Method to operate a combustor of a gas turbine
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United States of America Patent
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Sep 25, 2018
Grant Date -
Jul 7, 2016
app pub date -
Jun 4, 2013
filing date -
Dec 21, 2012
priority date (Note) -
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Abstract
A method to operate a combustor of a gas turbine is provided. The method includes monitoring the combustion gas temperature by temperature measurements downstream said combustor to measure a respective combustion gas temperature at different locations at respectively equal flow-distances to the burner of the combustion gas, comparing the temperature measurements, opening a valve or increasing the opening position of the valve to control the portion of oxygen containing gas to be tapped off when the comparison reveals that a difference between the temperature measurements exceeds a temperature difference threshold ΔT1.
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