Method for controlling a gas turbine operation with seleceted turbine outlet temperature measurements
A technology of gas turbine and outlet temperature, which is applied in the direction of fuel control of turbine/propulsion device, engine control, turbine/propulsion fuel delivery system, etc. Accurately estimate problems such as burner hot gas temperature, to achieve the effect of increasing the possibility of drift
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[0062] The control scheme for a sequential combustion gas turbine (known as, for example, the GT24 or GT26) is in figure 1 shown in . The gas turbine 10 includes a rotor 11 surrounded by a concentric casing. A compressor 12 compresses air passing through a plenum into a first combustion chamber 13 with burners. Fuel is supplied via a first combustor fuel supply 22 . The resulting hot gases leaving the first combustion chamber 13 drive a first turbine 14 . Downstream of the first turbine 14, combustion is injected into the exhaust gases of the first turbine 14 via fuel injectors 15, which still contain sufficient oxygen for further combustion. Fuel is combusted in the second combustion chamber 16 . The reheated gas drives the second turbine 17 and ultimately exits the gas turbine 10 . The first turbine outlet temperature measuring device 18 can also be integrated in or attached to the fuel spray gun 15 .
[0063] The first turbine 14 is also referred to as a high-pressure...
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