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    Systems and methods for use in operating turbine engines
    4.
    发明公开
    Systems and methods for use in operating turbine engines 审中-公开
    Systeme und Verfahren zum Betrieb von Turbinen

    公开(公告)号：EP2584177A2

    公开(公告)日：2013-04-24

    申请号：EP12188816.8

    申请日：2012-10-17

    申请人： General Electric Company

    发明人： Hughes, Michael John ,  Khan, Abdul Rafey ,  Romig, Bryan Wesley

    IPC分类号： F02C9/26

    CPC分类号： F02C9/26 ,  F02C3/22 ,  F02C9/28 ,  F02C9/34 ,  F02C9/40 ,  F05D2270/082

    摘要： A control system (130) for use with a turbine engine (100) that is configured to operate at a rated power output is provided. The control system includes a computing device (200) that includes a processor (214) that is programmed to calculate an amount of fluid to be supplied for combustion in the turbine engine. The processor is also programmed to designate at least one nozzle of a plurality of nozzles to receive the fluid. Moreover, the control system includes at least one control valve (201) coupled to the computing device. The control valve (201) is configured to receive at least one control parameter from the computing device (200) for use in modulating the amount of the fluid to be channeled to the nozzle such that the rated power output is generated while emission levels are maintained below a predefined emissions threshold level.

    摘要翻译： 提供了一种与被配置为以额定功率输出操作的涡轮发动机（100）一起使用的控制系统（130）。 控制系统包括计算装置（200），其包括处理器（214），该处理器被编程为计算供应用于在涡轮发动机中燃烧的流体的量。 处理器也被编程为指定多个喷嘴的至少一个喷嘴以接收流体。 此外，控制系统包括耦合到计算设备的至少一个控制阀（201）。 控制阀（201）被配置为从计算装置（200）接收至少一个控制参数，用于调节要引导到喷嘴的流体的量，使得在保持排放水平的同时产生额定功率输出 低于预定义的排放阈值水平。

    Premixing apparatus for gas turbine system
    5.
    发明公开
    Premixing apparatus for gas turbine system 有权
    Vormischvorrichtungfürein Gasturbinensystem

    公开(公告)号：EP2551595A2

    公开(公告)日：2013-01-30

    申请号：EP12176639.8

    申请日：2012-07-17

    申请人： General Electric Company

    发明人： Wu, Chunyang ,  Simons, Derrick Walter ,  Hughes, Michael John ,  Berry, Jonathan Dwight

    IPC分类号： F23R3/14 ,  F23R3/28

    CPC分类号： F23R3/14 ,  F05B2260/96 ,  F23R3/286 ,  F23R3/34 ,  F23R2900/00014

    摘要： A premixing apparatus (110) for a gas turbine system includes non-swirl elements (220) around a face (210) of the premixing apparatus (110) and one or more swirl assemblies (230) located on the face. The non-swirl elements (220) premix a premixture prior to the premixture being delivered to a combustor of the gas turbine system. Each swirl assembly (230) disturbs a flow of fluid prior to the fluid being delivered to the combustor. The premixture includes fuel and oxidant, and the fluid disturbed by the swirl assembly (230) includes the oxidant or the premixture.

    摘要翻译： 用于燃气涡轮机系统的预混合装置（110）包括围绕预混合装置（110）的表面（210）和位于表面上的一个或多个涡旋组件（230）的非涡流元件（220）。 非旋流元件（220）在预混合物被输送到燃气轮机系统的燃烧器之前预混合预混物。 每个旋流组件（230）在流体被输送到燃烧器之前会扰乱流体流动。 预混合物包括燃料和氧化剂，并且由旋流组件（230）扰动的流体包括氧化剂或预混合物。

    Systems and methods for use in operating turbine engines
    6.
    发明公开
    Systems and methods for use in operating turbine engines 审中-公开
    用于运行涡轮发动机的系统和方法

    公开(公告)号：EP2584177A3

    公开(公告)日：2018-04-11

    申请号：EP12188816.8

    申请日：2012-10-17

    申请人： General Electric Company

    发明人： Hughes, Michael John ,  Khan, Abdul Rafey ,  Romig, Bryan Wesley

    IPC分类号： F02C9/26 ,  F02C3/22 ,  F02C9/40 ,  F02C9/28

    CPC分类号： F02C9/26 ,  F02C3/22 ,  F02C9/28 ,  F02C9/34 ,  F02C9/40 ,  F05D2270/082

    摘要： A control system (130) for use with a turbine engine (100) that is configured to operate at a rated power output is provided. The control system includes a computing device (200) that includes a processor (214) that is programmed to calculate an amount of fluid to be supplied for combustion in the turbine engine. The processor is also programmed to designate at least one nozzle of a plurality of nozzles to receive the fluid. Moreover, the control system includes at least one control valve (201) coupled to the computing device. The control valve (201) is configured to receive at least one control parameter from the computing device (200) for use in modulating the amount of the fluid to be channeled to the nozzle such that the rated power output is generated while emission levels are maintained below a predefined emissions threshold level.

    摘要翻译： 提供了一种与配置成在额定功率输出下操作的涡轮发动机（100）一起使用的控制系统（130）。 该控制系统包括计算设备（200），该计算设备（200）包括处理器（214），该处理器被编程为计算将被供应用于涡轮发动机中的燃烧的流体的量。 处理器还被编程为指定多个喷嘴中的至少一个喷嘴以接收流体。 此外，控制系统包括耦合到计算设备的至少一个控制阀（201）。 控制阀（201）被配置为接收来自计算设备（200）的至少一个控制参数，以用于调节将被引导到喷嘴的流体的量，使得在保持排放水平的同时产生额定功率输出 低于预定义的排放阈值水平。

    System and method for producing hydrogen rich fuel
    7.
    发明公开
    System and method for producing hydrogen rich fuel 审中-公开
    系统和Verfahren zur Herstellung von wasserstoffreichem Brennstoff

    公开(公告)号：EP2664764A2

    公开(公告)日：2013-11-20

    申请号：EP13168027.4

    申请日：2013-05-16

    申请人： General Electric Company

    发明人： Hughes, Michael John ,  Berry, Jonathan Dwight

    IPC分类号： F02C3/22 ,  C01B3/02

    摘要： A system for providing hydrogen enriched fuel includes first and second gas turbines 12,14. The second gas turbine 14 receives a fuel from a fuel supply and portion 36 of compressed working fluid from the first gas turbine 12 and produces a reformed fuel, and a fuel skid 20 provides fluid communication between a turbine 54 in the second gas turbine 14 and a combustor 24 in the first gas turbine 12. A method for providing hydrogen enriched fuel includes diverting a portion of a first compressed working fluid from a first compressor to a second compressor and providing a second compressed working fluid from the second compressor. Mixing a first portion of a compressed fuel with the second compressed working fluid in a reformer to produce a reformed fuel, flowing a second portion of the compressed fuel to a second turbine for cooling, and flowing the reformed fuel through the second turbine to cool the reformed fuel.

    摘要翻译： 用于提供富氢燃料的系统包括第一和第二燃气轮机12,14。 第二燃气轮机14从第一燃气轮机12接收来自燃料供应源的燃料和压缩工作流体的部分36，并产生重整燃料，并且燃料滑板20提供第二燃气轮机14中的涡轮机54和 在第一燃气轮机12中的燃烧器24.用于提供富氢燃料的方法包括将第一压缩工作流体的一部分从第一压缩机转向第二压缩机并从第二压缩机提供第二压缩工作流体。 在重整器中将压缩燃料的第一部分与第二压缩工作流体混合以产生重整燃料，将压缩燃料的第二部分流动到第二涡轮机进行冷却，并使重整燃料流过第二涡轮以冷却 改装燃料

    Combustor and method for purging a combustor
    8.
    发明公开
    Combustor and method for purging a combustor 审中-公开
    Brennkammer和Verfahren zur Reinigung einer Brennkammer

    公开(公告)号：EP2631543A2

    公开(公告)日：2013-08-28

    申请号：EP12196996.8

    申请日：2012-12-13

    申请人： General Electric Company

    发明人： Bery, Jonathan Dwight ,  Hughes, Michael John

    IPC分类号： F23R3/10 ,  F23R3/28

    CPC分类号： F23R3/10 ,  F23D2209/30 ,  F23R3/286

    摘要： A combustor (10) includes an end cap (28). The end cap (28) includes a first surface (30) and a second surface (32) downstream from the first surface (30), a shroud (24) that circumferentially surrounds at least a portion of the first and second surfaces (30,32), a plate (34) that extends radially within the shroud (24), a plurality of tubes (36) that extend through the plate (34) and the first and second surfaces (30,32), and a first purge port that extends through one or more of the plurality of tubes, (36) wherein the purge port is axially aligned with the plate (34).

    摘要翻译： 燃烧器（10）包括端盖（28）。 端盖（28）包括第一表面（30）和位于第一表面（30）下游的第二表面（32），护罩（24）周向地围绕第一和第二表面（30,30）的至少一部分， 32），在所述护罩（24）内径向延伸的板（34），延伸穿过所述板（34）和所述第一和第二表面（30,32）的多个管（36），以及第一吹扫端口 其延伸穿过所述多个管中的一个或多个（36），其中所述清洗口与所述板（34）轴向对齐。