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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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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：US20110016866A1
公开(公告)日：2011-01-27
申请号：US12507298
申请日：2009-07-22
摘要： In one embodiment, a system includes a fuel injector including a liquid fuel passage extending to a first port in a tip portion. The fuel injector also includes a selectable flow passage extending to a second port in the tip portion. The selectable flow passage surrounds the liquid fuel passage to the tip portion, the selectable flow passage is configured to selectively receive a gas fuel flow and an air flow, and the selectable flow passage has a flow temperature configured to cool a liquid fuel flowing through the liquid fuel passage to reduce coking.
摘要翻译： 在一个实施例中，系统包括燃料喷射器，其包括延伸到尖端部分中的第一端口的液体燃料通道。 燃料喷射器还包括延伸到尖端部分中的第二端口的可选择的流动通道。 可选择的流动通道围绕到顶部的液体燃料通道，可选择的流动通道构造成选择性地接收气体燃料流和空气流，并且可选择的流动通道具有被配置为冷却流过 液体燃料通道减少焦化。
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公开(公告)号：US09157635B2
公开(公告)日：2015-10-13
申请号：US13342497
申请日：2012-01-03
CPC分类号： F23K5/06 , F02C7/222 , Y10T137/85938
摘要： A fuel distribution manifold comprises an outer shell having an inner surface. The outer shell defines an inlet for receiving fuel from a parent supply line, a base opposite the inlet, a central manifold axis that intersects the inlet, and a plurality of outlets for delivering fuel to offspring fuel lines, each outlet defining a respective outlet axis. In one exemplary embodiment, a fuel distribution manifold also comprises a center-body having an outer surface and being positioned within the outer shell wherein the outer surface of the center-body and the inner surface of the outer shell define a flow-path through which fluid flows from the inlet to the plurality of outlets. In another exemplary embodiment, at least one of the outlets is positioned adjacent to the base and oriented so that its respective outlet axis is rotated relatively to a radial direction that intersects the central manifold axis.
摘要翻译： 燃料分配歧管包括具有内表面的外壳。 外壳限定用于从母体供应管线接收燃料的入口，与入口相对的底座，与入口相交的中心歧管轴线以及用于将燃料输送到后代燃料管线的多个出口，每个出口限定相应的出口轴线 。 在一个示例性实施例中，燃料分配歧管还包括具有外表面并且位于外壳内的中心体，其中中心体的外表面和外壳的内表面限定了流动路径，通过该流路 流体从入口流到多个出口。 在另一个示例性实施例中，至少一个出口定位成与基座相邻并且定向成使得其相应的出口轴线相对于与中心歧管轴线相交的径向方向旋转。
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7.发明授权Fuel nozzle staging with water flowing prior to fuel in a main fuel circuit during start-up 有权燃油喷嘴在启动期间在主燃料回路中的燃料流动之前进行分级公开(公告)号：US08991190B2
公开(公告)日：2015-03-31
申请号：US13362059
申请日：2012-01-31
IPC分类号： F02C7/26
CPC分类号： F02C7/236 , F02C3/30 , F02C9/40 , F23D11/10 , F23D2209/30 , F23D2900/00016 , F23K5/14 , F23K5/18 , F23K2301/20 , F23N2027/02 , F23N2027/04
摘要： A method for transferring fuel includes flowing water to at least one nozzle of a main fuel circuit. Also included is flowing oil to the at least one nozzle of the main fuel circuit. Further included is flowing liquid fuel to the at least one nozzle of the main fuel circuit, wherein flowing water to the at least one nozzle of the main fuel circuit occurs prior to flowing oil to the at least one nozzle of the main fuel circuit and flowing liquid fuel to the at least one nozzle of the main fuel circuit.
摘要翻译： 一种用于输送燃料的方法包括将水流向主燃料回路的至少一个喷嘴。 还包括流动油到主燃料回路的至少一个喷嘴。 还包括流动的液体燃料到主燃料回路的至少一个喷嘴，其中流动的水到主燃料回路的至少一个喷嘴发生在将油流到主燃料回路的至少一个喷嘴并流动 液体燃料到主燃料回路的至少一个喷嘴。
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公开(公告)号：US08801428B2
公开(公告)日：2014-08-12
申请号：US13252279
申请日：2011-10-04
CPC分类号： F23R3/343 , F23D14/62 , F23R3/10 , F23R3/286 , F23R3/46 , F23R2900/00001 , F23R2900/03343
摘要： A combustor includes an end cap having upstream and downstream surfaces and a cap shield surrounding the upstream and downstream surfaces. First and second sets of premixer tubes extend from the upstream surface through the downstream surface. A first fuel conduit supplies fuel to the first set of premixer tubes. A casing circumferentially surrounds the cap shield to define an annular passage, and a second fuel conduit supplies fuel through the annular passage to the second set of premixer tubes. A method for supplying fuel to a combustor includes flowing a working fluid through first and second sets of premixer tubes, flowing a first fuel into the first set of premixer tubes, and flowing a second fuel through an annular passage surrounding the end cap and into the second set of premixer tubes.
摘要翻译： 燃烧器包括具有上游和下游表面的端盖和围绕上游表面和下游表面的盖罩。 第一组和第二组预混合管从上游表面延伸穿过下游表面。 第一燃料管道向第一组预混合器管供应燃料。 壳体周向地围绕盖罩以限定环形通道，并且第二燃料管道将燃料通过环形通道供应到第二组预混合器管。 用于向燃烧器供应燃料的方法包括使工作流体流过第一组和第二组预混合器管，将第一燃料流入第一组预混合器管，并使第二种燃料流过围绕端盖的环形通道并进入 第二组预混管。
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公开(公告)号：US20130192236A1
公开(公告)日：2013-08-01
申请号：US13362059
申请日：2012-01-31
IPC分类号： F02M61/16
CPC分类号： F02C7/236 , F02C3/30 , F02C9/40 , F23D11/10 , F23D2209/30 , F23D2900/00016 , F23K5/14 , F23K5/18 , F23K2301/20 , F23N2027/02 , F23N2027/04
摘要： A method for transferring fuel includes flowing water to at least one nozzle of a main fuel circuit. Also included is flowing oil to the at least one nozzle of the main fuel circuit. Further included is flowing liquid fuel to the at least one nozzle of the main fuel circuit, wherein flowing water to the at least one nozzle of the main fuel circuit occurs prior to flowing oil to the at least one nozzle of the main fuel circuit and flowing liquid fuel to the at least one nozzle of the main fuel circuit.
摘要翻译： 一种用于输送燃料的方法包括将水流向主燃料回路的至少一个喷嘴。 还包括流动油到主燃料回路的至少一个喷嘴。 还包括流动的液体燃料到主燃料回路的至少一个喷嘴，其中流动的水到主燃料回路的至少一个喷嘴发生在将油流到主燃料回路的至少一个喷嘴并流动 液体燃料到主燃料回路的至少一个喷嘴。
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公开(公告)号：US20130186094A1
公开(公告)日：2013-07-25
申请号：US13354897
申请日：2012-01-20
IPC分类号： F23R3/14
摘要： An axial flow fuel nozzle for a gas turbine includes a plurality of annular passages for delivering materials for combustion. An annular air passage receives compressor discharge air, and a plurality of swirler vane slots are positioned adjacent an axial end of the annular air passage. A first next annular passage is disposed radially inward of the annular air passage and includes first openings positioned adjacent an axial end of the first annular passage and downstream of the swirler vane slots. A second next annular passage is disposed radially inward of the first annular passage and includes second openings positioned adjacent an axial end of the second annular passage and downstream of the first openings.
摘要翻译： 用于燃气轮机的轴流式燃料喷嘴包括用于输送用于燃烧的材料的多个环形通道。 环形空气通道接收压缩机排放空气，并且多个旋流器叶片槽邻近环形空气通道的轴向端定位。 第一个下一个环形通道设置在环形空气通道的径向内侧，并且包括邻近第一环形通道的轴向端部并且位于旋流器叶片槽的下游的第一开口。 第二个下一个环形通道设置在第一环形通道的径向内侧，并且包括邻近第二环形通道的轴向端部和第一开口下游定位的第二开口。
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