Gas turbine fuel flow measurement using inert gas

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United States of America Patent

PATENT NO 9777637
APP PUB NO 20130232976A1
SERIAL NO

13719714

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Abstract

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The fuel flow rate to a gas turbine is measured using an inert gas. The inert gas is injected into the fuel flow and the concentration of the inert gas in the fuel/inert gas mixture is later measured. The concentration of the inert gas in the fuel/inert gas mixture is then used to calculate the mass flow rate of the fuel.

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Patent Owner(s)

  • GENERAL ELECTRIC COMPANY

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Cook, Jason Nathaniel Simpsonville, US 8 63
Tillery, Steven William Simpsonville, US 6 24

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