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21.发明申请Systems and Methods for Mitigating a Flashback Condition in a Premixed Combustor 审中-公开用于缓解预混燃烧器中闪回状态的系统和方法公开(公告)号：US20100180564A1
公开(公告)日：2010-07-22
申请号：US12356799
申请日：2009-01-21
IPC分类号： F02C9/28
CPC分类号： F23N5/022 , F02C9/28 , F02C9/32 , F05D2270/09 , F05D2270/303 , F23N5/082 , F23N5/16 , F23N5/242 , F23N2025/04 , F23N2029/20 , F23N2031/28 , F23N2035/14 , F23N2041/20 , F23R3/286 , F23R2900/00002 , F23R2900/00016
摘要： A method may mitigate a flashback condition in a gas turbine. The gas turbine may include a fuel nozzle. The method may include detecting the flashback condition in the fuel nozzle, and interrupting a flow of fuel to the fuel nozzle.
摘要翻译： 一种方法可以减轻燃气轮机中的回火状况。 燃气轮机可以包括燃料喷嘴。 该方法可以包括检测燃料喷嘴中的回火状态，并且中断燃料流向燃料喷嘴。
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公开(公告)号：US09322557B2
公开(公告)日：2016-04-26
申请号：US13343926
申请日：2012-01-05
CPC分类号： F23R3/283 , F23D2209/10 , F23D2209/20 , F23R3/286 , F23R2900/03044
摘要： A combustor includes a tube bundle that extends radially across at least a portion of the combustor. The tube bundle includes an upstream surface axially separated from a downstream surface. A plurality of tubes extends from the upstream surface through the downstream surface, and each tube provides fluid communication through the tube bundle. A baffle extends axially inside the tube bundle between adjacent tubes. A method for distributing fuel in a combustor includes flowing a fuel into a fuel plenum defined at least in part by an upstream surface, a downstream surface, a shroud, and a plurality of tubes that extend from the upstream surface to the downstream surface. The method further includes impinging the fuel against a baffle that extends axially inside the fuel plenum between adjacent tubes.
摘要翻译： 燃烧器包括径向延伸穿过燃烧器的至少一部分的管束。 管束包括从下游表面轴向分离的上游表面。 多个管从上游表面延伸穿过下游表面，并且每个管提供通过管束的流体连通。 挡板在相邻管之间的管束内部轴向延伸。 用于在燃烧器中分配燃料的方法包括使燃料流入至少部分地由上游表面，下游表面，护罩和从上游表面延伸到下游表面的多个管所限定的燃料增压室。 该方法还包括将燃料撞击在相邻管之间的燃料增压室内轴向延伸的挡板。
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公开(公告)号：US08789372B2
公开(公告)日：2014-07-29
申请号：US12499777
申请日：2009-07-08
CPC分类号： F23R3/28 , F23R2900/00014
摘要： The system may include a turbine engine. The turbine engine may include a fuel nozzle. The fuel nozzle may include an air path. The fuel nozzle may also include a fuel path such that the fuel nozzle is in communication with a combustion zone of the turbine engine. Furthermore, the fuel nozzle may include a resonator. The resonator may be disposed in the fuel nozzle directly adjacent to the combustion zone.
摘要翻译： 该系统可以包括涡轮发动机。 涡轮发动机可以包括燃料喷嘴。 燃料喷嘴可以包括空气路径。 燃料喷嘴还可以包括燃料路径，使得燃料喷嘴与涡轮发动机的燃烧区域连通。 此外，燃料喷嘴可以包括谐振器。 谐振器可以直接邻近燃烧区设置在燃料喷嘴中。
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公开(公告)号：US20130174568A1
公开(公告)日：2013-07-11
申请号：US13343926
申请日：2012-01-05
CPC分类号： F23R3/283 , F23D2209/10 , F23D2209/20 , F23R3/286 , F23R2900/03044
摘要： A combustor includes a tube bundle that extends radially across at least a portion of the combustor. The tube bundle includes an upstream surface axially separated from a downstream surface. A plurality of tubes extends from the upstream surface through the downstream surface, and each tube provides fluid communication through the tube bundle. A baffle extends axially inside the tube bundle between adjacent tubes. A method for distributing fuel in a combustor includes flowing a fuel into a fuel plenum defined at least in part by an upstream surface, a downstream surface, a shroud, and a plurality of tubes that extend from the upstream surface to the downstream surface. The method further includes impinging the fuel against a baffle that extends axially inside the fuel plenum between adjacent tubes.
摘要翻译： 燃烧器包括径向延伸穿过燃烧器的至少一部分的管束。 管束包括从下游表面轴向分离的上游表面。 多个管从上游表面延伸穿过下游表面，并且每个管提供通过管束的流体连通。 挡板在相邻管之间的管束内部轴向延伸。 用于在燃烧器中分配燃料的方法包括使燃料流入至少部分地由上游表面，下游表面，护罩和从上游表面延伸到下游表面的多个管所限定的燃料增压室。 该方法还包括将燃料撞击在相邻管之间的燃料增压室内轴向延伸的挡板。
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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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26.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：US20110179795A1
公开(公告)日：2011-07-28
申请号：US12499777
申请日：2009-07-08
IPC分类号： F02C7/24
CPC分类号： F23R3/28 , F23R2900/00014
摘要： The system may include a turbine engine. The turbine engine may include a fuel nozzle. The fuel nozzle may include an air path. The fuel nozzle may also include a fuel path such that the fuel nozzle is in communication with a combustion zone of the turbine engine. Furthermore, the fuel nozzle may include a resonator. The resonator may be disposed in the fuel nozzle directly adjacent to the combustion zone.
摘要翻译： 该系统可以包括涡轮发动机。 涡轮发动机可以包括燃料喷嘴。 燃料喷嘴可以包括空气路径。 燃料喷嘴还可以包括燃料路径，使得燃料喷嘴与涡轮发动机的燃烧区域连通。 此外，燃料喷嘴可以包括谐振器。 谐振器可以直接邻近燃烧区设置在燃料喷嘴中。
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公开(公告)号：US08511086B1
公开(公告)日：2013-08-20
申请号：US13409326
申请日：2012-03-01
IPC分类号： F02C1/00
CPC分类号： F23R3/286 , F23L2900/07002 , F23L2900/07008 , F23L2900/07009 , F23R2900/00013 , F23R2900/00014
摘要： A system for reducing combustion dynamics in a combustor includes an end cap having an upstream surface axially separated from a downstream surface, and tube bundles extend through the end cap. A diluent supply in fluid communication with the end cap provides diluent flow to the end cap. Diluent distributors circumferentially arranged inside at least one tube bundle extend downstream from the downstream surface and provide fluid communication for the diluent flow through the end cap. A method for reducing combustion dynamics in a combustor includes flowing fuel through tube bundles that extend axially through an end cap, flowing a diluent through diluent distributors into a combustion chamber, wherein the diluent distributors are circumferentially arranged inside at least one tube bundle and each diluent distributor extends downstream from the end cap, and forming a diluent barrier in the combustion chamber between at least one pair of adjacent tube bundles.
摘要翻译： 用于减少燃烧器中的燃烧动力学的系统包括具有从下游表面轴向分离的上游表面的端盖，并且管束延伸穿过端盖。 与端盖流体连通的稀释剂供应器提供了向端盖的稀释剂流。 周向布置在至少一个管束内的稀释剂分配器延伸到下游表面的下游，并且提供流过端盖的稀释剂流的流体连通。 一种用于减少燃烧动力学的方法，包括使燃料通过管束流动，所述管束轴向延伸穿过端盖，使稀释剂流经稀释剂分配器进入燃烧室，其中稀释剂分配器周向地布置在至少一个管束内，每个稀释剂 分配器从端盖延伸到下游，并且在燃烧室中在至少一对相邻的管束之间形成稀释剂阻挡层。
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公开(公告)号：US20130227953A1
公开(公告)日：2013-09-05
申请号：US13409309
申请日：2012-03-01
IPC分类号： F23R3/28
CPC分类号： F23R3/286 , F02C3/30 , F23C2900/07022 , F23D14/62 , F23R3/002 , F23R3/32 , F23R3/54 , F23R2900/00013
摘要： A system for reducing combustion dynamics in a combustor includes an end cap having an upstream surface axially separated from a downstream surface, and tube bundles extend from the upstream surface through the downstream surface. A divider inside a tube bundle defines a diluent passage that extends axially through the downstream surface, and a diluent supply in fluid communication with the divider provides diluent flow to the diluent passage. A method for reducing combustion dynamics in a combustor includes flowing a fuel through tube bundles, flowing a diluent through a diluent passage inside a tube bundle, wherein the diluent passage extends axially through at least a portion of the end cap into a combustion chamber, and forming a diluent barrier in the combustion chamber between the tube bundle and at least one other adjacent tube bundle.
摘要翻译： 用于减少燃烧器中的燃烧动力学的系统包括具有从下游表面轴向分离的上游表面的端盖，并且管束从上游表面延伸穿过下游表面。 管束内的分隔器限定了一个沿轴向延伸穿过下游表面的稀释剂通道，与分隔器流体连通的稀释剂供应器提供稀释剂流向稀释剂通道。 一种用于减少燃烧动力学的方法，包括使燃料通过管束流动，使稀释剂流过管束内的稀释剂通道，其中稀释剂通道轴向延伸通过端盖的至少一部分进入燃烧室，以及 在管束与至少一个其它相邻管束之间的燃烧室中形成稀释剂阻挡层。
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公开(公告)号：US20110252802A1
公开(公告)日：2011-10-20
申请号：US12759794
申请日：2010-04-14
IPC分类号： F02C7/22
摘要： A premixer is provided and includes a peripheral wall defining a mixing chamber therein through which a flow path for a fluid is defined, a nozzle including an annular splitter plate disposed in the flow path within the mixing chamber, the splitter plate including a trailing edge defined in relation to a predominant direction of fluid flow along the flow path and being formed to define a fuel line therein, which is receptive of oil fuel and an annular array of fuel injectors disposed at the trailing edge, which are each fluidly communicative with the fuel line and configured to inject at least the oil fuel into the flow path with the oil fuel being substantially atomized upon injection or substantially immediately after the injection by interaction with the fluid flowing along the flow path.
摘要翻译： 提供预混合器并且包括在其中限定混合室的外围壁，通过该混合室限定用于流体的流动路径，喷嘴，其包括设置在混合室内的流动路径中的环形分离板，分离板包括限定的后缘 相对于沿着流动路径的流体流动的主要方向并且被形成为在其中限定其中容纳油燃料的燃料管线和设置在后缘处的燃料喷射器的环形阵列，其各自与燃料流体连通 并且构造成至少将油燃料喷射到流动路径中，其中油燃料在注射时基本上雾化，或者基本上在注射之后立即与沿着流动路径流动的流体相互作用。
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