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    POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND TURBO-EXPANDER USING SAME
    2.
    发明申请
    POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND TURBO-EXPANDER USING SAME 有权
    具有压缩机的发电系统创造出更高的空气流量和使用其的涡轮膨胀机

    公开(公告)号：US20160273404A1

    公开(公告)日：2016-09-22

    申请号：US14662851

    申请日：2015-03-19

    Applicant: General Electric Company

    Inventor： Sanji Ekanayake ,  Kihyung Kim ,  Alston Ilford Scipio ,  Leslie Yung Min Tong ,  Michael Wesley Yarnold

    IPC: F01K23/10 ,  F02C3/32 ,  F02C6/08 ,  F02C3/04

    CPC classification number: F01K23/10 ,  F02C3/04 ,  F02C3/10 ,  F02C3/13 ,  F02C3/32 ,  F02C6/00 ,  F02C6/02 ,  F02C6/08 ,  F02C6/18 ,  F02C9/18 ,  F02C9/52 ,  F05D2220/72 ,  F05D2230/80 ,  F05D2260/601 ,  Y02E20/14 ,  Y02E20/16

    Abstract: A power generation system may include a generator, and a gas turbine system for powering the generator, the gas turbine system including a turbine component, an integral compressor and a combustor to which air from the integral compressor and fuel are supplied, the combustor arranged to supply hot combustion gases to the turbine component, and the integral compressor having a flow capacity greater than an intake capacity of at least one of the combustor and the turbine component, creating an excess air flow. A turbo-expander may also power the generator. A first control valve control flow of the excess air flow along an excess air flow path to an inlet of the turbo-expander. An educator may be positioned in the excess air flow path for using the excess air flow as a motive force to augment the excess air flow with additional air. A discharge of the turbo-expander is supplied to an inlet of the integral compressor.

    Abstract translation: 发电系统可以包括发电机和用于为发电机供电的燃气轮机系统，所述燃气轮机系统包括涡轮机部件，整体式压缩机和燃烧器，来自所述整体式压缩机和燃料的空气被供应到所述燃烧器，所述燃烧器布置成 向涡轮机部件供应热燃烧气体，并且整体压缩机具有大于燃烧器和涡轮机部件中的至少一个的进气容量的流量，产生过量空气流。 涡轮膨胀机也可以为发电机供电。 第一控制阀控制沿着过量空气流动路径的过量气流到涡轮膨胀机的入口的流动。 教育者可以定位在过量气流路径中，以使用过量的气流作为增加额外空气的过量气流的动力。 涡轮膨胀机的排放被供应到整体式压缩机的入口。

    COMBUSTOR ASSEMBLY FOR A GAS TURBINE ENGINE AND METHOD OF MAKING SAME
    4.
    发明申请
    COMBUSTOR ASSEMBLY FOR A GAS TURBINE ENGINE AND METHOD OF MAKING SAME 有权
    用于气体涡轮发动机的燃烧器组件及其制造方法

    公开(公告)号：US20170009996A1

    公开(公告)日：2017-01-12

    申请号：US14793000

    申请日：2015-07-07

    Applicant: General Electric Company

    Inventor： Kihyung Kim ,  Diego Fernando Rancruel ,  Prashant C. Mahalingappanavar

    IPC: F23R3/46 ,  F23R3/34

    CPC classification number: F23R3/46 ,  F02C7/22 ,  F02C7/222 ,  F02C7/228 ,  F02C9/26 ,  F02C9/28 ,  F05D2260/964 ,  F05D2270/14 ,  F05D2270/301 ,  F05D2270/333 ,  F23D2210/00 ,  F23N1/005 ,  F23N5/24 ,  F23N2037/02 ,  F23R3/34 ,  F23R2900/00013

    Abstract: A combustor can assembly includes a plurality of combustor cans spaced circumferentially about a gas turbine engine. Each combustor can is coupled in flow communication with at least one fuel manifold via a respective can fuel line. The combustor can assembly also includes a first interconnecting fuel line that includes a first end and a second end. The first end is coupled in flow communication with the can fuel line of a first combustor can, and the second end is coupled in flow communication with the can fuel line of a second combustor can that is not circumferentially adjacent to the first combustor can. The combustor can assembly further includes a first control device operatively coupled to the can fuel line of the first combustor can. The first control device is operable to change a dynamic operational characteristic of the first and second combustor cans independently of other combustor cans.

    Abstract translation: 燃烧器罐组件包括围绕燃气涡轮发动机周向间隔开的多个燃烧器罐。 每个燃烧器罐可以经由相应的罐燃料管线与至少一个燃料歧管流动连通地联接。 燃烧室组件还包括包括第一端和第二端的第一互连燃料管线。 第一端与第一燃烧器罐的罐燃料管线流动连通地联接，并且第二端部与第二燃烧器罐的罐燃料管线流动连通，第二燃烧器罐体不能在周向上邻近第一燃烧器罐。 燃烧室组件还包括可操作地连接到第一燃烧器罐的罐燃料管线的第一控制装置。 第一控制装置可操作以独立于其它燃烧器罐改变第一和第二燃烧器罐的动态操作特性。

    System and method for loading a combined cycle power plant
    5.
    发明授权
    System and method for loading a combined cycle power plant 有权
    装载联合循环发电厂的系统和方法

    公开(公告)号：US09523313B2

    公开(公告)日：2016-12-20

    申请号：US13798044

    申请日：2013-03-12

    Applicant: General Electric Company

    Inventor： Kihyung Kim ,  Seyfettin Can Gulen ,  Brett Matthew Thompson

    IPC: F02C1/00 ,  F02C7/057 ,  F02C6/18 ,  F02C9/20

    CPC classification number: F02C7/057 ,  F02C6/18 ,  F02C9/20 ,  Y02E20/16

    Abstract: A system including a gas turbine system configured to transition between a first load state and a second load state, wherein the gas turbine system comprises an airflow control module configured to adjust an airflow through the gas turbine system between a minimum airflow condition and a maximum airflow condition, and a controller configured to control the gas turbine system to operate with a load path between a first load path corresponding to the minimum airflow condition and a second load path corresponding to the maximum airflow condition, wherein the controller is configured to control the gas turbine system to transition between the first load state and the second load state using the load path between the first and second load paths.

    Abstract translation: 一种包括配置成在第一负载状态和第二负载状态之间转换的燃气轮机系统的系统，其中所述燃气涡轮机系统包括气流控制模块，所述气流控制模块被配置为在最小气流条件和最大气流之间调节通过所述燃气涡轮机系统的气流 条件，以及控制器，其被配置为控制所述燃气轮机系统与在与所述最小气流条件相对应的第一负载路径与对应于所述最大气流条件的第二负载路径之间的负载路径进行操作，其中所述控制器被配置为控制所述气体 涡轮机系统使用第一和第二负载路径之间的负载路径在第一负载状态和第二负载状态之间转换。

    POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND TURBO-EXPANDER FOR COOLING INLET AIR
    6.
    发明申请
    POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND TURBO-EXPANDER FOR COOLING INLET AIR 有权
    具有压缩机创造空气流的发电系统和用于冷却入口空气的涡轮膨胀机

    公开(公告)号：US20160273399A1

    公开(公告)日：2016-09-22

    申请号：US14662803

    申请日：2015-03-19

    Applicant: General Electric Company

    Inventor： Sanji Ekanayake ,  Thomas John Freeman ,  Kihyung Kim ,  Alston Ilford Scipio ,  Leslie Yung Min Tong

    IPC: F01K23/10 ,  F02C3/04 ,  F02C6/00

    CPC classification number: F01K23/10 ,  F02C3/04 ,  F02C3/13 ,  F02C6/00 ,  F02C6/08 ,  F02C9/18 ,  Y02E20/16

    Abstract: A power generation system may include: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which air from the first integral compressor and fuel are supplied. The first integral compressor has a flow capacity greater than an intake capacity of the first combustor and/or the first turbine component, creating an excess air flow. A second gas turbine system may include similar components to the first except but without excess capacity in its compressor. A turbo-expander may be operatively coupled to the second gas turbine system. Control valves may control flow of the excess air flow from the first gas turbine system to at least one of the second gas turbine system and the turbo-expander, and flow of a discharge of the turbo-expander to an inlet of at least one of the first integral compressor and the second compressor.

    Abstract translation: 发电系统可以包括：第一燃气轮机系统，其包括第一涡轮机部件，第一整体式压缩机和第一燃烧器，来自第一整体式压缩机和燃料的空气供应到第一燃烧器。 第一整体压缩机具有大于第一燃烧器和/或第一涡轮机部件的进气能力的流动能力，产生过量的气流。 第二燃气轮机系统可以包括与第一燃气涡轮机系统相似的组件，除了其压缩机中没有过剩的容量。 涡轮膨胀机可以可操作地联接到第二燃气轮机系统。 控制阀可以控制从第一燃气轮机系统到第二燃气轮机系统和涡轮膨胀机中的至少一个的过量空气流的流动，以及涡轮膨胀器的排放物流到至少一个 第一整体式压缩机和第二压缩机。

    COOLED COOLING AIR SYSTEM HAVING THERMOELECTRIC GENERATOR
    7.
    发明申请
    COOLED COOLING AIR SYSTEM HAVING THERMOELECTRIC GENERATOR 审中-公开
    具有热电发生器的冷却冷却空气系统

    公开(公告)号：US20150372214A1

    公开(公告)日：2015-12-24

    申请号：US14313640

    申请日：2014-06-24

    Applicant: General Electric Company

    Inventor： Kihyung Kim ,  Barrett David Gardiner

    IPC: H01L35/30

    CPC classification number: F25B27/02 ,  F02C6/18 ,  F04D19/002 ,  F04D29/582 ,  F05B2220/302 ,  F05B2220/706 ,  F25B21/02 ,  F25B49/00 ,  F25B2321/0251 ,  F25B2600/2515 ,  F25B2700/2102 ,  H01L35/32

    Abstract: Various embodiments include a cooled cooling-air system including: an inlet hot fluid conduit fluidly connected with a hot air source from a turbomachine; an inlet cold fluid conduit fluidly connected with a cold fluid source, the cold fluid source having a lower temperature than the hot air source; and a first thermoelectric generator fluidly connected with the inlet hot fluid conduit and the inlet cold fluid conduit, the first thermoelectric generator for cooling the inlet hot fluid conduit and simultaneously generating an electrical output.

    Abstract translation: 各种实施例包括冷却的冷却空气系统，其包括：与涡轮机的热空气源流体连接的入口热流体管道; 与冷流体源流体连接的入口冷流体导管，所述冷流体源具有比所述热空气源低的温度; 以及第一热电发电机，其与所述入口热流体管道和所述入口冷流体管道流体连接，所述第一热电发电机用于冷却所述入口热流体管道并同时产生电输出。

    System and Method for Loading a Combined Cycle Power Plant
    8.
    发明申请
    System and Method for Loading a Combined Cycle Power Plant 有权
    装载联合循环发电厂的系统和方法

    公开(公告)号：US20140260284A1

    公开(公告)日：2014-09-18

    申请号：US13798044

    申请日：2013-03-12

    Applicant: GENERAL ELECTRIC COMPANY

    Inventor： Kihyung Kim ,  Seyfettin Can Gulen ,  Brett Matthew Thompson

    IPC: F02C7/057

    CPC classification number: F02C7/057 ,  F02C6/18 ,  F02C9/20 ,  Y02E20/16

    Abstract: A system including a gas turbine system configured to transition between a first load state and a second load state, wherein the gas turbine system comprises an airflow control module configured to adjust an airflow through the gas turbine system between a minimum airflow condition and a maximum airflow condition, and a controller configured to control the gas turbine system to operate with a load path between a first load path corresponding to the minimum airflow condition and a second load path corresponding to the maximum airflow condition, wherein the controller is configured to control the gas turbine system to transition between the first load state and the second load state using the load path between the first and second load paths.

    Abstract translation: 一种包括配置成在第一负载状态和第二负载状态之间转换的燃气轮机系统的系统，其中所述燃气涡轮机系统包括气流控制模块，所述气流控制模块被配置为在最小气流条件和最大气流之间调节通过所述燃气涡轮机系统的气流 条件，以及控制器，其被配置为控制所述燃气轮机系统与在与所述最小气流条件相对应的第一负载路径与对应于所述最大气流条件的第二负载路径之间的负载路径进行操作，其中所述控制器被配置为控制所述气体 涡轮机系统使用第一和第二负载路径之间的负载路径在第一负载状态和第二负载状态之间转换。

    Systems for fuel distribution in a combustor assembly for a gas turbine engine
    10.
    发明授权
    Systems for fuel distribution in a combustor assembly for a gas turbine engine 有权

    公开(公告)号：US11085375B2

    公开(公告)日：2021-08-10

    申请号：US15624247

    申请日：2017-06-15

    Applicant: General Electric Company

    Inventor： Kihyung Kim ,  Anthony Whittenberg

    IPC: F02C7/22 ,  F23R3/34 ,  F02C7/232 ,  F02C3/04 ,  F23R3/28 ,  F02C9/34

    Abstract: A combustor assembly for a gas turbine engine includes a plurality of combustors spaced circumferentially about the gas turbine engine. Each of the combustors is coupled in flow communication with a manifold configured to channel a liquid to the plurality of combustors. A plurality of fuel lines is coupled in flow communication with the manifold. Each fuel line is coupled in flow communication with a respective combustor of the plurality of combustors. In addition, the combustor assembly includes a flow balance system having a plurality of flow balance devices. Each flow balance device is operatively coupled to one of the fuel lines. Each flow balance device is operative to reduce the flow of liquid to the respective combustor.

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