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公开(公告)号：US10727768B2
公开(公告)日：2020-07-28
申请号：US16121163
申请日：2018-09-04
Inventor： Richard A. Huntington , Karl Dean Minto , Bin Xu , Jonathan Carl Thatcher , Aaron Lavene Vorel
Abstract: A system includes a control system configured to control one or more parameters of an exhaust gas recirculation (EGR) gas turbine system to control a portion of electrical power for export from a generator driven by the turbine to an electrical grid. The control system includes a closed-loop controller configured to control parameters of the EGR gas turbine system and an open-loop controller configured to temporarily control the parameters of the EGR gas turbine system to increase the portion of the electrical power exported to the electrical grid to provide a Primary Frequency Response (PFR) in response to a transient event associated with the electrical power. The open-loop controller is configured to provide control signals to increase a concentration of an oxidant in a combustor to provide the PFR in response to the transient event when the EGR gas turbine system is operating in an emissions compliant mode.
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公开(公告)号：US10662959B2
公开(公告)日：2020-05-26
申请号：US15473776
申请日：2017-03-30
Applicant: General Electric Company
Inventor： Sidharth Abrol , Karl Dean Minto , Nisam Palakkavalappil Rahiman , Prabhanjana Kalya , Wrichik Basu , Corey Nicholas Bufi
Abstract: A non-transitory computer-readable storage medium storing one or more processor-executable instructions wherein the one or more instructions, when executed by a processor of a controller, cause acts to be performed including receiving signals representative of pressure between respective compressor blade tips and a casing of a compressor at one or more stages, generating multiple patterns based on a permutation entropy window and the signals, identifying multiple pattern categories in the multiple patterns, determining a permutation entropy based on the multiple patterns and the multiple pattern categories, predicting an anomaly in the compressor based on the permutation entropy, comparing the multiple pattern categories to determined permutations of pattern categories when an anomaly is present in the compressor, and predicting a category of the anomaly based on the comparison of the multiple pattern categories to the determined permutation of pattern categories.
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公开(公告)号：US20220356820A1
公开(公告)日：2022-11-10
申请号：US17313406
申请日：2021-05-06
Applicant: General Electric Company
Inventor： Karl Dean Minto , John Rogers Huey , Quentin Lorron
Abstract: A method for block loading an electrical grid with a combined cycle power plant (CCPP) includes operating a gas turbine system of the CCPP in an islanding mode with a steam turbine system of the CCPP off line with turning gear rotating only; loading the steam turbine system accordingly to temperature matching conditions of the steam turbine system, the loading of the steam turbine system includes controlling gas turbine exhaust fed to the steam turbine system and the gas turbine exhaust temperature heats the steam turbine system and to meet temperature matching conditions of the steam turbine system; wherein controlling gas turbine exhaust includes controlling fuel flow and air flow to the gas turbine system; and operating at least one of the gas turbine system and steam turbine system to block load the electrical grid from a load on at least one of gas turbine system and steam turbine system.
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公开(公告)号：US11248536B2
公开(公告)日：2022-02-15
申请号：US15187435
申请日：2016-06-20
Applicant: General Electric Company
Abstract: In an embodiment, a system includes a gas turbine controller. The gas turbine controller is configured to receive a plurality of sensor signals from a fuel composition sensor, a pressure sensor, a temperature sensor, a flow sensor, or a combination thereof, included in a gas turbine engine system. The controller is further configured to execute a gas turbine model by applying the plurality of sensor signals as input to derive a plurality of estimated gas turbine engine parameters. The controller is also configured to execute a flame holding model by applying the plurality of sensor signals and the plurality of estimated gas turbine engine parameters as input to derive a steam flow to fuel flow ratio that minimizes or eliminates flame holding in a fuel nozzle of the gas turbine engine system.
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公开(公告)号：US10079564B2
公开(公告)日：2018-09-18
申请号：US14585950
申请日：2014-12-30
Inventor： Richard A. Huntington , Karl Dean Minto , Bin Xu , Jonathan Carl Thatcher , Aaron Lavene Vorel
CPC classification number: H02P9/04 , E21B43/166 , F01D17/02 , F02C3/30 , F02C6/00 , F02C9/28 , F02C9/48 , F05D2220/32 , F05D2270/05 , F05D2270/08 , F05D2270/082 , H02K7/1823 , Y02E20/16 , Y02T50/677
Abstract: A non-transitory, computer readable medium stores instructions executable by a processor of an electronic device. The instructions include instructions to determine that a transient event is occurring in an electrical grid coupled to an EGR gas turbine system, wherein the transient event is an under-frequency or an under-voltage event. The instructions also include instructions to increase a flow rate of fuel to a combustor of the EGR gas turbine system in response to the transient event when the EGR gas turbine system is operating in a non-stoichiometric combustion mode. The instructions further include instructions to increase a flow rate of oxidant to the combustor before increasing the flow rate of fuel to the combustor, or to decrease a local consumption of the electrical power to increase a portion of the electrical power that is exported to the attached electrical grid, or both, in response to the transient event when the EGR gas turbine system is operating in a stoichiometric combustion mode.
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Patent Agency Ranking
公开(公告)号：US20170363015A1
公开(公告)日：2017-12-21
申请号：US15187435
申请日：2016-06-20
Applicant: General Electric Company
CPC classification number: F02C9/26 , F01D15/10 , F02C3/30 , F05D2270/05 , F05D2270/16 , F05D2270/3011 , F05D2270/303 , F05D2270/3061 , F05D2270/44 , F05D2270/71 , F23K2401/201 , F23K2900/05004 , F23N1/00 , F23N1/002 , F23N5/24 , F23N5/242 , F23N2005/185 , F23N2025/04 , F23N2025/26 , F23N2031/28 , F23N2037/22 , F23N2039/04 , F23R3/18 , F23R3/36
Abstract: In an embodiment, a system includes a gas turbine controller. The gas turbine controller is configured to receive a plurality of sensor signals from a fuel composition sensor, a pressure sensor, a temperature sensor, a flow sensor, or a combination thereof, included in a gas turbine engine system. The controller is further configured to execute a gas turbine model by applying the plurality of sensor signals as input to derive a plurality of estimated gas turbine engine parameters. The controller is also configured to execute a flame holding model by applying the plurality of sensor signals and the plurality of estimated gas turbine engine parameters as input to derive a steam flow to fuel flow ratio that minimizes or eliminates flame holding in a fuel nozzle of the gas turbine engine system.
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公开(公告)号：US20150226133A1
公开(公告)日：2015-08-13
申请号：US14144511
申请日：2013-12-30
Inventor： Karl Dean Minto , Jonathan Carl Thatcher , Brian Allen Rittenhouse , Aaron Vorel
CPC classification number: F02C9/48 , F01D15/10 , F02C1/005 , F02C1/08 , F02C3/34 , F02C7/22 , F02C9/52 , F02C9/54 , F05D2270/061 , F05D2270/304 , Y02C10/00 , Y02E20/14 , Y02E20/16
Abstract: A gas turbine system includes a combustor configured to combust an oxidant and a fuel in the presence of an exhaust gas diluent to produce combustion products, an oxidant supply path fluidly coupled to the combustor and configured to flow the oxidant to the combustor at an oxidant flow rate, and a turbine configured to extract work from the combustion products to produce an exhaust gas used to generate the exhaust gas diluent. The turbine causes a shaft of the gas turbine system to rotate when the work is extracted from the combustion products. The system also includes an electrical generator that generates electrical power in response to rotation by the shaft, and a controller that performs load control in response to a target load by adjusting the oxidant flow rate along the oxidant flow path as a primary load control parameter.
Abstract translation: 燃气轮机系统包括燃烧器，该燃烧器构造成在废气稀释剂存在下燃烧氧化剂和燃料以产生燃烧产物;氧化剂供给路径，其流体地联接到燃烧器并且被配置为以氧化剂流将氧化剂流到燃烧器 并且构造成从燃烧产物中提取工作以产生用于产生废气稀释剂的废气的涡轮机。 当从燃烧产物中取出工件时，涡轮机使燃气轮机系统的轴旋转。 该系统还包括响应于轴的旋转产生电力的发电机，以及控制器，其通过沿着氧化剂流动路径调节氧化剂流速作为主负载控制参数来响应于目标负载来执行负载控制。
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8.发明申请SYSTEM AND METHOD FOR CONTROLLING THE COMBUSTION PROCESS IN A GAS TURBINE OPERATING WITH EXHAUST GAS RECIRCULATION 有权用于控制气体再循环运行的燃气涡轮机中的燃烧过程的系统和方法公开(公告)号：US20150204239A1
公开(公告)日：2015-07-23
申请号：US14599739
申请日：2015-01-19
Inventor： Karl Dean Minto , Ilya Aleksandrovich Slobodyanskiy , Lewis Berkley Davis, Jr. , John Joseph Lipinski
CPC classification number: F02C3/34 , F02C7/228 , F02C7/232 , F02C9/26 , F02C9/50 , F05D2260/611 , Y02E20/16
Abstract: A system includes a fuel control system configured to control a fuel flow to one or more combustors and an oxidant control system configured to control an oxidant flow to each combustor of the one or more combustors, wherein the oxidant flow is configured to at least partially react with the fuel flow within the one or more combustors to form an exhaust gas flow. The system also includes an exhaust gas system configured to direct a recirculation flow of the exhaust gas flow to each combustor of the one or more combustors; and a controller coupled to the fuel control system, the oxidant control system, and the exhaust gas system. The controller is configured to independently control a fuel-to-oxidant ratio and an exhaust gas-to-oxidant ratio. The FOR is the fuel flow divided by the oxidant flow, and the EGOR is the recirculation flow divided by the oxidant flow.
Abstract translation: 一种系统包括燃料控制系统，该燃料控制系统被配置为控制到一个或多个燃烧器的燃料流量和被配置成控制向一个或多个燃烧器的每个燃烧器的氧化剂流量的氧化剂控制系统，其中氧化剂流被配置为至少部分地反应 燃料流在一个或多个燃烧器内以形成废气流。 该系统还包括排气系统，其构造成将废气流的再循环流引导到一个或多个燃烧器的每个燃烧器; 以及耦合到燃料控制系统，氧化剂控制系统和废气系统的控制器。 控制器被配置为独立地控制燃料与氧化剂的比例和排气与氧化剂之比。 FOR是燃料流除以氧化剂流，EGOR是再循环流除以氧化剂流。
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9.发明申请SYSTEM AND METHOD OF CONTROLLING COMBUSTION AND EMISSIONS IN GAS TURBINE ENGINE WITH EXHAUST GAS RECIRCULATION 有权用气体回收控制燃气轮机发动机的排放和排放的系统和方法公开(公告)号：US20150033749A1
公开(公告)日：2015-02-05
申请号：US14444601
申请日：2014-07-28
CPC classification number: F23N1/02 , F02C1/005 , F02C3/34 , F05D2260/61 , F05D2270/08 , F05D2270/083 , F23C9/00 , F23C9/08 , F23C2202/20 , F23C2202/30 , F23N2021/12 , F23N2041/20 , F23R3/002 , F23R3/16 , F23R3/26 , F23R3/40 , Y02E20/16 , Y02T50/677
Abstract: In one embodiment, a system includes a turbine combustor having a combustor liner disposed about a combustion chamber, a head end upstream of the combustion chamber relative to a downstream direction of a flow of combustion gases through the combustion chamber, a flow sleeve disposed at an offset about the combustor liner to define a passage, and a barrier within the passage. The head end is configured to direct an oxidant flow and a first fuel flow toward the combustion chamber. The passage is configured to direct a gas flow toward the head end and to direct a portion of the oxidant flow toward a turbine end of the turbine combustor. The gas flow includes a substantially inert gas. The barrier is configured to block the portion of the oxidant flow toward the turbine end and to block the gas flow toward the head end within the passage.
Abstract translation: 在一个实施例中，系统包括涡轮机燃烧器，其具有围绕燃烧室设置的燃烧器衬套，相对于通过燃烧室的燃烧气体的下游方向的燃烧室上游的头端;设置在燃烧室 偏置在燃烧器衬套周围以限定通道，以及通道内的阻挡层。 头端构造成将氧化剂流和第一燃料流引向燃烧室。 通道构造成引导朝向头端的气流，并将一部分氧化剂流引向涡轮机燃烧器的涡轮机端。 气流包括基本惰性的气体。 阻挡件被构造成阻挡氧化剂流向汽轮机端的部分并且阻挡朝向通道内的头端的气流。
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公开(公告)号：US20140093349A1
公开(公告)日：2014-04-03
申请号：US13630694
申请日：2012-09-28
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Daniel Richard Waugh , Karl Dean Minto , Scott William Szepek , Louis Veltre
IPC: F04D27/00
CPC classification number: F04D27/001 , F04D27/0253 , G01M15/14
Abstract: Certain embodiments of the disclosure may include systems, methods and apparatus for operating and validating a compressor. According to an example embodiment of the disclosure, a method is provided for validating compressor operation. The method can include receiving compressor operating parameter data from a plurality of sensors; and adjusting a portion of a variable flow area downstream of a compressor discharge to achieve a desired compressor pressure ratio.
Abstract translation: 本公开的某些实施例可以包括用于操作和验证压缩机的系统，方法和装置。 根据本公开的示例性实施例，提供了一种用于验证压缩机操作的方法。 该方法可以包括从多个传感器接收压缩机操作参数数据; 并且调节压缩机排放下游的可变流动区域的一部分以实现期望的压缩机压力比。
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