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1.发明申请SYSTEMS RELATING TO GEOTHERMAL ENERGY AND THE OPERATION OF GAS TURBINE ENGINES 审中-公开与地热能相关的系统和气体涡轮发动机的运行公开(公告)号：US20110132571A1
公开(公告)日：2011-06-09
申请号：US12631363
申请日：2009-12-04
IPC分类号： F24J3/08
CPC分类号： F02C1/04 , F05B2260/208 , F24T10/10 , F24T10/30 , Y02E10/12
摘要： A geothermal heat exchange system for use in a gas turbine power plant that includes an inlet plenum that directs a flow of air to a compressor that compresses a flow of air that is then mixed with a fuel and combusted in a combustor such that the resulting flow of hot gas is directed through a turbine, the geothermal heat exchange system comprising means for exchanging heat between a ground and the flow of air moving through the inlet plenum.
摘要翻译： 一种用于燃气轮机发电厂的地热热交换系统，其包括将空气流引导到压缩机的入口增压室，压缩机压缩空气流，然后将其与燃料混合并在燃烧器中燃烧，使得所得到的流 热气体引导通过涡轮机，地热换热系统包括用于在地面和通过入口气室移动的空气流之间进行热交换的装置。
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公开(公告)号：US20090067988A1
公开(公告)日：2009-03-12
申请号：US11732689
申请日：2007-04-04
申请人： Ravi Praveen S. Eluripati , David W. Ball, JR. , Kenneth N. Whaling , James L. Davis , Nattamai V. Saravanan , Ajit S. Sengar
发明人： Ravi Praveen S. Eluripati , David W. Ball, JR. , Kenneth N. Whaling , James L. Davis , Nattamai V. Saravanan , Ajit S. Sengar
CPC分类号： F02C7/141 , B01F3/02 , B01F5/0256 , F05D2260/601 , Y02T50/675
摘要： A system for mixing flows from a compressor is provided. The system comprises an ejector that combines a first flow and a second flow, from the compressor, into a third flow. A bypass flow is connected between the first flow and the third flow. A mixer combines the bypass flow and the third flow into a fourth flow. The fourth flow has a pressure and temperature intermediate the respective pressures and temperatures of the bypass flow and the third flow.
摘要翻译： 提供了一种用于混合来自压缩机的流的系统。 该系统包括将来自压缩机的第一流和第二流组合成第三流的喷射器。 旁通流连接在第一流和第三流之间。 混合器将旁路流和第三流合并成第四流。 第四流具有压力和温度在旁路流和第三流的相应压力和温度之间。
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3.发明授权公开(公告)号：US08474270B2
公开(公告)日：2013-07-02
申请号：US13396930
申请日：2012-02-15
申请人： Carl Gerard Schott , Kevin W. Kinzie , John Joseph Lynch , David W. Ball , Gunnar Leif Siden , Kenneth Neil Whaling
发明人： Carl Gerard Schott , Kevin W. Kinzie , John Joseph Lynch , David W. Ball , Gunnar Leif Siden , Kenneth Neil Whaling
CPC分类号： F02K1/386 , B01J2208/00106 , B01J2208/00442 , B01J2219/00247 , F04F5/46 , F04F5/54 , Y10T29/494
摘要： A method of assembling an ejector is provided, wherein the method includes providing a motive nozzle tip having a centerline axis and including a nozzle tip edge having at least one protrusion extending through a plane substantially normal to the centerline axis. The method also includes coupling the motive nozzle tip to the ejector.
摘要翻译： 提供了一种组装喷射器的方法，其中所述方法包括提供具有中心线轴线的动力喷嘴尖端，并且包括具有延伸穿过基本上垂直于中心线轴线的平面的至少一个突起的喷嘴尖端边缘。 该方法还包括将动力喷嘴尖端连接到喷射器。
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公开(公告)号：US07536864B2
公开(公告)日：2009-05-26
申请号：US11164836
申请日：2005-12-07
申请人： Christopher E. Wolfe , Douglas F. Beadie , Kenneth N. Whaling , David W. Ball , Kevin T. McGovern , Ravi Praveen Eluripati , Omprakash Samudrala
发明人： Christopher E. Wolfe , Douglas F. Beadie , Kenneth N. Whaling , David W. Ball , Kevin T. McGovern , Ravi Praveen Eluripati , Omprakash Samudrala
CPC分类号： F02C7/18 , F01D17/105 , F02C6/08 , F05D2220/321 , F05D2220/3212 , F05D2260/601 , F05D2270/301
摘要： A gas turbine engine system. The system includes a compressor with a first compressor stage and a second compressor stage, a turbine with a first turbine stage and a second turbine stage, a first flow path connecting the first compressor stage and the first turbine stage, a second flow path connecting the second compressor stage and the second turbine stage, a crossover flow path connecting the first flow path and the second flow path, and an ejector positioned about the crossover flow path and the first flow path. The ejector may be a variable motive nozzle ejector.
摘要翻译： 燃气涡轮发动机系统。 该系统包括具有第一压缩机级和第二压缩机级的压缩机，具有第一涡轮级和第二涡轮级的涡轮机，连接第一压缩机级和第一涡轮级的第一流动路径，连接第 第二压缩机级和第二涡轮级，连接第一流动路径和第二流动路径的交叉流动路径，以及围绕交叉流动路径和第一流动路径定位的喷射器。 喷射器可以是可变的喷射喷嘴。
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5.发明申请公开(公告)号：US20120137704A1
公开(公告)日：2012-06-07
申请号：US13396930
申请日：2012-02-15
申请人： Carl Gerard Schott , Kevin W. Kinzie , John Joseph Lynch , David W. Ball , Gunnar Leif Siden , Kenneth Neil Whaling
发明人： Carl Gerard Schott , Kevin W. Kinzie , John Joseph Lynch , David W. Ball , Gunnar Leif Siden , Kenneth Neil Whaling
CPC分类号： F02K1/386 , B01J2208/00106 , B01J2208/00442 , B01J2219/00247 , F04F5/46 , F04F5/54 , Y10T29/494
摘要： A method of assembling an ejector is provided, wherein the method includes providing a motive nozzle tip having a centerline axis and including a nozzle tip edge having at least one protrusion extending through a plane substantially normal to the centerline axis. The method also includes coupling the motive nozzle tip to the ejector.
摘要翻译： 提供了一种组装喷射器的方法，其中所述方法包括提供具有中心线轴线的动力喷嘴尖端，并且包括具有延伸穿过基本上垂直于中心线轴线的平面的至少一个突起的喷嘴尖端边缘。 该方法还包括将动力喷嘴尖端连接到喷射器。
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6.发明授权公开(公告)号：US08136361B2
公开(公告)日：2012-03-20
申请号：US11381598
申请日：2006-05-04
申请人： Carl Gerard Schott , Kevin W. Kinzie , John Joseph Lynch , David W. Ball , Gunnar Leif Siden , Kenneth Neil Whaling
发明人： Carl Gerard Schott , Kevin W. Kinzie , John Joseph Lynch , David W. Ball , Gunnar Leif Siden , Kenneth Neil Whaling
CPC分类号： F02K1/386 , B01J2208/00106 , B01J2208/00442 , B01J2219/00247 , F04F5/46 , F04F5/54 , Y10T29/494
摘要： A method of assembling an ejector is provided, wherein the method includes providing a motive nozzle tip having a centerline axis and including a nozzle tip edge having at least one protrusion extending through a plane substantially normal to the centerline axis. The method also includes coupling the motive nozzle tip to the ejector.
摘要翻译： 提供了一种组装喷射器的方法，其中所述方法包括提供具有中心线轴线的动力喷嘴尖端，并且包括具有延伸穿过基本上垂直于中心线轴线的平面的至少一个突起的喷嘴尖端边缘。 该方法还包括将动力喷嘴尖端连接到喷射器。
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公开(公告)号：US07698898B2
公开(公告)日：2010-04-20
申请号：US11732689
申请日：2007-04-04
申请人： Ravi Praveen S. Eluripati , David W. Ball, Jr. , Kenneth N. Whaling , James L. Davis , Nattamai V. Saravanan , Ajit S. Sengar
发明人： Ravi Praveen S. Eluripati , David W. Ball, Jr. , Kenneth N. Whaling , James L. Davis , Nattamai V. Saravanan , Ajit S. Sengar
IPC分类号： F02C6/04
CPC分类号： F02C7/141 , B01F3/02 , B01F5/0256 , F05D2260/601 , Y02T50/675
摘要： A system for mixing flows from a compressor is provided. The system comprises an ejector that combines a first flow and a second flow, from the compressor, into a third flow. A bypass flow is connected between the first flow and the third flow. A mixer combines the bypass flow and the third flow into a fourth flow. The fourth flow has a pressure and temperature intermediate the respective pressures and temperatures of the bypass flow and the third flow.
摘要翻译： 提供了一种用于混合来自压缩机的流的系统。 该系统包括将来自压缩机的第一流和第二流组合成第三流的喷射器。 旁通流连接在第一流和第三流之间。 混合器将旁路流和第三流合并成第四流。 第四流具有压力和温度在旁路流和第三流的相应压力和温度之间。
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