Invention Grant
- Patent Title: Retention system for gas turbine engine assemblies
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Application No.: US14971535Application Date: 2015-12-16
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Publication No.: US10941942B2Publication Date: 2021-03-09
- Inventor: Ted J. Freeman , Wayne S. Steffier
- Applicant: Rolls-Royce North American Technologies, Inc. , Rolls-Royce High Temperature Composites Inc.
- Applicant Address: US IN Indianapolis; US CA Cypress
- Assignee: Rolls-Royce North American Technologies, Inc.,Rolls-Royce High Temperature Composites Inc.
- Current Assignee: Rolls-Royce North American Technologies, Inc.,Rolls-Royce High Temperature Composites Inc.
- Current Assignee Address: US IN Indianapolis; US CA Cypress
- Agency: Barnes & Thornburg LLP
- Main IPC: F23R3/60
- IPC: F23R3/60 ; F01D25/28 ; F23R3/00 ; F01D11/08 ; F01D25/24
Abstract:
A combustor of a gas turbine engine and a turbine shroud for a turbine of a gas turbine engine are disclosed. The combustor is configured to ignite a mixture of compressed air and fuel in a combustion chamber included therein. The turbine shroud is configured to direct products of the combustion reaction toward a plurality of rotatable turbine blades of the turbine to cause the plurality of turbine blades to rotate.
Public/Granted literature
- US20160186999A1 RETENTION SYSTEM FOR GAS TURBINE ENGINE ASSEMBLIES Public/Granted day:2016-06-30
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