초록 ▼

Ambient air is compressed into a compressed ambient gas flow and delivered to a turbine combustor. At least one of an exhaust port, a bypass conduit, or an extraction conduit is opened to vent the power plant. A turbine shaft is rotated at an ignition speed and a fuel stream is delivered to the turb

Ambient air is compressed into a compressed ambient gas flow and delivered to a turbine combustor. At least one of an exhaust port, a bypass conduit, or an extraction conduit is opened to vent the power plant. A turbine shaft is rotated at an ignition speed and a fuel stream is delivered to the turbine combustor for mixing with the compressed ambient gas flow to form a combustible mixture. The combustible mixture is burned and forms a recirculated gas flow that drives the turbine. The recirculated gas flow is recirculated using the recirculation loop. The turbine is operated at a target operating speed and then reaches substantially stoichiometric combustion. At least a portion of the recirculated gas flow is extracted using an extraction conduit that is fluidly connected to the turbine compressor.

대표청구항 ▼

1. A method for starting-up a stoichiometric exhaust gas recirculation power plant arrangement, comprising the steps of: compressing ambient air into a compressed ambient gas flow with at least one main air compressor;delivering at least a first portion of the compressed ambient gas flow, with a com

1. A method for starting-up a stoichiometric exhaust gas recirculation power plant arrangement, comprising the steps of: compressing ambient air into a compressed ambient gas flow with at least one main air compressor;delivering at least a first portion of the compressed ambient gas flow, with a compressed ambient gas flow rate, to a turbine combustor that is fluidly connected to the at least one main air compressor;providing an extraction conduit that is fluidly connected to a turbine compressor;venting the power plant by opening a vent, wherein the vent comprises at least one of the extraction conduit or an exhaust port, wherein the exhaust port is fluidly connected to a recirculation looprotating a turbine shaft connecting a turbine to the turbine compressor at an ignition speed;delivering a fuel stream, having a fuel stream flow rate, to the turbine combustor for mixing with the at least a first portion of the compressed ambient gas flow from the at least one main air compressor and with at least a first portion of a recirculated gas flow from the turbine compressor to form a combustible mixture;burning the combustible mixture in the turbine combustor and thereby forming the recirculated gas flow and driving the turbine and the turbine compressor;recirculating the recirculated gas flow from the turbine to the turbine compressor using the recirculation loop;operating the turbine at a target operating speed, and, if necessary, accelerating the turbine to the target operating speed by adjusting the fuel stream flow rate and the compressed ambient gas flow rate;adjusting the fuel stream flow rate and the compressed ambient gas flow rate to reach substantially stoichiometric combustion; andextracting at least a second portion of the recirculated gas flow using the extraction conduit. 2. The method of claim 1, further comprising the step of synchronizing a turbine generator, mechanically connected to the turbine shaft, to a power grid. 3. The method of claim 2, further comprising the step of loading the turbine generator to a load point by increasing the fuel stream flow rate and the compressed ambient gas flow rate. 4. The method of claim 1, further comprising the step of purging the power plant arrangement before the step of delivering a fuel stream to the turbine combustor, wherein the turbine shaft is rotated at a purge speed and the at least a first portion of compressed ambient gas flow is used to vent substantially all combustibles from the power plant arrangement. 5. The method of claim 1, further comprising delivering a secondary flow through a secondary flow path, wherein the secondary flow path delivers at least a third portion of the recirculated gas flow from the turbine compressor to the turbine for cooling and sealing the turbine and thereafter into the recirculation loop. 6. The method of claim 1, further comprising delivering at least a third portion of the recirculated gas flow from the turbine compressor to a bypass conduit, wherein the bypass conduit is configured to deliver the recirculated gas flow to the recirculation loop downstream of the turbine. 7. The method of claim 1, wherein one or more steps are performed simultaneously. 8. The method of claim 1, wherein the step of accelerating the turbine to a target operating speed further comprises adjusting a variable bleed valve that is in fluid communication with the at least one main air compressor and that is configured to vent a portion, if any, of the compressed ambient gas flow to the atmosphere. 9. A method for starting-up at least one master train of a stoichiometric exhaust gas recirculation power plant arrangement, comprising the steps of: compressing ambient air into a compressed ambient gas flow with at least one main air compressor;delivering at least a first portion of the compressed ambient gas flow, with a master compressed ambient gas flow rate, to the master turbine combustor that is fluidly connected to the at least one main air compressor;providing a master extraction conduit that is fluidly connected to a master turbine compressor;venting the at least one master train by opening a master vent, wherein the master vent comprises at least one of the master extraction conduit or a master exhaust port, wherein the master exhaust port is fluidly connected to a master recirculation looprotating a master turbine shaft connecting a master turbine to the master turbine compressor at an ignition speed;delivering a master fuel stream, having a master fuel stream flow rate, to the master turbine combustor for mixing with the at least a first portion of the compressed ambient gas flow from the at least one main air compressor and with at least a first portion of a master recirculated gas flow from the master turbine compressor to form a master combustible mixture;burning the master combustible mixture in the master turbine combustor and thereby forming the master recirculated gas flow and driving the master turbine and the master turbine compressor;recirculating the master recirculated gas flow from the master turbine to the master turbine compressor using the master recirculation loop;operating the master turbine at a master target operating speed, and, if necessary, accelerating the master turbine to the master target operating speed by adjusting the master fuel stream flow rate and the master compressed ambient gas flow rate;adjusting the master fuel stream flow rate and the master compressed ambient gas flow rate to reach substantially stoichiometric combustion; andextracting at least a second portion of the master recirculated gas flow using the master extraction conduit. 10. The method of claim 9, further comprising the step of synchronizing a master turbine generator, mechanically connected to the master turbine shaft, to a power grid. 11. The method of claim 10, further comprising the step of loading the master turbine generator to a load point by increasing the master fuel stream flow rate and the master compressed ambient gas flow rate. 12. The method of claim 9, further comprising the step of purging the at least one master train before the step of delivering the master fuel stream to the master turbine combustor, wherein the master turbine shaft is rotated by external mechanical power and the at least a first portion of compressed ambient gas flow is used to vent substantially all combustibles from the at least one master train. 13. The method of claim 9, further comprising delivering a master secondary flow through a master secondary flow path, wherein the master secondary flow path delivers at least a third portion of the master recirculated gas flow from the master turbine compressor to the master turbine for cooling and sealing the master turbine and thereafter into the master recirculation loop. 14. The method of claim 9, wherein one or more of the steps are performed simultaneously. 15. The method of claim 9, wherein the step of accelerating the master turbine shaft to a target operating speed further comprises adjusting a master variable bleed valve that is in fluid communication with the main air compressor and that is configured to vent a portion, if any, of the compressed ambient gas flow to the atmosphere. 16. The method of claim 9, further comprising starting— up at least one slave train of a stoichiometric exhaust gas recirculation power plant arrangement, comprising the steps of: delivering at least a second portion of the compressed ambient gas flow, with a slave compressed ambient gas flow rate, to the slave turbine combustor that is fluidly connected to the at least one main air compressor;venting the at least one slave train by opening a slave vent, wherein the slave vent comprises at least one of the slave extraction conduit or a slave exhaust port, wherein the slave exhaust port is fluidly connected to a slave recirculation loop;rotating a slave turbine shaft connecting a slave turbine to the slave turbine compressor at an ignition speed;delivering a slave fuel stream, having a slave fuel stream flow rate, to the slave turbine combustor for mixing with the at least a second portion of the compressed ambient gas flow from the at least one main air compressor and with at least a first portion of a slave recirculated gas flow from the slave turbine compressor to form a slave combustible mixture;burning the slave combustible mixture in the slave turbine combustor and thereby forming the slave recirculated gas flow and driving the slave turbine and the slave turbine compressor;recirculating the slave recirculated gas flow from the slave turbine to the slave turbine compressor using the slave recirculation loop;operating the slave turbine at a slave target operating speed, and, if necessary, accelerating the slave turbine to the slave target operating speed by adjusting the slave fuel stream flow rate and the slave compressed ambient gas flow rate;adjusting the slave fuel stream flow rate and the slave compressed ambient gas flow rate to reach substantially stoichiometric combustion; andextracting at least a second portion of the slave recirculated gas flow using the slave extraction conduit. 17. The method of claim 16, further comprising the step of synchronizing a slave turbine generator, mechanically connected to the slave turbine shaft, to a power grid. 18. The method of claim 17, further comprising the step of loading the slave turbine generator to a load point by increasing the slave fuel stream flow rate and the slave compressed ambient gas flow rate. 19. The method of claim 16, further comprising the step of purging the at least one slave train before the step of delivering the slave fuel stream to the slave turbine combustor, wherein the slave turbine shaft is rotated by external mechanical power and the at least a second portion of compressed ambient gas flow is used to vent substantially all combustibles from the at least one slave train. 20. The method of claim 16, further comprising delivering a slave secondary flow through a slave secondary flow path, wherein the slave secondary flow path delivers at least a third portion of the slave recirculated gas flow from the slave turbine compressor to the slave turbine for cooling and sealing the slave turbine and thereafter into the slave recirculation loop.