Invention Application
- Patent Title: TURBINE SHROUD WITH FRICTION MOUNTED CERAMIC MATRIX COMPOSITE BLADE TRACK
-
Application No.: US17068268Application Date: 2020-10-12
-
Publication No.: US20210108532A1Publication Date: 2021-04-15
- Inventor: Ted J. Freeman , Aaron D. Sippel , Shaling Starr , Paulo Bazan , Adrian Harding , Jeffrey A. Walston
- Applicant: Rolls-Royce North American Technologies Inc. , Rolls-Royce Corporation , Rolls-Royce plc
- Applicant Address: US IN Indianapolis; US IN Indianapolis; GB London
- Assignee: Rolls-Royce North American Technologies Inc.,Rolls-Royce Corporation,Rolls-Royce plc
- Current Assignee: Rolls-Royce North American Technologies Inc.,Rolls-Royce Corporation,Rolls-Royce plc
- Current Assignee Address: US IN Indianapolis; US IN Indianapolis; GB London
- Main IPC: F01D11/08
- IPC: F01D11/08

Abstract:
A turbine shroud adapted for use in a gas turbine engine includes a seal segment and an attachment unit. The seal segment includes an arcuate shroud wall that extends circumferentially partway around an axis and a mount post that extends radially outward away from the shroud wall. The attachment unit includes a first carrier and a second carrier that cooperate to define a channel that receives at least a portion of the mount post.
Public/Granted literature
- US11220925B2 Turbine shroud with friction mounted ceramic matrix composite blade track Public/Granted day:2022-01-11
Information query