Invention Application
- Patent Title: TURBINE SHROUD ASSEMBLY WITH RADIALLY AND AXIALLY BIASED CERAMIC MATRIX COMPOSITE SHROUD SEGMENTS
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Application No.: US17329897Application Date: 2021-05-25
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Publication No.: US20220381152A1Publication Date: 2022-12-01
- Inventor: Ted J. Freeman , Aaron D. Sippel , David J. Thomas
- Applicant: Rolls-Royce Corporation
- Applicant Address: US IN Indianapolis
- Assignee: Rolls-Royce Corporation
- Current Assignee: Rolls-Royce Corporation
- Current Assignee Address: US IN Indianapolis
- Main IPC: F01D9/04
- IPC: F01D9/04 ; F01D25/00
Abstract:
A turbine shroud assembly adapted for use with a gas turbine engine includes a shroud segment and a carrier. The shroud segment extends circumferentially partway around an axis to define a gas path boundary of the turbine shroud assembly. The carrier is configured to support the shroud segment in position radially relative to the axis.
Public/Granted literature
- US11629607B2 Turbine shroud assembly with radially and axially biased ceramic matrix composite shroud segments Public/Granted day:2023-04-18
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