Invention Grant
- Patent Title: Gas turbine fuel nozzle with integrated flame ionization sensor and gas turbine engine
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Application No.: US15576036Application Date: 2016-05-23
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Publication No.: US11054135B2Publication Date: 2021-07-06
- Inventor: Stefano Cioncolini , Michele D'Ercole , Antonio Asti
- Applicant: Nuovo Pignone Tecnologie SRL
- Applicant Address: IT Florence
- Assignee: Nuovo Pignone Tecnologie SRL
- Current Assignee: Nuovo Pignone Tecnologie SRL
- Current Assignee Address: IT Florence
- Agency: Baker Hughes Patent Org.
- Priority: IT102015000017588 20150525
- International Application: PCT/EP2016/061576 WO 20160523
- International Announcement: WO2016/188954 WO 20161201
- Main IPC: F23R3/28
- IPC: F23R3/28 ; F23N5/12 ; F23N5/24
Abstract:
A gas turbine fuel nozzle for a combustor of a gas turbine engine comprises a sleeve with an internal duct for premixed fuel gas flow; it further comprises a flame ionization sensor located on the sleeve externally to the duct; typically, the combustor has a single annular-shaped chamber.
Public/Granted literature
- US20180156457A1 GAS TURBINE FUEL NOZZLE WITH INTEGRATED FLAME IONIZATION SENSOR AND GAS TURBINE ENGINE Public/Granted day:2018-06-07
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