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公开(公告)号：US09182123B2
公开(公告)日：2015-11-10
申请号：US13344033
申请日：2012-01-05
摘要： A combustor fuel nozzle includes a center body and an inner shroud that circumferentially surrounds at least a portion of the center body. The inner shroud has a downstream surface. The fuel nozzle includes an inner passage between the center body and the inner shroud, an outer passage that circumferentially surrounds at least a portion of the inner shroud and a first plurality of fuel ports extending substantially radially outward through the center body. The first plurality of fuel ports is upstream from the downstream surface of the inner shroud. A method for supplying fuel to a combustor fuel nozzle includes flowing a working fluid through an inner passage between a center body and an inner shroud, injecting a fuel from the center body against the inner shroud, and flowing a portion of the working fluid through an outer passage that surrounds at least a portion of the inner shroud.
摘要翻译： 燃烧器燃料喷嘴包括中心体和周向围绕中心体的至少一部分的内护罩。 内护罩具有下游表面。 燃料喷嘴包括在中心体和内护罩之间的内通道，周向围绕内护罩的至少一部分的外通道和基本上径向向外延伸穿过中心体的第一多个燃料口。 第一多个燃料口在内护罩的下游表面上游。 向燃烧器燃料喷嘴供给燃料的方法包括使工作流体流过中心体和内护罩之间的内部通道，将燃料从中心体喷射到内护罩上，并使工作流体的一部分流过 外通道围绕内护罩的至少一部分。
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公开(公告)号：US20130174563A1
公开(公告)日：2013-07-11
申请号：US13344033
申请日：2012-01-05
摘要： A combustor fuel nozzle includes a center body and an inner shroud that circumferentially surrounds at least a portion of the center body. The inner shroud has a downstream surface. The fuel nozzle includes an inner passage between the center body and the inner shroud, an outer passage that circumferentially surrounds at least a portion of the inner shroud and a first plurality of fuel ports extending substantially radially outward through the center body. The first plurality of fuel ports is upstream from the downstream surface of the inner shroud. A method for supplying fuel to a combustor fuel nozzle includes flowing a working fluid through an inner passage between a center body and an inner shroud, injecting a fuel from the center body against the inner shroud, and flowing a portion of the working fluid through an outer passage that surrounds at least a portion of the inner shroud.
摘要翻译： 燃烧器燃料喷嘴包括中心体和周向围绕中心体的至少一部分的内护罩。 内护罩具有下游表面。 燃料喷嘴包括在中心体和内护罩之间的内通道，周向围绕内护罩的至少一部分的外通道和基本上径向向外延伸穿过中心体的第一多个燃料口。 第一多个燃料口在内护罩的下游表面上游。 向燃烧器燃料喷嘴供给燃料的方法包括使工作流体流过中心体和内护罩之间的内部通道，将燃料从中心体喷射到内护罩上，并使工作流体的一部分流过 外通道围绕内护罩的至少一部分。
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公开(公告)号：US20130199188A1
公开(公告)日：2013-08-08
申请号：US13367686
申请日：2012-02-07
IPC分类号： F23R3/30
CPC分类号： F23R3/286 , F23R2900/00015
摘要： Embodiments of the present application include a combustor assembly. The combustor assembly may include an annular trapped vortex cavity located adjacent to a downstream end of a bundle of air/fuel premixing injection tubes. The annular trapped vortex cavity may include an opening at a radially inner portion of the annular trapped vortex cavity adjacent to the head end of the bundle of premixing tubes. The annular trapped vortex cavity may also include one or more air injection holes and one or more fuel sources disposed about the annular trapped vortex cavity such that the one or more air injection holes and the one or more fuel sources are configured to drive a vortex within the annular trapped vortex cavity.
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邻近空气/燃料预混合注射管束的下游端定位的环形捕获涡流腔。 环形捕获的涡流空腔可以包括在与预混合管束的头端相邻的环形捕获涡流腔的径向内部的开口。 环形捕获的涡流空腔还可以包括一个或多个空气喷射孔和围绕环形捕获的涡流腔设置的一个或多个燃料源，使得一个或多个空气喷射孔和一个或多个燃料源被配置成驱动内部的涡流 环形捕获涡流腔。
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公开(公告)号：US09074773B2
公开(公告)日：2015-07-07
申请号：US13367686
申请日：2012-02-07
CPC分类号： F23R3/286 , F23R2900/00015
摘要： A combustor assembly is disclosed. The combustor assembly may include an annular trapped vortex cavity located adjacent to a downstream end of a bundle of air/fuel premixing injection tubes. The annular trapped vortex cavity may include an opening at a radially inner portion of the annular trapped vortex cavity adjacent to the head end of the bundle of premixing tubes. The annular trapped vortex cavity may also include one or more air injection holes and one or more fuel sources disposed about the annular trapped vortex cavity such that the one or more air injection holes and the one or more fuel sources are configured to drive a vortex within the annular trapped vortex cavity.
摘要翻译： 公开了一种燃烧器组件。 燃烧器组件可以包括邻近空气/燃料预混合注射管束的下游端定位的环形捕获涡流腔。 环形捕获的涡流空腔可以包括在与预混合管束的头端相邻的环形捕获涡流腔的径向内部的开口。 环形捕获的涡流空腔还可以包括一个或多个空气喷射孔和围绕环形捕获的涡流腔设置的一个或多个燃料源，使得一个或多个空气喷射孔和一个或多个燃料源被配置成驱动内部的涡流 环形捕获涡流腔。
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5.发明授权Systems and methods for suppressing combustion driven pressure fluctuations with a premix combustor having multiple premix times 有权用具有多个预混时间的预混合燃烧器抑制燃烧驱动的压力波动的系统和方法公开(公告)号：US09212823B2
公开(公告)日：2015-12-15
申请号：US13604952
申请日：2012-09-06
申请人： Gregory Allen Boardman , Ronald James Chila , Mark Allan Hadley , Johnie Franklin McConnaughhay , Sarah Lori Crothers
发明人： Gregory Allen Boardman , Ronald James Chila , Mark Allan Hadley , Johnie Franklin McConnaughhay , Sarah Lori Crothers
IPC分类号： F23R3/28
CPC分类号： F23R3/286 , F23R2900/00014 , F23R2900/03043 , F23R2900/03045
摘要： A combustor having a combustion chamber is provided with an external flow sleeve and a combustor liner surrounding the combustion chamber. A plurality of flow channels are provided on the combustor liner and a plurality of nozzles are disposed at predetermined locations on the flow channels. The locations of the nozzles are selected to provide different mixing times for fuel injected through the nozzles.
摘要翻译： 具有燃烧室的燃烧器设置有外部流动套筒和围绕燃烧室的燃烧室衬套。 多个流动通道设置在燃烧器衬套上，并且多个喷嘴设置在流动通道上的预定位置处。 选择喷嘴的位置以为通过喷嘴喷射的燃料提供不同的混合时间。
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6.发明申请Systems and Methods For Suppressing Combustion Driven Pressure Fluctuations With a Premix Combustor Having Multiple Premix Times 有权用具有多个预混时间的预混合燃烧器抑制燃烧驱动的压力波动的系统和方法公开(公告)号：US20140060063A1
公开(公告)日：2014-03-06
申请号：US13604952
申请日：2012-09-06
申请人： Gregory Allen Boardman , Ronald James Chila , Mark Allan Hadley , Johnie Franklin McConnaughhay , Sarah Lori Crothers
发明人： Gregory Allen Boardman , Ronald James Chila , Mark Allan Hadley , Johnie Franklin McConnaughhay , Sarah Lori Crothers
CPC分类号： F23R3/286 , F23R2900/00014 , F23R2900/03043 , F23R2900/03045
摘要： A combustor having a combustion chamber is provided with an external flow sleeve and a combustor liner surrounding the combustion chamber. A plurality of flow channels are provided on the combustor liner and a plurality of nozzles are disposed at predetermined locations on the flow channels. The locations of the nozzles are selected to provide different mixing times for fuel injected through the nozzles.
摘要翻译： 具有燃烧室的燃烧器设置有外部流动套筒和围绕燃烧室的燃烧室衬套。 多个流动通道设置在燃烧器衬套上，并且多个喷嘴设置在流动通道上的预定位置处。 选择喷嘴的位置以为通过喷嘴喷射的燃料提供不同的混合时间。
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公开(公告)号：US20110113783A1
公开(公告)日：2011-05-19
申请号：US12618636
申请日：2009-11-13
申请人： Gregory Allen Boardman , David Martin Johnson , Ronald James Chila , Nishant Govindbhai Parsania , Hasan Karim , Joseph Citeno
发明人： Gregory Allen Boardman , David Martin Johnson , Ronald James Chila , Nishant Govindbhai Parsania , Hasan Karim , Joseph Citeno
摘要： In one embodiment, a system includes a fuel nozzle that includes a fuel injector that includes a fuel port and a premixer tube. The premixer tube includes a wall disposed about a central passage, multiple air ports extending through the wall into the central passage, and a catalytic region. The catalytic region includes a catalyst, disposed inside the wall along the central passage, configured to increase a reaction of fuel and air.
摘要翻译： 在一个实施例中，系统包括燃料喷嘴，其包括燃料喷射器，燃料喷射器包括燃料口和预混合管。 预混合管包括围绕中心通道设置的壁，多个空气端口延伸穿过壁进入中心通道，以及催化区域。 催化区域包括沿着中心通道设置在壁内的催化剂，构造成增加燃料和空气的反应。
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公开(公告)号：US08683804B2
公开(公告)日：2014-04-01
申请号：US12618636
申请日：2009-11-13
申请人： Gregory Allen Boardman , David Martin Johnson , Ronald James Chila , Nishant Govindbhai Parsania , Hasan Karim , Joseph Citeno
发明人： Gregory Allen Boardman , David Martin Johnson , Ronald James Chila , Nishant Govindbhai Parsania , Hasan Karim , Joseph Citeno
摘要： In one embodiment, a system includes a fuel nozzle that includes a fuel injector that includes a fuel port and a premixer tube. The premixer tube includes a wall disposed about a central passage, multiple air ports extending through the wall into the central passage, and a catalytic region. The catalytic region includes a catalyst, disposed inside the wall along the central passage, configured to increase a reaction of fuel and air.
摘要翻译： 在一个实施例中，系统包括燃料喷嘴，其包括燃料喷射器，燃料喷射器包括燃料口和预混合管。 预混合管包括围绕中心通道设置的壁，多个空气端口延伸穿过壁进入中心通道，以及催化区域。 催化区域包括沿着中心通道设置在壁内的催化剂，构造成增加燃料和空气的反应。
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9.发明申请Hybrid Prefilming Airblast, Prevaporizing, Lean-Premixing Dual-Fuel Nozzle for a Gas Turbine Combustor 有权用于燃气轮机燃烧器的混合预吹风机，预蒸发，预混合双燃料喷嘴公开(公告)号：US20110289933A1
公开(公告)日：2011-12-01
申请号：US12787990
申请日：2010-05-26
CPC分类号： F23R3/36 , F23D2900/11101 , F23D2900/14004 , F23R3/14 , F23R3/286
摘要： A dual fuel nozzle for a gas turbine combustor includes a hub defining a fuel inlet and a plurality of liquid fuel jets disposed at a downstream end of the hub. The fuel jets are oriented to eject liquid fuel radially outward from the hub. An annular air passage includes a swirler that imparts swirl to air flowing in the annular air passage, and a splitter ring is disposed in the annular air passage and surrounds the plurality of liquid fuel jets. The nozzle allows liquid fuels to be injected into a swirling annular airstream and then atomized, dispersed and vaporized inside a lean premixing dual fuel nozzle for a gas turbine combustor.
摘要翻译： 用于燃气轮机燃烧器的双燃料喷嘴包括限定燃料入口的轮毂和设置在轮毂的下游端的多个液体燃料喷嘴。 燃料喷嘴被定向成从轮毂径向向外喷射液体燃料。 环形空气通道包括向在环形空气通道中流动的空气产生漩涡的旋流器，并且分离环设置在环形空气通道中并围绕多个液体燃料喷嘴。 喷嘴允许将液体燃料注入旋转的环形空气流中，然后在用于燃气轮机燃烧器的贫预混合双燃料喷嘴内雾化，分散和蒸发。
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10.发明授权Hybrid prefilming airblast, prevaporizing, lean-premixing dual-fuel nozzle for gas turbine combustor 有权用于燃气轮机燃烧器的混合预吹风机，预蒸发，预混合双燃料喷嘴公开(公告)号：US08671691B2
公开(公告)日：2014-03-18
申请号：US12787990
申请日：2010-05-26
CPC分类号： F23R3/36 , F23D2900/11101 , F23D2900/14004 , F23R3/14 , F23R3/286
摘要： A dual fuel nozzle for a gas turbine combustor includes a hub defining a fuel inlet and a plurality of liquid fuel jets disposed at a downstream end of the hub. The fuel jets are oriented to eject liquid fuel radially outward from the hub. An annular air passage includes a swirler that imparts swirl to air flowing in the annular air passage, and a splitter ring is disposed in the annular air passage and surrounds the plurality of liquid fuel jets. The nozzle allows liquid fuels to be injected into a swirling annular airstream and then atomized, dispersed and vaporized inside a lean premixing dual fuel nozzle for a gas turbine combustor.
摘要翻译： 用于燃气轮机燃烧器的双燃料喷嘴包括限定燃料入口的轮毂和设置在轮毂的下游端的多个液体燃料喷嘴。 燃料喷嘴被定向成从轮毂径向向外喷射液体燃料。 环形空气通道包括向在环形空气通道中流动的空气产生漩涡的旋流器，并且分离环设置在环形空气通道中并围绕多个液体燃料喷嘴。 喷嘴允许将液体燃料注入旋转的环形空气流中，然后在用于燃气轮机燃烧器的贫预混合双燃料喷嘴内雾化，分散和蒸发。
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