Invention Grant
- Patent Title: System and methods for controlling surge margin in the compressor section of a gas turbine engine
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Application No.: US17494339Application Date: 2021-10-05
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Publication No.: US11519339B2Publication Date: 2022-12-06
- Inventor: Benjamin Michael Iwrey , Graham Adam Burkholder
- Applicant: Rolls-Royce North American Technologies Inc.
- Applicant Address: US IN Indianapolis
- Assignee: Rolls-Royce North American Technologies Inc.
- Current Assignee: Rolls-Royce North American Technologies Inc.
- Current Assignee Address: US IN Indianapolis
- Agency: Barnes & Thornburg LLP
- Main IPC: F02C9/18
- IPC: F02C9/18 ; F01D19/00 ; F02C3/10 ; F02C7/32 ; F02C6/08

Abstract:
Systems and methods are disclosed for controlling surge margin in the compressor section of a gas turbine engine. A first compressor section and a second compressor section are in fluid communication with a bypass conduit. An auxiliary turbine and discharge conduit are positioned in the bypass conduit. Fluid flow from the compressor sections into the bypass conduit is controlled by bypass control valves.
Public/Granted literature
- US20220025824A1 SYSTEM AND METHODS FOR CONTROLLING SURGE MARGIN IN THE COMPRESSOR SECTION OF A GAS TURBINE ENGINE Public/Granted day:2022-01-27
Information query
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