the mask to the fibers comprises applying a chemical substance soluble in water or organic solvent to the fibers extending away from each respective ply body, and the step of firing the stacked structure comprises firing the stacked structure to burn off the chemical mask applied to the fibers.

10. The process of claim 8 , wherein the mask comprises a mechanical mask, the mechanical mask comprising a mesh screen having a porosity sized to receive the fibers and inhibit flow of the ceramic matrix slurry into the masked edge during infiltration, and the step of applying the mask to the fibers comprises placing the mesh screen perpendicular to a direction of the fibers and weaving or inserting the fibers into pores included in the mesh screen and the step of firing the stacked structure comprises the initial step, prior to the firing, of removing the mesh screen from the fibers after the stacked structure is cured into the rigid green body.

11. The process of claim 10 , wherein the step of placing the mesh screen perpendicular to the direction of the fibers and weaving or inserting the fibers into pores comprises orientating the direction of the fibers upright such that the fibers once woven or inserted into the pores are positioned upward relative to ply body.

12. The process of claim 11 , wherein the step of infiltrating the plurality of plies having the mask applied to the fibers comprises applying a negative pressure to an end of the respective ply body opposite the mesh screen using a vacuum system.

13. The process of claim 8 , wherein the mask comprises a mechanical mask, the mechanical mask comprising parallel clamping plates sized to receive the fibers and extend to the predetermined depth toward the respective ply body and configured to provide a clamping force to minimize spacing between the fibers and withstand a flow of the ceramic matrix slurry between the fibers, and the step of applying the mask to the fibers comprises placing the fibers between the parallel clamping plates and the step of firing the stacked structure comprises the initial step, prior to the firing, of removing the parallel plates from the fibers after the stacked structure is cured into the rigid green body.

14. The process of claim 13 , wherein the step of placing the fibers between the parallel clamping plates comprises orientating the parallel clamping plates upright such that the fibers placed between the parallel clamping plates are upward relative to ply body.

15. The process of claim 14 , wherein the step of infiltrating the plurality of plies having the mask applied to the fibers comprises applying a positive pressure to a transition region at an edge of the parallel clamping plates between the fibers and the respective ply body with a compressor system.

16. The process of claim 8 , wherein the mask comprises a material being removed after some stage of composite processing to leave a void, wherein the material comprises particles, pecks, flakes, shaving, pellets, or some combination thereof, and the step of applying the mask to the fibers comprises the step of inserting the material along a transition between the fibers and the ply body.

17. The process of claim 8 , wherein firing the stacked structure to form a ceramic seal component comprises the initial steps, prior to the firing step, of removing the mask applied to the fibers along one or more edges of the rigid green body and deinfiltrating with a deinfiltration fluid the one

Assignees

• Rolls Royce Nam Tech Inc

Inventors

• Overholser Ronald Walter

Classifications

• B32B18/00

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

• F02K1/805

  Sealing devices therefor, e.g. for movable parts of jet pipes or nozzle flaps · CPC title

• F05D2300/6033

  Ceramic matrix composites [CMC] · CPC title

• F16J15/3288

  Filamentary structures, e.g. brush seals · CPC title

• F02C7/28

  Arrangement of seals · CPC title