INLET AIR FILTRATION SYSTEM
    14.
    发明申请
    INLET AIR FILTRATION SYSTEM 有权
    入口空气过滤系统

    公开(公告)号:US20120000168A1

    公开(公告)日:2012-01-05

    申请号:US12826727

    申请日:2010-06-30

    IPC分类号: B01D50/00

    摘要: Embodiments of the present invention provide an inertial filtration system for air-ingesting machines. The inertial filter 100 may comprise a reducer 133 downstream of a vortex generator. The reducer 133 decreases the area that the airstream flows through, which may increase the angular momentum and the centrifugal forces acting on the particles of the ingested airstream. This may increase the cleaning performance and a decrease in the pressure drop across the inertial filter 100. Generally, the inertial filter functions such that flow components of higher density are separated from the rest of the airstream. The higher density flow components are bled out of the inertial filter 100 via an outlet 135. The remaining flow components flow downstream to compressor section 535.

    摘要翻译: 本发明的实施例提供一种用于吸气机的惯性过滤系统。 惯性过滤器100可以包括在涡流发生器下游的减速器133。 减速器133减少气流流过的面积,这可能增加作用在被摄取的气流的颗粒上的角动量和离心力。 这可能增加清洁性能并降低穿过惯性过滤器100的压降。通常,惯性过滤器起作用,使得较高密度的流动分量与气流的其余部分分离。 较高密度的流动部件经由出口135从惯性过滤器100排出。剩余的流动组分在下游流到压缩机部分535。

    Quick disconnect combustion endcover
    15.
    发明授权
    Quick disconnect combustion endcover 有权
    快速断开燃烧端盖

    公开(公告)号:US09267691B2

    公开(公告)日:2016-02-23

    申请号:US13342629

    申请日:2012-01-03

    IPC分类号: F23R3/60 F16B2/06

    摘要: A clamp assembly for facilitating attachment and removal of a first component to or from a second component includes plural clamp bodies, each having at least two mutually perpendicular surfaces arranged about the first component. A substantially rigid ring is located between one surface of the clamp body and a surface of the first component. At least one fastener is provided for each of the plural clamp bodies, adapted to extend through a respective one of the plural clamp bodies and into the second component. Tooling is provided to allow for simultaneous tightening or loosening of all bolts on a single combustor.

    摘要翻译: 用于有助于将第一部件附接到第二部件或从第二部件移除的夹具组件包括多个夹具体,每个夹具体具有围绕第一部件布置的至少两个相互垂直的表面。 基本刚性的环位于夹具主体的一个表面和第一部件的表面之间。 为多个夹具体中的每一个提供至少一个紧固件,其适于延伸穿过多个夹具本体中的相应一个并进入第二部件。 提供模具以允许在单个燃烧器上同时拧紧或松开所有螺栓。

    MOISTURE DIVERSION APPARATUS FOR AIR INLET SYSTEM AND METHOD
    18.
    发明申请
    MOISTURE DIVERSION APPARATUS FOR AIR INLET SYSTEM AND METHOD 失效
    用于空气入口系统和方法的湿度分流装置

    公开(公告)号:US20120199001A1

    公开(公告)日:2012-08-09

    申请号:US13022020

    申请日:2011-02-07

    IPC分类号: B01D50/00 B01D46/00 B01D45/00

    CPC分类号: B01D45/08

    摘要: A moisture diversion system for a gas turbine inlet. The moisture diversion system comprises a housing that is operably connected with a gas turbine and defines an opening through which air flows to the gas turbine. A hood is attached to the housing adjacent the opening. The hood has a surface disposed at an acute angle relative to horizontal. A device is disposed relative to the hood to separate moisture from air flowing through the device. Separated moisture is directed onto the hood. A gutter is disposed adjacent an edge of the hood to collect moisture from the hood. A conduit is fluidly connected with the gutter to conduct water away from the gutter and the opening in the housing to inhibit separated moisture from re-entering the air flow through the opening to the gas turbine.

    摘要翻译: 用于燃气轮机入口的湿气分配系统。 湿气分配系统包括壳体,其与燃气涡轮机可操作地连接并限定空气流过燃气轮机的开口。 在靠近开口的情况下将罩附接到壳体。 罩具有相对于水平面成锐角设置的表面。 设备相对于机罩设置,以将水分与流过设备的空气分离。 分离的水分被引导到罩上。 靠近罩的边缘设置沟槽以从罩收集水分。 导管与沟槽流体连接以将水远离沟槽和壳体中的开口,以防止分离的水分重新进入通过燃气涡轮机的开口的空气流。

    SYSTEM FOR CONTROLLING FUEL SUPPLY FOR A GAS TURBINE ENGINE
    19.
    发明申请
    SYSTEM FOR CONTROLLING FUEL SUPPLY FOR A GAS TURBINE ENGINE 审中-公开
    用于控制燃气涡轮发动机燃料供应的系统

    公开(公告)号:US20120192542A1

    公开(公告)日:2012-08-02

    申请号:US13015518

    申请日:2011-01-27

    IPC分类号: F02C3/20

    CPC分类号: F02C9/40 F05D2260/80

    摘要: A system includes a turbine fuel controller configured to control a first supply of a first fuel to a turbine engine, a second supply of a second fuel to the turbine engine, and a transition between the first fuel and the second fuel. The turbine fuel controller includes a fuel integrity control logic configured to control a volume of the first fuel in a first fuel line to maintain a first fuel integrity while the turbine engine is operating on the second fuel rather than the first fuel.

    摘要翻译: 一种系统包括:涡轮燃料控制器,其被配置为控制向涡轮发动机的第一燃料的第一供应,到所述涡轮发动机的第二燃料的第二供应以及所述第一燃料和所述第二燃料之间的转变。 涡轮燃料控制器包括燃料完整性控制逻辑,该燃料完整性控制逻辑被配置为在第一燃料管线中控制第一燃料的体积以在涡轮发动机在第二燃料上操作而不是第一燃料时保持第一燃料完整性。