Invention Grant
- Patent Title: Turbine shroud with mounted full hoop blade track
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Application No.: US15000655Application Date: 2016-01-19
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Publication No.: US10247040B2Publication Date: 2019-04-02
- Inventor: Bruce E. Varney , Jack D. Petty , Daniel K. Vetters , Eugene Clemens
- Applicant: Rolls-Royce Corporation , Rolls-Royce North American Technologies, Inc.
- Applicant Address: US IN Indianapolis US IN Indianapolis
- Assignee: Rolls-Royce North American Technologies Inc.,Rolls-Royce Corporation
- Current Assignee: Rolls-Royce North American Technologies Inc.,Rolls-Royce Corporation
- Current Assignee Address: US IN Indianapolis US IN Indianapolis
- Agency: Barnes & Thornburg LLP
- Main IPC: F01D25/24
- IPC: F01D25/24 ; F01D11/24
Abstract:
A gas turbine engine includes a turbine having a plurality of vanes, a plurality of blades, a turbine shroud arranged around the vanes and blades, and a turbine case arranged around the turbine shroud. The turbine shroud is sized to block combustion products from passing over the blades without pushing the blades to rotate. The turbine shroud includes a runner arranged around the blades and a carrier arranged around the runner.
Public/Granted literature
- US20170204744A1 TURBINE SHROUD WITH MOUNTED FULL HOOP BLADE TRACK Public/Granted day:2017-07-20
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