Invention Grant
- Patent Title: Turbine shroud ring segments with ceramic matrix composite components
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Application No.: US16856752Application Date: 2020-04-23
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Publication No.: US11208911B2Publication Date: 2021-12-28
- Inventor: Keith Sadler , Ted J. Freeman , Aaron D. Sippel , Alexandra Baucco
- Applicant: Rolls-Royce plc , Rolls-Royce North American Technologies Inc. , Rolls-Royce Corporation
- Applicant Address: GB London; US IN Indianapolis; US IN Indianapolis
- Assignee: Rolls-Royce plc,Rolls-Royce North American Technologies Inc.,Rolls-Royce Corporation
- Current Assignee: Rolls-Royce plc,Rolls-Royce North American Technologies Inc.,Rolls-Royce Corporation
- Current Assignee Address: GB London; US IN Indianapolis; US IN Indianapolis
- Agency: Barnes & Thornburg LLP
- Main IPC: F01D11/08
- IPC: F01D11/08 ; F01D25/24 ; F01D9/04 ; F01D11/00
Abstract:
An assembly adapted for use in a gas turbine engine includes a carrier and a blade track segment. The carrier extends at least partway about an axis. The blade track segment is supported by the carrier radially relative to the axis to define a portion of a gas path of the assembly.
Public/Granted literature
- US20210332713A1 TURBINE SHROUD RING SEGMENTS WITH CERAMIC MATRIX COMPOSITE COMPONENTS Public/Granted day:2021-10-28
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