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1.发明授权System and method for heating a fuel using an exhaust gas recirculation system 有权使用排气再循环系统加热燃料的系统和方法公开(公告)号：US08534073B2
公开(公告)日：2013-09-17
申请号：US12258670
申请日：2008-10-27
IPC分类号： F02C3/34
摘要： An embodiment of the present invention may take the form of a system that may use the heat removed from an exhaust stream during an exhaust gas recirculation process to heat the fuel consumed by a turbomachine.
摘要翻译： 本发明的一个实施例可以采用系统的形式，该系统可以在废气再循环过程中使用从废气流中除去的热量来加热由涡轮机消耗的燃料。
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公开(公告)号：US08443584B2
公开(公告)日：2013-05-21
申请号：US13028526
申请日：2011-02-16
IPC分类号： F02G5/02 , F02G7/052 , F02G7/055 , F02M35/024 , F02M25/07 , F02M35/00 , B01D50/00 , B01D19/00
CPC分类号： F02C1/005 , F02C3/34 , F02C7/05 , F05D2270/08
摘要： An embodiment of the present invention takes the form of a system that may recirculate a portion of the exhaust of at least one turbomachine where it may be mixed with the inlet air and re-enter the turbomachine without affecting reliability and availability of the unit. An embodiment of the present invention provides an inlet system for an exhaust gas recirculation system. This inlet system may take a variety of forms and may optimize the direction that the portion of the recirculated exhaust stream flows within the inlet system.
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3.发明申请SYSTEM AND METHOD FOR HEATING A FUEL USING AN EXHAUST GAS RECIRCULATION SYSTEM 有权使用排气回收系统加热燃料的系统和方法公开(公告)号：US20100101543A1
公开(公告)日：2010-04-29
申请号：US12258670
申请日：2008-10-27
IPC分类号： F02G5/02
摘要： An embodiment of the present invention may take the form of a system that may use the heat removed from an exhaust stream during an exhaust gas recirculation process to heat the fuel consumed by a turbomachine.
摘要翻译： 本发明的一个实施例可以采用系统的形式，该系统可以在废气再循环过程中使用从废气流中除去的热量来加热由涡轮机消耗的燃料。
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公开(公告)号：US08397484B2
公开(公告)日：2013-03-19
申请号：US13028498
申请日：2011-02-16
CPC分类号： F02C1/005 , F02C3/34 , F02C7/05 , F05D2270/08
摘要： An embodiment of the present invention takes the form of a system that may recirculate a portion of the exhaust of at least one turbomachine where it may be mixed with the inlet air and re-enter the turbomachine without affecting reliability and availability of the unit. An embodiment of the present invention provides an inlet system for an exhaust gas recirculation system. This inlet system may take a variety of forms and may optimize the direction that the portion of the recirculated exhaust stream flows within the inlet system.
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公开(公告)号：US20110138768A1
公开(公告)日：2011-06-16
申请号：US13028510
申请日：2011-02-16
CPC分类号： F02C1/005 , F02C3/34 , F02C7/05 , F05D2270/08
摘要： An embodiment of the present invention takes the form of a system that may recirculate a portion of the exhaust of at least one turbomachine where it may be mixed with the inlet air and re-enter the turbomachine without affecting reliability and availability of the unit.An embodiment of the present invention provides an inlet system for an exhaust gas recirculation system. This inlet system may take a variety of forms and may optimize the direction that the portion of the recirculated exhaust stream flows within the inlet system.
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公开(公告)号：US20110138767A1
公开(公告)日：2011-06-16
申请号：US13028498
申请日：2011-02-16
CPC分类号： F02C1/005 , F02C3/34 , F02C7/05 , F05D2270/08
摘要： An embodiment of the present invention takes the form of a system that may recirculate a portion of the exhaust of at least one turbomachine where it may be mixed with the inlet air and re-enter the turbomachine without affecting reliability and availability of the unit.An embodiment of the present invention provides an inlet system for an exhaust gas recirculation system. This inlet system may take a variety of forms and may optimize the direction that the portion of the recirculated exhaust stream flows within the inlet system.
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7.发明申请System and Method of Cooling Turbine Airfoils with Sequestered Carbon Dioxide 失效用隔离二氧化碳冷却涡轮机翼的系统和方法公开(公告)号：US20100247292A1
公开(公告)日：2010-09-30
申请号：US12413854
申请日：2009-03-30
申请人： Lewis Berkley Davis, JR. , Andres Garcia-Crespo, JR. , George M. Gilchrist, III , Amit S. Toprani
发明人： Lewis Berkley Davis, JR. , Andres Garcia-Crespo, JR. , George M. Gilchrist, III , Amit S. Toprani
摘要： A turbine power generation system with enhanced cooling provided by a stream of carbon dioxide from a carbon dioxide source and a method of using a stream of carbon dioxide to cool hot gas path components. The turbine power generating system includes a compressor, a combustor, a turbine, a generator, and at least one shaft linking the compressor and turbine and generator together such that mechanical energy produced from the turbine is used to drive the compressor and the generator. Carbon dioxide that is sequestered from the exhaust of the turbine may be stored and injected back into the turbine to cool hot gas path components of the turbine.
摘要翻译： 具有由来自二氧化碳源的二氧化碳流提供的具有增强的冷却的涡轮发电系统以及使用二氧化碳流来冷却热气体路径部件的方法。 涡轮发电系统包括压缩机，燃烧器，涡轮机，发电机以及连接压缩机和涡轮机和发电机的至少一个轴，使得从涡轮机产生的机械能被用于驱动压缩机和发电机。 从涡轮机的排气隔离的二氧化碳可以被储存并注入到涡轮机中以冷却涡轮机的热气体路径部件。
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公开(公告)号：US08402737B2
公开(公告)日：2013-03-26
申请号：US13028510
申请日：2011-02-16
CPC分类号： F02C1/005 , F02C3/34 , F02C7/05 , F05D2270/08
摘要： An embodiment of the present invention takes the form of a system that may recirculate a portion of the exhaust of at least one turbomachine where it may be mixed with the inlet air and re-enter the turbomachine without affecting reliability and availability of the unit. An embodiment of the present invention provides an inlet system for an exhaust gas recirculation system. This inlet system may take a variety of forms and may optimize the direction that the portion of the recirculated exhaust stream flows within the inlet system.
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公开(公告)号：US08397483B2
公开(公告)日：2013-03-19
申请号：US13028490
申请日：2011-02-16
IPC分类号： F02G5/02 , F02C7/052 , F02C7/055 , F02M35/024 , F02M25/07
CPC分类号： F02C1/005 , F02C3/34 , F02C7/05 , F05D2270/08
摘要： An embodiment of the present invention takes the form of a system that may recirculate a portion of the exhaust of at least one turbomachine where it may be mixed with the inlet air and re-enter the turbomachine without affecting reliability and availability of the unit. An embodiment of the present invention provides an inlet system for an exhaust gas recirculation system. This inlet system may take a variety of forms and may optimize the direction that the portion of the recirculated exhaust stream flows within the inlet system.
摘要翻译： 本发明的一个实施例采用的系统的形式可以使至少一个涡轮机的排气的一部分再循环，在那里它可以与入口空气混合并重新进入涡轮机，而不会影响单元的可靠性和可用性。 本发明的实施例提供了一种用于废气再循环系统的入口系统。 该入口系统可以采取各种形式并且可优化再循环排气流的部分在入口系统内流动的方向。
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公开(公告)号：US20110131982A1
公开(公告)日：2011-06-09
申请号：US13028526
申请日：2011-02-16
CPC分类号： F02C1/005 , F02C3/34 , F02C7/05 , F05D2270/08
摘要： An embodiment of the present invention takes the form of a system that may recirculate a portion of the exhaust of at least one turbomachine where it may be mixed with the inlet air and re-enter the turbomachine without affecting reliability and availability of the unit.An embodiment of the present invention provides an inlet system for an exhaust gas recirculation system. This inlet system may take a variety of forms and may optimize the direction that the portion of the recirculated exhaust stream flows within the inlet system.
摘要翻译： 本发明的一个实施例采用的系统的形式可以使至少一个涡轮机的排气的一部分再循环，在那里它可以与入口空气混合并重新进入涡轮机，而不会影响单元的可靠性和可用性。 本发明的实施例提供了一种用于废气再循环系统的入口系统。 该入口系统可以采取各种形式并且可优化再循环排气流的部分在入口系统内流动的方向。
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