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公开(公告)号：US20160376991A1
公开(公告)日：2016-12-29
申请号：US14753066
申请日：2015-06-29
Applicant: General Electric Company
Inventor： Lewis Berkley Davis, JR. , Parag Prakash Kulkarni , Robert Joseph Reed
CPC classification number: F02C7/141 , F01D25/305 , F01N3/2066 , F02C6/08 , F02C7/18 , F02C9/18 , F02K3/00 , F05D2270/082
Abstract: An airflow control system for a gas turbine according to an embodiment includes: an airflow generation system for attachment to a rotatable shaft of a gas turbine system, the airflow generation system drawing in an excess flow of air through an air intake section; a mixing area for receiving an exhaust gas stream of the gas turbine system; an air extraction system for: extracting at least a portion of the excess flow of air generated by the airflow generation system to provide bypass air; and diverting the bypass air into the mixing area to reduce a temperature of the exhaust gas stream; and an exhaust processing system for processing the reduced temperature exhaust gas stream.
Abstract translation: 根据实施例的用于燃气轮机的气流控制系统包括：用于附接到燃气轮机系统的可旋转轴的气流产生系统，所述气流产生系统通过进气部分吸入空气过量; 用于接收燃气轮机系统的废气流的混合区域; 空气提取系统，用于：提取由气流发生系统产生的空气过剩的至少一部分，以提供旁路空气; 并将旁路空气转移到混合区域中以降低废气流的温度; 以及用于处理降温废气流的废气处理系统。
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公开(公告)号：US20160376908A1
公开(公告)日：2016-12-29
申请号：US14753088
申请日：2015-06-29
Applicant: General Electric Company
Inventor： Robert Joseph Reed , Lewis Berkley Davis, JR. , Parag Prakash Kulkarni
CPC classification number: F01D15/10 , F01D25/305 , F01N3/2066 , F02C3/04 , F02C7/057 , F02C7/14 , F02C7/18 , F02C9/18 , F02K1/386 , F05D2260/606 , H02K7/1823
Abstract: A power generation system according to an embodiment includes: a gas turbine system including a compressor component, a combustor component, and a turbine component; a shaft driven by the turbine component; an airflow generation system coupled to the shaft upstream of the gas turbine system, the airflow generation system and the compressor component drawing in an excess flow of air through an air intake section; a mixing area for receiving an exhaust gas stream produced by the gas turbine system; an air extraction system for: extracting at least a portion of an excess flow of air generated by the airflow generation system and the compressor component to provide bypass air; and diverting the bypass air into the mixing area to reduce a temperature of the exhaust gas stream; an exhaust processing system for processing the reduced temperature exhaust gas stream; and an air diversion system for diverting a portion of the bypass air to the exhaust processing system.
Abstract translation: 根据实施例的发电系统包括：燃气轮机系统，包括压缩机部件，燃烧器部件和涡轮部件; 由涡轮机部件驱动的轴; 气流发生系统，其连接到所述燃气轮机系统上游的所述轴，所述气流发生系统和所述压缩机部件在通过进气部分的空气中吸入; 用于接收由所述燃气轮机系统产生的废气流的混合区域; 空气提取系统，用于：提取由所述气流发生系统和所述压缩机部件产生的空气的至少一部分空气以提供旁路空气; 并将旁路空气转移到混合区域中以降低废气流的温度; 用于处理降温废气流的废气处理系统; 以及用于将旁路空气的一部分转向排气处理系统的空气引导系统。
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13.发明申请APPLICATION OF PROBABILISTIC CONTROL IN GAS TURBINE TUNING FOR EMISSIONS-FUEL FLOW PARAMETERS, RELATED CONTROL SYSTEMS, COMPUTER PROGRAM PRODUCTS AND METHODS 有权气体涡轮调节在排放 - 燃料流量参数，相关控制系统，计算机程序产品和方法中的应用公开(公告)号：US20160305343A1
公开(公告)日：2016-10-20
申请号：US14686183
申请日：2015-04-14
Applicant: General Electric Company
CPC classification number: F02C9/28 , F05D2260/12 , F05D2260/81 , F05D2260/83 , F05D2270/306
Abstract: Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective emissions value to match a nominal emissions value, and subsequently measuring an actual fuel flow value for each GT; and adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual fuel flow value and a nominal fuel flow value at the ambient condition.
Abstract translation: 各种实施例包括一种系统，其具有：至少一个计算装置，其配置成通过执行动作来调节一组燃气轮机（GT），所述动作包括：基于每个所测量的环境条件，将所述GT组中的每个GT命令为基本负载水平 GT 指挥GT集合中的每个GT，以调整相应的排放值以匹配名义排放值，然后测量每个GT的实际燃油流量值; 并且基于各个测量的实际燃料流量值和环境条件下的标称燃料流量值之间的差异来调整GT组中的每个GT的操作条件。
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14.发明申请APPLICATION OF PROBABILISTIC CONTROL IN GAS TURBINE TUNING FOR FUEL FLOW-EMISSIONS PARAMETERS, RELATED CONTROL SYSTEMS, COMPUTER PROGRAM PRODUCTS AND METHODS 有权燃气流量调节参数，相关控制系统，计算机程序产品和方法在气体涡轮调谐中的应用公开(公告)号：US20160305339A1
公开(公告)日：2016-10-20
申请号：US14686126
申请日：2015-04-14
Applicant: General Electric Company
CPC classification number: F02C9/28 , F01D17/08 , F01D21/003 , F01D21/14 , F05D2260/81 , F05D2270/05 , F05D2270/0831
Abstract: Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective fuel flow to match a nominal fuel flow value, and subsequently measuring an actual emissions value for each GT; and adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual emissions value and a nominal emissions value at the ambient condition.
Abstract translation: 各种实施例包括一种系统，其具有：至少一个计算装置，其配置成通过执行动作来调节一组燃气轮机（GT），所述动作包括：基于每个所测量的环境条件，将所述GT组中的每个GT命令为基本负载水平 GT 指挥GT集合中的每个GT，以调整相应的燃料流量以匹配标称燃料流量值，然后测量每个GT的实际排放值; 并且基于各个测量的实际排放值和环境条件下的标称排放值之间的差异来调整GT组中的每个GT的运行状况。
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15.发明申请SYSTEMS AND APPARATUS RELATING TO DOWNSTREAM FUEL AND AIR INJECTION IN GAS TURBINES 有权与天然气涡轮机相关的下游燃料和空气注入系统和装置公开(公告)号：US20140260269A1
公开(公告)日：2014-09-18
申请号：US13836503
申请日：2013-03-15
Applicant: General Electric Company
IPC: F23R3/28
Abstract: A gas turbine engine that includes: a combustor coupled to a turbine and a downstream injection system that includes two injection stages, a first stage and a second stage, positioned within an interior flowpath, wherein the first stage comprises an axial position that is aft of the primary air and fuel injection system and the second stage comprising an axial position that is aft of the first stage. Each of the first stage and the second stage include a plurality of circumferentially spaced injectors, each injector of which is configured to inject air and fuel into a flow through the interior flowpath. The first stage and the second stage have a configuration that limits a fuel injected at the second stage to less than 50% of a fuel injected at the first stage.
Abstract translation: 一种燃气涡轮发动机，其包括：联接到涡轮机的燃烧器和下游喷射系统，其包括位于内部流路内的两个喷射级，第一级和第二级，其中所述第一级包括位于后方的轴向位置 主空气和燃料喷射系统以及第二级包括位于第一级后部的轴向位置。 第一阶段和第二阶段中的每一个包括多个周向间隔开的喷射器，其每个喷射器构造成将空气和燃料喷射到通过内部流动路径的流中。 第一阶段和第二阶段具有将在第二阶段喷射的燃料限制为小于第一阶段喷射的燃料的50％的构造。
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Patent Agency Ranking
公开(公告)号：US20180238214A1
公开(公告)日：2018-08-23
申请号：US15437785
申请日：2017-02-21
Applicant: General Electric Company
Inventor： Parag Prakash Kulkarni , Naresh Kumar Amineni , Lewis Berkley Davis, JR. , Gordon Raymond Smith
CPC classification number: F01N3/0211 , F01D25/305 , F01K7/18 , F01K23/10 , F01K23/103 , F01K23/106 , F01N3/035 , F01N2250/02 , F01N2610/05 , F02C6/18 , F02C7/26 , F02C9/28 , F05D2220/72 , F05D2270/08 , F05D2270/082 , Y02E20/16
Abstract: Embodiments of emission reduction system including various embodiments of an emission filters for a power plant including a gas turbine are disclosed. The system includes: an emission filter; and a retraction system operably coupled to an exhaust passage of the gas turbine. The exhaust passage defines an exhaust path of exhaust from the gas turbine. The retraction system selectively moves the emission filter between a first location within the exhaust path and a second location out of the exhaust path. In a combined cycle power plant, the first location is upstream of a heat recovery steam generator (HRSG). The systems and filters described allow for temporary positioning of emission filter(s) just downstream of a gas turbine exhaust outlet, or upstream of an HRSG, where provided, for emission reduction at low loads or startup conditions, and removal of the emission filter(s) once operations move to higher loads.
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公开(公告)号：US20180058337A1
公开(公告)日：2018-03-01
申请号：US15247146
申请日：2016-08-25
Applicant: General Electric Company
IPC: F02C9/50 , F01D21/00 , F02C3/04 , F02C6/18 , F01D25/00 , F02C7/04 , F01K13/00 , F01K23/10 , G05D7/06 , G05B19/418
CPC classification number: F02C9/50 , F01D21/00 , F01D21/003 , F01D25/002 , F01K13/003 , F01K23/10 , F02C3/04 , F02C6/18 , F02C7/04 , F02C7/232 , F02C9/00 , F05D2220/32 , F05D2220/72 , F05D2240/35 , F05D2270/303 , F05D2270/304 , F05D2270/306 , F05D2270/54 , F16T1/00 , G05B19/41835 , G05B2219/34315 , G05D7/0623
Abstract: A system includes a controller including a memory storing instructions to perform operations of a power generation system and a processor that executes the instructions. The instructions cause the controller to control purging fluid flow to an inlet of a gas turbine, an exhaust of the gas turbine, or a combustion section of the gas turbine. The instructions cause the controller to receive a first temperature at the inlet, a rotational speed of the gas turbine, and a purging fluid flow rate. The instructions cause the controller to calculate an exhaust flow rate of the system based on at least the first temperature, the rotational speed, and the purging fluid flow rate. The instructions cause the controller to control the system to isolate a fuel source from the gas turbine at a portion of normal operating speed sufficient to achieve a purging volume during coast down.
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公开(公告)号：US20170175648A1
公开(公告)日：2017-06-22
申请号：US14971721
申请日：2015-12-16
Applicant: General Electric Company
Inventor： Harold Lamar Jordan, JR. , Lewis Berkley Davis, JR. , Scott Arthur Day , David Spencer Ewens , Rex Allen Morgan
IPC: F02C9/28
CPC classification number: F02C9/28 , F02C9/42 , F05D2220/32 , F05D2270/082 , F05D2270/13 , F05D2270/44
Abstract: Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective power output to match a nominal power output value, and subsequently measuring an actual emissions value for each GT; adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual emissions value and a nominal emissions value at the ambient condition; and setting a target operating condition for each GT to match the adjusted operating condition after the adjusting of the operating condition.
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公开(公告)号：US20170175647A1
公开(公告)日：2017-06-22
申请号：US14971680
申请日：2015-12-16
Applicant: General Electric Company
Inventor： Lewis Berkley Davis, JR. , Scott Arthur Day , Timothy Andrew Healy , Rebecca Kathryn Jaiven , Harold Lamar Jordan, JR. , Rex Allen Morgan
IPC: F02C9/28
CPC classification number: F02C9/28 , F02C9/00 , F05D2220/32 , F05D2240/40 , F05D2270/082 , F05D2270/71 , G05B2219/41108
Abstract: Commanding GTs to base load level based upon measured ambient condition for each GT; commanding each GT to adjust a power output to match scaled power output value equal to a fraction of a difference between the respective power output and a nominal power output value, and measuring actual emissions value for each GT during the adjusting of the respective power output; and adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual emissions value, a nominal emissions value at the ambient condition and an emissions scale factor, wherein the nominal emissions value at the ambient condition and the emissions scale factor are stored in a pre-existing emissions model for the GT.
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公开(公告)号：US20170159575A1
公开(公告)日：2017-06-08
申请号：US14960930
申请日：2015-12-07
Applicant: General Electric Company
IPC: F02C9/28 , G05B19/042
CPC classification number: F02C9/28 , F02C9/00 , F02C9/42 , F05D2220/32 , F05D2270/082 , F05D2270/312 , F05D2270/313 , G05B19/042 , G05B2219/2639
Abstract: Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective power output to match a scaled power output value equal to a fraction of a difference between the respective power output and a nominal power output value, and subsequently measuring an actual emissions value for each GT; and adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual emissions value, a nominal emissions value at the ambient condition and a nominal emissions value at the ambient condition.
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