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    COMBUSTOR ASSEMBLY FOR USE IN A TURBINE ENGINE AND METHODS OF ASSEMBLING SAME
    2.
    发明申请
    COMBUSTOR ASSEMBLY FOR USE IN A TURBINE ENGINE AND METHODS OF ASSEMBLING SAME 审中-公开
    用于涡轮发动机的燃烧器组件及其装配方法

    公开(公告)号：US20120324898A1

    公开(公告)日：2012-12-27

    申请号：US13164948

    申请日：2011-06-21

    申请人： Kevin Weston McMahan ,  Ronald James Chila ,  David Richard Johns

    发明人： Kevin Weston McMahan ,  Ronald James Chila ,  David Richard Johns

    IPC分类号： F23R3/02 ,  B21D53/00 ,  F02C3/00

    CPC分类号： F23R3/002 ,  F01D9/023 ,  F23R3/425 ,  F23R2900/03044 ,  Y10T29/49348

    摘要： A combustor assembly for use with a turbine engine that includes a rotor assembly. The combustor assembly includes a casing that includes a plenum and a combustor liner that is spaced a distance from the plenum and that defines a combustion chamber therein. A transition nozzle extends between the combustor liner and the rotor assembly for channeling combustion gases from the combustion chamber to the rotor assembly. The transition nozzle includes a transition portion and a nozzle portion integrally formed with the transition portion. An annular flowsleeve is coupled radially outward from the transition nozzle such that an annular flow path is defined between the flowsleeve and the transition nozzle. The flowsleeve includes a plurality of openings extending through an outer surface of the flowsleeve for providing flow communication between the plenum and the annular flow path to facilitate impingement cooling of the flowsleeve.

    摘要翻译： 一种与包括转子组件的涡轮发动机一起使用的燃烧器组件。 燃烧器组件包括壳体，其包括气室和与集气室隔开一定距离且在其中限定燃烧室的燃烧器衬套。 过渡喷嘴在燃烧器衬套和转子组件之间延伸，用于将燃烧气体从燃烧室引导至转子组件。 过渡喷嘴包括过渡部分和与过渡部分一体形成的喷嘴部分。 环形流动体从过渡喷嘴径向向外耦合，使得在流动流体和过渡喷嘴之间限定环形流动路径。 流动通道包括延伸穿过流动的外表面的多个开口，用于提供气室与环形流路之间的流动连通，以便于流动的冲击冷却。

    EFFUSION COOLED ONE-PIECE CAN COMBUSTOR
    8.
    发明申请
    EFFUSION COOLED ONE-PIECE CAN COMBUSTOR 有权
    有效冷却单罐CAN COMBUSTOR

    公开(公告)号：US20100218502A1

    公开(公告)日：2010-09-02

    申请号：US12395739

    申请日：2009-03-02

    申请人： Ronald James Chila ,  Kevin Weston McMahan

    发明人： Ronald James Chila ,  Kevin Weston McMahan

    IPC分类号： F23R3/42

    CPC分类号： F23R3/06 ,  F23R3/002 ,  F23R3/005 ,  F23R3/46 ,  F23R2900/03041

    摘要： A combustor for an industrial turbine includes a single transition piece transitioning directly from a combustor head-end to a turbine inlet. The transition piece includes an inner surface and an outer surface. The inner surface bounds an interior space for combusted gas flow from the combustor head-end to the turbine inlet. The outer surface at least partially defines an area for compressor discharge air flow. The transition piece includes a plurality of apertures configured to allow compressor discharge air flow into the interior space. Each of the plurality of apertures extends from an entry portion on the outer surface to an exit portion on the inner surface.

    摘要翻译： 用于工业涡轮机的燃烧器包括直接从燃烧器头端转换到涡轮机入口的单个过渡件。 过渡件包括内表面和外表面。 内表面限定用于从燃烧器头端到涡轮机入口的燃烧气体流的内部空间。 外表面至少部分地限定用于压缩机排出气流的区域。 过渡件包括多个孔，其构造成允许压缩机排出空气流入内部空间。 多个孔中的每一个从外表面上的入口部分延伸到内表面上的出口部分。

    High temperature seal for a turbine engine
    10.
    发明授权
    High temperature seal for a turbine engine 有权
    涡轮发动机的高温密封

    公开(公告)号：US08322976B2

    公开(公告)日：2012-12-04

    申请号：US12098860

    申请日：2008-04-07

    申请人： Ronald James Chila ,  Kevin Weston McMahan ,  Timur Repikov

    发明人： Ronald James Chila ,  Kevin Weston McMahan ,  Timur Repikov

    IPC分类号： F04D29/04

    CPC分类号： F01D9/023 ,  F01D11/005 ,  F02C7/28 ,  F05D2240/57 ,  F16J15/0887 ,  F16J15/104

    摘要： A turbine includes a static member, a moveable member fluidly connected to the static member, and a flexible seal. The flexible seal includes a spring component having a base section mounted to one of the static member and the moveable member of the turbine and a plurality of biasing members. Each of the plurality of biasing members includes a first portion extending from the base section and a cantilevered portion. The flexible seal further includes a seal component provided on the cantilevered portion of each of the plurality of biasing members. The seal component is biased into contact with the other of the static member and the moveable member.

    摘要翻译： 涡轮机包括静态构件，流体连接到静止构件的可动构件和柔性密封件。 柔性密封件包括弹簧部件，其具有安装到涡轮机的静止部件和可移动部件之一的基部以及多个偏置部件。 多个偏置构件中的每一个包括从基部延伸的第一部分和悬臂部分。 柔性密封件还包括设置在多个偏置构件中的每一个的悬臂部分上的密封部件。 密封部件被偏置成与静止部件和可移动部件中的另一个接触。