Combustor fuel nozzle and method for supplying fuel to a combustor
    1.
    发明授权
    Combustor fuel nozzle and method for supplying fuel to a combustor 有权
    燃烧器燃料喷嘴和用于向燃烧器供应燃料的方法

    公开(公告)号:US09182123B2

    公开(公告)日:2015-11-10

    申请号:US13344033

    申请日:2012-01-05

    IPC分类号: F23R3/14 F23R3/28

    CPC分类号: F23R3/14 F23R3/286

    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。

    Fuel distribution manifold
    2.
    发明授权
    Fuel distribution manifold 有权
    燃油分配歧管

    公开(公告)号:US09157635B2

    公开(公告)日:2015-10-13

    申请号:US13342497

    申请日:2012-01-03

    IPC分类号: B01F5/00 F23K5/06 F02C7/22

    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。

    Combustor and method for supplying fuel to a combustor
    4.
    发明授权
    Combustor and method for supplying fuel to a combustor 有权
    用于向燃烧器供应燃料的燃烧器和方法

    公开(公告)号:US08801428B2

    公开(公告)日:2014-08-12

    申请号:US13252279

    申请日:2011-10-04

    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。

    Axial Flow Fuel Nozzle with a Stepped Center Body
    6.
    发明申请
    Axial Flow Fuel Nozzle with a Stepped Center Body 有权
    具有阶梯式中心体的轴流式燃油喷嘴

    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。

    Fuel nozzle assembly for gas turbine system
    7.
    发明授权
    Fuel nozzle assembly for gas turbine system 有权
    燃气轮机系统燃油喷嘴总成

    公开(公告)号:US08418469B2

    公开(公告)日:2013-04-16

    申请号:US12890903

    申请日:2010-09-27

    IPC分类号: F02C1/00

    摘要: A fuel nozzle assembly is disclosed. The fuel nozzle assembly comprises an outer burner tube and an inner burner tube defining a pre-mixing annulus therebetween. The fuel nozzle assembly further comprises a swirler assembly, the swirler assembly comprising a plurality of swirler vanes disposed in an annular array about the inner burner tube and configured to interact with primary air upstream of the pre-mixing annulus. The fuel nozzle assembly further comprises an air injection feature configured to flow secondary air into the pre-mixing annulus downstream of the swirler assembly such that the secondary air flows in a generally linear path longitudinally with respect to the pre-mixing annulus and adjacent at least one of the outer burner tube and the inner burner tube.

    摘要翻译: 公开了一种燃料喷嘴组件。 燃料喷嘴组件包括外部燃烧器管和在其间限定预混合环的内部燃烧器管。 所述燃料喷嘴组件还包括旋流器组件,所述旋流器组件包括围绕所述内部燃烧器管设置成环形阵列并被配置为与所述预混合环空上游的一次空气相互作用的多个旋流器叶片。 燃料喷嘴组件还包括空气喷射特征,该空气喷射特征构造成将二次空气流入旋流器组件下游的预混合环空,使得二次空气相对于预混气环纵向流动,并且至少相邻 外部燃烧器管和内部燃烧器管之一。

    APPARATUS AND METHOD FOR EXTERNALLY LOADED LIQUID FUEL INJECTION FOR LEAN PREVAPORIZED PREMIXED AND DRY LOW NOX COMBUSTOR
    9.
    发明申请
    APPARATUS AND METHOD FOR EXTERNALLY LOADED LIQUID FUEL INJECTION FOR LEAN PREVAPORIZED PREMIXED AND DRY LOW NOX COMBUSTOR 审中-公开
    用于精细预处理的优质低温NOX混合机的外装液体燃料注入装置和方法

    公开(公告)号:US20090044537A1

    公开(公告)日:2009-02-19

    申请号:US11840521

    申请日:2007-08-17

    IPC分类号: F02C3/00

    CPC分类号: F23R3/286

    摘要: A fuel injector stick for a gas turbine includes: a body of a length, L, the body including an annular shape forming a fuel channel and adapted for insertion into a premixer of the gas turbine; a mounting section for mounting the injector stick to the gas turbine; and a nozzle for injecting fuel into the premixer of the gas turbine. A gas turbine combustor and a method for changing fuel injector sticks are provided.

    摘要翻译: 一种用于燃气轮机的燃料喷射器棒包括:主体L,主体包括形成燃料通道并适于插入燃气轮机预混合器的环形; 用于将喷射器杆安装到燃气轮机上的安装部分; 以及用于将燃料喷射到燃气轮机的预混合器中的喷嘴。 提供燃气轮机燃烧器和改变燃料喷射器棒的方法。