Gas turbine fuel nozzle with integrated flame ionization sensor and gas turbine engine

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United States of America Patent

PATENT NO 11054135
APP PUB NO 20180156457A1
SERIAL NO

15576036

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Abstract

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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.

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Patent Owner(s)

Patent OwnerAddress
NUOVO PIGNONE TECNOLOGIE SRL50127 FLORENCE

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Asti, Antonio Florence, IT 16 133
Cioncolini, Stefano Florence, IT 4 15
D'Ercole, Michele Letany, CZ 13 94

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