Invention Grant
- Patent Title: Turbine shroud assembly with dovetail retention system
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Application No.: US16876865Application Date: 2020-05-18
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Publication No.: US11111796B1Publication Date: 2021-09-07
- Inventor: Ted J. Freeman , Aaron D. Sippel , Alexandra Baucco , Anthony Razzell , Michael J. Whittle , Jeffrey Crutchfield
- Applicant: Rolls-Royce North American Technologies , Rolls-Royce Corporation , Rolls-Royce plc
- Applicant Address: US IN Indianapolis; US IN Indianapolis
- Assignee: Rolls-Royce North American Technologies,Rolls-Royce Corporation,Rolls-Royce plc
- Current Assignee: Rolls-Royce North American Technologies,Rolls-Royce Corporation,Rolls-Royce plc
- Current Assignee Address: US IN Indianapolis; US IN Indianapolis
- Agency: Barnes & Thornburg LLP
- Main IPC: F01D5/22
- IPC: F01D5/22 ; F01D25/28 ; F01D25/24
Abstract:
A turbine shroud assembly for use with a gas turbine engine includes a turbine outer case, a blade track segment, and a carrier assembly. The turbine outer case is arranged around an axis. The blade track segment is configured to define a portion of a gas path of the gas turbine engine. The carrier assembly is coupled to the turbine outer case and supports the blade track segment.
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