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1.发明申请Heat Engine and Heat to Electricity Systems and Methods with Working Fluid Mass Management Control 有权热力发动机和热量到电力系统和工作流体质量管理控制的方法公开(公告)号：US20140096524A1
公开(公告)日：2014-04-10
申请号：US14102628
申请日：2013-12-11
CPC分类号： F01K3/185 , F01K7/08 , F01K25/103 , F24H2240/12
摘要： Aspects of the disclosure generally provide a heat engine system and a method for regulating a pressure and an amount of a working fluid in a working fluid circuit during a thermodynamic cycle. A mass management system may be employed to regulate the working fluid circulating throughout the working fluid circuit. The mass management systems may have a mass control tank fluidly coupled to the working fluid circuit at one or more strategically-located tie-in points. A heat exchanger coil may be used in conjunction with the mass control tank to regulate the temperature of the fluid within the mass control tank, and thereby determine whether working fluid is either extracted from or injected into the working fluid circuit. Regulating the pressure and amount of working fluid in the working fluid circuit selectively increases or decreases the suction pressure of the pump to increase system efficiency.
摘要翻译： 本公开的方面通常提供热力发动机系统和用于在热力循环期间调节工作流体回路中的工作流体的压力和量的方法。 可以采用质量管理系统来调节在整个工作流体回路中循环的工作流体。 质量管理系统可以具有在一个或多个战略位置的联结点处流体地联接到工作流体回路的质量控制罐。 热交换器盘管可以与质量控制箱一起使用，以调节质量控制箱内的流体的温度，从而确定工作流体是从工作流体回路中提取还是从工作流体回路中注入。 调节工作流体回路中的工作流体的压力和量选择性地增加或减小了泵的吸入压力，以提高系统效率。
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2.发明授权Gas turbine engine combustor circumferential acoustic reduction using flame temperature nonuniformities 有权燃气轮机发动机燃烧器采用周边声学还原使用火焰温度不均匀性公开(公告)号：US08631656B2
公开(公告)日：2014-01-21
申请号：US12059256
申请日：2008-03-31
CPC分类号： F23R3/50 , F23R2900/00013 , F23R2900/00014
摘要： A gas turbine engine combustor includes an annulus with one or more circular rows of burners and a means for providing a number of equiangular spaced apart flame temperature nonuniformities around the annulus during engine operation. The number of the flame temperature nonuniformities being equal to a circumferential acoustic mode to be attenuated in the combustor (i.e three, five, or seven). Fuel lines and/or water lines in supply communication with the burners and metering orifices in a portion of the fuel lines and/or the water lines may be used to produce the flame temperature nonuniformities. The annulus of the burners may have an equal number of equiangular spaced apart first and second arcuate segments of the burners and a means for operating the burners in the first segments and operating the burners in the second segments at different first and second flame temperatures respectively.
摘要翻译： 燃气涡轮发动机燃烧器包括具有一个或多个圆形排燃烧器的环形空间，以及用于在发动机运行期间在环空周围提供多个等角间隔开的火焰温度不均匀性的装置。 火焰温度不均匀性的数量等于在燃烧器中被衰减的周向声学模式（即三个，五个或七个）。 可以使用与燃料管线和/或水管线的一部分中的燃烧器和计量孔供应连通的燃料管线和/或水管线来产生火焰温度不均匀性。 燃烧器的环带可以具有相等数量的燃烧器的等角度间隔开的第一和第二弧形段，以及用于在第一段中操作燃烧器并分别在不同的第一和第二火焰温度下操作第二段中的燃烧器的装置。
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公开(公告)号：US20130036736A1
公开(公告)日：2013-02-14
申请号：US13590853
申请日：2012-08-21
申请人： Katherine Hart , Timothy James Held
发明人： Katherine Hart , Timothy James Held
IPC分类号： F01K13/02
CPC分类号： F01K13/02 , F01K3/185 , F01K11/00 , F01K25/103 , G05D7/0617
摘要： Embodiments of the invention generally provide a heat engine system, a mass management system (MMS), and a method for regulating pressure in the heat engine system while generating electricity. In one embodiment, the MMS contains a tank fluidly coupled to a pump, a turbine, a heat exchanger, an offload terminal, and a working fluid contained in the tank at a storage pressure. The working fluid may be at a system pressure proximal an outlet of the heat exchanger, at a low-side pressure proximal a pump inlet, and at a high-side pressure proximal a pump outlet. The MMS contains a controller communicably coupled to a valve between the tank and the heat exchanger outlet, a valve between the tank and the pump inlet, a valve between the tank and the pump outlet, and a valve between the tank and the offload terminal.
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公开(公告)号：US08281597B2
公开(公告)日：2012-10-09
申请号：US12347165
申请日：2008-12-31
IPC分类号： F02C1/00
CPC分类号： F23R3/286 , F23R3/14 , F23R3/20 , F23R3/343 , F23R2900/03044 , Y02T50/675
摘要： A combustor swirl cup includes coaxial inner and outer swirlers separated by a tubular centerbody. The centerbody includes a bypass inlet surrounding the inner swirler and diverges aft along a perforate inner nozzle to terminate at an annular flameholder. An impingement ring is spaced forward from the flameholder in flow communication with the bypass inlet for receiving cooling air therefrom to impingement cool the flameholder.
摘要翻译： 燃烧器旋流杯包括由管状中心体分开的同心的内旋流器和外旋流器。 中心体包括围绕内旋流器的旁路入口，并沿着穿孔内喷嘴向后分叉，以终止于环形火焰稳定器。 冲击环与火焰稳压器间隔开，与旁路入口流动连通，以从其中接收冷却空气，以冲击冷却火焰稳定器。
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公开(公告)号：US20120131921A1
公开(公告)日：2012-05-31
申请号：US13291086
申请日：2011-11-07
申请人： Timothy James Held
发明人： Timothy James Held
CPC分类号： F01K25/08
摘要： A system for converting thermal energy to work. The system includes a working fluid circuit, and a precooler configured to receive the working fluid. The system also includes a compression stages and intercoolers. At least one of the precooler and the intercoolers is configured to receive a heat transfer medium from a high temperature ambient environment. The system also includes heat exchangers coupled to a source of heat and being configured to receive the working fluid. The system also includes turbines coupled to one or more of the heat exchangers and configured to receive heated working fluid therefrom. The system further includes recuperators fluidly coupled to the turbines, the precooler, the compressor, and at least one of the heat exchangers. The recuperators transfer heat from the working fluid downstream from the turbines, to the working fluid upstream from at least one of the heat exchangers.
摘要翻译： 将热能转换为工作的系统。 该系统包括工作流体回路和构造成接收工作流体的预冷器。 该系统还包括压缩级和中间冷却器。 预冷却器和中间冷却器中的至少一个被配置为从高温环境环境接收传热介质。 该系统还包括耦合到热源的热交换器并且被配置为接收工作流体。 该系统还包括联接到一个或多个热交换器并被配置为从其接收加热的工作流体的涡轮机。 该系统还包括流体耦合到涡轮机，预冷器，压缩机和至少一个热交换器的换热器。 换热器将热量从涡轮下游的工作流体传递到来自至少一个热交换器的上游的工作流体。
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6.发明申请GAS TURBINE ENGINE COMBUSTOR CIRCUMFERENTIAL ACOUSTIC REDUCTION USING FLAME TEMPERATURE NONUNIFORMITIES 有权气体涡轮发动机燃烧器使用火焰温度非均匀性进行循环减震公开(公告)号：US20090241548A1
公开(公告)日：2009-10-01
申请号：US12059256
申请日：2008-03-31
IPC分类号： F02C1/00
CPC分类号： F23R3/50 , F23R2900/00013 , F23R2900/00014
摘要： A gas turbine engine combustor includes an annulus with one or more circular rows of burners and a means for providing a number of equiangular spaced apart flame temperature nonuniformities around the annulus during engine operation. The number of the flame temperature nonuniformities being equal to a circumferential acoustic mode to be attenuated in the combustor (i.e three, five, or seven). Fuel lines and/or water lines in supply communication with the burners and metering orifices in a portion of the fuel lines and/or the water lines may be used to produce the flame temperature nonuniformities. The annulus of the burners may have an equal number of equiangular spaced apart first and second arcuate segments of the burners and a means for operating the burners in the first segments and operating the burners in the second segments at different first and second flame temperatures respectively.
摘要翻译： 燃气涡轮发动机燃烧器包括具有一个或多个圆形排燃烧器的环形空间，以及用于在发动机运行期间在环空周围提供多个等角间隔开的火焰温度不均匀性的装置。 火焰温度不均匀性的数量等于在燃烧器中被衰减的周向声学模式（即三个，五个或七个）。 可以使用与燃料管线和/或水管线的一部分中的燃烧器和计量孔供应连通的燃料管线和/或水管线来产生火焰温度不均匀性。 燃烧器的环带可以具有相等数量的燃烧器的等角度间隔开的第一和第二弧形段，以及用于在第一段中操作燃烧器并分别在不同的第一和第二火焰温度下操作第二段中的燃烧器的装置。
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公开(公告)号：US20080078181A1
公开(公告)日：2008-04-03
申请号：US11537100
申请日：2006-09-29
IPC分类号： F02C7/26
CPC分类号： F23R3/286 , F23R3/343 , F23R2900/00014 , F23R2900/03343
摘要： A method for operating a combustion system is provided. The method includes coupling the main swirler to the pilot swirler such that the main swirler substantially circumscribes the pilot swirler, supplying fuel to a first fuel circuit defined in the main swirler, and inducing swirling to the supplied fuel via a first set of swirler vanes positioned within the main swirler. The method also includes supplying fuel to a second fuel circuit defined in the main swirler, inducing swirling to the supplied fuel via a second set of swirler vanes positioned within the main swirler, each of the second set of swirler vanes comprising at least one second fuel passage defined therein, and coupling a shroud in flow communication to at least one of the first set of swirler vanes and the second set of swirler vanes, the shroud comprising at least one third fuel passage defined therein.
摘要翻译： 提供了一种操作燃烧系统的方法。 该方法包括将主旋流器连接到先导旋流器，使得主旋流器基本上限制先导旋流器，将燃料供应到在主旋流器中限定的第一燃料回路，并通过定位在第一组旋流器叶片上的所述供应燃料旋转 在主旋流器内。 该方法还包括将燃料供应到在主旋流器中限定的第二燃料回路，通过位于主旋流器内的第二组旋流器叶片引起向供应的燃料的旋转，第二组旋流器叶片中的每一个包括至少一个第二燃料 通道，并且将与流动连通的护罩耦合到第一组旋流器叶片和第二组旋流器叶片中的至少一个，所述护罩包括限定在其中的至少一个第三燃料通道。
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公开(公告)号：US07340900B2
公开(公告)日：2008-03-11
申请号：US11012638
申请日：2004-12-15
申请人： Jun Xu , Timothy James Held
发明人： Jun Xu , Timothy James Held
CPC分类号： F23R3/286 , F23R3/14 , F23R3/343 , F23R2900/00014
摘要： A method for decreasing combustor acoustics in gas turbine engines is provided. The method includes fabricating a plurality of premixers, chamfering a trailing edge of a main swirler shroud of each premixer, coupling a respective one of the chamfered premixers to each of a plurality of combustor domes, and coupling the plurality of combustor domes to an inlet of a combustor in a circumferential arrangement such that, during operation, the chamfered edge facilitates reducing combustor acoustics.
摘要翻译： 提供了一种用于降低燃气涡轮发动机中的燃烧器声学的方法。 该方法包括制造多个预混合器，对每个预混合器的主旋流器护罩的后缘进行倒角，将倒角预混合器中的相应一个连接到多个燃烧器圆顶中的每一个，以及将多个燃烧器穹顶连接到 周向布置的燃烧器，使得在操作期间，倒角边缘有助于降低燃烧器声学。
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公开(公告)号：US07059135B2
公开(公告)日：2006-06-13
申请号：US11312273
申请日：2005-12-20
申请人： Timothy James Held , Mark Anthony Mueller , Jun Xu
发明人： Timothy James Held , Mark Anthony Mueller , Jun Xu
IPC分类号： F23R3/14
摘要： A method for operating a gas turbine engine facilitates reducing an amount of emissions from a combustor. The combustor includes a mixer assembly including a pilot mixer, a main mixer, and an annular centerbody extending therebetween. The method comprises injecting at least one of fuel and airflow into the combustor through at least one swirler positioned within the pilot mixer, and injecting fuel into the combustor through at least one swirler positioned within the main mixer, such that the fuel is directed into a combustion chamber downstream from the main mixer.
摘要翻译： 用于操作燃气涡轮发动机的方法有助于减少来自燃烧器的排放量。 燃烧器包括一个混合器组件，该混合器组件包括一个先导式混合器，一个主混合器和一个在其间延伸的环形中心体。 该方法包括通过位于先导混合器内的至少一个旋流器将燃料和气流中的至少一种喷射到燃烧器中，并且通过位于主混合器内的至少一个旋流器将燃料喷射到燃烧器中，使得燃料被引导到 燃烧室主搅拌机下游。
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公开(公告)号：US20140345279A1
公开(公告)日：2014-11-27
申请号：US14450410
申请日：2014-08-04
CPC分类号： F01K25/103 , F01K3/185 , F01K3/186 , F01K7/165 , F24H2240/12 , Y02T10/16
摘要： A method for converting thermal energy into mechanical energy in a thermodynamic cycle includes placing a thermal energy source in thermal communication with a heat exchanger arranged in a working fluid circuit containing a working fluid (e.g., sc-CO2) and having a high pressure side and a low pressure side. The method also includes regulating an amount of working fluid within the working fluid circuit via a mass management system having a working fluid vessel, pumping the working fluid through the working fluid circuit, and expanding the working fluid to generate mechanical energy. The method further includes directing the working fluid away from the expander through the working fluid circuit, controlling a flow of the working fluid in a supercritical state from the high pressure side to the working fluid vessel, and controlling a flow of the working fluid from the working fluid vessel to the low pressure side.
摘要翻译： 一种在热循环中将热能转换为机械能的方法包括将热能源与布置在包含工作流体（例如，sc-CO 2）并且具有高压侧的工作流体回路中的热交换器热连通， 低压侧。 该方法还包括通过具有工作流体容器的质量管理系统来调节工作流体回路内的工作流体的量，将工作流体泵送通过工作流体回路，以及膨胀工作流体以产生机械能。 该方法还包括将工作流体从膨胀机引导通过工作流体回路，控制工作流体在超临界状态从高压侧流向工作流体容器的流动，以及控制工作流体从 工作流体容器到低压侧。
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