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    METHODS AND SYSTEMS FOR OPERATING GAS TURBINE ENGINES
    1.
    发明申请
    METHODS AND SYSTEMS FOR OPERATING GAS TURBINE ENGINES 有权
    操作气体涡轮发动机的方法和系统

    公开(公告)号：US20100043387A1

    公开(公告)日：2010-02-25

    申请号：US11933898

    申请日：2007-11-01

    申请人： Geoffrey David Myers ,  David August Snider ,  Eric Motter ,  Daniel R. Tegel ,  James Harper ,  Stephen R. Watts ,  Joseph Citeno

    发明人： Geoffrey David Myers ,  David August Snider ,  Eric Motter ,  Daniel R. Tegel ,  James Harper ,  Stephen R. Watts ,  Joseph Citeno

    IPC分类号： F02C9/00 ,  F02C7/22

    CPC分类号： F02C7/228

    摘要： Methods and systems for delivering fuel in a gas turbine engine are provided. The system includes a plurality of can annular combustors that includes at least a first set of combustors of the plurality of can annular combustors and at least a second set of combustors of the plurality of can annular combustors wherein each set of combustors is supplied by a separately controllable respective fuel delivery system. The method includes supplying fuel at a first fuel schedule to the first set of combustors and supplying fuel at a second fuel schedule to the second set of combustors during a first mode of operation wherein the second fuel schedule is different than the first fuel schedule, and supplying fuel at the second fuel schedule to the first and second sets of combustors during a second mode of operation.

    摘要翻译： 提供了用于在燃气涡轮发动机中输送燃料的方法和系统。 该系统包括多个罐式环形燃烧器，其包括多个罐环形燃烧器中的至少第一组燃烧器和多个罐形环形燃烧器的至少第二组燃烧器，其中每组燃烧器由单独的 可控的燃油输送系统。 该方法包括以第一燃料排程向第一组燃料供应燃料，并在第一燃料运行方式下将第二燃料的燃料供应给第二组燃烧器，其中第二燃料计划与第一燃料排程不同，以及 在第二工作模式期间将第二燃料计划的燃料供应给第一和第二组燃烧器。

    Methods and systems for operating gas turbine engines
    2.
    发明授权
    Methods and systems for operating gas turbine engines 有权
    运行燃气涡轮发动机的方法和系统

    公开(公告)号：US08122725B2

    公开(公告)日：2012-02-28

    申请号：US11933898

    申请日：2007-11-01

    申请人： Geoffrey David Myers ,  David August Snider ,  Eric Motter ,  Daniel R. Tegel ,  James Harper ,  Stephen R. Watts ,  Joseph Citeno

    发明人： Geoffrey David Myers ,  David August Snider ,  Eric Motter ,  Daniel R. Tegel ,  James Harper ,  Stephen R. Watts ,  Joseph Citeno

    IPC分类号： F02C7/22 ,  F02C9/26 ,  F02C9/00 ,  F02C3/00

    CPC分类号： F02C7/228

    摘要： Methods and systems for delivering fuel in a gas turbine engine are provided. The system includes a plurality of can annular combustors that includes at least a first set of combustors of the plurality of can annular combustors and at least a second set of combustors of the plurality of can annular combustors wherein each set of combustors is supplied by a separately controllable respective fuel delivery system. The method includes supplying fuel at a first fuel schedule to the first set of combustors and supplying fuel at a second fuel schedule to the second set of combustors during a first mode of operation wherein the second fuel schedule is different than the first fuel schedule, and supplying fuel at the second fuel schedule to the first and second sets of combustors during a second mode of operation.

    摘要翻译： 提供了用于在燃气涡轮发动机中输送燃料的方法和系统。 该系统包括多个罐式环形燃烧器，其包括多个罐环形燃烧器中的至少第一组燃烧器和多个罐形环形燃烧器的至少第二组燃烧器，其中每组燃烧器由单独的 可控的燃油输送系统。 该方法包括以第一燃料排程向第一组燃料供应燃料，并在第一燃料运行方式中将第二燃料的燃料供应给第二组燃料，其中第二燃料计划与第一燃料计划不同，以及 在第二工作模式期间将第二燃料计划的燃料供应到第一和第二组燃烧器。

    Methods and Systems for Controlling a Combustor in Turbine Engines
    3.
    发明申请
    Methods and Systems for Controlling a Combustor in Turbine Engines 有权
    用于控制涡轮发动机燃烧器的方法和系统

    公开(公告)号：US20100162724A1

    公开(公告)日：2010-07-01

    申请号：US12347147

    申请日：2008-12-31

    申请人： Geoffrey David Myers ,  Lewis Berkley Davis, JR. ,  Timothy Andrew Healy ,  Joseph Citeno

    发明人： Geoffrey David Myers ,  Lewis Berkley Davis, JR. ,  Timothy Andrew Healy ,  Joseph Citeno

    IPC分类号： F02C9/00

    CPC分类号： F23R3/26 ,  F23N5/00 ,  F23N2041/20 ,  F23R2900/00013

    摘要： Embodiments of methods and systems for controlling a combustor for a gas turbine engine are provided. According to one example embodiment, a system includes an air control assembly associated with at least one air path of a combustor for a gas turbine engine. Additionally, the system also includes at least one sensor for sensing at least one operating parameter of the gas turbine engine. Further, the system also includes a controller operable to receive at least one operating parameter sensed by the at least one sensor, and further operable to selectively control an air control assembly based at least in part on the at least one operating parameter sensed by the at least one sensor.

    摘要翻译： 提供了用于控制燃气涡轮发动机的燃烧器的方法和系统的实施例。 根据一个示例性实施例，系统包括与用于燃气涡轮发动机的燃烧器的至少一个空气路径相关联的空气控制组件。 另外，该系统还包括用于感测燃气涡轮发动机的至少一个操作参数的至少一个传感器。 此外，该系统还包括可操作以接收由至少一个传感器感测的至少一个操作参数的控制器，并且还可操作以至少部分地基于由所述至少一个传感器感测的至少一个操作参数来选择性地控制空气控制组件 至少一个传感器。

    Combustor and method of supplying fuel to the combustor
    6.
    发明授权
    Combustor and method of supplying fuel to the combustor 有权
    向燃烧器供应燃料的燃烧器和方法

    公开(公告)号：US09593851B2

    公开(公告)日：2017-03-14

    申请号：US14122697

    申请日：2011-06-30

    申请人： Borys Borysovych Shershnyov ,  Geoffrey David Myers ,  Leonid Yulyevich Ginesin

    发明人： Borys Borysovych Shershnyov ,  Geoffrey David Myers ,  Leonid Yulyevich Ginesin

    IPC分类号： F23R3/28 ,  F23R3/34 ,  F02C7/22 ,  F23D11/40 ,  F23R3/54

    CPC分类号： F23R3/28 ,  F23D11/408 ,  F23R3/283 ,  F23R3/346 ,  F23R3/54

    摘要： A combustor (10) includes a combustion chamber (18), a liner (12) surrounding the combustion chamber, and a flow sleeve (52) surrounding the liner. An annular passage is between the liner and the flow sleeve, and a fuel injector (50) is located partially in the annular passage and extending through the liner into the combustion chamber. The fuel injector includes an outer tube, an inner tube, and a flow passage. A method of supplying a fuel to a combustor includes flowing a diluent inside an outer tube extending along a liner and flowing a liquid or gaseous fuel inside an inner tube extending inside a portion of the outer tube. The method further includes flowing the diluent and the liquid or gaseous fuel through the liner and into a combustion chamber surrounded by the liner.

    摘要翻译： 燃烧器（10）包括燃烧室（18），围绕燃烧室的衬套（12）和围绕衬套的流动套管（52）。 环形通道在衬套和流动套筒之间，燃料喷射器（50）部分地位于环形通道中并且延伸穿过衬套进入燃烧室。 燃料喷射器包括外管，内管和流路。 向燃烧器供应燃料的方法包括使稀释剂在沿着衬套延伸的外管内流动，并使液体或气体燃料在延伸到外管的一部分内的内管内流动。 该方法还包括使稀释剂和液体或气态燃料流过衬套并进入由衬套围绕的燃烧室。

    System and method for operating a gas turbine
    10.
    发明授权
    System and method for operating a gas turbine 有权
    用于操作燃气轮机的系统和方法

    公开(公告)号：US08650883B2

    公开(公告)日：2014-02-18

    申请号：US12854361

    申请日：2010-08-11

    申请人： Shahryar Rabiei ,  Gilbert Otto Kraemer ,  Geoffrey David Myers

    发明人： Shahryar Rabiei ,  Gilbert Otto Kraemer ,  Geoffrey David Myers

    IPC分类号： F02C9/20 ,  G01J5/10

    CPC分类号： F02C9/28 ,  F05D2270/083 ,  Y02T50/67

    摘要： A system for operating a gas turbine includes a compressor, a combustor, and a turbine. The combustor and turbine define a hot gas path. A sensor disposed outside the hot gas path measures internal thermal emissions from the combustor or turbine and generates a first signal reflective of the internal thermal emissions. The internal thermal emissions are infrared or ultraviolet emissions. A controller connected to the sensor receives the first signal and adjusts the compressor, combustor, or turbine in response to the first signal from the sensor. A method for operating a gas turbine includes measuring internal thermal emissions from inside a combustor or turbine using a sensor disposed outside the hot gas path. The method further includes generating a first signal reflective of the internal thermal emissions and adjusting the operation of the compressor, combustor, or turbine in response to the first signal from the sensor.

    摘要翻译： 用于操作燃气轮机的系统包括压缩机，燃烧器和涡轮机。 燃烧器和涡轮限定热气路径。 设置在热气路径之外的传感器测量来自燃烧器或涡轮机的内部热量排放，并产生反映内部热辐射的第一信号。 内部热辐射是红外线或紫外线辐射。 连接到传感器的控制器响应于来自传感器的第一信号接收第一信号并调节压缩机，燃烧器或涡轮机。 用于操作燃气轮机的方法包括使用设置在热气体路径外部的传感器来测量来自燃烧室或涡轮机内部的热量排放。 该方法还包括响应于来自传感器的第一信号产生反映内部热量排放的第一信号和调节压缩机，燃烧室或涡轮机的运行。