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公开(公告)号：US20100084490A1
公开(公告)日：2010-04-08
申请号：US12245266
申请日：2008-10-03
IPC分类号： B05B15/00
摘要： An injection nozzle having a main body portion with an outer peripheral wall is disclosed. The nozzle includes a plurality of fuel/air mixing tubes disposed within the main body portion and a fuel flow passage fluidly connected to the plurality of fuel/air mixing tubes. Fuel and air are partially premixed inside the plurality of the tubes. A second body portion, having an outer peripheral wall extending between a first end and an opposite second end, is connected to the main body portion. The partially premixed fuel and air mixture from the first body portion gets further mixed inside the second body portion. The second body portion converges from the first end toward said second end. The second body portion also includes cooling passages that extend along all the walls around the second body to provide thermal damage resistance for occasional flame flash back into the second body.
摘要翻译： 公开了一种具有外周壁的主体部分的喷嘴。 喷嘴包括设置在主体部分内的多个燃料/空气混合管和流体连接到多个燃料/空气混合管的燃料流动通道。 燃料和空气在多个管内部分地预混合。 具有在第一端和相对的第二端之间延伸的外周壁的第二主体部分连接到主体部分。 来自第一主体部分的部分预混合的燃料和空气混合物在第二主体部分内被进一步混合。 第二主体部分从第一端朝向所述第二端收敛。 第二主体部分还包括沿着围绕第二主体的所有壁延伸的冷却通道，以提供对偶尔的火焰闪回第二主体的热损伤性。
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62.发明授权Reduced center burner in multi-burner combustor and method for operating the combustor 有权多燃烧器燃烧器中的减少中心燃烧器和操作燃烧器的方法公开(公告)号：US07185494B2
公开(公告)日：2007-03-06
申请号：US10821975
申请日：2004-04-12
IPC分类号： F23R3/36
CPC分类号： F23R3/286 , F23D14/74 , F23D2900/14004 , Y02E20/344
摘要： A single stage combustor for a gas turbine having an annular array of outer fuel nozzles arranged about a center axis of the combustor; a center fuel nozzle aligned with the center axis, wherein the center fuel nozzle is substantially smaller than each of the outer fuel nozzles, wherein the combustor includes a pre-mix operating mode in which the center nozzle receives a fuel rich air-fuel mixture.
摘要翻译： 一种用于燃气轮机的单级燃烧器，具有围绕燃烧器的中心轴线布置的外部燃料喷嘴的环形阵列; 中心燃料喷嘴与中心轴线对准，其中中心燃料喷嘴基本上小于每个外部燃料喷嘴，其中燃烧器包括预混合操作模式，其中中心喷嘴接收富燃料空气混合物。
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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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64.发明授权公开(公告)号：US09303874B2
公开(公告)日：2016-04-05
申请号：US13423854
申请日：2012-03-19
IPC分类号： F23R3/28
CPC分类号： F23R3/286 , F23R2900/00002
摘要： Embodiments of the present application include a combustor assembly. The combustor assembly may include a combustion chamber, a first plenum, a second plenum, and one or more elongate air/fuel premixing injection tubes. Each of the elongate air/fuel premixing injection tubes may include a first length at least partially disposed within the first plenum and configured to receive a first fluid from the first plenum. Moreover, each of the elongate air/fuel premixing injection tubes may include a second length disposed downstream of the first length and at least partially disposed within the second plenum. The second length may be formed of a porous wall configured to allow a second fluid from the second plenum to enter the second length and create a boundary layer about the porous wall.
摘要翻译： 本申请的实施例包括燃烧器组件。 燃烧器组件可以包括燃烧室，第一增压室，第二增压室和一个或多个细长的空气/燃料预混合注入管。 细长空气/燃料预混合注入管中的每一个可以包括至少部分地设置在第一集气室内并被配置为从第一集气室接收第一流体的第一长度。 此外，细长空气/燃料预混合注射管中的每一个可以包括设置在第一长度的下游并且至少部分地设置在第二增压室内的第二长度。 第二长度可以由多孔壁形成，多孔壁被构造成允许来自第二增压室的第二流体进入第二长度并且围绕多孔壁产生边界层。
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公开(公告)号：US09080513B2
公开(公告)日：2015-07-14
申请号：US11931801
申请日：2007-10-31
CPC分类号： F02C3/22 , F02C9/40 , F23N2037/08 , F23N2041/20 , F23R3/36
摘要： A method for operating a combustor is provided. The method includes supplying a predetermined amount of a first gaseous fuel to the combustor, wherein the first gaseous fuel has a first Modified Wobbe Index (MWI) and a first fuel reactivity, and supplying a predetermined amount of a second gaseous fuel to the combustor, wherein the second gaseous fuel has a second MWI that is lower than the first MWI and a second fuel reactivity that is higher than the first fuel reactivity. The method also includes mixing the first and second gaseous fuels together to form a blended gaseous fuel, and injecting the blended gaseous fuel into the combustor.
摘要翻译： 提供了一种操作燃烧器的方法。 该方法包括向燃烧器供应预定量的第一气体燃料，其中第一气态燃料具有第一改性沃泊指数（MWI）和第一燃料反应性，并向燃烧器供应预定量的第二气态燃料， 其中所述第二气体燃料具有低于所述第一MWI的第二MWI和高于所述第一燃料反应性的第二燃料反应性。 该方法还包括将第一和第二气体燃料混合在一起以形成混合的气体燃料，以及将混合的气态燃料注入燃烧器。
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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：US08613187B2
公开(公告)日：2013-12-24
申请号：US12604435
申请日：2009-10-23
IPC分类号： F02C3/20
CPC分类号： F02C7/22
摘要： A combustor may include a number of nozzles, a first fuel source with a low reactivity fuel therein, a second fuel source with a high reactivity fuel therein, and a primary valve for varying the flow of the low reactivity fuel and the high reactivity fuel delivered to the nozzles.
摘要翻译： 燃烧器可以包括多个喷嘴，其中具有低反应性燃料的第一燃料源，其中具有高反应性燃料的第二燃料源和用于改变低反应性燃料和高反应性燃料的流动的主阀 到喷嘴。
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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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69.发明申请SYSTEMS AND METHODS FOR BULK TEMPERATURE VARIATION REDUCTION OF A GAS TURBINE THROUGH CAN-TO-CAN FUEL TEMPERATURE MODULATION 审中-公开通过CAN-to-CAN燃料温度调节对气体涡轮机进行温度变化的系统和方法公开(公告)号：US20130014514A1
公开(公告)日：2013-01-17
申请号：US13182956
申请日：2011-07-14
CPC分类号： F23R3/46 , F02C7/224 , F23K5/20 , F23K2301/204 , F23R3/28 , F23R2900/00013
摘要： A gas turbine includes a plurality of combustion chambers; at least one fuel nozzle for each of the combustion chambers; at least one fuel line for each fuel nozzle in each of the combustion chambers; at least one heat exchanger for each fuel line configured to adjust a temperature of a fuel flow to each fuel nozzle; and a controller configured to control each of the heat exchangers to reduce temperature variations amongst the combustion chambers.
摘要翻译： 燃气轮机包括多个燃烧室; 用于每个燃烧室的至少一个燃料喷嘴; 用于每个燃烧室中的每个燃料喷嘴的至少一个燃料管线; 每个燃料管线的至少一个热交换器被配置为调节到每个燃料喷嘴的燃料流的温度; 以及控制器，被配置为控制每个所述热交换器以减少所述燃烧室之间的温度变化。
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公开(公告)号：US08276386B2
公开(公告)日：2012-10-02
申请号：US12889512
申请日：2010-09-24
申请人： Willy Steve Ziminsky , Christopher Edward Wolfe , Sergey Anatolievich Meshkov , Sergey Adolfovich Oskin
发明人： Willy Steve Ziminsky , Christopher Edward Wolfe , Sergey Anatolievich Meshkov , Sergey Adolfovich Oskin
IPC分类号： F02C7/08
CPC分类号： F23R3/16
摘要： A combustor includes an end cover and a combustion chamber downstream of the end cover. The combustor further includes nozzles disposed radially in the end cover and a shroud surrounding at least one of the nozzles and extending downstream into the combustion chamber. The shroud includes an inner wall surface and an outer wall surface. A method for operating a combustor includes flowing compressed working fluid through nozzles into a combustion chamber, flowing fuel through each nozzle in a first subset of the nozzles into the combustion chamber, and igniting the fuel from each nozzle in the first subset of nozzles in the combustion chamber. In addition, the method includes extending into the combustion chamber a separate shroud around each nozzle in a second subset of the nozzles and isolating fuel to each nozzle in the second subset of nozzles.
摘要翻译： 燃烧器包括端盖和端盖下游的燃烧室。 燃烧器还包括径向设置在端盖中的喷嘴和围绕至少一个喷嘴并在下游延伸到燃烧室中的护罩。 护罩包括内壁表面和外壁表面。 一种用于操作燃烧器的方法包括将压缩的工作流体通过喷嘴流入燃烧室，使燃料通过喷嘴的第一子集中的每个喷嘴流入燃烧室，并且从喷嘴的第一子集中的每个喷嘴点燃燃料 燃烧室。 此外，该方法包括在喷嘴的第二子集中的每个喷嘴周围延伸到燃烧室中的单独的护罩，并将燃料与第二喷嘴子集中的每个喷嘴隔离。
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