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公开(公告)号：US08276385B2
公开(公告)日：2012-10-02
申请号：US12575929
申请日：2009-10-08
IPC分类号： F02C1/00
CPC分类号： F23R3/286 , F23D14/64 , F23R3/36 , F23R2900/00002
摘要： A fuel injection nozzle includes a body member having an upstream wall opposing a downstream wall, and an internal wall disposed between the upstream wall and the downstream wall, a first chamber partially defined by the an inner surface of the upstream wall and a surface of the internal wall, a second chamber partially defined by an inner surface of the downstream wall and a surface of the internal wall a first gas inlet communicative with the first chamber operative to emit a first gas into the first chamber, a second gas inlet communicative with the second chamber operative to emit a second gas into the second 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 third gas.
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和设置在上游壁和下游壁之间的内壁，第一室部分地由上游壁的内表面和 内壁，由所述下游壁的内表面部分地限定的第二室和所述内壁的表面，与所述第一室连通的第一气体入口，其操作以将第一气体发射到所述第一室中;第二气体入口， 第二室，用于将第二气体发射到第二室中，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，其可操作以接收 第三气。
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公开(公告)号：US20120175430A1
公开(公告)日：2012-07-12
申请号：US12985572
申请日：2011-01-06
CPC分类号： F23R3/14 , F23C2900/07001 , F23D2900/14004 , F23D2900/14021 , F23R3/286
摘要： A nozzle includes a center body that defines an axial centerline and a shroud circumferentially surrounding at least a portion of the center body to define an annular passage between the center body and the shroud. A plurality of vanes between the center body and the shroud comprise a radially outward portion separated from the shroud. A method for enhancing flow through a nozzle includes flowing a fuel through a center body and flowing a fluid stream across a vane located between the center body and a shroud surrounding at least a portion of the center body. The method further includes flowing the fluid stream between a radially outward portion of the vane and the shroud, wherein the radially outward portion of the vane is separated from the shroud.
摘要翻译： 喷嘴包括限定轴向中心线的中心体和周向围绕中心体的至少一部分的护罩，以在中心体和护罩之间限定环形通道。 中心体和护罩之间的多个叶片包括与护罩分离的径向向外部分。 用于增强通过喷嘴的流动的方法包括使燃料流过中心体并使流体流穿过位于中心体和围绕中心体的至少一部分的护罩之间的叶片。 该方法还包括使流体流在叶片的径向向外部分和护罩之间流动，其中叶片的径向向外部分与护罩分离。
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公开(公告)号：US20120096866A1
公开(公告)日：2012-04-26
申请号：US12909092
申请日：2010-10-21
IPC分类号： F02C7/22
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：US20120055167A1
公开(公告)日：2012-03-08
申请号：US12877385
申请日：2010-09-08
IPC分类号： F02C7/22
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：US08007274B2
公开(公告)日：2011-08-30
申请号：US12249158
申请日：2008-10-10
申请人： Thomas Edward Johnson , Willy Steve Ziminsky , Benjamin Paul Lacey , William David York , Christian Xavier Stevenson
发明人： Thomas Edward Johnson , Willy Steve Ziminsky , Benjamin Paul Lacey , William David York , Christian Xavier Stevenson
IPC分类号： F23N1/10
CPC分类号： F23D14/82
摘要： A fuel nozzle assembly is provided. The assembly includes an outer nozzle body having a first end and a second end and at least one inner nozzle tube having a first end and a second end. One of the nozzle body or nozzle tube includes a fuel plenum and a fuel passage extending therefrom, while the other of the nozzle body or nozzle tube includes a fuel injection hole slidably aligned with the fuel passage to form a fuel flow path therebetween at an interface between the body and the tube. The nozzle body and the nozzle tube are fixed against relative movement at the first ends of the nozzle body and nozzle tube, enabling the fuel flow path to close at the interface due to thermal growth after a flame enters the nozzle tube.
摘要翻译： 提供燃料喷嘴组件。 组件包括具有第一端和第二端的外部喷嘴本体和具有第一端和第二端的至少一个内部喷嘴管。 喷嘴体或喷嘴管中的一个包括燃料增压室和从其延伸的燃料通道，而喷嘴体或喷嘴管中的另一个包括与燃料通道可滑动地对准的燃料喷射孔，以在界面处形成燃料流动路径 在身体和管之间。 喷嘴体和喷嘴管相对于喷嘴体和喷嘴管的第一端处的相对运动被固定，使得燃料流路在火焰进入喷嘴管之后由于热生长而在界面处闭合。
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76.发明授权Systems and methods of monitoring acoustic pressure to detect a flame condition in a gas turbine 有权监测声压的系统和方法，以检测燃气轮机中的火焰状况公开(公告)号：US07942038B2
公开(公告)日：2011-05-17
申请号：US12356828
申请日：2009-01-21
IPC分类号： G01M15/14
CPC分类号： F23N5/16 , F23N5/242 , F23N2025/04 , F23N2031/28 , F23N2041/20 , F23R3/286 , F23R2900/00002 , F23R2900/00013 , F23R2900/00016
摘要： A method may detect a flashback condition in a fuel nozzle of a combustor. The method may include obtaining a current acoustic pressure signal from the combustor, analyzing the current acoustic pressure signal to determine current operating frequency information for the combustor, and indicating that the flashback condition exists based at least in part on the current operating frequency information.
摘要翻译： 一种方法可以检测燃烧器的燃料喷嘴中的回火状态。 该方法可以包括从燃烧器获得当前声压信号，分析当前声压信号以确定燃烧器的当前工作频率信息，并且至少部分地基于当前工作频率信息来指示闪回状态存在。
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公开(公告)号：US20100218501A1
公开(公告)日：2010-09-02
申请号：US12394544
申请日：2009-02-27
申请人： William David York , Willy Steve Ziminsky , Thomas Edward Johnson , Benjamin Lacy , Baifang Zuo , Jong Ho Uhm
发明人： William David York , Willy Steve Ziminsky , Thomas Edward Johnson , Benjamin Lacy , Baifang Zuo , Jong Ho Uhm
IPC分类号： F02C7/22
CPC分类号： F23R3/286 , F23D14/02 , F23D14/82 , F23D2209/10 , F23R2900/03282
摘要： A fuel/air mixing disk for use in a fuel/air mixing combustor assembly is provided. The disk includes a first face, a second face, and at least one fuel plenum disposed therebetween. A plurality of fuel/air mixing tubes extend through the pre-mixing disk, each mixing tube including an outer tube wall extending axially along a tube axis and in fluid communication with the at least one fuel plenum. At least a portion of the plurality of fuel/air mixing tubes further includes at least one fuel injection hole have a fuel injection hole diameter extending through said 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/空气混合燃烧器组件的燃料/空气混合盘。 盘包括第一面，第二面和设置在它们之间的至少一个燃料增压室。 多个燃料/空气混合管延伸穿过预混合盘，每个混合管包括沿管轴线轴向延伸并与至少一个燃料增压室流体连通的外管壁。 多个燃料/空气混合管的至少一部分还包括至少一个燃料喷射孔，其具有延伸穿过所述外管壁的燃料喷射孔直径，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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78.发明申请Systems and Methods of Monitoring Acoustic Pressure to Detect a Flame Condition in a Gas Turbine 有权监测声压的系统和方法来检测燃气轮机中的火焰状况公开(公告)号：US20100180674A1
公开(公告)日：2010-07-22
申请号：US12356828
申请日：2009-01-21
IPC分类号： G01M15/14
CPC分类号： F23N5/16 , F23N5/242 , F23N2025/04 , F23N2031/28 , F23N2041/20 , F23R3/286 , F23R2900/00002 , F23R2900/00013 , F23R2900/00016
摘要： A method may detect a flashback condition in a fuel nozzle of a combustor. The method may include obtaining a current acoustic pressure signal from the combustor, analyzing the current acoustic pressure signal to determine current operating frequency information for the combustor, and indicating that the flashback condition exists based at least in part on the current operating frequency information.
摘要翻译： 一种方法可以检测燃烧器的燃料喷嘴中的回火状态。 该方法可以包括从燃烧器获得当前声压信号，分析当前声压信号以确定燃烧器的当前工作频率信息，并且至少部分地基于当前工作频率信息来指示闪回状态存在。
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79.发明申请公开(公告)号：US20100101229A1
公开(公告)日：2010-04-29
申请号：US12256901
申请日：2008-10-23
CPC分类号： F23R3/286 , F23D14/62 , F23D2214/00 , F23R3/283
摘要： A fuel nozzle with active cooling is provided. It includes an outer peripheral wall, a nozzle center body concentrically disposed within the outer wall in a fuel and air pre-mixture. The fuel and air pre-mixture includes an air inlet, a fuel inlet and a premixing passage defined between the outer wall in the center body. A gas fuel flow passage is provided. A first cooling passage is included within the center body in a second cooling passage is defined between the center body and the outer wall.
摘要翻译： 提供具有主动冷却的燃料喷嘴。 它包括外周壁，在燃料和空气预混合物中同心地设置在外壁内的喷嘴中心体。 燃料和空气预混合物包括空气入口，燃料入口和限定在中心体的外壁之间的预混合通道。 提供了一种气体燃料流动通道。 第一冷却通道包括在中心体内，第二冷却通道限定在中心体和外壁之间。
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公开(公告)号：US20100008179A1
公开(公告)日：2010-01-14
申请号：US12169865
申请日：2008-07-09
申请人： Benjamin Paul Lacy , Balachandar Varatharajan , Willy Steve Ziminsky , Gilbert Otto Kraemer , Ertan Yilmaz , Patrick Benedict Melton , Baifang Zuo , Christian Xavier Stevenson , David Kenton Felling , Jong Ho Uhm
发明人： Benjamin Paul Lacy , Balachandar Varatharajan , Willy Steve Ziminsky , Gilbert Otto Kraemer , Ertan Yilmaz , Patrick Benedict Melton , Baifang Zuo , Christian Xavier Stevenson , David Kenton Felling , Jong Ho Uhm
IPC分类号： B01F15/02
摘要： A pre-mixing apparatus for a turbine engine includes a main body having an inlet portion, an outlet portion and an exterior wall that collectively establish at least one fluid delivery plenum, and a plurality of fluid delivery tubes extending through at least a portion of the at least one fluid delivery plenum. Each of the plurality of fluid delivery tubes includes at least one fluid delivery opening fluidly connected to the at least one fluid delivery plenum. With this arrangement, a first fluid is selectively delivered to the at least one fluid delivery plenum, passed through the at least one fluid delivery opening and mixed with a second fluid flowing through the plurality of fluid delivery tubes prior to being combusted in a combustion chamber of a turbine engine.
摘要翻译： 用于涡轮发动机的预混合装置包括主体，其具有共同建立至少一个流体输送气室的入口部分，出口部分和外壁，以及延伸穿过至少一部分流体输送管道的多个流体输送管 至少一个流体输送室。 多个流体输送管中的每一个包括流体连接到至少一个流体输送室的至少一个流体输送开口。 通过这种布置，第一流体被选择性地输送到至少一个流体输送气室，通过至少一个流体输送口，并且在燃烧在燃烧室中之前与流过多个流体输送管的第二流体混合 的涡轮发动机。
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