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    • 2. 发明申请
    • Integrated fuel cell hybrid power plant with controlled oxidant flow for combustion of spent fuel
    • 具有受控氧化剂流量的燃料电池混合动力发电厂用于乏燃料燃烧
    • US20050079395A1
    • 2005-04-14
    • US10681704
    • 2003-10-09
    • Balachandar VaratharajanChellappa BalanDebashis Dey
    • Balachandar VaratharajanChellappa BalanDebashis Dey
    • H01M8/04H01M8/06H01M8/12
    • H01M8/04111H01M8/04022H01M8/04708H01M8/04738H01M8/04776H01M8/0612H01M2008/1293H01M2250/407Y02E20/16Y02E60/563Y02P90/40
    • A hybrid power generation system for generating electrical power comprises a compressor for producing a compressed oxidant and a recuperator in flow communication with the compressor. The hybrid power generation system further comprises a fuel cell assembly comprising a plurality of fuel cells in flow communication with the recuperator to provide the compressed oxidant for the fuel cell assembly. The fuel cell assembly further comprises a cathode inlet for receiving the compressed oxidant, an anode inlet for receiving a fuel stream, an anode outlet in flow communication with an anode exhaust stream and a cathode outlet in flow communication with a cathode exhaust stream, wherein at least a portion of the fuel reacts with the oxidant to produce electrical power. The hybrid power generation system further comprises a tail gas burner in flow communication with the anode outlet and the cathode outlet. The tail gas burner is configured for combusting a mixture of at least a portion of the anode exhaust stream and at least a portion of the cathode exhaust stream and producing a hot compressed gas. A control system is used for controlling the amount of the cathode exhaust stream introduced in the tail gas burner for stable combustion and reduction of fuel and carbon monoxide emission. The hot compressed gas from the tail gas burner is introduced to a turbine, where the hot compressed gas is expanded, thereby producing electrical power and an expanded gas.
    • 用于产生电力的混合动力发电系统包括用于生产压缩氧化剂的压缩机和与压缩机流动连通的换热器。 混合动力发电系统还包括燃料电池组件,该燃料电池组件包括多个燃料电池,其与该换热器流体连通以提供用于燃料电池组件的压缩氧化剂。 燃料电池组件还包括用于接收压缩氧化剂的阴极入口,用于接收燃料流的阳极入口,与阳极废气流流动连通的阳极出口和与阴极排气流流动连通的阴极出口,其中在 燃料的至少一部分与氧化剂反应产生电力。 混合发电系统还包括与阳极出口和阴极出口流动连通的尾气燃烧器。 尾气燃烧器被配置用于燃烧阳极废气流的至少一部分和阴极废气流的至少一部分的混合物并产生热压缩气体。 控制系统用于控制引入尾气燃烧器中的阴极排气流的量,用于稳定燃烧和减少燃料和一氧化碳排放。 来自尾气燃烧器的热压缩气体被引入涡轮机,其中热压缩气体膨胀,从而产生电力和膨胀气体。
    • 8. 发明申请
    • COANDA INJECTION SYSTEM FOR AXIALLY STAGED LOW EMISSION COMBUSTORS
    • 用于轴向低排放燃烧器的COANDA注射系统
    • US20100011771A1
    • 2010-01-21
    • US12175050
    • 2008-07-17
    • Andrei Tristan EvuletBalachandar VaratharajanGilbert Otto KraemerAhmed Mostafa ElkadyBenjamin Paul Lacy
    • Andrei Tristan EvuletBalachandar VaratharajanGilbert Otto KraemerAhmed Mostafa ElkadyBenjamin Paul Lacy
    • F02C7/22F02C7/00F02C7/228
    • F23R3/34F23R3/286
    • The low emission combustor includes a combustor housing defining a combustion chamber having a plurality of combustion zones. A liner sleeve is disposed in the combustion housing with a gap formed between the liner sleeve and the combustor housing. A secondary nozzle is disposed along a centerline of the combustion chamber and configured to inject a first fluid comprising air, at least one diluent, fuel, or combinations thereof to a downstream side of a first combustion zone among the plurality of combustion zones. A plurality of primary fuel nozzles is disposed proximate to an upstream side of the combustion chamber and located around the secondary nozzle and configured to inject a second fluid comprising air and fuel to an upstream side of the first combustion zone. The combustor also includes a plurality of tertiary coanda nozzles. Each tertiary coanda nozzle is coupled to a respective dilution hole. The tertiary coanda nozzles are configured to inject a third fluid comprising air, at least one other diluent, fuel, or combinations thereof to one or more remaining combustion zones among the plurality of combustion zones.
    • 低排放燃烧器包括限定具有多个燃烧区域的燃烧室的燃烧器壳体。 衬套套筒设置在燃烧壳体中,在衬套和燃烧器壳体之间形成间隙。 辅助喷嘴沿着燃烧室的中心线布置,并被配置为将多个燃烧区中的第一燃烧区域的第一流体喷射到第一燃烧区域的下游侧,该第一流体包括空气,至少一种稀释剂,燃料或其组合。 多个主要燃料喷嘴设置在燃烧室的上游侧附近并且位于二次喷嘴周围,并被配置为将包含空气和燃料的第二流体喷射到第一燃烧区域的上游侧。 燃烧器还包括多个三级共挤出喷嘴。 每个三级共挤出喷嘴连接到相应的稀释孔。 三级大空中喷嘴构造成将包括空气,至少一种其它稀释剂,燃料或其组合的第三流体喷射到多个燃烧区域中的一个或多个剩余燃烧区域。
    • 10. 发明授权
    • Lean direct injection diffusion tip and related method
    • 精益直接注射扩散尖及相关方法
    • US08240150B2
    • 2012-08-14
    • US12222423
    • 2008-08-08
    • Balachandar VaratharajanWilly S. ZiminskyJohn LipinskiGilbert O. KraemerErtan YilmazBenjamin Lacy
    • Balachandar VaratharajanWilly S. ZiminskyJohn LipinskiGilbert O. KraemerErtan YilmazBenjamin Lacy
    • F02C1/00F02G3/00
    • F23R3/14F23D2900/00008F23D2900/14004F23R3/286F23R3/343
    • A nozzle for a gas turbine combustor includes a first radially outer tube defining a first passage having an inlet and an outlet, the inlet adapted to supply air to a reaction zone of the combustor. A center body is located within the first radially outer tube, the center body including a second radially intermediate tube for supplying fuel to the reaction zone and a third radially inner tube for supplying air to the reaction zone. The second intermediate tube has a first outlet end closed by a first end wall that is formed with a plurality of substantially parallel, axially-oriented air outlet passages for the additional air in the third radially inner tube, each air outlet passage having a respective plurality of associated fuel outlet passages in the first end wall for the fuel in the second radially intermediate tube. The respective plurality of associated fuel outlet passages have non-parallel center axes that intersect a center axis of the respective air outlet passage to locally mix fuel and air exiting said center body.
    • 用于燃气轮机燃烧器的喷嘴包括限定具有入口和出口的第一通道的第一径向外管,该入口适于将空气供应到燃烧器的反应区。 中心体位于第一径向外管内,中心体包括用于向反应区供应燃料的第二径向中间管和用于向反应区供应空气的第三径向内管。 第二中间管具有由第一端壁封闭的第一出口端,第一端壁形成有用于第三径向内管中的附加空气的多个基本上平行的轴向定向的空气出口通道,每个空气出口通道具有相应的多个 在第二径向中间管中用于燃料的第一端壁中的相关燃料出口通道。 相应的多个相关联的燃料出口通道具有与相应空气出口通道的中心轴线相交的非平行的中心轴线,以局部混合离开所述中心体的燃料和空气。