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    Nozzle for a turbomachine
    1.
    发明授权
    Nozzle for a turbomachine 有权
    喷嘴用于涡轮机

    公开(公告)号：US08297059B2

    公开(公告)日：2012-10-30

    申请号：US12357638

    申请日：2009-01-22

    申请人： Benjamin Paul Lacy ,  Gilbert Otto Kraemer ,  Ertan Yilmaz ,  Patrick Benedict Melton

    发明人： Benjamin Paul Lacy ,  Gilbert Otto Kraemer ,  Ertan Yilmaz ,  Patrick Benedict Melton

    IPC分类号： F02C1/00 ,  F02G3/00

    CPC分类号： F23R3/286 ,  F23R3/14

    摘要： A turbomachine includes a compressor, a combustor operatively connected to the compressor, and an injection nozzle operatively connected to the combustor. The injection nozzle includes a main body having a first end section that extends to a second end section to define an inner flow path. The injection nozzle further includes an outlet arranged at the second end section of the main body, at least one passage that extends within the main body and is fluidly connected to the outlet, and at least one conduit extending between the inner flow path and the at least one passage.

    摘要翻译： 涡轮机包括压缩机，可操作地连接到压缩机的燃烧器和可操作地连接到燃烧器的喷射喷嘴。 注射喷嘴包括主体，其具有延伸到第二端部以限定内部流动路径的第一端部。 喷嘴还包括布置在主体的第二端部处的出口，至少一个在主体内延伸并且流体连接到出口的通道，以及至少一个在内部流动路径和在该流体通道之间延伸的导管 最少一个段落

    NOZZLE FOR A TURBOMACHINE
    2.
    发明申请
    NOZZLE FOR A TURBOMACHINE 有权
    涡轮喷嘴

    公开(公告)号：US20100180600A1

    公开(公告)日：2010-07-22

    申请号：US12357638

    申请日：2009-01-22

    申请人： Benjamin Paul Lacy ,  Gilbert Otto Kraemer ,  Ertan Yilmaz ,  Patrick Benedict Melton

    发明人： Benjamin Paul Lacy ,  Gilbert Otto Kraemer ,  Ertan Yilmaz ,  Patrick Benedict Melton

    IPC分类号： F02C7/22 ,  B05B7/04

    CPC分类号： F23R3/286 ,  F23R3/14

    摘要： A turbomachine includes a compressor, a combustor operatively connected to the compressor, and an injection nozzle operatively connected to the combustor. The injection nozzle includes a main body having a first end section that extends to a second end section to define an inner flow path. The injection nozzle further includes an outlet arranged at the second end section of the main body, at least one passage that extends within the main body and is fluidly connected to the outlet, and at least one conduit extending between the inner flow path and the at least one passage.

    摘要翻译： 涡轮机包括压缩机，可操作地连接到压缩机的燃烧器和可操作地连接到燃烧器的喷射喷嘴。 注射喷嘴包括主体，其具有延伸到第二端部以限定内部流动路径的第一端部。 喷嘴还包括布置在主体的第二端部处的出口，至少一个在主体内延伸并且流体连接到出口的通道，以及至少一个在内部流动路径和在该流体通道之间延伸的导管 最少一个段落

    METHODS AND SYSTEMS TO FACILITATE REDUCING FLASHBACK/FLAME HOLDING IN COMBUSTION SYSTEMS
    6.
    发明申请
    METHODS AND SYSTEMS TO FACILITATE REDUCING FLASHBACK/FLAME HOLDING IN COMBUSTION SYSTEMS 失效
    减少燃烧系统中的闪回/火焰控制的方法和系统

    公开(公告)号：US20090320484A1

    公开(公告)日：2009-12-31

    申请号：US11741483

    申请日：2007-04-27

    申请人： Benjamin Paul Lacy ,  Gilbert Otto Kraemer ,  Balachandar Varatharajan ,  Ertan Yilmaz ,  Baifang Zuo

    发明人： Benjamin Paul Lacy ,  Gilbert Otto Kraemer ,  Balachandar Varatharajan ,  Ertan Yilmaz ,  Baifang Zuo

    IPC分类号： F02C7/22 ,  F02C7/00 ,  B21D39/03

    CPC分类号： F23R3/10 ,  F23R3/14 ,  Y10T29/49826

    摘要： A method for assembling a premixing injector is provided. The method includes providing a centerbody including a center axis and a radially outer surface, and providing an inlet flow conditioner. The inlet flow conditioner includes a radially outer wall, a radially inner wall, and an end wall coupled substantially perpendicularly between the outer wall and the inner wall. Each of the outer wall and the end wall include a plurality of openings defined therein. The outer wall, the inner wall, and the end wall define a first passage therebetween. The method also includes coupling the inlet flow conditioner to the centerbody such that the inlet flow conditioner substantially circumscribes the centerbody, such that the inner wall is substantially parallel to the centerbody outer surface, and such that a second passage is defined between the centerbody outer surface and the inner wall.

    摘要翻译： 提供了一种组装预混喷射器的方法。 该方法包括提供包括中心轴线和径向外表面的中心体，并提供入口流动调节器。 入口流动调节器包括径向外壁，径向内壁和基本上垂直于外壁和内壁连接的端壁。 外壁和端壁中的每一个包括限定在其中的多个开口。 外壁，内壁和端壁在其间限定第一通道。 该方法还包括将入口流动调节器联接到中心体，使得入口流动调节器基本上限制中心体，使得内壁基本上平行于中心体外表面，并且使得第二通道限定在中心体外表面 和内壁。

    PREMIXING DEVICE FOR ENHANCED FLAMEHOLDING AND FLASH BACK RESISTANCE
    8.
    发明申请
    PREMIXING DEVICE FOR ENHANCED FLAMEHOLDING AND FLASH BACK RESISTANCE 审中-公开
    用于增强防火和防反射电阻的优先设备

    公开(公告)号：US20090139236A1

    公开(公告)日：2009-06-04

    申请号：US11946892

    申请日：2007-11-29

    申请人： Ertan Yilmaz ,  Balachandar Varatharajan ,  Gilbert Otto Kraemer ,  Benjamin Paul Lacy ,  Baifang Zuo

    发明人： Ertan Yilmaz ,  Balachandar Varatharajan ,  Gilbert Otto Kraemer ,  Benjamin Paul Lacy ,  Baifang Zuo

    IPC分类号： F23R3/42 ,  F02C1/00

    CPC分类号： F23R3/14 ,  F23R3/286

    摘要： A premixing device is provided. The premixing device includes a fuel inlet configured to introduce a fuel within the premixing device and an air inlet configured to introduce air within the premixing device. The premixing device also includes a plurality of swirler vanes configured to provide a swirl movement to the fuel and/or air to facilitate mixing of the fuel and air to form a gaseous pre-mix, wherein a shape of each of the plurality of swirler vanes is selected to control an axial velocity profile of the fuel and/or air within the premixing device.

    摘要翻译： 提供预混装置。 预混合装置包括配置成在预混合装置内引入燃料的燃料入口和配置成在预混合装置内引入空气的空气入口。 预混合装置还包括多个旋流器叶片，其构造成向燃料和/或空气提供涡流运动，以促进燃料和空气的混合以形成气态预混合物，其中多个旋流叶片 被选择以控制预混合装置内的燃料和/或空气的轴向速度分布。

    METHODS AND SYSTEMS TO FACILITATE OPERATING WITHIN FLAME-HOLDING MARGIN
    9.
    发明申请
    METHODS AND SYSTEMS TO FACILITATE OPERATING WITHIN FLAME-HOLDING MARGIN 审中-公开
    促进火焰控制操作的方法和系统

    公开(公告)号：US20080267783A1

    公开(公告)日：2008-10-30

    申请号：US11741454

    申请日：2007-04-27

    申请人： Gilbert Otto Kraemer ,  Benjamin Paul Lacy ,  Balachandar Varatharajan ,  Ertan Yilmaz

    发明人： Gilbert Otto Kraemer ,  Benjamin Paul Lacy ,  Balachandar Varatharajan ,  Ertan Yilmaz

    IPC分类号： F01D5/18

    CPC分类号： F23R3/14 ,  F02C9/40 ,  F23R3/286

    摘要： A method to facilitate controlling flame-holding margins in a turbine engine is provided. The method includes coupling at least one turbine nozzle segment within the turbine engine, wherein the at least one turbine nozzle segment includes at least one vane extending between an inner band and an outer band. The method also includes positioning at least one fuel injection orifice in a surface of the at least one vane, channeling a fuel through the at least one fuel injection orifice into a compressed fluid flow to establish a jet penetration height, and defining an operating window by adjusting an operating parameter of the fuel to reduce the jet penetration height and to facilitate reducing the flame-holding margins.

    摘要翻译： 提供了一种便于控制涡轮发动机中的火焰保持余量的方法。 该方法包括联接涡轮发动机内的至少一个涡轮喷嘴段，其中至少一个涡轮喷嘴段包括在内带和外带之间延伸的至少一个叶片。 该方法还包括将至少一个燃料喷射孔定位在至少一个叶片的表面中，将燃料通过至少一个燃料喷射孔引导到压缩流体流中以建立喷射穿透高度，并且通过 调整燃料的操作参数以减小喷射穿透高度并且有助于减少火焰保持余量。