Invention Grant
- Patent Title: Turbine shroud segment with load distribution springs
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Application No.: US16227986Application Date: 2018-12-20
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Publication No.: US10934879B2Publication Date: 2021-03-02
- Inventor: Mark O'Leary , Daniel K. Vetters , Matthew R. Brandt , Ted J. Freeman
- Applicant: Rolls-Royce North American Technologies Inc. , Rolls-Royce Corporation
- 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: F01D11/12
- IPC: F01D11/12 ; F01D11/00 ; F01D25/00 ; F01D25/12 ; F01D25/24 ; F01D9/04

Abstract:
A turbine shroud adapted for use in a gas turbine engine includes a plurality of metallic carrier segments and a plurality of blade track segments mounted to corresponding metallic carrier segments. Cooling air is directed onto the blade track segments to cool the blade track segments when exposed to high temperatures in a gas turbine engine.
Public/Granted literature
- US20200025013A1 TURBINE SHROUD SEGMENT WITH LOAD DISTRIBUTION SPRINGS Public/Granted day:2020-01-23
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