Invention Grant
- Patent Title: Turbine shroud with axially separated pressure compartments
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Application No.: US15048271Application Date: 2016-02-19
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Publication No.: US10221715B2Publication Date: 2019-03-05
- Inventor: Bruce E. Varney , Daniel K. Vetters
- 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: F01D11/08
- IPC: F01D11/08 ; F01D25/12
Abstract:
A turbine shroud for a gas turbine engine includes an annular metallic carrier and a blade track. One or more cavities are formed between the carrier and blade track to provide cooling air to the blade track.
Public/Granted literature
- US20160258311A1 TURBINE SHROUD WITH AXIALLY SEPARATED PRESSURE COMPARTMENTS Public/Granted day:2016-09-08
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