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1.发明申请POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND SUPPLEMENTAL COMPRESSOR THEREFOR 审中-公开具有压缩机创造空气流量的发电系统及其补充压缩机公开(公告)号：US20160273397A1
公开(公告)日：2016-09-22
申请号：US14662796
申请日：2015-03-19
Applicant: General Electric Company
Inventor： Sanji Ekanayake , Dale Joel Davis , William Theadore Fisher , Robert Michael Orenstein , Alston Ilford Scipio
CPC classification number: F01K23/10 , F01K23/101 , F01K23/16 , F02C3/04 , F02C6/00 , F02C6/08 , F02C9/18 , Y02E20/16
Abstract: A power generation system includes: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which air from the first integral compressor and fuel are supplied, the first combustor arranged to supply hot combustion gases to the first turbine component, and the first integral compressor having a flow capacity greater than an intake capacity of the first combustor and/or the first turbine component, creating an excess air flow. A second gas turbine system may include similar components to the first except but without excess capacity in its compressor. A control valve system controls flow of the excess air flow from the first gas turbine system to the second gas turbine system. A supplemental compressor may be coupled to the excess air flow path for augmenting the excess air flow with additional air.
Abstract translation: 发电系统包括：第一燃气轮机系统，其包括第一涡轮机部件，第一整体式压缩机和第一燃烧器，来自第一整体式压缩机和燃料的空气供应到第一燃烧器，第一燃烧器布置成将热燃烧气体供应到第一 涡轮机部件和第一整体式压缩机，其流量大于第一燃烧器和/或第一涡轮机部件的进气容量，产生过量的气流。 第二燃气轮机系统可以包括与第一燃气涡轮机系统相似的组件，除了其压缩机中没有过剩的容量。 控制阀系统控制从第一燃气轮机系统到第二燃气轮机系统的多余空气流的流动。 补充的压缩机可以耦合到过量的空气流动路径，以用额外的空气来增加过量的气流。
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2.发明申请POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND STORAGE VESSEL FOR AUGMENTING EXCESS AIR FLOW 审中-公开具有压缩机的发电系统创造过高的空气流量和储存空气流的储存容器公开(公告)号：US20160273398A1
公开(公告)日：2016-09-22
申请号：US14662800
申请日：2015-03-19
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Sanji Ekanayake , Joseph Philip Klosinski , Robert Michael Orenstein , Alston Ilford Scipio , Lisa Anne Wichmann
CPC classification number: F01K23/10 , F02C3/04 , F02C6/00 , F02C6/08 , F02C6/16 , F02C9/18 , Y02E20/16 , Y02E60/15
Abstract: A power generation system includes: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which air from the first integral compressor and fuel are supplied, the first combustor arranged to supply hot combustion gases to the first turbine component, and the first integral compressor having a flow capacity greater than an intake capacity of the first combustor and/or the first turbine component, creating an excess air flow. A second gas turbine system may include similar components to the first except but without excess capacity in its compressor. A control valve system controls flow of the excess air flow from the first gas turbine system to the second gas turbine system. A storage vessel may be coupled to the excess air flow path for augmenting the excess air flow with additional air during a peak demand period.
Abstract translation: 发电系统包括：第一燃气轮机系统，其包括第一涡轮机部件，第一整体式压缩机和第一燃烧器，来自第一整体式压缩机和燃料的空气供应到第一燃烧器，第一燃烧器布置成将热燃烧气体供应到第一 涡轮机部件和第一整体式压缩机，其流量大于第一燃烧器和/或第一涡轮机部件的进气容量，产生过量的气流。 第二燃气轮机系统可以包括与第一燃气涡轮机系统相似的组件，除了其压缩机中没有过剩的容量。 控制阀系统控制从第一燃气轮机系统到第二燃气轮机系统的多余空气流的流动。 储存容器可以联接到过量空气流动路径，以在峰值需求时段期间用额外的空气增加过量的气流。
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Patent Agency Ranking
3.发明申请公开(公告)号：US20160273393A1
公开(公告)日：2016-09-22
申请号：US14662760
申请日：2015-03-19
Applicant: General Electric Company
Inventor： Sanji Ekanayake , William Theadore Fisher , Mark Stefan Maier , Robert Michael Orenstein , Alston Ilford Scipio
CPC classification number: F01K23/10 , F01D13/003 , F02C3/13 , F02C6/00 , F02C6/02 , F02C6/08 , F02C9/18 , F05D2220/72 , F05D2230/80 , F05D2260/606 , Y02E20/16
Abstract: A power generation system includes: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which air from the first integral compressor and fuel are supplied, the first combustor arranged to supply hot combustion gases to the first turbine component, and the first integral compressor having a flow capacity greater than an intake capacity of the first combustor and/or the first turbine component, creating an excess air flow. A second gas turbine system may include a second turbine component, a second compressor and a second combustor to which air from the second compressor and fuel are supplied, the second combustor arranged to supply hot combustion gases to the second turbine component. A control valve system controls flow of the excess air flow from the first gas turbine system to the second gas turbine system.
Abstract translation: 发电系统包括：第一燃气轮机系统，其包括第一涡轮机部件，第一整体式压缩机和第一燃烧器，来自第一整体式压缩机和燃料的空气供应到第一燃烧器，第一燃烧器布置成将热燃烧气体供应到第一 涡轮机部件和第一整体式压缩机，其流量大于第一燃烧器和/或第一涡轮机部件的进气容量，产生过量的气流。 第二燃气轮机系统可以包括第二涡轮机部件，第二压缩机和第二燃烧器，来自第二压缩机和燃料的空气被供应到第二燃烧器，第二燃烧器布置成将热燃烧气体供应到第二涡轮机部件。 控制阀系统控制从第一燃气轮机系统到第二燃气轮机系统的多余空气流的流动。
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4.发明申请POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND HEAT EXCHANGER THEREFOR 审中-公开具有压缩机创造空气流量的发电系统及其换热器公开(公告)号：US20160273396A1
公开(公告)日：2016-09-22
申请号：US14662785
申请日：2015-03-19
Applicant: General Electric Company
Inventor： Sanji Ekanayake , William Theadore Fisher , Joseph Philip Klosinski , Mark Stefan Maier , George Vargese Mathai , Ryan Eric Obenhoff , Robert Michael Orenstein , Alston Ilford Scipio , Gordon Raymond Smith
CPC classification number: F01K23/10 , F01D13/003 , F01K5/00 , F02C3/13 , F02C6/00 , F02C6/02 , F02C6/08 , F02C6/18 , F02C7/185 , F05D2240/40 , F05D2250/511 , F05D2260/213 , Y02E20/16
Abstract: A power generation system includes: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which air from the first integral compressor and fuel are supplied, the first combustor arranged to supply hot combustion gases to the first turbine component, and the first integral compressor having a flow capacity greater than an intake capacity of the first combustor and/or the first gas turbine component, creating an excess air flow. A second gas turbine system may include similar components to the first except but without excess capacity in its compressor. A control valve system controls flow of the excess air flow from the first gas turbine system to the second gas turbine system. A heat exchanger may be coupled to the excess air flow path for exchanging heat with the excess air flow.
Abstract translation: 发电系统包括：第一燃气轮机系统，其包括第一涡轮机部件，第一整体式压缩机和第一燃烧器，来自第一整体式压缩机和燃料的空气供应到第一燃烧器，第一燃烧器布置成将热燃烧气体供应到第一 涡轮机部件和第一整体式压缩机，其流量大于第一燃烧器和/或第一燃气轮机部件的进气容量，产生过量的气流。 第二燃气轮机系统可以包括与第一燃气涡轮机系统相似的组件，除了其压缩机中没有过剩的容量。 控制阀系统控制从第一燃气轮机系统到第二燃气轮机系统的多余空气流的流动。 热交换器可以连接到过量的空气流动路径上，以与多余的空气流交换热量。
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5.发明申请POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND EDUCTOR AUGMENTATION 审中-公开具有压缩机的发电系统创造空气流动和教育机会公开(公告)号：US20160273394A1
公开(公告)日：2016-09-22
申请号：US14662770
申请日：2015-03-19
Applicant: General Electric Company
Inventor： Sanji Ekanayake , Dale Joel Davis , Joseph Philip Klosinski , Robert Michael Orenstein , Alston Ilford Scipio
CPC classification number: F01K23/10 , F02C3/32 , F02C6/00 , F02C6/08 , F02C9/18 , F05D2260/601 , Y02E20/16
Abstract: A power generation system includes: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which air from the first integral compressor and fuel are supplied, the first combustor arranged to supply hot combustion gases to the first turbine component, and the first integral compressor having a flow capacity greater than an intake capacity of the first combustor and/or the first turbine component, creating an excess air flow. A second gas turbine system may include similar components to the first except but without excess capacity in its compressor. A control valve system controls flow of the excess air flow to the second gas turbine system. An eductor may be positioned in the excess air flow path for using the excess air flow as a motive fluid to augment the excess air flow to the second gas turbine with additional air.
Abstract translation: 发电系统包括：第一燃气轮机系统，包括第一涡轮机部件，第一整体式压缩机和第一燃烧器，来自第一整体式压缩机和燃料的空气被供应到第一燃烧器，第一燃烧器布置成将热燃烧气体供应到第一 涡轮机部件和第一整体式压缩机，其流量大于第一燃烧器和/或第一涡轮机部件的进气容量，产生过量的气流。 第二燃气轮机系统可以包括与第一燃气涡轮机系统相似的组件，除了其压缩机中没有过剩的容量。 控制阀系统控制到第二燃气轮机系统的过量气流的流动。 喷射器可以定位在过量空气流动路径中，以使用过量气流作为运动流体，以增加具有额外空气的到第二燃气轮机的过量气流。
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6.发明申请POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW FOR SCR UNIT 审中-公开具有压缩机的发电系统为SCR单元创造空气流公开(公告)号：US20160271560A1
公开(公告)日：2016-09-22
申请号：US14662858
申请日：2015-03-19
Applicant: General Electric Company
Inventor： Sanji Ekanayake , Lewis Berkley Davis, JR. , Parag Prakash Kulkarni , Robert Michael Orenstein , Alston Ilford Scipio
CPC classification number: B01D53/8625 , F02C3/04 , F02C6/08 , F02C7/18 , F02C9/18 , F05D2260/601 , F05D2270/082 , F05D2270/101 , F23J15/02 , Y02E20/16
Abstract: A power generation system includes a gas turbine system including a turbine component, an integral compressor and a combustor to which air from the integral compressor and fuel are supplied, the combustor arranged to supply hot combustion gases to the turbine component, and the integral compressor having a flow capacity greater than an intake capacity of at least one of the combustor and the turbine component, creating an excess air flow. A first control valve system controls flow of the excess air flow along an excess air flow path to an exhaust of the turbine component. A selective catalytic reduction (SCR) unit may be coupled to an exhaust of the turbine component, the SCR unit receiving the exhaust and the excess air flow. An eductor may be positioned in the excess air flow path for using the excess air flow as a motive force to augment the excess air flow with additional air, creating an augmented excess air flow.
Abstract translation: 发电系统包括燃气轮机系统，其包括涡轮机部件，一体式压缩机和燃烧器，来自整体式压缩机和燃料的空气供应到该燃烧器中，该燃烧器布置成将热燃烧气体供应到涡轮部件，并且该整体压缩机具有 流量大于燃烧器和涡轮机部件中的至少一个的进气容量，产生过量的气流。 第一控制阀系统控制过量空气流沿着多余的气流路径流到涡轮机部件的排气口。 选择性催化还原（SCR）单元可以耦合到涡轮机部件的排气，SCR单元接收排气和多余的空气流。 喷射器可以定位在过量空气流动路径中，以使用过量气流作为动力，用额外的空气来增加过量的气流，产生增加的过量气流。
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公开(公告)号：US20160076455A1
公开(公告)日：2016-03-17
申请号：US14484774
申请日：2014-09-12
Applicant: General Electric Company
Inventor： Sanji Ekanayake , Dale Joel Davis , Robert Michael Orenstein , Alston Ilford Scipio , Raub Warfield Smith
CPC classification number: F02C7/30 , F01D25/002 , F01D25/007 , F02C7/04 , F02C9/00 , F05D2260/95 , F05D2270/30 , F05D2270/80
Abstract: Disclosed herein are systems and methods for protecting a surface from corrosive pollutants. A method includes detecting airborne corrosive pollutants proximate to a surface using at least one sensor adapted to detect a concentration of the airborne corrosive pollutants and/or one or more types of airborne corrosive pollutants, the concentration of the airborne corrosive pollutants being an instantaneous concentration value or a time-weighted-integrated concentration value; selecting a fluid to deliver to at least a portion of the surface based upon a predetermined type and/or concentration of the airborne corrosive pollutants detected by the at least one sensor; and initiating a fluid treatment to deliver the selected fluid such that the selected fluid contacts the at least a portion of the surface.
Abstract translation: 本文公开了用于保护表面免受腐蚀性污染物的系统和方法。 一种方法包括使用适于检测机载腐蚀性污染物浓度和/或一种或多种空气腐蚀性污染物的至少一种传感器来检测靠近表面的机载腐蚀性污染物，空气中腐蚀性污染物的浓度为瞬时浓度值 或时间加权积分浓度值; 基于由所述至少一个传感器检测到的机载腐蚀性污染物的预定类型和/或浓度，选择流体输送到所述表面的至少一部分; 以及启动流体处理以递送所选择的流体，使得所选择的流体接触所述表面的至少一部分。
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