System and method of recirculating exhaust gas for use in a plurality of flow paths in a gas turbine engine
A method includes generating an exhaust gas from combustion gases with a turbine; recirculating the exhaust gas along an exhaust recirculation flow path; reducing moisture within the exhaust gas along the exhaust recirculation path with an exhaust gas processing system; providing the exhaust gas to a first exhaust gas inlet of an exhaust gas compressor for compression; and providing the exhaust gas from the exhaust recirculation path to a second exhaust gas inlet separate from the first exhaust gas inlet for cooling, preheating, sealing, or any combination thereof.
1. A system, comprising:
a gas turbine system, comprising:
a turbine combustor;
a turbine driven by combustion products from the turbine combustor;
an exhaust gas compressor driven by the turbine, wherein the exhaust gas compressor is configured to compress and supply an exhaust gas comprising 5% or less oxidant by volume to the turbine combustor; and
an oxidant compression system configured to supply a compressed oxidant to the turbine combustor, wherein the oxidant compression system comprises an oxidant compressor configured to compress an oxidant to generate the compressed oxidant, and to supply the compressed oxidant to the turbine combustor, and wherein the oxidant compression system comprises one or more machine components including the oxidant compressor; and
an exhaust gas recirculation (EGR) system, wherein the EGR system is configured to recirculate the exhaust gas from the turbine along one or more exhaust recirculation paths to first and second exhaust gas inlets of the gas turbine system, and the exhaust recirculation system comprises a scrubbing system and a moisture separator upstream of at least the second exhaust gas inlet;
wherein the first exhaust gas inlet is positioned at the exhaust gas compressor to intake the exhaust gas for exhaust gas compression, wherein the second exhaust gas inlet is separate from the first exhaust gas inlet, and wherein the second exhaust gas inlet is coupled to at least one of the one or more machine components of the oxidant compression system;
wherein a flow control system having a flow control manifold is positioned downstream of the scrubbing system and the moisture separator, and wherein the second exhaust gas inlet receives exhaust gas from a point upstream of the flow control manifold and the first gas exhaust inlet receives exhaust gas downstream of the flow control manifold.
2. The system of claim 1 , wherein the second exhaust gas inlet is positioned so as to enable the exhaust gas from at least one of the one or more exhaust recirculation paths to enter into a cooling channel, a sealing channel, a heating channel, a purging channel, or any combination thereof.
3. The system of claim 2 , wherein the at least one of the one or more machine components of the oxidant compression system comprises a compressor bearing assembly, and wherein the second exhaust gas inlet is positioned so as to enable the exhaust gas from the at least one of the one or more exhaust recirculation paths to enter into the compressor bearing assembly to enable cooling, purging, sealing, or any combination thereof of the the compressor bearing assembly.
4. The system of claim 2 , wherein the second exhaust gas inlet is positioned so as to enable the exhaust gas from the at least one of the one or more exhaust recirculation paths to enter into a compressor plenum formed between inner and outer compressor casings of the oxidant compressor to temperature control of one or more compressor stages of the oxidant gas compressor.
5. The system of claim 1 , wherein the second exhaust gas inlet is positioned at the at least one of the one or more machine components of the oxidant compression system, between compressor stages of the oxidant compressor.
6. The system of claim 1 , wherein the oxidant compressor is driven by the gas turbine system and a gearbox configured to enable the oxidant compressor to operate at a different operational speed than the gas turbine system, wherein the second exhaust gas inlet is positioned at the gearbox and the at least one of the one or more machine components of the oxidant compression system comprises the gearbox.
7. The system of claim 1 , comprising an electrical generator driven by the gas turbine system and configured to generate electrical power.
8. The system of claim 1 , wherein the flow control system comprises one or more booster compressors configured to boost a pressure of the exhaust gas provided to the first exhaust gas inlet.
9. The system of claim 1 , comprising a control system comprising:
one or more tangible, non-transitory, machine readable media collectively storing one or more sets of instructions; and
one or more processing devices configured to execute the one or more sets of instructions to:
receive data indicative of an operational parameter of the turbine, the exhaust gas compressor, or another component of the system, or any combination thereof, and
adjust a parameter of the exhaust gas provided to the first exhaust gas inlet, the second exhaust gas inlet, or both, as a result of the received data.
10. The system of claim 9 , comprising one or more sensors configured to generate feedback indicative of temperature, pressure, moisture, flow rate, or any combination thereof, wherein the one or more sensors are communicatively coupled to the control system, and the one or more sensors are configured to provide the feedback to the control system as the data indicative of the operational parameter.
11. The system of claim 10 , wherein the one or more processing devices are configured to execute the one or more sets of instructions to monitor the feedback generated by the one or more sensors and adjust a parameter of the exhaust gas provided to the second exhaust gas inlet as a result of the feedback.
12. The system of claim 11 , wherein the feedback generated by the one or more sensors is indicative of a temperature, and the one or more processing devices are configured to execute the one or more sets of instructions to adjust a flow rate, a temperature, or a combination thereof, of the exhaust gas provided to the second exhaust gas inlet as a result of the feedback.
13. The system of claim 11 , wherein the feedback generated by the one or more sensors is indicative of a pressure at or between turbine stages of the turbine, and the one or more processing devices are configured to execute the one or more sets of instructions to adjust a flow rate, a temperature, or a combination thereof, of the exhaust gas provided to the second exhaust gas inlet as a result of the feedback.
14. The system of claim 10 , wherein the one or more sensors are positioned at the exhaust gas compressor, and the one or more processing devices are configured to execute the one or more sets of instructions to monitor the feedback generated by the one or more sensors and adjust a parameter of the exhaust gas provided to the second exhaust gas inlet as a result of the feedback.
15. The system of claim 14 , wherein the feedback generated by the one or more sensors is indicative of a pressure at or between compressor stages of the exhaust gas compressor, and the one or more processing devices are configured to execute the one or more sets of instructions to adjust a flow rate, a temperature, or a combination thereof, of the exhaust gas provided to the second exhaust gas inlet as a result of the feedback.
16. The system of claim 1 , comprising a stoichiometric combustion system having the turbine combustor configured to combust a fuel/oxidant mixture in a combustion equivalence ratio of between 0.95 and 1.05 fuel to oxygen in the oxidant.
17. A method, comprising:
generating an exhaust gas from combustion gases with a turbine;
recirculating the exhaust gas along an exhaust recirculation flow path;
reducing moisture within the exhaust gas along the exhaust recirculation path with an exhaust gas processing system;
providing the exhaust gas to a first exhaust gas inlet of an exhaust gas compressor for compression;
providing the exhaust gas from the exhaust recirculation path to a second exhaust gas inlet separate from the first exhaust gas inlet for temperature control, clearance control, pressure control, sealing, or any combination thereof;
monitoring feedback indicative of a temperature and/or pressure of the turbine with a control system, wherein providing the exhaust gas from the exhaust recirculation path to the second exhaust gas inlet comprises providing the exhaust gas to a turbine inlet that leads to a turbine plenum positioned between inner and outer turbine casings of the turbine; and
adjusting, as a result of the monitoring, a flow rate of the exhaust gas provided to the turbine plenum via the turbine inlet, adjusting a temperature of the exhaust gas provided to the turbine plenum via the turbine inlet, adjusting a pressure of the exhaust gas provided to the turbine plenum via the turbine inlet, or any combination thereof.
18. The method of claim 17 , comprising combusting a fuel/oxidant mixture in a combustion equivalence ratio of between 0.95 and 1.05 fuel to oxygen in the oxidant within a turbine combustor to generate the combustion gases.
19. A method, comprising:
generating an exhaust gas from combustion gases with a turbine;
recirculating the exhaust gas along an exhaust recirculation flow path;
reducing moisture within the exhaust gas along the exhaust recirculation path with an exhaust gas processing system;
providing the exhaust gas to a first exhaust gas inlet of an exhaust gas compressor for compression;
providing the exhaust gas from the exhaust recirculation path to a second exhaust gas inlet separate from the first exhaust gas inlet for temperature control, clearance control, pressure control, sealing, or any combination thereof;
monitoring feedback indicative of a temperature and/or pressure of the exhaust gas compressor with a control system, wherein providing the exhaust gas from the exhaust recirculation path to the second exhaust gas inlet comprises providing the exhaust gas to an exhaust gas compressor inlet that leads to an exhaust gas compressor plenum positioned between inner and outer compressor casings of the exhaust gas compressor; and
adjusting, as a result of the monitoring, a flow rate of the exhaust gas provided to the exhaust gas compressor plenum via the exhaust gas compressor inlet, adjusting a temperature of the exhaust gas provided to the exhaust gas compressor plenum via the exhaust gas compressor inlet, adjusting a pressure of the exhaust gas provided to the exhaust gas compressor plenum via the exhaust gas compressor inlet, or any combination thereof.
20. The method of claim 19 comprising combusting a fuel/oxidant mixture in a combustion equivalence ratio of between 0.95 and 1.05 fuel to oxygen in the oxidant within a turbine combustor to generate the combustion gases.