System and method for turbine combustor fuel assembly
    1.
    发明授权
    System and method for turbine combustor fuel assembly 有权
    涡轮燃烧器燃油组件的系统和方法

    公开(公告)号:US09267433B2

    公开(公告)日:2016-02-23

    申请号:US13280237

    申请日:2011-10-24

    IPC分类号: F02C3/30

    摘要: A system includes a turbine fuel supply system. The turbine fuel supply system includes a first turbine fuel mixer configured to mix a first liquid fuel and a first deaerated water to generate a first fuel mixture. The first fuel mixture is configured to combust in a combustor of a gas turbine engine. The turbine fuel supply system also includes a deaerated water flow path configured to route the first deaerated water to the first turbine fuel mixer and a liquid fuel flow path configured to route the first liquid fuel to the first turbine fuel mixer.

    摘要翻译: 一种系统包括涡轮燃料供应系统。 涡轮燃料供应系统包括构造成混合第一液体燃料和第一脱气水以产生第一燃料混合物的第一涡轮燃料混合器。 第一燃料混合物构造成在燃气涡轮发动机的燃烧器中燃烧。 涡轮燃料供应系统还包括一个脱气水流通道,其配置成将第一除气水路由第一涡轮燃料混合器和将第一液体燃料路由到第一涡轮燃料混合器的液体燃料流路。

    SYSTEM AND METHOD FOR TURBINE COMBUSTOR FUEL ASSEMBLY
    2.
    发明申请
    SYSTEM AND METHOD FOR TURBINE COMBUSTOR FUEL ASSEMBLY 有权
    用于涡轮机燃油组件的系统和方法

    公开(公告)号:US20130098056A1

    公开(公告)日:2013-04-25

    申请号:US13280237

    申请日:2011-10-24

    IPC分类号: F02C9/26 F02C3/30

    摘要: A system includes a turbine fuel supply system. The turbine fuel supply system includes a first turbine fuel mixer configured to mix a first liquid fuel and a first deaerated water to generate a first fuel mixture. The first fuel mixture is configured to combust in a combustor of a gas turbine engine. The turbine fuel supply system also includes a deaerated water flow path configured to route the first deaerated water to the first turbine fuel mixer and a liquid fuel flow path configured to route the first liquid fuel to the first turbine fuel mixer.

    摘要翻译: 一种系统包括涡轮燃料供应系统。 涡轮燃料供应系统包括构造成混合第一液体燃料和第一脱气水以产生第一燃料混合物的第一涡轮燃料混合器。 第一燃料混合物构造成在燃气涡轮发动机的燃烧器中燃烧。 涡轮燃料供应系统还包括一个脱气水流通道,其配置成将第一除气水路由第一涡轮燃料混合器和将第一液体燃料路由到第一涡轮燃料混合器的液体燃料流路。

    Combustor nozzle and method for supplying fuel to a combustor
    5.
    发明授权
    Combustor nozzle and method for supplying fuel to a combustor 有权
    燃烧器喷嘴和用于向燃烧器供应燃料的方法

    公开(公告)号:US09371989B2

    公开(公告)日:2016-06-21

    申请号:US13110256

    申请日:2011-05-18

    摘要: A combustor nozzle includes a first and second liquid fuel passages that terminate at first and second fuel ports. A first diluent passage terminates at a first diluent outlet radially surrounding the second fuel ports. A second diluent passage terminates at a second diluent outlet between the first diluent outlet and the second fuel ports. A third diluent passage surrounds at least a portion of the first and second diluent passages. A method for supplying fuel to a combustor includes flowing a liquid fuel through a first fuel passage and flowing an emulsified liquid fuel through a second fuel passage. The method further includes flowing a first diluent through a shroud surrounding the second fuel passage to a first diluent passage surrounding at least a portion of the second fuel passage and flowing a second diluent through a second diluent passage radially disposed between the first diluent passage and the second fuel passage.

    摘要翻译: 燃烧器喷嘴包括在第一和第二燃料端口处终止的第一和第二液体燃料通道。 第一稀释剂通道终止于径向围绕第二燃料端口的第一稀释剂出口。 第二稀释剂通道在第一稀释剂出口和第二燃料端口之间终止于第二稀释剂出口。 第三稀释剂通道围绕第一和第二稀释剂通道的至少一部分。 用于向燃烧器供应燃料的方法包括使液体燃料流过第一燃料通道并使乳化液体燃料流过第二燃料通道。 该方法还包括使第一稀释剂流过围绕第二燃料通道的护罩到围绕第二燃料通道的至少一部分的第一稀释剂通道,并使第二稀释剂流过放射状设置在第一稀释剂通道和第二稀释剂通道 第二燃料通道。

    COMBUSTOR NOZZLE AND METHOD FOR SUPPLYING FUEL TO A COMBUSTOR
    6.
    发明申请
    COMBUSTOR NOZZLE AND METHOD FOR SUPPLYING FUEL TO A COMBUSTOR 有权
    燃烧器喷嘴和向燃烧器供应燃料的方法

    公开(公告)号:US20120291447A1

    公开(公告)日:2012-11-22

    申请号:US13110256

    申请日:2011-05-18

    IPC分类号: F02C7/22

    摘要: A combustor nozzle includes a first and second liquid fuel passages that terminate at first and second fuel ports. A first diluent passage terminates at a first diluent outlet radially surrounding the second fuel ports. A second diluent passage terminates at a second diluent outlet between the first diluent outlet and the second fuel ports. A third diluent passage surrounds at least a portion of the first and second diluent passages. A method for supplying fuel to a combustor includes flowing a liquid fuel through a first fuel passage and flowing an emulsified liquid fuel through a second fuel passage. The method further includes flowing a first diluent through a shroud surrounding the second fuel passage to a first diluent passage surrounding at least a portion of the second fuel passage and flowing a second diluent through a second diluent passage radially disposed between the first diluent passage and the second fuel passage.

    摘要翻译: 燃烧器喷嘴包括在第一和第二燃料端口处终止的第一和第二液体燃料通道。 第一稀释剂通道终止于径向围绕第二燃料端口的第一稀释剂出口。 第二稀释剂通道在第一稀释剂出口和第二燃料端口之间终止于第二稀释剂出口。 第三稀释剂通道围绕第一和第二稀释剂通道的至少一部分。 用于向燃烧器供应燃料的方法包括使液体燃料流过第一燃料通道并使乳化液体燃料流过第二燃料通道。 该方法还包括使第一稀释剂流过围绕第二燃料通道的护罩到围绕第二燃料通道的至少一部分的第一稀释剂通道,并使第二稀释剂流过放射状设置在第一稀释剂通道和第二稀释剂通道 第二燃料通道。

    FUEL DISTRIBUTION MANIFOLD
    7.
    发明申请
    FUEL DISTRIBUTION MANIFOLD 有权
    燃油分配管理

    公开(公告)号:US20130167954A1

    公开(公告)日:2013-07-04

    申请号:US13342497

    申请日:2012-01-03

    IPC分类号: F16L41/00

    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。

    FUEL NOZZLE AND METHOD FOR OPERATING A COMBUSTOR
    8.
    发明申请
    FUEL NOZZLE AND METHOD FOR OPERATING A COMBUSTOR 有权
    燃油喷嘴和操作燃烧器的方法

    公开(公告)号:US20120266604A1

    公开(公告)日:2012-10-25

    申请号:US13449695

    申请日:2012-04-18

    IPC分类号: F02C7/22 F23D14/48 F02C7/264

    摘要: A fuel nozzle and a method for operating a combustor are disclosed. The method includes flowing a fuel and an oxidizer through a fuel nozzle, the fuel nozzle comprising an inner tube, an intermediate tube, and an outer tube each configured for flowing one of the fuel or the oxidizer therethrough. At least one of the inner tube, the intermediate tube, or the outer tube includes a plurality of swirler vanes. The method further includes imparting a swirl to the fuel and the oxidizer in the fuel nozzle, and exhausting the fuel and the oxidizer from the fuel nozzle into a combustion zone.

    摘要翻译: 公开了燃料喷嘴和操作燃烧器的方法。 该方法包括使燃料和氧化剂流过燃料喷嘴,燃料喷嘴包括内管,中间管和外管,每个都配置成使燃料或氧化剂之一流过其中。 内管,中间管或外管中的至少一个包括多个旋流叶片。 该方法还包括向燃料喷嘴中的燃料和氧化剂施加漩涡,并将燃料和氧化剂从燃料喷嘴排出到燃烧区中。

    Fuel nozzle and method for operating a combustor
    9.
    发明授权
    Fuel nozzle and method for operating a combustor 有权
    燃料喷嘴和操作燃烧器的方法

    公开(公告)号:US09500369B2

    公开(公告)日:2016-11-22

    申请号:US13449695

    申请日:2012-04-18

    摘要: A fuel nozzle and a method for operating a combustor are disclosed. The method includes flowing a fuel and an oxidizer through a fuel nozzle, the fuel nozzle comprising an inner tube, an intermediate tube, and an outer tube each configured for flowing one of the fuel or the oxidizer therethrough. At least one of the inner tube, the intermediate tube, or the outer tube includes a plurality of swirler vanes. The method further includes imparting a swirl to the fuel and the oxidizer in the fuel nozzle, and exhausting the fuel and the oxidizer from the fuel nozzle into a combustion zone.

    摘要翻译: 公开了燃料喷嘴和操作燃烧器的方法。 该方法包括使燃料和氧化剂流过燃料喷嘴,燃料喷嘴包括内管,中间管和外管,每个都配置成使燃料或氧化剂之一流过其中。 内管,中间管或外管中的至少一个包括多个旋流叶片。 该方法还包括向燃料喷嘴中的燃料和氧化剂施加漩涡,并将燃料和氧化剂从燃料喷嘴排出到燃烧区中。

    METHOD OF OPERATING A COMBUSTOR FROM A LIQUID FUEL TO A GAS FUEL OPERATION
    10.
    发明申请
    METHOD OF OPERATING A COMBUSTOR FROM A LIQUID FUEL TO A GAS FUEL OPERATION 有权
    将燃料从液体燃料运送到燃油运行的方法

    公开(公告)号:US20130227956A1

    公开(公告)日:2013-09-05

    申请号:US13412110

    申请日:2012-03-05

    IPC分类号: F02C3/24 F02C3/30

    摘要: A method of operating a combustor having a central nozzle and a plurality of outer nozzles surrounding the central nozzle is provided. The method includes providing a liquid fuel to only the plurality of outer nozzles at a specified total energy input. The method includes decreasing the liquid fuel to the plurality of outer nozzles while simultaneously increasing a gas fuel to the central nozzle and the plurality of outer nozzles to substantially maintain the specified total energy input. The method includes supplying a fuel-air ratio of the gas fuel to the central nozzle that exceeds a threshold value such that a central nozzle flame is anchored. An air-fuel ratio of the gas fuel to the plurality of outer nozzles is less than the threshold value such that a plurality of outer nozzle flames are lifted until a purge flow is supplied to the outer nozzles.

    摘要翻译: 提供一种操作具有中心喷嘴和围绕中心喷嘴的多个外喷嘴的燃烧器的方法。 该方法包括以指定的总能量输入仅向多个外部喷嘴提供液体燃料。 该方法包括将液体燃料减少到多个外部喷嘴,同时将气体燃料同时增加到中心喷嘴和多个外部喷嘴以基本维持指定的总能量输入。 该方法包括将中央喷嘴的气体燃料的燃料空气比提供超过阈值,使得中心喷嘴火焰被锚定。 气体燃料与多个外部喷嘴的空燃比小于阈值,使得多个外部喷嘴火焰被提升直到向外部喷嘴供应净化流。