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1.发明授权公开(公告)号：US10544739B2
公开(公告)日：2020-01-28
申请号：US15049674
申请日：2016-02-22
发明人： Alston Ilford Scipio , Michael Anthony Cocca , Thomas John Freeman , Michael Wesley Yarnold , Ryan Eric Obenhoff , Sanji Ekanayake , Douglas Corbin Warwick , Joseph Philip Klosinski
IPC分类号： F02C6/08 , F02C9/18 , F02C3/34 , F02C9/22 , F02C9/26 , F01K23/10 , F02C3/13 , F02C9/28 , F23R3/26
摘要： A gas turbine system includes a compressor protection subsystem; a hibernation mode subsystem; and a control subsystem that controls the compressor subsystem and the hibernation subsystem. At partial loads on the turbine system, the compressor protection subsystem maintains an air flow through a compressor at an airflow coefficient for the partial load above a minimum flow rate coefficient where aeromechanical stresses occur in the compressor. The air fuel ratio in a combustor is maintained where exhaust gas emission components from the turbine are maintained below a predetermined component emission level while operating at partial loads.
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公开(公告)号：US10344677B2
公开(公告)日：2019-07-09
申请号：US14290608
申请日：2014-05-29
摘要： Systems and methods for preheating fuel in a gas turbine engine are provided. In one embodiment, a system may include a gas turbine engine, a fuel line in fluid communication with the gas turbine engine, a gas turbine compartment disposed about the gas turbine engine, and a first conduit in fluid communication with the gas turbine compartment. The first conduit may include ventilation discharge air from the gas turbine compartment. The system also may include a first heat exchanger in communication with the fuel line and the first conduit. The first heat exchanger may be configured to exchange heat between the fuel and the ventilation discharge air from the gas turbine compartment.
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公开(公告)号：US10253652B2
公开(公告)日：2019-04-09
申请号：US14969051
申请日：2015-12-15
发明人： George Vargese Mathai , Alston Ilford Scipio , Harold Lamar Jordan, Jr. , Sanji Ekanayake , Joseph Philip Klosinski
摘要： A system for controlling gas turbine output for a gas turbine power plant is disclosed herein. The power plant includes a gas turbine including a combustor downstream from a compressor, a turbine downstream from the combustor and an exhaust duct downstream from the outlet of the turbine. The exhaust duct receives exhaust gas from the turbine outlet. The system further includes an exhaust damper operably connected to a downstream end of the exhaust duct. The exhaust damper increases backpressure at the turbine outlet and restricts axial exit velocity of the exhaust gas exiting the turbine outlet when the exhaust damper is partially closed. A method for controlling gas turbine output is also provided herein.
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公开(公告)号：US20180216499A1
公开(公告)日：2018-08-02
申请号：US15420776
申请日：2017-01-31
发明人： George Vargese Mathai , Joseph Philip Klosinski , Sanji Ekanayake , Alston Ilford Scipio , William Theadore Fisher
CPC分类号： F01K13/025 , F01D25/10 , F01K13/003 , F01K17/025 , F01K23/10 , F02C6/06 , F02C6/18 , F05D2220/72 , Y02E20/14 , Y02E20/16
摘要： The present application provides a power generation system. The power generation system may include a gas turbine engine, a steam turbine, and a steam turbine preheating system. The steam turbine preheating system may include a steam generator that creates a flow of steam to preheat the steam turbine from an extraction of the gas turbine engine.
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公开(公告)号：US10036321B2
公开(公告)日：2018-07-31
申请号：US14290580
申请日：2014-05-29
CPC分类号： F02C7/08 , F01D25/145 , F02C1/08 , F02C7/047 , F02C9/18
摘要： Systems and methods for utilizing gas turbine compartment ventilation discharge air. In one embodiment, a system may include a gas turbine engine having a compressor. The system also may include a gas turbine compartment disposed about the gas turbine engine. Moreover, the system may include an inlet bleed heat (IBH) manifold in fluid communication with the compressor. The gas turbine compartment may be in fluid communication with the IBH manifold for providing the IBH manifold with ventilation discharge air from the gas turbine compartment.
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公开(公告)号：US09909507B2
公开(公告)日：2018-03-06
申请号：US14606548
申请日：2015-01-27
CPC分类号： F02C9/26 , F02C9/28 , F05D2270/3015
摘要： A control system for a combustor system including a plurality of can combustors, each can combustor accommodating combustion of a plurality of combustion fluids in a combustion chamber thereof is provided. The control system may include a calculator calculating: a) a pressure drop for each respective can combustor of the plurality of can combustors between a selected combustion fluid upstream of the combustion chamber and a combustion flow within the combustion chamber of the respective can combustor, and b) a differential between the respective pressure drop for each of the plurality of can combustors and an average pressure drop across all of the plurality of can combustors. The differentials identify can-to-can variation. A controller can modify a combustion parameter of at least one can combustor to reduce the differential for the at least one can combustor. The system can work iteratively to reduce can-to-can variation.
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公开(公告)号：US09816391B2
公开(公告)日：2017-11-14
申请号：US14493378
申请日：2014-09-23
CPC分类号： F01D25/002 , B05B7/0892 , B08B3/02 , B08B9/00
摘要： The present application thus provides a cleaning system for use with a compressor of a turbine engine. The cleaning system may include a wash nozzle positioned about the compressor and a spheroid injection port to inject a number of spheroids therein.
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公开(公告)号：US20170218852A1
公开(公告)日：2017-08-03
申请号：US15012473
申请日：2016-02-01
发明人： Joseph Philip Klosinski , Alston Ilford Scipio , Alex Clinton Solomon , Sanji Ekanayake , Hannah Louise Dombek
CPC分类号： F02C9/18 , F02C7/047 , F05D2220/32 , F05D2260/232 , F05D2270/101
摘要： An inlet bleed heat system for use with a turbine assembly includes a first discharge line coupled in flow communication between a compressor and an intake manifold assembly. A first control valve that is coupled to the first discharge line and operable to control a first discharge flow through the first discharge line from the compressor to the intake manifold assembly during a first operational mode. A second discharge line that is coupled in flow communication between the compressor and the intake manifold assembly and a second control valve that is coupled to the second discharge line and operable to control a second discharge flow through the second discharge line from the compressor to the intake manifold assembly during a second operational mode.
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公开(公告)号：US20170167377A1
公开(公告)日：2017-06-15
申请号：US14969079
申请日：2015-12-15
CPC分类号： F02C6/06 , F01D25/305 , F01K17/02 , F01K17/06 , F01K23/10 , F02C3/04 , F02C6/08 , F02C6/18 , F02C7/141 , F02C7/185 , F02C9/18 , H02K7/1823 , Y02E20/14 , Y02E20/16
摘要： A power plant includes a turbine disposed downstream from a combustor. The turbine includes an extraction port that is in fluid communication with a hot gas path of the turbine and which provides a flow path for a stream of combustion gas to flow out of the turbine. An exhaust duct is disposed downstream from the turbine and receives exhaust gas from the turbine. An ejector coupled to the extraction port and to an air supply cools the stream of combustion gas upstream from the exhaust duct. The cooled combustion gas flows into the exhaust duct at a higher temperature than the exhaust gas. The cooled combustion gas mixes with the exhaust gas within the exhaust duct to provide a heated exhaust gas mixture to a heat exchanger disposed downstream from the exhaust duct. The heat exchanger may extract thermal energy from the exhaust gas mixture to produce steam.
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公开(公告)号：US20170167376A1
公开(公告)日：2017-06-15
申请号：US14969067
申请日：2015-12-15
发明人： Joseph Philip Klosinski , Michael Anthony Cocca , Alston Ilford Scipio , Sanji Ekanayake , Jason Brian Shaffer
CPC分类号： F02C6/06 , F01D25/305 , F01K23/10 , F01K23/101 , F02C3/04 , F02C6/18 , H02K7/1823 , Y02E20/14 , Y02E20/16
摘要： A power plant includes a turbine having a plurality of turbine stages and an extraction port in fluid communication with one or more of the turbine stages. The extraction port provides a flow path for a stream of combustion gas to flow out of the turbine. An exhaust duct is disposed downstream from the turbine and receives exhaust gas from the turbine. The exhaust duct is fluid communication with the extraction port. A coolant injection system injects a coolant into the stream of combustion gas to provide cooled combustion gas to the exhaust duct. The cooled combustion gas flows into the exhaust duct at a temperature that is higher than a temperature of the exhaust gas, thereby increasing the temperature of the exhaust gas within the exhaust duct. The increase in thermal energy may be used to produce steam downstream from the exhaust duct.
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