System and method for heating combustor fuel
    1.
    发明授权
    System and method for heating combustor fuel 有权
    用于加热燃烧器燃料的系统和方法

    公开(公告)号:US09435258B2

    公开(公告)日:2016-09-06

    申请号:US13651813

    申请日:2012-10-15

    CPC classification number: F02C3/34 F02C6/06 F02C7/224

    Abstract: A system for heating combustor fuel includes a turbine exhaust plenum and a heat exchanger downstream from the turbine exhaust plenum. The heat exchanger has an exhaust inlet, an exhaust outlet, a fuel inlet, and a fuel outlet. An exhaust recirculation plenum has a recirculation inlet connection downstream from the exhaust outlet and a recirculation outlet connection upstream from the exhaust inlet. The system further includes structure for controlling a recirculated exhaust flow from the exhaust outlet into the exhaust recirculation plenum.

    Abstract translation: 用于加热燃烧器燃料的系统包括涡轮排气增压室和在涡轮排气增压室下游的热交换器。 热交换器具有排气入口,排气出口,燃料入口和燃料出口。 排气再循环增压室具有从排气出口下游的再循环入口连接和在排气入口上游的再循环出口连接。 该系统还包括用于控制从排气出口进入排气再循环增压室的再循环排气流的结构。

    System and method for generating nitrogen from a gas turbine
    2.
    发明授权
    System and method for generating nitrogen from a gas turbine 有权
    从燃气轮机产生氮气的系统和方法

    公开(公告)号:US09527736B2

    公开(公告)日:2016-12-27

    申请号:US13851891

    申请日:2013-03-27

    CPC classification number: C01B21/0438 F02C6/08 F05D2270/082

    Abstract: A system includes a gas turbine. The gas turbine includes a first compressor configured to provide a first portion of a discharge air to a combustor. The gas turbine also includes the combustor configured to combust a mixture of the first portion of the discharge air and fuel to generate an exhaust gas and to provide the exhaust gas to a turbine. The gas turbine also includes an exhaust outlet coupled to the turbine and configured to enable the exhaust gas to exit the gas turbine. The system also includes a nitrogen purification system coupled to the gas turbine. The nitrogen purification system includes a membrane nitrogen generator configured to receive a second portion of the discharge air from the compressor or a portion of the exhaust gas from the exhaust outlet, wherein the membrane nitrogen generator is configured to generate nitrogen from the second portion of the discharge air or the portion of the exhaust gas.

    Abstract translation: 一种系统包括燃气轮机。 燃气轮机包括第一压缩机,其被配置为向燃烧器提供排出空气的第一部分。 燃气轮机还包括被配置为燃烧排出空气的第一部分和燃料的混合物以产生废气并将排气提供给涡轮机的燃烧器。 燃气涡轮机还包括联接到涡轮机并被配置为使排气能够离开燃气轮机的排气出口。 该系统还包括耦合到燃气轮机的氮气净化系统。 氮气净化系统包括膜氮发生器,其被配置为从压缩机或排气出口排出的一部分废气中接收排出空气的第二部分,其中膜氮发生器构造成从第二部分产生氮气 排出空气或废气的一部分。

    SYSTEM AND METHOD FOR GENERATING NITROGEN FROM A GAS TURBINE
    3.
    发明申请
    SYSTEM AND METHOD FOR GENERATING NITROGEN FROM A GAS TURBINE 有权
    用于从气体涡轮机产生氮气的系统和方法

    公开(公告)号:US20140290260A1

    公开(公告)日:2014-10-02

    申请号:US13851891

    申请日:2013-03-27

    CPC classification number: C01B21/0438 F02C6/08 F05D2270/082

    Abstract: A system includes a gas turbine. The gas turbine includes a first compressor configured to provide a first portion of a discharge air to a combustor. The gas turbine also includes the combustor configured to combust a mixture of the first portion of the discharge air and fuel to generate an exhaust gas and to provide the exhaust gas to a turbine. The gas turbine also includes an exhaust outlet coupled to the turbine and configured to enable the exhaust gas to exit the gas turbine. The system also includes a nitrogen purification system coupled to the gas turbine. The nitrogen purification system includes a membrane nitrogen generator configured to receive a second portion of the discharge air from the compressor or a portion of the exhaust gas from the exhaust outlet, wherein the membrane nitrogen generator is configured to generate nitrogen from the second portion of the discharge air or the portion of the exhaust gas.

    Abstract translation: 一种系统包括燃气轮机。 燃气轮机包括第一压缩机,其被配置为向燃烧器提供排出空气的第一部分。 燃气轮机还包括被配置为燃烧排出空气的第一部分和燃料的混合物以产生废气并将排气提供给涡轮机的燃烧器。 燃气涡轮机还包括联接到涡轮机并被配置为使排气能够离开燃气轮机的排气出口。 该系统还包括耦合到燃气轮机的氮气净化系统。 氮气净化系统包括膜氮发生器,其被配置为从压缩机或排气出口排出的一部分废气中接收排出空气的第二部分,其中膜氮发生器构造成从第二部分产生氮气 排出空气或废气的一部分。

    SYSTEM AND METHOD FOR HEATING COMBUSTOR FUEL
    4.
    发明申请
    SYSTEM AND METHOD FOR HEATING COMBUSTOR FUEL 有权
    用于加热燃料燃料的系统和方法

    公开(公告)号:US20140102105A1

    公开(公告)日:2014-04-17

    申请号:US13651813

    申请日:2012-10-15

    CPC classification number: F02C3/34 F02C6/06 F02C7/224

    Abstract: A system for heating combustor fuel includes a turbine exhaust plenum and a heat exchanger downstream from the turbine exhaust plenum. The heat exchanger has an exhaust inlet, an exhaust outlet, a fuel inlet, and a fuel outlet. An exhaust recirculation plenum has a recirculation inlet connection downstream from the exhaust outlet and a recirculation outlet connection upstream from the exhaust inlet. The system further includes structure for controlling a recirculated exhaust flow from the exhaust outlet into the exhaust recirculation plenum.

    Abstract translation: 用于加热燃烧器燃料的系统包括涡轮排气增压室和在涡轮排气增压室下游的热交换器。 热交换器具有排气入口,排气出口,燃料入口和燃料出口。 排气再循环增压室具有从排气出口下游的再循环入口连接和在排气入口上游的再循环出口连接。 该系统还包括用于控制从排气出口进入排气再循环增压室的再循环排气流的结构。

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