Invention Grant
- Patent Title: Sequential combustion arrangement with cooling gas for dilution
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Application No.: US15234605Application Date: 2016-08-11
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Publication No.: US10677453B2Publication Date: 2020-06-09
- Inventor: Wilhelm Reiter , Jürgen Gerhard Hoffmann
- Applicant: ANSALDO ENERGIA SWITZERLAND AG
- Applicant Address: CH Baden
- Assignee: ANSALDO ENERGIA SWITZERLAND AG
- Current Assignee: ANSALDO ENERGIA SWITZERLAND AG
- Current Assignee Address: CH Baden
- Agency: Buchanan Ingersoll & Rooney PC
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@1f101069
- Main IPC: F23C6/04
- IPC: F23C6/04 ; F23R3/34 ; F01D5/18 ; F01D9/04 ; F01D25/12 ; F23R3/02 ; F23R3/36

Abstract:
A gas turbine with a sequential combustor arrangement as disclosed includes a first combustor with a first burner for admitting a first fuel into a combustor inlet gas during operation and a first combustion chamber for burning the first fuel, a dilution gas admixer for admixing a dilution gas to the first combustor combustion products leaving the first combustion chamber, a second burner for admixing a second fuel and a second combustion chamber. To assure a temperature profile after the dilution gas admixer and to increase the gas turbine's power and efficiency a vane and/or blade of the turbine has a closed loop cooling. The outlet of the closed loop cooling is connected to the dilution gas admixer for admixing the heated cooling gas leaving the vane and/or blade into the first combustor combustion products.
Public/Granted literature
- US20170045228A1 SEQUENTIAL COMBUSTION ARRANGEMENT WITH COOLING GAS FOR DILUTION Public/Granted day:2017-02-16
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