Flow conditioner for use in gas turbine component in which combustion occurs
    1.
    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

    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
    2.
    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

    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 STRUCTURE
    5.
    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

    IPC分类号: F02C1/00

    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。

    Mug
    10.
    外观设计
    Mug 有权

    公开(公告)号:USD962002S1

    公开(公告)日:2022-08-30

    申请号:US29808797

    申请日:2021-09-23

    申请人: Wei Chen

    设计人: Wei Chen