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    Combustor assembly for a turbomachine
    4.
    发明授权
    Combustor assembly for a turbomachine 有权
    用于涡轮机的燃烧器组件

    公开(公告)号：US08281596B1

    公开(公告)日：2012-10-09

    申请号：US13108164

    申请日：2011-05-16

    申请人： Robert Joseph Rohrssen ,  Erich Daniel Charters ,  Abdul Rafey Khan ,  Patrick Benedict Melton ,  John Drake Vanselow

    发明人： Robert Joseph Rohrssen ,  Erich Daniel Charters ,  Abdul Rafey Khan ,  Patrick Benedict Melton ,  John Drake Vanselow

    IPC分类号： F23R3/14 ,  F02C3/14

    CPC分类号： F23R3/06 ,  F23D2900/14004 ,  F23R3/002 ,  F23R3/286 ,  F23R2900/00014 ,  F23R2900/03042

    摘要： A combustor assembly for a turbomachine includes combustor housing and a flow sleeve arranged between the combustor housing and a combustor liner. The flow sleeve defines a first annular fluid passage, and a second annular fluid passage. A quaternary cap is mounted to the combustor housing. The quaternary cap includes a first fluid plenum fluidly connected to the first annular fluid passage, a second fluid plenum fluidly connected to the second annular fluid passage, and a plurality of vanes fluidly connected to each of the first and second fluid plenums. Each of the plurality of vanes includes a body portion having a first fluid channel coupled to the first fluid plenum, and a second fluid channel coupled to the second fluid plenum. The first fluid channel extends completely through the body portion and the second fluid channel extends partially into the body portion.

    摘要翻译： 用于涡轮机的燃烧器组件包括燃烧器壳体和布置在燃烧器壳体和燃烧器衬套之间的流动套筒。 流动套管限定第一环形流体通道和第二环形流体通道。 四角帽安装在燃烧器壳体上。 四级盖包括流体连接到第一环形流体通道的第一流体增压室，与第二环形流体通道流体连接的第二流体室，以及与第一和第二流体通道中的每一个流体连接的多个叶片。 多个叶片中的每一个包括主体部分，其具有联接到第一流体增压室的第一流体通道和联接到第二流体增压室的第二流体通道。 第一流体通道完全延伸穿过主体部分，并且第二流体通道部分地延伸到主体部分中。

    SYSTEM FOR CONDITIONING FLOW THROUGH A COMBUSTOR
    5.
    发明申请
    SYSTEM FOR CONDITIONING FLOW THROUGH A COMBUSTOR 审中-公开
    通过燃烧器调节流量的系统

    公开(公告)号：US20120305670A1

    公开(公告)日：2012-12-06

    申请号：US13153531

    申请日：2011-06-06

    申请人： Luis Manuel Flamand ,  Kwanwoo Kim ,  Patrick Benedict Melton

    发明人： Luis Manuel Flamand ,  Kwanwoo Kim ,  Patrick Benedict Melton

    IPC分类号： B05B1/26

    CPC分类号： F23R3/10 ,  F23D14/82 ,  F23D2209/10 ,  F23R3/46

    摘要： A system for conditioning flow through a combustor includes a nozzle, and a shroud circumferentially surrounds at least a portion of the nozzle. The shroud defines an upstream opening, and a plurality of vanes extends radially inward from the shroud. A circumferential slot extends through the shroud between the upstream opening and the plurality of vanes.

    摘要翻译： 用于调节通过燃烧器的流动的系统包括喷嘴，并且护罩周向地围绕喷嘴的至少一部分。 护罩限定上游开口，并且多个叶片从护罩径向向内延伸。 周向狭槽在上游开口和多个叶片之间延伸穿过护罩。

    Gas turbine combustor endcover assembly with integrated flow restrictor and manifold seal
    6.
    发明授权
    Gas turbine combustor endcover assembly with integrated flow restrictor and manifold seal 有权
    具有集成流量限制器和歧管密封件的燃气轮机燃烧器整流器组件

    公开(公告)号：US08820086B2

    公开(公告)日：2014-09-02

    申请号：US13008399

    申请日：2011-01-18

    申请人： Donald Mark Bailey ,  Donald Timothy Lemon ,  Kwanwoo Kim ,  Patrick Benedict Melton

    发明人： Donald Mark Bailey ,  Donald Timothy Lemon ,  Kwanwoo Kim ,  Patrick Benedict Melton

    IPC分类号： F02C1/00

    CPC分类号： F23R3/283 ,  F23K5/14 ,  F23K2900/05142 ,  F23R2900/00005 ,  F23R2900/00012

    摘要： An endcover assembly for a turbine combustor adapted to support one or more combustor nozzles includes a substantially flat plate having one side which in use, faces a combustion chamber and an opposite side which, in use, faces away from the combustion chamber. At least one fuel passage extends through the substantially flat plate. A fuel manifold porting block is secured to the opposite side of the flat plate with at least one port aligned with the at least one passage. A fuel restrictor insert formed with multiple flow orifices is located between the flat plate and the fuel manifold porting block in alignment with the at least one fuel passage and the at least one port.

    摘要翻译： 适于支撑一个或多个燃烧器喷嘴的用于涡轮机燃烧器的封盖组件包括基本平坦的板，其具有一个侧面，其在使用中面向燃烧室，在使用中相对侧面远离燃烧室。 至少一个燃料通道延伸穿过基本平坦的板。 燃料歧管移动块被固定到平板的相对侧，其中至少一个端口与至少一个通道对准。 形成有多个流动孔的燃料限制器插件位于平板和燃料歧管移动块之间，与至少一个燃料通道和至少一个端口对准。