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1. 发明授权

US09593851B2 Combustor and method of supplying fuel to the combustor 有权
标题翻译：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。

2. 发明授权

US09429325B2 Combustor and method of supplying fuel to the combustor 有权
标题翻译：向燃烧器供应燃料的燃烧器和方法
公开(公告)号：US09429325B2
公开(公告)日：2016-08-30
申请号：US14122694
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 , F23R3/54 , F23R3/14
CPC分类号： F23R3/286 , F23R3/14 , F23R3/34 , F23R3/343 , F23R3/54
摘要： A combustor (10) includes a liner (12) that defines a combustion chamber (18) first pre-mix chamber (14) is upstream of the combustion chamber, and a fuel plenum (40) in fluid communication with the first pre-mix chamber surrounds a least a portion of the first pre-mix chamber. A method of supplying a fuel to combustor includes flowing the fuel over an outer surface of a first pre-mix chamber and into the first pre-mix chamber.
摘要翻译：燃烧器（10）包括限定燃烧室（18）的衬套（12），第一预混合室（14）在燃烧室的上游，以及与第一预混合物流体连通的燃料增压室（40）腔室围绕第一预混合室的至少一部分。向燃烧器供应燃料的方法包括将燃料流过第一预混合室的外表面并进入第一预混合室。

3. 发明申请

US20140137566A1 COMBUSTOR AND METHOD OF SUPPLYING FUEL TO THE COMBUSTOR 有权
标题翻译：燃料和燃料供应给燃烧器的方法
公开(公告)号：US20140137566A1
公开(公告)日：2014-05-22
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
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。

4. 发明申请

US20140123671A1 COMBUSTOR AND METHOD OF SUPPLYING FUEL TO THE COMBUSTOR 有权
标题翻译：燃料和燃料供应给燃烧器的方法
公开(公告)号：US20140123671A1
公开(公告)日：2014-05-08
申请号：US14122694
申请日：2011-06-30
申请人： Borys Borysovich Shershnyov , Geoffrey David Myers , Leonid Yulyevich Ginesin
发明人： Borys Borysovich Shershnyov , Geoffrey David Myers , Leonid Yulyevich Ginesin
IPC分类号： F23R3/28 , F23R3/14 , F23R3/34
CPC分类号： F23R3/286 , F23R3/14 , F23R3/34 , F23R3/343 , F23R3/54
摘要： A combustor (10) includes a liner (12) that defines a combustion chamber (18) first pre-mix chamber (14) is upstream of the combustion chamber, and a fuel plenum (40) in fluid communication with the first pre-mix chamber surrounds a least a portion of the first pre-mix chamber. A method of supplying a fuel to combustor includes flowing the fuel over an outer surface of a first pre-mix chamber and into the first pre-mix chamber.
摘要翻译：燃烧器（10）包括限定燃烧室（18）的衬套（12），第一预混合室（14）在燃烧室的上游，以及与第一预混合物流体连通的燃料增压室（40）腔室围绕第一预混合室的至少一部分。向燃烧器供应燃料的方法包括将燃料流过第一预混合室的外表面并进入第一预混合室。

5. 发明授权

US09097184B2 Gas turbine system having premixed injector vanes 有权
标题翻译：燃气轮机系统具有预混喷油器叶片
公开(公告)号：US09097184B2
公开(公告)日：2015-08-04
申请号：US12981451
申请日：2010-12-29
申请人： Sergey Aleksandrovich Stryapunin , Kevin Weston McMahan , Geoffrey David Myers
发明人： Sergey Aleksandrovich Stryapunin , Kevin Weston McMahan , Geoffrey David Myers
IPC分类号： F02C7/22 , F02C9/26 , F23R3/20 , F23R3/34
CPC分类号： F02C7/22 , F02C9/26 , F23R3/20 , F23R3/34 , F23R2900/03341 , Y02E20/16 , Y02T50/67
摘要： In certain exemplary embodiments, a system includes an annular duct having an inner annular wall and an outer annular wall. The system also includes a plurality of injector vanes configured to mix air and fuel to produce an air-fuel mixture, and configured to inject the air-fuel mixture into a central chamber between the inner and outer annular walls.
摘要翻译：在某些示例性实施例中，系统包括具有内环形壁和外环形壁的环形管道。该系统还包括多个喷射器叶片，其构造成混合空气和燃料以产生空气 - 燃料混合物，并且构造成将空气 - 燃料混合物喷射到内部和外部环形壁之间的中心室中。

6. 发明授权

US08915089B2 System and method for detecting and controlling flashback and flame holding within a combustor 有权
标题翻译：用于检测和控制燃烧器内的回火和火焰保持的系统和方法
公开(公告)号：US08915089B2
公开(公告)日：2014-12-23
申请号：US12692942
申请日：2010-01-25
申请人： Geoffrey David Myers , Timothy Joseph Rehg , Timothy Andrew Healy , Anthony Wayne Krull
发明人： Geoffrey David Myers , Timothy Joseph Rehg , Timothy Andrew Healy , Anthony Wayne Krull
IPC分类号： F02G3/00 , F02C3/00 , F02C6/00 , F02C1/00 , F02C9/00 , F23N1/02 , F23D5/12 , F23N5/08 , G01J5/02 , F23N5/04 , F23N5/24 , F23D14/82 , F23R3/28
CPC分类号： F23N5/08 , F23D14/82 , F23D2208/10 , F23D2209/10 , F23D2900/00008 , F23N5/04 , F23N5/082 , F23N5/242 , F23N2041/20 , F23R3/286 , F23R2900/00002
摘要： A system is provided for detecting and controlling flashback and flame holding in a combustor of a gas turbine. The system includes at least one flame indicator disposed in a combustor and at least one detector disposed downstream from the flame indicator. The flame indicator may be configured to produce light when exposed to a flame and the detector may be configured to detect the light produced by the flame indicator.
摘要翻译：提供一种用于检测和控制燃气轮机的燃烧器中的回火和火焰保持的系统。该系统包括设置在燃烧器中的至少一个火焰指示器和设置在火焰指示器下游的至少一个检测器。火焰指示器可以被配置为当暴露于火焰时产生光，并且检测器可以被配置为检测由火焰指示器产生的光。

7. 发明授权

US08650883B2 System and method for operating a gas turbine 有权
标题翻译：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。

8. 发明申请

US20130098040A1 SYSTEM FOR TURBINE COMBUSTOR FUEL ASSEMBLY 有权
标题翻译：涡轮机燃油组件系统
公开(公告)号：US20130098040A1
公开(公告)日：2013-04-25
申请号：US13280200
申请日：2011-10-24
申请人： Hua Zhang , Douglas Frank Beadie , Geoffrey David Myers , Fabien Thibault Codron , Gregory Allen Boardman
发明人： Hua Zhang , Douglas Frank Beadie , Geoffrey David Myers , Fabien Thibault Codron , Gregory Allen Boardman
IPC分类号： F23R3/28
CPC分类号： F02C3/305 , F02C9/48 , F05D2270/08 , F05D2270/112
摘要： A system includes a gas turbine engine having a combustor, a liquid fuel supply coupled to the combustor, and a water supply coupled to the liquid fuel supply. The water supply is configured to flow water through the liquid fuel supply while the liquid fuel supply is not in use to flow a liquid fuel.
摘要翻译：一种系统包括具有燃烧器，连接到燃烧器的液体燃料供应的燃气涡轮发动机和与液体燃料供应相连接的供水。供水构造成在液体燃料供应不用于流动液体燃料的同时使水流过液体燃料供应。

9. 发明申请

US20120036862A1 SYSTEM AND METHOD FOR OPERATING A GAS TURBINE 有权
标题翻译：用于运行气体涡轮机的系统和方法
公开(公告)号：US20120036862A1
公开(公告)日：2012-02-16
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： F02C7/22 , F02C1/00
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。

10. 发明授权

US08019523B2 Late lean injection with adjustable air splits 有权
公开(公告)号：US08019523B2
公开(公告)日：2011-09-13
申请号：US12349933
申请日：2009-01-07
申请人： Lewis Berkley Davis, Jr. , Krishna Kumar Venkataraman , Willy Steve Ziminsky , Geoffrey David Myers
发明人： Lewis Berkley Davis, Jr. , Krishna Kumar Venkataraman , Willy Steve Ziminsky , Geoffrey David Myers
IPC分类号： F02C3/00 , G06F19/00
摘要： A gas turbine engine is provided and includes a combustor having a first interior in which a first fuel is combustible, a turbine into which products of at least the combustion of the first fuel are receivable, a transition zone, including a second interior in which a second fuel and the products of the combustion of the first fuel are combustible, a plurality of fuel injectors which are configured to supply the second fuel to the second interior in any one of a single axial stage, multiple axial stages, a single axial circumferential stage and multiple axial circumferential stages, a compressor, by which air is supplied to the first and second interiors for the combustion therein, and a control system configured to control relative amounts of the air to the first and second interiors and relative amounts of the first and second fuels supplied to the first and second interiors.

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