SYSTEM AND METHOD FOR A GAS TURBINE EXHAUST DIFFUSER
    1.
    发明申请
    SYSTEM AND METHOD FOR A GAS TURBINE EXHAUST DIFFUSER 审中-公开
    燃气轮机排气歧管系统与方法

    公开(公告)号:US20120186261A1

    公开(公告)日:2012-07-26

    申请号:US13010272

    申请日:2011-01-20

    IPC分类号: F02C7/00

    摘要: In one aspect, an exhaust diffuser for a gas turbine is disclosed. The exhaust diffuser may generally include an inner casing and an outer casing spaced radially apart from the inner casing so as to define a passage for receiving exhaust gases of the gas turbine. Additionally, the exhaust diffuser may include a fluid outlet configured to inject a fluid into the exhaust gases flowing through the passage.

    摘要翻译: 一方面,公开了一种用于燃气轮机的排气扩散器。 排气扩散器通常可以包括内壳和与内壳径向分开的外壳,以便限定用于接收燃气轮机废气的通道。 此外,排气扩散器可以包括被配置为将流体喷射到流过通道的废气中的流体出口。

    SYSTEM AND METHOD FOR PRODUCING A HYDROGEN ENRICHED FUEL
    2.
    发明申请
    SYSTEM AND METHOD FOR PRODUCING A HYDROGEN ENRICHED FUEL 审中-公开
    生产氢化燃料的系统和方法

    公开(公告)号:US20120204573A1

    公开(公告)日:2012-08-16

    申请号:US13026385

    申请日:2011-02-14

    IPC分类号: F02C6/18 F02B43/00

    CPC分类号: F02C3/20 Y02E20/16

    摘要: A system for producing a hydrogen enriched fuel includes a gas turbine comprising a compressor, a combustor, and a turbine. A fuel reformer is connected between the compressor and the combustor. The fuel reformer comprises an inlet connected to the compressor and an outlet connected to the combustor, and the fuel reformer produces the hydrogen enriched fuel. A method for producing a hydrogen enriched fuel includes compressing a working fluid with a compressor to produce a compressed working fluid and diverting a first portion of the compressed working fluid to a fuel reformer. The method further includes mixing a fuel with the compressed working fluid in the fuel reformer to produce the hydrogen enriched fuel and an exhaust stream and flowing the exhaust stream to a combustor

    摘要翻译: 一种用于生产富氢燃料的系统包括一个包括压缩机,燃烧室和涡轮机的燃气轮机。 燃料重整器连接在压缩机和燃烧器之间。 燃料重整器包括连接到压缩机的入口和连接到燃烧器的出口,并且燃料重整器产生富氢燃料。 一种制造富氢燃料的方法包括用压缩机压缩工作流体以产生压缩的工作流体并将压缩的工作流体的第一部分转向燃料重整器。 该方法还包括在燃料重整器中将燃料与压缩的工作流体混合以产生富氢燃料和排气流并使废气流流到燃烧室

    SYSTEM AND METHOD FOR COOLING USING SYSTEM EXHAUST
    3.
    发明申请
    SYSTEM AND METHOD FOR COOLING USING SYSTEM EXHAUST 审中-公开
    使用系统排气冷却的系统和方法

    公开(公告)号:US20100071878A1

    公开(公告)日:2010-03-25

    申请号:US12233979

    申请日:2008-09-19

    IPC分类号: F28D15/00

    摘要: A method for operating a system comprising a number of fluid streams and a number of components include a device is provided. The method comprises separating a cooling fluid from an exhaust stream discharged from a device and transferring heat to the cooling fluid from at least one of the number of fluid streams, at least one of the number of components, or both. A system comprising a number of fluid streams, a number of components including a device comprising an exhaust for discharging an exhaust stream, a separator for separating a cooling fluid from the exhaust stream, and a heat exchanger is provided. The heat exchanger transfers heat to the cooling fluid from at least one of the number of fluid streams, at least one of the number of components, or both.

    摘要翻译: 一种用于操作包括多个流体流和多个部件的系统的方法包括设备。 该方法包括从从装置排出的废气流中分离冷却流体,并从多个流体流中的至少一个,多个组分中的至少一个或两者传递热量至冷却流体。 提供了包括多个流体流的系统,包括包括用于排出排气流的排气的装置的多个部件,用于从排气流分离冷却流体的分离器和热交换器。 热交换器从多个流体流中的至少一个,多个部件中的至少一个或两者传递热量至冷却流体。

    Oxyfuel gas turbine system and method
    4.
    发明授权
    Oxyfuel gas turbine system and method 有权
    氧气燃气轮机系统及方法

    公开(公告)号:US08479488B2

    公开(公告)日:2013-07-09

    申请号:US12509684

    申请日:2009-07-27

    IPC分类号: F02C1/00 F02C6/00

    CPC分类号: F02C3/22 F02C3/34 F02C7/222

    摘要: A gas turbine includes a compressor with a plurality of pressure plates, a combustor downstream from the compressor, and a turbine downstream from the combustor and axially aligned with the compressor. The combustor produces combustion gases that flow to the turbine. A first manifold connected to the combustor contains a first process gas for combustion in the combustor. A second manifold connected upstream of the turbine contains a second process gas, and a portion of the second process gas flows to the plurality of pressure plates.

    摘要翻译: 燃气轮机包括具有多个压力板的压缩机,来自压缩机的下游的燃烧器,以及在燃烧器下游并与压缩机轴向对准的涡轮机。 燃烧器产生流到涡轮机的燃烧气体。 连接到燃烧器的第一歧管包含用于在燃烧器中燃烧的第一工艺气体。 连接在涡轮机上游的第二歧管包含第二工艺气体,第二工艺气体的一部分流到多个压力板。

    OXYFUEL GAS TURBINE SYSTEM AND METHOD
    5.
    发明申请
    OXYFUEL GAS TURBINE SYSTEM AND METHOD 有权
    OXYFUEL气体涡轮机系统和方法

    公开(公告)号:US20110016872A1

    公开(公告)日:2011-01-27

    申请号:US12509684

    申请日:2009-07-27

    IPC分类号: F02C1/00

    CPC分类号: F02C3/22 F02C3/34 F02C7/222

    摘要: A gas turbine includes a compressor with a plurality of pressure plates, a combuster downstream from the compressor, and a turbine downstream from the combustor and axially aligned with the compressor. The combustor produces combustion gases that flow to the turbine. A first manifold connected to the combustor contains a first process gas for combustion in the combustor. A second manifold connected upstream of the turbine contains a second process gas, and a portion of the second process gas flows to the plurality of pressure plates.

    摘要翻译: 燃气涡轮机包括具有多个压力板的压缩机,来自压缩机的下游的燃烧器,以及在燃烧器下游并与压缩机轴向对准的涡轮机。 燃烧器产生流到涡轮机的燃烧气体。 连接到燃烧器的第一歧管包含用于在燃烧器中燃烧的第一工艺气体。 连接在涡轮机上游的第二歧管包含第二工艺气体,第二工艺气体的一部分流到多个压力板。