Method for operating a gas turbine
View Patent ↗A gas turbine includes a compressor, a combustor, a turbine, and a flow path diverting an excess portion of the compressed air produced by the compressor around the turbine. The flow path conducts the excess portion into a turbine exhaust gas flow producing a cooled exhaust gas. A method of operating the gas turbine includes opening an inlet guide vane of the compressor to allow the compressor to produce an increased volume of compressed air. The increased volume exceeds a volume of compressed air needed to support combustion. An excess portion of the compressed air is directed into the exhaust gas to produce a cooled exhaust. In a combined cycle power plant, the cooled exhaust from the gas turbine may be used to warm a steam turbine portion to a desired temperature while allowing operation of the gas turbine at a power level that produces exhaust gas at a temperature higher than the desired temperature.
1. A gas turbine comprising:
a compressor producing compressed air;
a combustor receiving a combustion portion of the compressed air and producing a hot combustion gas;
a turbine receiving the hot combustion gas and producing an exhaust gas;
an inlet guide vane upstream of the compressor for controlling a volume of ambient air delivered to the compressor;
a controller for generating an inlet guide vane control signal to adjust a position of the inlet guide vane for providing a desired volume of ambient air delivered to the compressor that allows the compressor to produce a volume of compressed air exceeding a volume of compressed air needed to support combustion during at least startup; and
a flow path receiving an excess portion of the compressed air produced by the compressor but not needed to support combustion and conducting the excess portion into the exhaust gas to produce a cooled exhaust gas during at least startup.
2. The gas turbine of claim 1 , further comprising a metering valve, responsive to a valve control signal, positioned in the flow path.
3. The gas turbine of claim 2 , wherein the controller is further configured for generating the valve control signal responsive to at least one of the group consisting of a temperature of the exhaust gas and a temperature of the cooled exhaust gas.
4. The gas turbine of claim 1 , wherein the compressor comprises stages numbering 1 Through N consecutively from a lowest pressure stage to a highest pressure stage, an inlet of the flow path disposed in a stage having a stage number less than N/2.
5. The gas turbine of claim 4 , wherein the inlet comprises a pressure tap port on the compressor.
6. The gas turbine of claim 1 , wherein the gas turbine is configured to operate at a power level sufficiently high to enable satisfying an emissions regulation while conducting the excess portion into the exhaust gas to produce the cooled exhaust gas.
7. The gas turbine of claim 1 , wherein at least a portion of the exhaust gas from the gas turbine is delivered to a downstream steam turbine portion of a plant, the gas turbine being configured to operate at a power level that produces hot exhaust gas at a temperature greater than a temperature desired for warming the steam turbine portion of the plant.
8. The gas turbine of claim 1 , wherein the inlet guide vane control signal comprises an instruction to open the inlet guide vane during a start-up period of the gas turbine.
9. A gas turbine having a compressor, a combustor, and a turbine, the gas turbine comprising:
means for opening an inlet guide vane upstream of the compressor to allow the compressor to produce a volume of compressed air exceeding a volume of compressed air needed to support combustion during at least startup;
means for extracting an excess portion of the compressed air produced but not needed to support combustion; and
means for combining the excess portion with an exhaust gas generated by the turbine to produce a cooled exhaust gas during at least startup.
10. The gas turbine of claim 9 , wherein the gas turbine is configured to operate at a power level sufficiently high to enable satisfying an emissions regulation while combining the excess portion with the exhaust gas.
11. The gas turbine of claim 9 , wherein means for opening the inlet guide vane is operable in response to a temperature of the cooled exhaust gas.
12. The gas turbine of claim 9 , further comprising means for controlling a flow rate of the excess portion.
13. The gas turbine of claim 12 , wherein means for controlling a flow rate of the excess portion is operable in response to one of the group consisting of a temperature of the exhaust gas and a temperature of the cooled exhaust gas.
14. A gas turbine comprising:
a compressor producing compressed air;
a combustor receiving a combustion portion of the compressed air and producing a hot combustion gas;
a turbine receiving the hot combustion gas and producing an exhaust gas for delivery to a downstream steam turbine;
an inlet guide vane upstream of the compressor for controlling a volume of ambient air delivered to the compressor;
a controller for generating an inlet guide vane control signal to open the inlet guide vane for providing an increased volume of ambient air delivered to the compressor during at least startup that allows the compressor to produce an air volume inexcess of what is needed to sustain combustion at a power level of the gas turbine that produces hot exhaust gas at a temperature for warming a downstream steam turbine portion of a plant; and
a flow path for receiving an excess portion of the compressed air produced by the compressor but not needed to sustain combustion at the power level and for conducting the excess portion into the exhaust gas during at least startup to produce a cooled exhaust gas for delivery to the downstream steam turbine portion of the plant.
15. The gas turbine of claim 14 , further comprising operating the gas turbine at a power level sufficiently high to enable satisfying an emissions regulation while conducting the excess portion into the exhaust gas to produce the cooled exhaust gas.
16. The gas turbine of claim 14 , further comprising a metering valve, responsive to a valve control signal, positioned in the flow path.
17. The gas turbine of claim 16 , wherein the controller is further configured for generating the valve control signal responsive to at least one of the group of a temperature of the exhaust gas and a temperature of the cooled exhaust gas.
18. The gas turbine of claim 14 , wherein the compressor comprises stages numbering 1 Through N consecutively from a lowest pressure stage to a highest pressure stage, an inlet of the flow path disposed in a stage having a stage number less than N/2.
19. The gas turbine of claim 18 , wherein the inlet comprises a pressure tap port on the compressor.