Invention Grant
- Patent Title: Ceramic seal component for gas turbine engine and process of making the same
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Application No.: US15443715Application Date: 2017-02-27
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Publication No.: US10794205B2Publication Date: 2020-10-06
- Inventor: Ronald Walter Overholser
- Applicant: Rolls-Royce North American Technologies Inc.
- Applicant Address: US IN Indianapolis
- Assignee: Rolls-Royce North American Technologies Inc.
- Current Assignee: Rolls-Royce North American Technologies Inc.
- Current Assignee Address: US IN Indianapolis
- Agency: Brinks Gilson & Lione
- Main IPC: C04B35/80
- IPC: C04B35/80 ; B32B18/00 ; F01D11/00 ; F16J15/3288 ; F02C7/28 ; F02K1/80 ; C04B35/565

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.
Public/Granted literature
- US20180266261A1 CERAMIC SEAL COMPONENT FOR GAS TURBINE ENGINE AND PROCESS OF MAKING THE SAME Public/Granted day:2018-09-20
Information query
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