Fuel/air mixing system for fuel nozzle

    公开(公告)号:US10415479B2

    公开(公告)日:2019-09-17

    申请号:US15058418

    申请日:2016-03-02

    Abstract: A fuel nozzle includes an inner wall defining a central passage extending in an axial direction of the fuel nozzle, a hub wall surrounding the inner wall and defining a first annular passage, an outer wall surrounding the hub wall and defining a second annular passage, and a shroud surrounding the outer wall and defining a third annular passage. A swirler may receive air and direct the air into the first annular passage. The swirler includes at least one swirl vane extending from the shroud to the hub wall that has an air passage extending between the shroud and the hub wall. The air passage is coupled to the first annular passage and has a first width adjacent the shroud and a second width adjacent the hub wall. The second width is larger than the first width defining a diverging outlet into the first annular passage.

    PREMIXER WITH DILUENT FLUID AND FUEL TUBES HAVING CHEVRON OUTLETS
    2.
    发明申请
    PREMIXER WITH DILUENT FLUID AND FUEL TUBES HAVING CHEVRON OUTLETS 审中-公开
    具有液体流体的优先和具有CHEVRON出口的燃油管

    公开(公告)号:US20140144141A1

    公开(公告)日:2014-05-29

    申请号:US13684906

    申请日:2012-11-26

    CPC classification number: F23R3/286 F23C2202/10 F23L7/00 F23L2900/07002

    Abstract: A premixer includes an air tube formed in a burner tube defining a longitudinal axis, and a coaxially disposed fuel tube with a turbulence enhancing chevron outlet. The fuel tube may include an exterior tube and an interior tube with the interior tube, the exterior tube or both having chevron outlets. The chevron outlets may be tapered and notched.

    Abstract translation: 预混合器包括形成在限定纵向轴线的燃烧器管中的空气管和具有湍流增强人字形出口的同轴布置的燃料管。 燃料管可以包括外管和具有内管,外管或两者都具有人字形出口的内管。 人字形出口可以是锥形和凹口。

    ANNULAR PREMIXED PILOT IN FUEL NOZZLE
    3.
    发明申请
    ANNULAR PREMIXED PILOT IN FUEL NOZZLE 审中-公开
    燃油喷嘴中的ANNULAR PREMIXED PILOT

    公开(公告)号:US20150253011A1

    公开(公告)日:2015-09-10

    申请号:US14719356

    申请日:2015-05-22

    Abstract: A combustor for a gas turbine engine has a head end portion that carries at least one fuel/air nozzle. Each fuel/air nozzle includes a premixed pilot nozzle having premix conduits where each premix conduit has an upstream end defining an opening and having a central axis and downstream end defining an outlet and having a central axis where the central axis of the downstream end is non-parallel with a central axis of a center body of the fuel/air nozzle. The premixed pilot nozzle can include an annular channel disposed radially outwardly from the premix conduits and may include air jets that direct air radially outwardly from the premix conduits.

    Abstract translation: 用于燃气涡轮发动机的燃烧器具有承载至少一个燃料/空气喷嘴的头端部分。 每个燃料/空气喷嘴包括具有预混合管道的预混合先导喷嘴,其中每个预混管道具有限定开口的上游端,并且具有中心轴线和下游端限定出口,并且具有中心轴线,其中下游端的中心轴线不是 与燃料/空气喷嘴的中心体的中心轴平行。 预混合引导喷嘴可以包括从预混合管道径向向外设置的环形通道,并且可以包括从预混管道径向向外引导空气的空气射流。

    Premixer With Fuel Tubes Having Chevron Outlets
    4.
    发明申请
    Premixer With Fuel Tubes Having Chevron Outlets 审中-公开
    具有燃料管的预混合器具有雪佛龙出口

    公开(公告)号:US20140144152A1

    公开(公告)日:2014-05-29

    申请号:US13684891

    申请日:2012-11-26

    CPC classification number: F02C7/22 F23D14/48 F23D14/62 F23R3/286

    Abstract: A premixer includes an air tube formed in a burner tube defining a longitudinal axis, and a coaxially disposed fuel tube with a turbulence enhancing chevron outlet. The fuel tube may include an exterior tube and an interior tube with the interior tube, the exterior tube or both having chevron outlets. The chevron outlets may be tapered and notched.

    Abstract translation: 预混合器包括形成在限定纵向轴线的燃烧器管中的空气管和具有湍流增强人字纹出口的同轴布置的燃料管。 燃料管可以包括外管和具有内管,外管或两者都具有人字形出口的内管。 人字形出口可以是锥形和凹口。

    FUEL/AIR MIXING SYSTEM FOR FUEL NOZZLE
    5.
    发明申请
    FUEL/AIR MIXING SYSTEM FOR FUEL NOZZLE 有权
    用于燃油喷嘴的燃油/空气混合系统

    公开(公告)号:US20140238036A1

    公开(公告)日:2014-08-28

    申请号:US13776620

    申请日:2013-02-25

    Abstract: A fuel nozzle includes an inner wall defining a central passage extending in an axial direction of the fuel nozzle, a hub wall surrounding the inner wall and defining a first annular passage, an outer wall surrounding the hub wall and defining a second annular passage, and a shroud surrounding the outer wall and defining a third annular passage. A swirler may receive air and direct the air into the first annular passage. The swirler includes at least one swirl vane extending from the shroud to the hub wall that has an air passage extending between the shroud and the hub wall. The air passage is coupled to the first annular passage and has a first width adjacent the shroud and a second width adjacent the hub wall. The second width is larger than the first width defining a diverging outlet into the first annular passage.

    Abstract translation: 燃料喷嘴包括限定沿着燃料喷嘴的轴向方向延伸的中心通道的内壁,围绕内壁并限定第一环形通道的毂壁,围绕毂壁并限定第二环形通道的外壁,以及 围绕外壁并限定第三环形通道的护罩。 旋流器可以接收空气并将空气引导到第一环形通道中。 旋流器包括从护罩延伸到毂壁的至少一个旋流叶片,其具有在护罩和轮毂壁之间延伸的空气通道。 空气通道联接到第一环形通道并且具有与护罩相邻的第一宽度和邻近轮毂壁的第二宽度。 第二宽度大于限定到第一环形通道的发散出口的第一宽度。

    FUEL/AIR MIXING SYSTEM FOR FUEL NOZZLE
    6.
    发明申请
    FUEL/AIR MIXING SYSTEM FOR FUEL NOZZLE 审中-公开
    用于燃油喷嘴的燃油/空气混合系统

    公开(公告)号:US20140238025A1

    公开(公告)日:2014-08-28

    申请号:US13776638

    申请日:2013-02-25

    CPC classification number: F23R3/286 F23R3/14

    Abstract: A system includes a fuel nozzle. The fuel nozzle includes a central hub with a first annular passage extending along a longitudinal axis of the fuel nozzle. A flow conditioner is disposed along the first annular passage. The flow conditioner includes at least one of a straightening vane, a mesh screen, or a multi-passage body having multiple passages generally parallel with the longitudinal axis. An outer shroud is disposed about the central hub to define a second annular passage extending along the longitudinal axis of the fuel nozzle.

    Abstract translation: 系统包括燃料喷嘴。 燃料喷嘴包括具有沿着燃料喷嘴的纵向轴线延伸的第一环形通道的中心毂。 流动调节器沿着第一环形通道设置。 流动调节器包括矫直叶片,筛网或具有多个与纵向轴线平行的多个通道的多通道体中的至少一个。 围绕中心毂布置外护罩以限定沿着燃料喷嘴的纵向轴线延伸的第二环形通道。

    SYSTEM FOR REDUCING COMBUSTION DYNAMICS AND NOx IN A COMBUSTOR
    7.
    发明申请
    SYSTEM FOR REDUCING COMBUSTION DYNAMICS AND NOx IN A COMBUSTOR 有权
    减少燃烧动力学和NOx排放的系统

    公开(公告)号:US20140157779A1

    公开(公告)日:2014-06-12

    申请号:US13709320

    申请日:2012-12-10

    Abstract: A combustor includes an end cap that extends radially across at least a portion of the combustor. The end cap includes an upstream surface axially separated from a downstream surface. A plurality of tubes extend from the upstream surface through the downstream surface of the end cap to provide fluid communication through the end cap. Each tube in a first set of the plurality of tubes has an inlet proximate to the upstream surface and an outlet downstream from the downstream surface. Each outlet has a first portion that extends a different axial distance from the inlet than a second portion.

    Abstract translation: 燃烧器包括沿着燃烧器的至少一部分径向延伸的端盖。 端盖包括从下游表面轴向分离的上游表面。 多个管从上游表面延伸通过端盖的下游表面以提供通过端盖的流体连通。 多个管的第一组中的每个管具有靠近上游表面的入口和从下游表面下游的出口。 每个出口具有第一部分,该第一部分与第二部分相比延伸与入口不同的轴向距离。

    FUEL/AIR MIXING SYSTEM FOR FUEL NOZZLE
    8.
    发明申请
    FUEL/AIR MIXING SYSTEM FOR FUEL NOZZLE 有权
    用于燃油喷嘴的燃油/空气混合系统

    公开(公告)号:US20160177837A1

    公开(公告)日:2016-06-23

    申请号:US15058418

    申请日:2016-03-02

    Abstract: A fuel nozzle includes an inner wall defining a central passage extending in an axial direction of the fuel nozzle, a hub wall surrounding the inner wall and defining a first annular passage, an outer wall surrounding the hub wall and defining a second annular passage, and a shroud surrounding the outer wall and defining a third annular passage. A swirler may receive air and direct the air into the first annular passage. The swirler includes at least one swirl vane extending from the shroud to the hub wall that has an air passage extending between the shroud and the hub wall. The air passage is coupled to the first annular passage and has a first width adjacent the shroud and a second width adjacent the hub wall. The second width is larger than the first width defining a diverging outlet into the first annular passage.

    Abstract translation: 燃料喷嘴包括限定沿着燃料喷嘴的轴向方向延伸的中心通道的内壁,围绕内壁并限定第一环形通道的毂壁,围绕毂壁并限定第二环形通道的外壁,以及 围绕外壁并限定第三环形通道的护罩。 旋流器可以接收空气并将空气引导到第一环形通道中。 旋流器包括从护罩延伸到毂壁的至少一个旋流叶片,其具有在护罩和轮毂壁之间延伸的空气通道。 空气通道联接到第一环形通道并且具有与护罩相邻的第一宽度和邻近轮毂壁的第二宽度。 第二宽度大于限定到第一环形通道的发散出口的第一宽度。

    System for reducing combustion dynamics and NOx in a combustor
    9.
    发明授权
    System for reducing combustion dynamics and NOx in a combustor 有权
    用于减少燃烧器中的燃烧动力学和NOx的系统

    公开(公告)号:US09353950B2

    公开(公告)日:2016-05-31

    申请号:US13709320

    申请日:2012-12-10

    Abstract: A combustor includes an end cap that extends radially across at least a portion of the combustor. The end cap includes an upstream surface axially separated from a downstream surface. A plurality of tubes extend from the upstream surface through the downstream surface of the end cap to provide fluid communication through the end cap. Each tube in a first set of the plurality of tubes has an inlet proximate to the upstream surface and an outlet downstream from the downstream surface. Each outlet has a first portion that extends a different axial distance from the inlet than a second portion.

    Abstract translation: 燃烧器包括沿着燃烧器的至少一部分径向延伸的端盖。 端盖包括从下游表面轴向分离的上游表面。 多个管从上游表面延伸通过端盖的下游表面以提供通过端盖的流体连通。 多个管的第一组中的每个管具有靠近上游表面的入口和从下游表面下游的出口。 每个出口具有第一部分,该第一部分与第二部分相比延伸与入口不同的轴向距离。

    Fuel/air mixing system for fuel nozzle
    10.
    发明授权
    Fuel/air mixing system for fuel nozzle 有权
    燃油喷嘴燃油/空气混合系统

    公开(公告)号:US09297535B2

    公开(公告)日:2016-03-29

    申请号:US13776620

    申请日:2013-02-25

    Abstract: A fuel nozzle includes an inner wall defining a central passage extending in an axial direction of the fuel nozzle, a hub wall surrounding the inner wall and defining a first annular passage, an outer wall surrounding the hub wall and defining a second annular passage, and a shroud surrounding the outer wall and defining a third annular passage. A swirler may receive air and direct the air into the first annular passage. The swirler includes at least one swirl vane extending from the shroud to the hub wall that has an air passage extending between the shroud and the hub wall. The air passage is coupled to the first annular passage and has a first width adjacent the shroud and a second width adjacent the hub wall. The second width is larger than the first width defining a diverging outlet into the first annular passage.

    Abstract translation: 燃料喷嘴包括限定沿着燃料喷嘴的轴向方向延伸的中心通道的内壁,围绕内壁并限定第一环形通道的毂壁,围绕毂壁并限定第二环形通道的外壁,以及 围绕外壁并限定第三环形通道的护罩。 旋流器可以接收空气并将空气引导到第一环形通道中。 旋流器包括从护罩延伸到毂壁的至少一个旋流叶片,其具有在护罩和轮毂壁之间延伸的空气通道。 空气通道联接到第一环形通道并且具有与护罩相邻的第一宽度和邻近轮毂壁的第二宽度。 第二宽度大于限定到第一环形通道的发散出口的第一宽度。

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