Invention Grant
- Patent Title: Brazed blade track for a gas turbine engine
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Application No.: US16661572Application Date: 2019-10-23
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Publication No.: US11053806B2Publication Date: 2021-07-06
- Inventor: Aaron D. Sippel , Daniel K. Vetters , Jun Shi , David J. Thomas , Andrew J. Eifert , Peter Broadhead
- Applicant: Rolls-Royce Corporation , Rolls-Royce North American Technologies, Inc. , Rolls-Royce plc
- Applicant Address: US IN Indianapolis; US IN Indianapolis; GB London
- Assignee: Rolls-Royce Corporation,Rolls-Royce North American Technologies, Inc.,Rolls-Royce plc
- Current Assignee: Rolls-Royce Corporation,Rolls-Royce North American Technologies, Inc.,Rolls-Royce plc
- Current Assignee Address: US IN Indianapolis; US IN Indianapolis; GB London
- Agency: Barnes & Thornburg LLP
- Main IPC: F01D9/04
- IPC: F01D9/04 ; F01D9/02 ; F01D25/24
Abstract:
A blade track for a gas turbine engine includes segments and joints that couple the segments together. Each segment extends part-way around a central axis of the engine and the joints couple together adjacent segments to form a full hoop.
Public/Granted literature
- US20200056493A1 BRAZED BLADE TRACK FOR A GAS TURBINE ENGINE Public/Granted day:2020-02-20
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