System and method for supporting fuel nozzles inside a combustor
    1.
    发明授权
    System and method for supporting fuel nozzles inside a combustor 有权
    用于在燃烧器内支撑燃料喷嘴的系统和方法

    公开(公告)号:US09366445B2

    公开(公告)日:2016-06-14

    申请号:US13439973

    申请日:2012-04-05

    IPC分类号: F23R3/60

    摘要: A system for supporting fuel nozzles inside a combustor includes a ring that circumferentially surrounds the fuel nozzles inside the combustor, a support plate that extends radially inside at least a portion of the ring, and a first connection between the support plate and at least one of the fuel nozzles inside the combustor. A second connection is between the support plate and the ring. A method for supporting fuel nozzles in a combustor includes surrounding the fuel nozzles with a ring, connecting a support plate to the ring, and connecting the support plate to at least one fuel nozzle.

    摘要翻译: 用于在燃烧器内部支撑燃料喷嘴的系统包括周向围绕燃烧器内的燃料喷嘴的环,支撑板,其在环的至少一部分的径向内延伸,以及在支撑板和至少一个之间的第一连接 燃烧器内部的燃料喷嘴。 支撑板和环之间的第二连接。 用于在燃烧器中支撑燃料喷嘴的方法包括用环围绕燃料喷嘴,将支撑板连接到环上,并将支撑板连接到至少一个燃料喷嘴。

    System and method for supplying a working fluid to a combustor via a non-uniform distribution manifold
    2.
    发明授权
    System and method for supplying a working fluid to a combustor via a non-uniform distribution manifold 有权
    通过不均匀的分配歧管向燃烧器供应工作流体的系统和方法

    公开(公告)号:US09188337B2

    公开(公告)日:2015-11-17

    申请号:US13349906

    申请日:2012-01-13

    摘要: A system for supplying a working fluid to a combustor includes a fuel nozzle and a combustion chamber downstream from the fuel nozzle. A flow sleeve circumferentially surrounds the combustion chamber, and fuel injectors provide fluid communication to the combustion chamber. A distribution manifold circumferentially surrounds the fuel injectors and defines an annular plenum. A fluid passage through the distribution manifold provides fluid communication through the distribution manifold. A radial cross-sectional area of the annular plenum varies around the flow sleeve. A method for supplying a working fluid to a combustor includes flowing a working fluid through a combustion chamber, diverting a portion of the working fluid through a distribution manifold that circumferentially surrounds fuel injectors circumferentially arranged around the combustion chamber, and changing at least one of a pressure or flow rate of the diverted portion of the working fluid.

    摘要翻译: 用于向燃烧器供应工作流体的系统包括燃料喷嘴和燃料喷嘴下游的燃烧室。 流动套筒周向地围绕燃烧室,并且燃料喷射器提供与燃烧室的流体连通。 分配歧管周向地包围燃料喷射器并且限定环形增压室。 通过分配歧管的流体通道提供通过分配歧管的流体连通。 环形增压室的径向横截面面积围绕流动套管变化。 用于将工作流体供应到燃烧室的方法包括使工作流体流过燃烧室,使工作流体的一部分通过周向围绕燃烧室周围布置的燃料喷射器的分配歧管转向,并且改变至少一个 工作流体的转向部分的压力或流量。

    Micromixer combustion head end assembly
    3.
    发明授权
    Micromixer combustion head end assembly 有权
    微混合器燃烧头端组件

    公开(公告)号:US09163839B2

    公开(公告)日:2015-10-20

    申请号:US13423894

    申请日:2012-03-19

    IPC分类号: B01F3/04 F23R3/28

    CPC分类号: F23R3/286

    摘要: Embodiments of the present application can provide systems and methods for a micromixer combustion head end assembly. The micromixer may include one or more base nozzle structures. The base nozzle structures may include coaxial tubes. The coaxial tubes may include an inner tube and an outer tube. The micromixer may also include one or more segmented mixing tube bundles at least partially supported by a respective base nozzle structure. Moreover, the micromixer may include an end cap assembly disposed about the one or more segmented mixing tube bundles.

    摘要翻译: 本申请的实施例可以提供用于微混合器燃烧头端组件的系统和方法。 微混合器可以包括一个或多个基本喷嘴结构。 基座喷嘴结构可以包括同轴管。 同轴管可包括内管和外管。 微混合器还可以包括至少部分由相应的基座喷嘴结构支撑的一个或多个分段的混合管束。 此外,微混合器可以包括围绕一个或多个分段的混合管束设置的端盖组件。

    Combustor with a pre-nozzle mixing cap assembly
    5.
    发明授权
    Combustor with a pre-nozzle mixing cap assembly 有权
    具有预喷嘴混合盖组件的燃烧器

    公开(公告)号:US09068750B2

    公开(公告)日:2015-06-30

    申请号:US13040289

    申请日:2011-03-04

    CPC分类号: F23R3/286 F02C7/22

    摘要: The present application and the resulting patent provide a pre-nozzle mixing cap assembly positioned about a cap member of a combustor for mixing a flow of air and a flow of fuel. The pre-nozzle mixing cap assembly may include a fuel plenum in communication with the flow of fuel and a number of tubes in communication with the flow of air and extending through the fuel plenum. Each of the tubes may include a number of fuel holes therein such that the flow of fuel in the fuel plenum passes through the fuel holes and mixes with the flow of air.

    摘要翻译: 本申请和所得专利提供了一种预喷嘴混合盖组件,其围绕燃烧器的盖构件定位,以混合空气流和燃料流。 预喷嘴混合盖组件可以包括与燃料流连通的燃料增压室和与空气流连通并延伸通过燃料增压室的多个管。 每个管可以在其中包括多个燃料孔,使得燃料气室中的燃料流通过燃料孔并与空气流混合。

    Combustor nozzle and method for modifying the combustor nozzle
    6.
    发明授权
    Combustor nozzle and method for modifying the combustor nozzle 有权
    燃烧器喷嘴和用于改变燃烧器喷嘴的方法

    公开(公告)号:US09052113B1

    公开(公告)日:2015-06-09

    申请号:US13153499

    申请日:2011-06-06

    IPC分类号: F23R3/28

    摘要: A combustor nozzle includes a downstream surface having an axial centerline. A plurality of passages through the downstream surface provide fluid communication through the downstream surface, and a downstream section of each passage has at least one of a frusto-conical or frusto-spherical shape. A method for modifying a combustor nozzle includes machining a downstream side of a body to remove a recast surface in a plurality of passages that provide fluid communication through the body. The method may further include machining a downstream section in each passage to form at least one of a frusto-conical or frusto-spherical surface in each passage proximate to the downstream side of the body.

    摘要翻译: 燃烧器喷嘴包括具有轴向中心线的下游表面。 通过下游表面的多个通道提供通过下游表面的流体连通,并且每个通道的下游部分具有截头圆锥形或截头圆球形的至少一个。 一种用于改变燃烧器喷嘴的方法包括机械加工主体的下游侧以去除多个通道中的重铸表面,该多个通道提供通过本体的流体连通。 该方法可以进一步包括加工每个通道中的下游部分以在靠近主体的下游侧的每个通道中形成截头圆锥形或截头圆球形表面中的至少一个。

    Combustor
    7.
    发明授权
    Combustor 有权
    燃烧器

    公开(公告)号:US09016064B2

    公开(公告)日:2015-04-28

    申请号:US13545231

    申请日:2012-07-10

    IPC分类号: F01D25/28 F02C7/22

    CPC分类号: F02C7/22

    摘要: A combustor includes a breech end, a plurality of fuel nozzles connected to the breech end and extending downstream from the breech end; and a shroud that circumferentially surrounds the plurality of fuel nozzles inside the combustor. A support extends radially inside at least a portion of the shroud, and a lip seal is between the support and at least one of the plurality of fuel nozzles.

    摘要翻译: 燃烧器包括后膛端,连接到后膛端并从后膛末端延伸的多个燃料喷嘴; 以及周向围绕燃烧器内部的多个燃料喷嘴的护罩。 支撑件径向地延伸到护罩的至少一部分内,并且唇形密封件位于支撑件和多个燃料喷嘴中的至少一个之间。

    System and method for flow control in gas turbine engine
    8.
    发明授权
    System and method for flow control in gas turbine engine 有权
    燃气轮机发动机流量控制系统及方法

    公开(公告)号:US08919127B2

    公开(公告)日:2014-12-30

    申请号:US13115058

    申请日:2011-05-24

    CPC分类号: F23R3/02 F23R3/286

    摘要: A system includes a gas turbine combustor, which includes a combustion liner disposed about a combustion region, a flow sleeve disposed about the combustion liner, an air passage between the combustion liner and the flow sleeve, and a structure between the combustion liner and the flow sleeve. The structure obstructs an airflow through the air passage. The gas turbine combustor also includes a wake reducer disposed adjacent the structure. The wake reducer directs a flow into a wake region downstream of the structure.

    摘要翻译: 一种系统包括燃气轮机燃烧器,其包括围绕燃烧区域设置的燃烧衬套,围绕燃烧衬套设置的流动套筒,在燃烧衬套和流动套筒之间的空气通道,以及燃烧衬套与流体之间的结构 袖。 该结构阻碍通过空气通道的气流。 燃气轮机燃烧器还包括邻近结构布置的尾流减速器。 尾流减速器将流动引导到结构下游的尾流区域。

    Combustor and method for supplying fuel to a combustor
    9.
    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。

    System for supplying a working fluid to a combustor
    10.
    发明授权
    System for supplying a working fluid to a combustor 失效
    用于向燃烧器供应工作流体的系统

    公开(公告)号:US08677753B2

    公开(公告)日:2014-03-25

    申请号:US13466184

    申请日:2012-05-08

    IPC分类号: F02C1/00

    CPC分类号: F23R3/346 F23R2900/03341

    摘要: A system for supplying a working fluid to a combustor includes a fuel nozzle, a combustion chamber downstream from the fuel nozzle, and a flow sleeve that circumferentially surrounds the combustion chamber. A plurality of fuel injectors are circumferentially arranged around the flow sleeve to provide fluid communication through the flow sleeve to the combustion chamber. A distribution manifold circumferentially surrounds the plurality of fuel injectors, and a fluid passage through the flow sleeve and into the distribution manifold provides fluid communication through the flow sleeve to the plurality of fuel injectors.

    摘要翻译: 用于向燃烧器供应工作流体的系统包括燃料喷嘴,燃料喷嘴下游的燃烧室和周向围绕燃烧室的流动套筒。 多个燃料喷射器周向地布置在流动套筒周围,以提供通过流动套筒到燃烧室的流体连通。 分配歧管周向地围绕多个燃料喷射器,并且通过流动套管并进入分配歧管的流体通道提供通过流动套筒到多个燃料喷射器的流体连通。