System and method for determining combustion temperature using infrared emissions
AssigneeAmetex AG
InventorsWilliam M. Glasheen, Charles DeMilo, Helmar R. Steglich
Life of this patent
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Abstract
The present invention relates to a combustion temperature sensor, and, more particularly, to a combustion temperature sensor that measures infrared energy emitted at several preselected wavelengths from a flame and/or a flame's hot gas at a turbine inlet location and applies the energy signals to a calculation model to yield temperature.
Claims9
In a system for measuring IR radiation of a flame in a gas turbine having a combustion chamber and a turbine section, the improvement comprising a lens for collecting infrared radiation from a portion of the flame nearest to an inlet to the turbine section, said lens focusing said infrared radiation on one end of an optical fiber, said lens and optical fiber comprising sapphire, a first mounting means for supporting said lens and the one end of the optical fiber in fixed relation to the flame, means for supplying compressed air to said mounting means to shield said mounting means and said lens from combustion gases in said flame, means for positioning a second end of the optical fiber in position to direct said infrared radiation transmitted by the fiber onto a first infrared filter having a first infrared transmission of 2.28 μm (+/−0.005 μm), a second infrared filter having a second infrared transmission of 2.6 μm (+/−0.015 μm), a third infrared filter having a third infrared transmission of 2.7 μm (+/−0.015 μm), and a fourth infrared filter having a fourth infrared transmission of 2.8 μm (+/−0.005 μm), said first infrared filter generating a discrete background infrared radiation wavelength, said second, third and fourth infrared filter each generating a discrete infrared radiation corresponding to CO2 and H2O gas emissions, each said filter directing said discrete infrared radiation wavelength onto an associated detector, and optical chopping means for interrupting the infrared radiation at a predetermined frequency before it reaches said spectral IR filters.
In a system for measuring discrete IR energies of a flame in a turbine having a combustion chamber and a gas turbine section, the improvement comprising a lens for collecting infrared radiation from a portion of the flame nearest an inlet to the turbine section, said lens focusing said IR radiation on one end of an optical fiber, said lens and optical fiber comprising sapphire, a first mounting means for supporting said lens and one end of the optical fiber in fixed relation to the flame, means for supplying compressed air to said mounting means to shield said mounting means from combustion gases, means for positioning a second end of the optical fiber in position to direct said IR radiation transmitted by the fiber onto a first infrared transmission of 2.28 μm (+/−0.005 μm), a second infrared filter having a second infrared transmission of 2.6 μm (+/−0.015 μm), a third infrared filter having a third infrared transmission of 2.7 μm (+/−0.015 μm), and a fourth infrared filter having a fourth infrared transmission of 2.8 μm (+/−0.005 μm), said first infrared filter generating a discrete background infrared radiation wavelength, said second, third and fourth infrared filters each generating a discrete infrared radiation wavelength corresponding to CO2 and H2O gas emissions, and optical chopping means for interrupting the infrared radiation at a predetermined frequency before it impinges on said filter means, and means for controlling the temperature of said detectors.
Dependencies are inferred from the claim text.