Invention Grant
- Patent Title: Gas turbine engine and control method
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Application No.: US16753827Application Date: 2018-10-23
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Publication No.: US11274608B2Publication Date: 2022-03-15
- Inventor: Diana Bulat , Dorian Skipper , Michael Smith
- Applicant: Siemens Energy Global GmbH & Co. KG
- Applicant Address: DE Munich
- Assignee: Siemens Energy Global GmbH & Co. KG
- Current Assignee: Siemens Energy Global GmbH & Co. KG
- Current Assignee Address: DE Munich
- Priority: EP17199218 20171030
- International Application: PCT/EP2018/078973 WO 20181023
- International Announcement: WO2019/086293 WO 20190509
- Main IPC: F02C9/28
- IPC: F02C9/28 ; F02C9/18 ; F02C9/20

Abstract:
A method of controlling a gas turbine engine capable of operating in at least a high, medium-high, medium, medium-low, and low output power ranges. The method includes during the medium-high output power range varying the angle of the variable guide vanes so that a third predetermined temperature of the combustor is maintained, during the medium output power range the variable guide vanes are closed and bleeding a gas from a downstream part of the compressor to an upstream part of the compressor so that a first predetermined temperature of the combustor is maintained, during the medium-low output power range the variable guide vanes are closed and bleeding a gas from a downstream part of the compressor to an upstream part of the compressor and bleeding a gas from the downstream part of the compressor to the exhaust so that a second predetermined temperature of the combustor is maintained.
Public/Granted literature
- US20200291871A1 GAS TURBINE ENGINE AND CONTROL METHOD Public/Granted day:2020-09-17
Information query
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