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公开(公告)号：US20060260319A1
公开(公告)日：2006-11-23
申请号：US10908643
申请日：2005-05-20
申请人： Willy Ziminsky , Scott Kopcho , Mark Bombard , Anthony Antonucci
发明人： Willy Ziminsky , Scott Kopcho , Mark Bombard , Anthony Antonucci
IPC分类号： F02C7/00
CPC分类号： F02C7/228 , F02C7/222 , F02C9/263 , F02C9/28 , F02C9/32 , F05D2250/312 , F05D2270/082 , F05D2270/31
摘要： An embodiment may comprise a system for controlling NOx emissions from a turbine having combustion chambers. The system may comprise a center fuel flow and a plurality of outer fuel flows for each of a plurality of combustion chambers. An outer fuel flow is set to achieve a desired level of combustion dynamics for at least one of the plurality of combustion chambers. A delta adjustment value is determined for the center fuel flow that will result in a desired level of NOx emissions from the turbine, and for adjusting the center fuel flow according to the determined delta adjustment value to obtain the desired level of NOx emissions from the turbine.
摘要翻译： 实施例可以包括用于控制具有燃烧室的涡轮机的NOx排放的系统。 该系统可以包括用于多个燃烧室中的每一个的中心燃料流和多个外部燃料流。 外部燃料流被设定成为多个燃烧室中的至少一个实现期望的燃烧动态水平。 确定中心燃料流量的增量调整值，其将导致来自涡轮机的期望水平的NOx排放，并且用于根据确定的增量调节值来调节中心燃料流量，以获得来自涡轮机的期望的NOx排放水平 。
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公开(公告)号：US07441398B2
公开(公告)日：2008-10-28
申请号：US10908643
申请日：2005-05-20
IPC分类号： F02C9/26
CPC分类号： F02C7/228 , F02C7/222 , F02C9/263 , F02C9/28 , F02C9/32 , F05D2250/312 , F05D2270/082 , F05D2270/31
摘要： An embodiment may comprise a system for controlling NOx emissions from a turbine having combustion chambers. The system may comprise a center fuel flow and a plurality of outer fuel flows for each of a plurality of combustion chambers. An outer fuel flow is set to achieve a desired level of combustion dynamics for at least one of the plurality of combustion chambers. A delta adjustment value is determined for the center fuel flow that will result in a desired level of NOx emissions from the turbine, and for adjusting the center fuel flow according to the determined delta adjustment value to obtain the desired level of NOx emissions from the turbine.
摘要翻译： 实施例可以包括用于控制具有燃烧室的涡轮机的NOx排放的系统。 该系统可以包括用于多个燃烧室中的每一个的中心燃料流和多个外部燃料流。 外部燃料流被设定成为多个燃烧室中的至少一个实现期望的燃烧动态水平。 确定中心燃料流量的增量调整值，其将导致来自涡轮机的期望水平的NOx排放，并且用于根据确定的增量调节值来调节中心燃料流量，以获得来自涡轮机的期望的NOx排放水平 。
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公开(公告)号：US20090007566A1
公开(公告)日：2009-01-08
申请号：US12212812
申请日：2008-09-18
IPC分类号： F02C7/00
CPC分类号： F02C7/228 , F02C7/222 , F02C9/263 , F02C9/28 , F02C9/32 , F05D2250/312 , F05D2270/082 , F05D2270/31
摘要： A method for controlling NOx emissions from a gas turbine having a fuel adjustment system may include setting an outer nozzle fuel flow to achieve a desired level of combustion dynamics for at least one of a plurality of combustion chambers, determining a delta adjustment value for a center nozzle fuel flow that will result in a desired level of NOx emissions from the gas turbine, and adjusting the center nozzle fuel flow according to the determined delta adjustment value to obtain the desired level of NOx emissions from the gas turbine.
摘要翻译： 用于控制具有燃料调节系统的燃气轮机的NOx排放的方法可包括设定外部喷嘴燃料流量以实现多个燃烧室中的至少一个燃烧室的期望水平的燃烧动态，确定中心的增量调节值 喷嘴燃料流量将导致来自燃气轮机的期望水平的NOx排放，并且根据确定的增量调节值调节中心喷嘴燃料流量，以获得来自燃气轮机的期望的NOx排放水平。
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公开(公告)号：US08033117B2
公开(公告)日：2011-10-11
申请号：US12212812
申请日：2008-09-18
IPC分类号： F02C7/22
CPC分类号： F02C7/228 , F02C7/222 , F02C9/263 , F02C9/28 , F02C9/32 , F05D2250/312 , F05D2270/082 , F05D2270/31
摘要： A method for controlling NOx emissions from a gas turbine having a fuel adjustment system may include setting an outer nozzle fuel flow to achieve a desired level of combustion dynamics for at least one of a plurality of combustion chambers, determining a delta adjustment value for a center nozzle fuel flow that will result in a desired level of NOx emissions from the gas turbine, and adjusting the center nozzle fuel flow according to the determined delta adjustment value to obtain the desired level of NOx emissions from the gas turbine.
摘要翻译： 用于控制具有燃料调节系统的燃气轮机的NOx排放的方法可包括设定外部喷嘴燃料流量以实现多个燃烧室中的至少一个燃烧室的期望水平的燃烧动态，确定中心的增量调节值 喷嘴燃料流量将导致来自燃气轮机的期望水平的NOx排放，并且根据确定的增量调节值调节中心喷嘴燃料流量，以获得来自燃气轮机的期望的NOx排放水平。
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公开(公告)号：US20070062196A1
公开(公告)日：2007-03-22
申请号：US11229168
申请日：2005-09-16
申请人： Eamon Gleeson , Warren Mick , George Williams , Fei Han , Shivakumar Srinivasan , Scott Kopcho , Ilan Leibu
发明人： Eamon Gleeson , Warren Mick , George Williams , Fei Han , Shivakumar Srinivasan , Scott Kopcho , Ilan Leibu
IPC分类号： F02C7/00
CPC分类号： F23N5/242 , F23N5/16 , F23N2031/10 , F23N2041/20
摘要： A method for determining when a combustor is experiencing hardware damage includes sensing acoustic vibrations of a plurality of combustor cans, determining a center frequency for each acoustic tone of the sensed acoustic vibrations within a predetermined frequency range, and indicating an alarm when a center frequency of one or more of the combustor cans changes in a different manner compared to a representative center frequency of the plurality of combustor cans.
摘要翻译： 一种用于确定燃烧器何时经历硬件损坏的方法包括：感测多个燃烧器罐的声振动，确定预定频率范围内感测到的声振动的每个声音的中心频率，并且当中心频率为 与多个燃烧器罐的代表性中心频率相比，一个或多个燃烧器罐以不同的方式改变。
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6.发明授权Systems and methods for detecting the flame state of a combustor of a turbine engine 有权用于检测涡轮发动机的燃烧器的火焰状态的系统和方法公开(公告)号：US08601861B1
公开(公告)日：2013-12-10
申请号：US13572107
申请日：2012-08-10
IPC分类号： G01M15/14
摘要： Systems and methods of determining a flame state within a combustor of a turbine engine make use of characteristics of an output pressure of a compressor of the turbine engine and a temperature of exhaust gases of the turbine engine to make a determination. If the first and/or second derivatives of the output pressure of the compressor and the first and/or second derivatives of the exhaust gas temperature of the turbine engine are all positive during at least portions of a predetermined period of time, one can determine that a flame has ignited in the combustor. If those values are negative during at least portions of a predetermined period of time, one can determine that a flame has been extinguished in the combustor.
摘要翻译： 确定涡轮发动机的燃烧器内的火焰状态的系统和方法利用涡轮发动机的压缩机的输出压力和涡轮发动机的废气温度的特性进行确定。 如果压缩机的输出压力的第一和/或二阶导数和涡轮发动机的排气温度的第一和/或第二导数在预定时间段的至少部分期间都是正的，则可以确定 火焰在燃烧器中点燃。 如果在预定时间段的至少部分期间这些值是负的，则可以确定燃烧器中的火焰已经熄灭。
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7.发明申请METHOD AND SYSTEM FOR DETERMINING LEAN BLOW OUT CONDITION FOR GAS TURBINE COMBUSTION CANS 有权用于确定燃气涡轮机燃烧罐的亮度冷却条件的方法和系统公开(公告)号：US20060248893A1
公开(公告)日：2006-11-09
申请号：US10908309
申请日：2005-05-06
申请人： Warren Mick , George Williams , Fei Han , Eamon Gleeson , Shiva Srinivasan , Scott Kopcho , Ilan Leibu
发明人： Warren Mick , George Williams , Fei Han , Eamon Gleeson , Shiva Srinivasan , Scott Kopcho , Ilan Leibu
IPC分类号： F02C7/00
CPC分类号： F02C9/00 , F01D21/003 , F05D2270/092 , F05D2270/14 , F05D2270/301 , F23N5/242 , F23N2025/04 , F23N2031/06
摘要： A method for determining a lean blow out condition for a combustor. In an exemplary embodiment, the method includes determining acoustical frequency data for the combustor, determining a combustor flame temperature based on the acoustical frequency data, determining an existing fuel/air ratio in the combustor based on the combustor flame temperature, and comparing the existing fuel/ratio to a lean blow out fuel/air ratio. A lean blow out condition for the combustor is indicated when the existing fuel/air ratio is about equal to the lean blow out fuel/air ratio.
摘要翻译： 一种用于确定燃烧器的稀薄吹出条件的方法。 在示例性实施例中，该方法包括确定燃烧器的声频数据，基于声频数据确定燃烧器火焰温度，基于燃烧器火焰温度确定燃烧器中的现有燃料/空气比，以及比较现有燃料 /比与精馏燃料/空气比。 当现有燃料/空气比约等于稀吹出燃料/空气比时，指示燃烧器的稀薄吹出条件。
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