Invention Grant
- Patent Title: Turbine shroud with split pin mounted ceramic matrix composite blade track
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Application No.: US17351736Application Date: 2021-06-18
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Publication No.: US11441441B1Publication Date: 2022-09-13
- Inventor: Ted J. Freeman , Aaron D. Sippel , David J. Thomas
- Applicant: Rolls-Royce Corporation
- Applicant Address: US IN Indianapolis
- Assignee: Rolls-Royce Corporation
- Current Assignee: Rolls-Royce Corporation
- Current Assignee Address: US IN Indianapolis
- Agency: Barnes & Thornburg LLP
- Main IPC: F01D11/08
- IPC: F01D11/08
Abstract:
A turbine shroud assembly adapted for use with a gas turbine engine includes a carrier, a seal segment, and a mount assembly. The carrier is configured to be coupled to a turbine case. The seal segment is shaped to define a gas path boundary of the shroud assembly. The mounting assembly is configured to couple the seal segment to the carrier.
Information query
