초록 ▼

A method and installation are disclosed which can, for example, provide for reliable, low-Nox-emission operation of a gas turbine installation with hydrogen-rich fuel gas. An exemplary gas turbine installation includes an arrangement for flue gas recirculation into a compressor inlet and for fuel ga

A method and installation are disclosed which can, for example, provide for reliable, low-Nox-emission operation of a gas turbine installation with hydrogen-rich fuel gas. An exemplary gas turbine installation includes an arrangement for flue gas recirculation into a compressor inlet and for fuel gas dilution. Oxygen content in combustion air can be reduced by recirculation of recooled flue gas, and the fuel gas can be diluted with compressed flue gas. The oxygen reduction in the combustion air can lead to minimum residual oxygen in the flue gas which can be used for fuel gas dilution. As a result of the flue gas recirculation, water content in the combustion air can be increased by feedback of the water which results as a combustion product. The oxygen reduction, increased water content, and fuel dilution can reduce the flame velocity of hydrogen-rich fuel gases and enable a robust, reliable and low-emission combustion.

대표청구항 ▼

1. A method for operating a gas turbine installation with hydrogen-rich fuel gas, comprising: cooling at least a portion of a flue gas in a recooler;recirculating at least the portion of flue gas mass flow into an intake air of a compressor, wherein the portion of recirculated flue gas mass flow is

1. A method for operating a gas turbine installation with hydrogen-rich fuel gas, comprising: cooling at least a portion of a flue gas in a recooler;recirculating at least the portion of flue gas mass flow into an intake air of a compressor, wherein the portion of recirculated flue gas mass flow is controlled by at least one suitable control element;providing as a control reference value for the control element, at least one of a residual oxygen content of the flue gas and an oxygen content of combustion air;selecting the reference value for controlling the oxygen content dependent upon operating parameters of the gas turbine installation; andseparating condensate which occurs during the recooling of the recirculated flue gases in a condensate separator. 2. The method as claimed in claim 1, comprising: guiding the flue gas through a boiler; andsplitting the flue gas, after discharging from the boiler, into two partial flows, at least one of the two partial flows being further cooled in a recooler and recirculated into intake air of the compressor. 3. The method as claimed in claim 1, comprising: processing separated-out condensate; andinjecting the separated-out condensate for cooling and/or intercooling in an atomized state into the intake air and/or into the recirculated flue gas which is provided for fuel dilution. 4. The method as claimed in claim 1, comprising: selecting the reference value for controlling the residual oxygen content in the flue gas or in the combustion air as a constant; orselecting the reference value of the oxygen content dependent upon fuel gas composition and selecting the reference value of the residual oxygen content inversely proportional to hydrogen content in the fuel gas. 5. The method as claimed in claim 1, wherein the selected reference value for controlling the residual oxygen content depends on at least one of: a compressor inlet temperature;a hot gas temperature; anda position of compressor inlet guide vanes. 6. The method as claimed in claim 1, wherein the selected reference value for controlling the residual oxygen content is increased at a partial load compared to the content at full load. 7. A method for operating a gas turbine installation with hydrogen-rich fuel gas, comprising: cooling at least a portion of a flue gas in a recooler;recirculating at least the portion of flue gas mass flow into an intake air of a compressor, wherein the portion of recirculated flue gas mass flow is controlled by at least one suitable control element; andproviding as a control reference value for the control element, at least one of a residual oxygen content of the flue gas and an oxygen content of combustion air, andwherein the method comprises at least one of:compressing and mixing cooled flue gas with fuel gas for fuel gas dilution; andcompressing the cooled flue gas with intercooling, mixing the flue gas with fuel for fuel gas dilution, and directing the diluted fuel into at least one burner. 8. A method for operating a gas turbine installation with hydrogen-rich fuel gas, comprising: cooling at least a portion of a flue gas in a recooler;recirculating at least the portion of flue gas mass flow into an intake air of a compressor, wherein the portion of recirculated flue gas mass flow is controlled by at least one suitable control element; andproviding as a control reference value for the control element, at least one of a residual oxygen content of the flue gas and an oxygen content of combustion air;wherein the hydrogen-rich fuel gas is pure hydrogen to produce a CO-free and UHC (unburnt hydrocarbon)-free combustion without CO2 emission. 9. A method for operating a gas turbine installation with hydrogen-rich fuel gas, comprising: cooling at least a portion of a flue gas in a recooler;recirculating at least the portion of flue gas mass flow into an intake air of a compressor, wherein the portion of recirculated flue gas mass flow is controlled by at least one suitable control element; andproviding as a control reference value for the control element, at least one of a residual oxygen content of the flue gas and an oxygen content of combustion air, andwherein the method comprises at least one of:using a supplemental combusting of hydrogen-rich fuel gas for starting and/or during transient operation of the gas turbine installation; andcontrolling the oxygen content for the transient operation with a supplemental feed forward control of the recirculated flue gas mass flow. 10. A gas turbine installation comprising: at least one compressor;at least one combustion chamber;at least one turbine;at least one flow splitter in an flue gas passage;a first flue gas line from the flow splitter to an exhaust stack;a second flue gas line from the flow splitter to an inlet of the compressor for flue gas recirculation;at least one control element for controlling a portion of recirculated flue gas mass flow, wherein a control reference value of the control element is at least one of a residual oxygen content of the flue gas and an oxygen content of combustion air, the reference value of the control element being dependent upon operating parameters of the gas turbine installation; andat least one device for recooling of the recirculated flue gas flow, andwherein the flow splitter includes at least one of: a. an adjustable flap for variable flow splitting; andb. a mechanically fixed splitter followed by at least one of an adjustable flap, a valve in a feed line to the exhaust stack, and a valve in a recirculation line. 11. A gas turbine installation comprising: at least one compressor;at least one combustion chamber;at least one turbine;at least one flow splitter in an flue gas passage;a first flue gas line from the flow splitter to an exhaust stack;a second flue gas line from the flow splitter to an inlet of the compressor for flue gas recirculation;at least one control element for controlling a portion of recirculated flue gas mass flow, wherein a control reference value of the control element is at least one of a residual oxygen content of the flue gas and an oxygen content of combustion air, the reference value of the control element being dependent upon operating parameters of the gas turbine installation; andat least one device for recooling of the recirculated flue gas flow, andwherein the gas turbine installation comprises at least one of:a. condensate separator; andb. a condensate processing plant, a line to an inlet of the compressor, and a pump for water injection into an intake mass flow. 12. The gas turbine installation as claimed in claim 11, comprising at least one of: a. a flue gas compressor which compresses at least some recirculated flue gas to a pressure which is high enough for introduction into a fuel gas, flue gas lines to a fuel gas system, at least one device for introducing the flue gas into the fuel gas for fuel gas dilution, at least one control valve for controlling the dilution mass flow, and a fuel gas distribution system which directs diluted fuel gas to at least one burner; andb. a condensate processing plant, lines to an flue gas compressor and at least one pump for injection of water into the flue gas compressor for intercooling. 13. A gas turbine installation comprising: at least one compressor;at least one combustion chamber;at least one turbine;at least one flow splitter in a flue gas passage;a first flue gas line from the flow splitter to an exhaust stack;a second flue gas line from the flow splitter to an inlet of the compressor for flue gas recirculation;at least one control element for controlling a portion of recirculated flue gas mass flow, wherein a control reference value of the control element is at least one of a residual oxygen content of the flue gas and an oxygen content of combustion air; andat least one device for recooling of the recirculated flue gas flow, andwherein the gas turbine installation comprises at least one of:a. a flue gas compressor which compresses at least some recirculated flue gas to a pressure which is high enough for introduction into the fuel gas, flue gas lines to a fuel gas system, at least one device for introducing the flue gas into the fuel gas for fuel gas dilution, at least one control valve for controlling the dilution mass flow, and a fuel gas distribution system which directs diluted fuel gas to at least one burner; andb. a condensate processing plant, lines to an flue gas compressor and at least one pump for injection of water into the flue gas compressor for intercooling. 14. A gas turbine installation comprising: at least one compressor;at least one combustion chamber;at least one turbine;at least one flow splitter in an flue gas passage;a first flue gas line from the flow splitter to an exhaust stack;a second flue gas line from the flow splitter to an inlet of the compressor for flue gas recirculation;at least one control element for controlling a portion of recirculated flue gas mass flow, wherein a control reference value of the control element is at least one of a residual oxygen content of the flue gas and an oxygen content of combustion air, the reference value of the control element being dependent upon operating parameters of the gas turbine installation; andat least one device for recooling of the recirculated flue gas flow, andwherein the gas turbine installation comprises at least one of:a. a measuring instrument for direct oxygen content measuring;b. an online gas analyzer;c. a device for indirect determination of oxygen content which calculates residual oxygen from compressor intake mass flow, the portions of flue gas mass flow, fuel gas composition and fuel quantity measurement; andd. a device for online analysis of a fuel gas.