SYSTEM AND METHOD FOR EXPANDING A COMPRESSOR BLEED FLOW
    1.
    发明申请
    SYSTEM AND METHOD FOR EXPANDING A COMPRESSOR BLEED FLOW 有权
    膨胀压缩机流动的系统和方法

    公开(公告)号:US20140182307A1

    公开(公告)日:2014-07-03

    申请号:US13759975

    申请日:2013-02-05

    Abstract: A system includes a bleed system configured to direct a bleed flow from a high pressure region to a low pressure region. The bleed system includes a valve configured to control the bleed flow through the bleed system and a staged bleed conduit configured to incrementally depressurize the bleed flow. The staged bleed conduit includes an inlet coupled to the valve, a first stage configured to depressurize the bleed flow that is coupled to the inlet, a second stage configured to depressurize the bleed flow that is coupled to the first stage, and an outlet coupled to the second stage. The outlet is configured to direct the bleed flow to the low pressure region. The inlet, the first stage, the second stage, and the outlet are disposed along parallel axes.

    Abstract translation: 系统包括排放系统,其配置为将排出流从高压区域引导到低压区域。 排放系统包括构造成控制通过排放系统的排出流量的阀门和被配置成递增地减压排放流量的分段排放导管。 分级排放导管包括联接到阀的入口,被配置为对与入口联接的排出流减压的第一级,被配置为减压联接到第一级的排出流的第二级,以及连接到 第二阶段 出口构造成将排出流引导到低压区域。 入口,第一阶段,第二阶段和出口沿着平行的轴线设置。

    Radial Diffuser Exhaust System
    2.
    发明申请
    Radial Diffuser Exhaust System 有权
    径向扩散器排气系统

    公开(公告)号:US20140271168A1

    公开(公告)日:2014-09-18

    申请号:US13798614

    申请日:2013-03-13

    CPC classification number: F01D25/30

    Abstract: The present application provides a radial diffuser exhaust system for use with a gas turbine engine. The radial diffuser exhaust system may include a radial diffuser positioned within an asymmetric exhaust collector. The asymmetric exhaust collector may include a closed end chamber and an exhaust end chamber. The closed end chamber may have a first size, the exhaust end chamber may have a second size, and the first size may be smaller than the second size.

    Abstract translation: 本申请提供了一种与燃气涡轮发动机一起使用的径向扩散器排气系统。 径向扩散器排气系统可以包括位于不对称排气收集器内的径向扩散器。 不对称排气收集器可以包括封闭端室和排气端室。 封闭端室可以具有第一尺寸,排气端室可以具有第二尺寸,并且第一尺寸可以小于第二尺寸。

    System and method for expanding a compressor bleed flow
    3.
    发明授权
    System and method for expanding a compressor bleed flow 有权
    扩大压缩机排放流量的系统和方法

    公开(公告)号:US09347380B2

    公开(公告)日:2016-05-24

    申请号:US13759975

    申请日:2013-02-05

    Abstract: A system includes a bleed system configured to direct a bleed flow from a high pressure region to a low pressure region. The bleed system includes a valve configured to control the bleed flow through the bleed system and a staged bleed conduit configured to incrementally depressurize the bleed flow. The staged bleed conduit includes an inlet coupled to the valve, a first stage configured to depressurize the bleed flow that is coupled to the inlet, a second stage configured to depressurize the bleed flow that is coupled to the first stage, and an outlet coupled to the second stage. The outlet is configured to direct the bleed flow to the low pressure region. The inlet, the first stage, the second stage, and the outlet are disposed along parallel axes.

    Abstract translation: 系统包括排放系统,其配置为将排出流从高压区域引导到低压区域。 排放系统包括构造成控制通过排放系统的排出流量的阀门和被配置成递增地减压排放流量的分段排放导管。 分级排放导管包括联接到阀的入口,被配置为对与入口联接的排出流减压的第一级,被配置为减压联接到第一级的排出流的第二级,以及连接到 第二阶段 出口构造成将排出流引导到低压区域。 入口,第一阶段,第二阶段和出口沿着平行的轴线设置。

    System for managing exhaust flow for a gas turbine
    5.
    发明授权
    System for managing exhaust flow for a gas turbine 有权
    用于管理燃气轮机排气流的系统

    公开(公告)号:US09085996B2

    公开(公告)日:2015-07-21

    申请号:US13789573

    申请日:2013-03-07

    CPC classification number: F01D25/305 F01D25/30 F02C7/00 Y02E20/16 Y02E20/18

    Abstract: A system includes a gas turbine enclosure. The system also includes a gas turbine engine disposed in the gas turbine enclosure, wherein the gas turbine engine is configured to output an exhaust flow. The system further includes an exhaust driven eductor configured to draw an air flow through and out of the gas turbine engine enclosure using the exhaust flow. The system yet further includes an exhaust stack coupled to the gas turbine enclosure, wherein the exhaust stack is configured to output a mixed flow of the exhaust flow and the air flow. The system still further includes a diffuser plate disposed within the exhaust stack, wherein the diffuser plate is configured to provide a homogenous flow distribution for the mixed flow downstream of the diffuser plate.

    Abstract translation: 一种系统包括燃气轮机壳体。 该系统还包括设置在燃气涡轮机壳体中的燃气涡轮发动机,其中燃气涡轮发动机被配置为输出排气流。 该系统还包括被排气驱动的喷射器,该排气驱动的喷射器被构造成使用排气流将气流抽出和流出燃气涡轮发动机外壳。 该系统还包括联接到燃气涡轮机壳体的排气叠层,其中排气叠层构造成输出排气流和空气流的混合流。 该系统还包括设置在排气叠层内的扩散板,其中扩散板被配置成为扩散板下游的混合流提供均匀的流动分布。

    SYSTEM FOR MANAGING EXHAUST FLOW FOR A GAS TURBINE
    6.
    发明申请
    SYSTEM FOR MANAGING EXHAUST FLOW FOR A GAS TURBINE 有权
    用于管理燃气涡轮机排气流的系统

    公开(公告)号:US20140157778A1

    公开(公告)日:2014-06-12

    申请号:US13789573

    申请日:2013-03-07

    CPC classification number: F01D25/305 F01D25/30 F02C7/00 Y02E20/16 Y02E20/18

    Abstract: A system includes a gas turbine enclosure. The system also includes a gas turbine engine disposed in the gas turbine enclosure, wherein the gas turbine engine is configured to output an exhaust flow. The system further includes an exhaust driven eductor configured to draw an air flow through and out of the gas turbine engine enclosure using the exhaust flow. The system yet further includes an exhaust stack coupled to the gas turbine enclosure, wherein the exhaust stack is configured to output a mixed flow of the exhaust flow and the air flow. The system still further includes a diffuser plate disposed within the exhaust stack, wherein the diffuser plate is configured to provide a homogenous flow distribution for the mixed flow downstream of the diffuser plate.

    Abstract translation: 一种系统包括燃气轮机壳体。 该系统还包括设置在燃气涡轮机壳体中的燃气涡轮发动机,其中燃气涡轮发动机被配置为输出排气流。 该系统还包括被排气驱动的喷射器,该排气驱动的喷射器被构造成使用排气流将气流抽出和流出燃气涡轮发动机外壳。 该系统还包括联接到燃气涡轮机壳体的排气叠层,其中排气叠层构造成输出排气流和空气流的混合流。 该系统还包括设置在排气叠层内的扩散板,其中扩散板被配置成为扩散板下游的混合流提供均匀的流动分布。

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