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    COMBUSTOR STRUCTURE
    2.
    发明申请
    COMBUSTOR STRUCTURE 审中-公开
    COMBUSTOR结构

    公开(公告)号：US20100005804A1

    公开(公告)日：2010-01-14

    申请号：US12171386

    申请日：2008-07-11

    申请人： Wei Chen ,  David Martin Johnson ,  Ronald James Chila ,  Joseph Citeno

    发明人： Wei Chen ,  David Martin Johnson ,  Ronald James Chila ,  Joseph Citeno

    IPC分类号： F02C1/00

    CPC分类号： F23R3/16 ,  F01D9/023 ,  F23R3/002 ,  F23R2900/00014 ,  F23R2900/03044

    摘要： A combustor includes at least one combustor liner defining a combustion chamber capable of directing combustion products toward a turbine. At least one combustor sleeve is located outside of the combustion chamber and is capable of reducing a magnitude of acoustic waves in the combustion chamber. The at least one combustor liner and the at least one combustor sleeve define at least one flow channel therebetween. Further, a combustor includes at least one combustor liner defining a combustion chamber capable of directing combustion products toward turbomachinery. At least one combustor sleeve disposed outside of the combustion chamber and is capable of controlling distribution of fluid flow in the combustor to modify a uniformity of the fluid flow to the combustion chamber.

    摘要翻译： 燃烧器包括限定燃烧室的至少一个燃烧器衬套，其能够将燃烧产物引向涡轮。 至少一个燃烧器套筒位于燃烧室的外部，并且能够减小燃烧室中的声波的大小。 所述至少一个燃烧器衬套和所述至少一个燃烧器套筒在其间限定至少一个流动通道。 此外，燃烧器包括限定能够将燃烧产物引导到涡轮机械的燃烧室的至少一个燃烧器衬套。 至少一个燃烧器套筒设置在燃烧室的外部，并且能够控制燃烧器中的流体流动的分布，以改变流向燃烧室的流体的均匀性。

    Flow conditioner for use in gas turbine component in which combustion occurs
    5.
    发明授权
    Flow conditioner for use in gas turbine component in which combustion occurs 失效
    用于燃烧发生的燃气轮机部件的流量​​调节器

    公开(公告)号：US08387397B2

    公开(公告)日：2013-03-05

    申请号：US12360490

    申请日：2009-01-27

    申请人： Wei Chen ,  Ronald James Chila ,  Eric William King

    发明人： Wei Chen ,  Ronald James Chila ,  Eric William King

    IPC分类号： F02C1/00 ,  F02G3/00

    CPC分类号： F23R3/06 ,  F23R2900/03045

    摘要： A gas turbine component in which combustion occurs. The gas turbine component includes a liner, including a first surface facing a first space and a second surface facing a second space, the liner being interposed between the first and second spaces and having a through-hole defined therein extending from the first to the second surface by which incoming flows proceed from the first space and to the second space. At least the first surface is formed to flow condition the incoming flows to resist separating from sidewalls of the through-hole.

    摘要翻译： 燃烧发生的燃气轮机部件。 所述燃气涡轮机部件包括衬套，所述衬套包括面对第一空间的第一表面和面向第二空间的第二表面，所述衬垫插入在所述第一和第二空间之间，并且具有限定在其中的通孔，所述通孔从所述第一空间延伸到第二空间 输入流从第一空间和第二空间进入的表面。 至少第一表面形成为使进入的流动流动以抵抗与通孔的侧壁分离。

    FLOW CONDITIONER FOR USE IN GAS TURBINE COMPONENT IN WHICH COMBUSTION OCCURS
    6.
    发明申请
    FLOW CONDITIONER FOR USE IN GAS TURBINE COMPONENT IN WHICH COMBUSTION OCCURS 失效
    用于燃气燃烧的燃气涡轮机组件中的流量调节器

    公开(公告)号：US20100186416A1

    公开(公告)日：2010-07-29

    申请号：US12360490

    申请日：2009-01-27

    申请人： Wei Chen ,  Ronald James Chila ,  Eric William King

    发明人： Wei Chen ,  Ronald James Chila ,  Eric William King

    IPC分类号： F23R3/42

    CPC分类号： F23R3/06 ,  F23R2900/03045

    摘要： A gas turbine component in which combustion occurs. The gas turbine component includes a liner, including a first surface facing a first space and a second surface facing a second space, the liner being interposed between the first and second spaces and having a through-hole defined therein extending from the first to the second surface by which incoming flows proceed from the first space and to the second space. At least the first surface is formed to flow condition the incoming flows to resist separating from sidewalls of the through-hole.

    摘要翻译： 燃烧发生的燃气轮机部件。 所述燃气涡轮机部件包括衬套，所述衬套包括面对第一空间的第一表面和面向第二空间的第二表面，所述衬垫插入在所述第一和第二空间之间，并且具有限定在其中的通孔，所述通孔从所述第一空间延伸到第二空间 输入流从第一空间和第二空间进入的表面。 至少第一表面形成为使进入的流动流动以抵抗与通孔的侧壁分离。

    Combustor assembly for a turbine engine with enhanced cooling
    8.
    发明授权
    Combustor assembly for a turbine engine with enhanced cooling 有权
    用于具有增强冷却的涡轮发动机的燃烧器组件

    公开(公告)号：US08646276B2

    公开(公告)日：2014-02-11

    申请号：US12616304

    申请日：2009-11-11

    申请人： Lewis Berkley Davis, Jr. ,  Ronald James Chila

    发明人： Lewis Berkley Davis, Jr. ,  Ronald James Chila

    IPC分类号： F02C1/00

    CPC分类号： F23R3/005 ,  F23R3/06 ,  F23R3/54 ,  F23R2900/03043 ,  F23R2900/03044

    摘要： A combustor assembly for a turbine engine includes a combustor liner and a flow sleeve which surrounds the combustor liner. Compressed air flows through an annular space located between an outer surface of the combustor liner and an inner surface of the flow sleeve. A plurality of cooling holes are formed through the flow sleeve to allow compressed air to flow from a position outside the flow sleeve, through the cooling holes, and into the annular space. The height of the annular space may vary along the length of the combustor assembly. Thus, the flow sleeve may have reduced diameter portions which result in the height of the annular space being smaller in certain locations than at other locations along the length of the combustor assembly.

    摘要翻译： 用于涡轮发动机的燃烧器组件包括燃烧器衬套和围绕燃烧器衬套的流动套管。 压缩空气流过位于燃烧器衬套的外表面和流动套管的内表面之间的环形空间。 通过流动套筒形成多个冷却孔，以允许压缩空气从流动套筒外部的位置流过冷却孔并进入环形空间。 环形空间的高度可以沿着燃烧器组件的长度而变化。 因此，流动套管可以具有减小的直径部分，这导致环形空间的高度在某些位置比沿着燃烧器组件的长度的其它位置更小。

    Combustor having a flow sleeve
    10.
    发明授权
    Combustor having a flow sleeve 有权
    具有流动套筒的燃烧器

    公开(公告)号：US08359867B2

    公开(公告)日：2013-01-29

    申请号：US12756329

    申请日：2010-04-08

    申请人： Ronald James Chila ,  Martin Ronald Watts ,  Sheng-Yi Wu

    发明人： Ronald James Chila ,  Martin Ronald Watts ,  Sheng-Yi Wu

    IPC分类号： F02C1/00 ,  F02G3/00

    CPC分类号： F23R3/02 ,  F23R3/44 ,  F23R2900/03043

    摘要： A combustor is provided and includes a liner through which fluid fed from at least two injection points flows from a head end to an interior of a transition piece, a first one of the at least two injection points being axially proximate to a fluid impenetrable coupling between the liner and the transition piece and defining apertures disposed in fluid communication with a first passage leading to the head end, and a second one of the at least two injection points being disposed axially between the apertures and the head end and upstream from the apertures relative to a direction of fluid flow through the first passage, the second one of the at least two injection points being formed of openings disposed in fluid communication with a second passage leading to the head end.

    摘要翻译： 提供燃烧器并且包括衬套，通过所述衬套从至少两个注射点供给的流体从头端流动到过渡件的内部，所述至少两个注射点中的第一个轴向靠近液体不可穿透的联接 所述衬套和所述过渡件并且限定出孔设置成与通向所述头端的第一通道流体连通，并且所述至少两个注射点中的第二个注射点轴向地设置在所述孔和所述头部端部之间以及所述孔的相对上游 流体流过第一通道的方向，所述至少两个注射点中的第二个注射点由与通向头端的第二通道流体连通的开口形成。