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41.发明申请Active Control of Flame Holding and Flashback in Turbine Combustor Fuel Nozzle 审中-公开涡轮燃烧器燃油喷嘴中火焰保持和闪回的主动控制公开(公告)号：US20110005189A1
公开(公告)日：2011-01-13
申请号：US12499772
申请日：2009-07-08
CPC分类号： F23R3/14 , F23C2900/07001 , F23D14/82 , F23D2209/10 , F23N5/242 , F23N2029/00 , F23N2031/28 , F23R3/286 , F23R3/34
摘要： A system includes a turbine combustor fuel nozzle. The turbine combustor fuel nozzle includes a swirl vane. The turbine combustor fuel nozzle also includes an injection hole configured to inject fluid in a downstream region of the swirl vane. The injection of fluid in a downstream region of the swirl vane may be in response to detection of a condition indicative of a flame inside the turbine combustor fuel nozzle.
摘要翻译： 一种系统包括涡轮机燃烧器燃料喷嘴。 涡轮机燃烧器燃料喷嘴包括旋流叶片。 涡轮机燃烧器燃料喷嘴还包括配置成在涡旋叶片的下游区域中喷射流体的喷射孔。 在涡流叶片的下游区域中注入流体可以响应于检测到表示涡轮机燃烧器燃料喷嘴内的火焰的状态。
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公开(公告)号：US20100252652A1
公开(公告)日：2010-10-07
申请号：US12417896
申请日：2009-04-03
CPC分类号： F23D14/62 , F23R3/10 , F23R3/286 , F23R2900/00002
摘要： A fuel injection nozzle comprises a body member having an upstream wall opposing a downstream wall, a baffle member having an upstream surface and a downstream surface, a first chamber, a second chamber, a fuel inlet communicative with the first chamber operative to emit a first gas into the first chamber, and a plurality of mixing tubes, each of the mixing tubes having a tube inner surface, a tube outer surface, a first inlet communicative with an aperture in the upstream wall operative to receive a second gas, a second inlet communicative with the tube outer surface and the tube inner surface operative to translate the first gas into the mixing tube, a mixing portion operative to mix the first gas and the second gas, and an outlet communicative with an aperture in the downstream wall operative to emit the mixed first and second gasses.
摘要翻译： 燃料喷射喷嘴包括主体构件，其具有与下游壁相对的上游壁，具有上游表面和下游表面的挡板构件，第一腔室，第二腔室，与第一腔室连通的燃料入口，其操作以发射第一 气体进入第一室，以及多个混合管，每个混合管具有管内表面，管外表面，与上游壁中的孔连通的第一入口，用于接收第二气体，第二入口 与管外表面和管内表面通信，其可操作以将第一气体平移到混合管中，混合部分可操作以混合第一气体和第二气体，以及与下游壁中的孔连通的出口，其可操作地发射 混合的第一和第二气体。
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公开(公告)号：US07565805B2
公开(公告)日：2009-07-28
申请号：US11284491
申请日：2005-11-22
申请人： Charles Evan Steber , Massoud Parisay , Ravindra Annigeri , Willy Steve Ziminsky , John Stephen Henderson
发明人： Charles Evan Steber , Massoud Parisay , Ravindra Annigeri , Willy Steve Ziminsky , John Stephen Henderson
CPC分类号： F23N5/003 , F23N2021/10 , F23N2041/20 , F23R3/00 , Y02T50/677
摘要： Methods and systems for operating a gas turbine engine system include an electrical generator configured to provide electrical energy to a load, a gas turbine engine including at least one combustor that includes a plurality of fuel injection points configured to inject a fuel into the combustor at a plurality of different locations wherein the combustor configured to combust the fuel and the gas turbine engine is rotatably coupled to the generator through a shaft. The gas turbine engine system includes a control system including a plurality of sensors positioned about the gas turbine engine system and configured to measure at least one parameter associated with the sensor, a processor programmed to receive a signal indicative of a heating value of the fuel, and automatically control a fuel split between the fuel injection points on the combustor using the determined heating value.
摘要翻译： 用于操作燃气涡轮发动机系统的方法和系统包括被配置为向负载提供电能的发电机，包括至少一个燃烧器的燃气涡轮发动机，该至少一个燃烧器包括多个燃料喷射点，燃料喷射点被配置成在 多个不同的位置，其中构造成燃烧燃料和燃气涡轮发动机的燃烧器通过轴可旋转地联接到发电机。 所述燃气涡轮发动机系统包括控制系统，所述控制系统包括围绕所述燃气涡轮发动机系统定位的多个传感器，所述多个传感器被配置为测量与所述传感器相关联的至少一个参数，被编程为接收指示所述燃料的热值的信号的处理器 并使用所确定的热值自动控制燃烧器上的燃料喷射点之间的燃料分配。
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公开(公告)号：US20090007566A1
公开(公告)日：2009-01-08
申请号：US12212812
申请日：2008-09-18
IPC分类号： F02C7/00
CPC分类号： F02C7/228 , F02C7/222 , F02C9/263 , F02C9/28 , F02C9/32 , F05D2250/312 , F05D2270/082 , F05D2270/31
摘要： A method for controlling NOx emissions from a gas turbine having a fuel adjustment system may include setting an outer nozzle fuel flow to achieve a desired level of combustion dynamics for at least one of a plurality of combustion chambers, determining a delta adjustment value for a center nozzle fuel flow that will result in a desired level of NOx emissions from the gas turbine, and adjusting the center nozzle fuel flow according to the determined delta adjustment value to obtain the desired level of NOx emissions from the gas turbine.
摘要翻译： 用于控制具有燃料调节系统的燃气轮机的NOx排放的方法可包括设定外部喷嘴燃料流量以实现多个燃烧室中的至少一个燃烧室的期望水平的燃烧动态，确定中心的增量调节值 喷嘴燃料流量将导致来自燃气轮机的期望水平的NOx排放，并且根据确定的增量调节值调节中心喷嘴燃料流量，以获得来自燃气轮机的期望的NOx排放水平。
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公开(公告)号：US08800289B2
公开(公告)日：2014-08-12
申请号：US12877385
申请日：2010-09-08
CPC分类号： F23R3/286 , F01D9/023 , F23R3/005 , F23R3/54 , F23R2900/00002
摘要： A nozzle includes a fuel plenum and an air plenum downstream of the fuel plenum. A primary fuel channel includes an inlet in fluid communication with the fuel plenum and a primary air port in fluid communication with the air plenum. Secondary fuel channels radially outward of the primary fuel channel include a secondary fuel port in fluid communication with the fuel plenum. A shroud circumferentially surrounds the secondary fuel channels. A method for mixing fuel and air in a nozzle prior to combustion includes flowing fuel to a fuel plenum and flowing air to an air plenum downstream of the fuel plenum. The method further includes injecting fuel from the fuel plenum through a primary fuel passage, injecting fuel from the fuel plenum through secondary fuel passages, and injecting air from the air plenum through the primary fuel passage.
摘要翻译： 喷嘴包括燃料增压室和在燃料增压室下游的空气增压室。 主要燃料通道包括与燃料增压室流体连通的入口和与空气压力室流体连通的主空气端口。 主要燃料通道径向向外的次级燃料通道包括与燃料增压室流体连通的次级燃料口。 护罩周向地包围二次燃料通道。 在燃烧之前将燃料和空气混合在喷嘴中的方法包括将燃料流入燃料增压室并将空气流到燃料增压室下游的空气压力室。 该方法还包括从燃料通风室喷射燃料通过主燃料通道，从燃料通风室喷射燃料通过二次燃料通道，以及从空气通风室喷射空气通过主燃料通道。
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公开(公告)号：US08677760B2
公开(公告)日：2014-03-25
申请号：US12652858
申请日：2010-01-06
CPC分类号： F23R3/286 , F23R3/343 , F23R2900/03343
摘要： Disclosed is a method of operating a secondary fuel nozzle for a turbomachine combustor including delivering a flow of pilot fuel through a pilot fuel channel toward a combustion zone and delivering a flow of air through a plurality of transfer passages arranged around the pilot fuel channel toward the combustion zone. The flow of pilot fuel and the flow of air are combusted in the combustion zone, and a flow of transfer fuel is delivered through the plurality of transfer passages for combustion. A secondary fuel nozzle includes a pilot fuel channel extending along the fuel nozzle to deliver a flow of pilot fuel to a combustion zone. A plurality of transfer passages are arranged around the pilot fuel channel and are configured to deliver a flow of air for combustion with the flow of pilot fuel and to deliver a flow of transfer fuel to the combustion zone.
摘要翻译： 公开了一种操作用于涡轮机燃烧器的二次燃料喷嘴的方法，包括将先导燃料流通过引导燃料通道朝向燃烧区输送，并且将空气流通过布置在引燃燃料通道周围的多个输送通道朝向 燃烧区。 先导燃料的流动和空气的流动在燃烧区燃烧，并且传输燃料的流动通过多个传送通道被输送用于燃烧。 辅助燃料喷嘴包括沿着燃料喷嘴延伸的导向燃料通道，以将引导燃料流输送到燃烧区。 多个传送通道布置在引燃燃料通道周围，并被构造成输送用于与引燃燃料流一起燃烧的空气流并将传输燃料流传送到燃烧区。
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公开(公告)号：US08539773B2
公开(公告)日：2013-09-24
申请号：US12365382
申请日：2009-02-04
申请人： Willy Steve Ziminsky , Thomas Edward Johnson , Benjamin Paul Lacy , William David York , Jong Ho Uhm , Baifang Zuo
发明人： Willy Steve Ziminsky , Thomas Edward Johnson , Benjamin Paul Lacy , William David York , Jong Ho Uhm , Baifang Zuo
CPC分类号： F23R3/286 , F23D2900/00008 , F23D2900/00012 , F23R3/10 , F23R3/34
摘要： A fuel/air mixing tube for use in a fuel/air mixing tube bundle is provided. The fuel/air mixing tube includes an outer tube wall extending axially along a tube axis between an inlet end and an exit end, the outer tube wall having a thickness extending between an inner tube surface having a inner diameter and an outer tube surface having an outer tube diameter. The tube further includes at least one fuel injection hole having a fuel injection hole diameter extending through the outer tube wall, the fuel injection hole having an injection angle relative to the tube axis. The invention provides good fuel air mixing with low combustion generated NOx and low flow pressure loss translating to a high gas turbine efficiency, that is durable, and resistant to flame holding and flash back.
摘要翻译： 提供了一种用于燃料/空气混合管束的燃料/空气混合管。 燃料/空气混合管包括沿入口端和出口端之间的管轴线轴向延伸的外管壁，外管壁具有在具有内径的内管表面和外管表面之间延伸的厚度， 外管直径。 该管还包括至少一个具有延伸穿过外管壁的燃料喷射孔直径的燃料喷射孔，燃料喷射孔相对于管轴具有喷射角。 本发明提供了具有低燃烧产生的NOx和低流量压力损失的良好的燃料空气混合，转化为高燃气轮机效率，耐久性，并且耐火焰保持和回闪。
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公开(公告)号：US08464537B2
公开(公告)日：2013-06-18
申请号：US12909092
申请日：2010-10-21
IPC分类号： F02C1/00
CPC分类号： F23R3/286 , F23R3/343 , F23R2900/03343
摘要： A nozzle for a combustor is disclosed. The nozzle includes a center body, a burner tube provided around the center body and defining a fuel-air mixing passage therebetween, and an outer peripheral wall provided around the burner tube and defining an air flow passage therebetween. The nozzle further includes a nozzle tip connected to the center body. The nozzle tip includes a pilot fuel passage configured to deliver a flow of pilot fuel to a combustion zone, and a plurality of transfer passages. The plurality of transfer passages are configured to deliver a flow of air for combustion with the flow of pilot fuel in the combustion zone and further configured to deliver a flow of transfer fuel to the combustion zone.
摘要翻译： 公开了一种用于燃烧器的喷嘴。 喷嘴包括中心体，燃烧器管设置在中心体周围并在其间限定燃料 - 空气混合通道，外周壁设置在燃烧器管周围并且在其间限定空气流动通道。 喷嘴还包括连接到中心体的喷嘴尖端。 喷嘴尖端包括引导燃料通道，其构造成将先导燃料流输送到燃烧区域，以及多个输送通道。 所述多个传送通道构造成输送用于燃烧的空气流与所述燃烧区域中的引燃燃料流，并且进一步构造成将传输燃料流输送到所述燃烧区。
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公开(公告)号：US20130061593A1
公开(公告)日：2013-03-14
申请号：US13229950
申请日：2011-09-12
CPC分类号： F23N5/082 , F23N2029/20 , F23R3/286
摘要： A system and method for controlling a combustor assembly are disclosed. The system includes a combustor assembly. The combustor assembly includes a combustor and a fuel nozzle assembly. The combustor includes a casing. The fuel nozzle assembly is positioned at least partially within the casing and includes a fuel nozzle. The fuel nozzle assembly further defines a head end. The system further includes a viewing device configured for capturing an image of at least a portion of the head end, and a processor communicatively coupled to the viewing device, the processor configured to compare the image to a standard image for the head end.
摘要翻译： 公开了一种用于控制燃烧器组件的系统和方法。 该系统包括燃烧器组件。 燃烧器组件包括燃烧器和燃料喷嘴组件。 燃烧器包括壳体。 燃料喷嘴组件至少部分地定位在壳体内并且包括燃料喷嘴。 燃料喷嘴组件还限定了头端。 该系统还包括被配置为捕获头端的至少一部分的图像的观察装置，以及通信地耦合到观看装置的处理器，所述处理器被配置为将图像与用于头端的标准图像进行比较。
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公开(公告)号：US08387399B1
公开(公告)日：2013-03-05
申请号：US13229950
申请日：2011-09-12
IPC分类号： F02C1/00
CPC分类号： F23N5/082 , F23N2029/20 , F23R3/286
摘要： A system and method for controlling a combustor assembly are disclosed. The system includes a combustor assembly. The combustor assembly includes a combustor and a fuel nozzle assembly. The combustor includes a casing. The fuel nozzle assembly is positioned at least partially within the casing and includes a fuel nozzle. The fuel nozzle assembly further defines a head end. The system further includes a viewing device configured for capturing an image of at least a portion of the head end, and a processor communicatively coupled to the viewing device, the processor configured to compare the image to a standard image for the head end.
摘要翻译： 公开了一种用于控制燃烧器组件的系统和方法。 该系统包括燃烧器组件。 燃烧器组件包括燃烧器和燃料喷嘴组件。 燃烧器包括壳体。 燃料喷嘴组件至少部分地定位在壳体内并且包括燃料喷嘴。 燃料喷嘴组件还限定了头端。 该系统还包括被配置为捕获头端的至少一部分的图像的观察装置，以及通信地耦合到观看装置的处理器，所述处理器被配置为将图像与用于头端的标准图像进行比较。
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