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1.发明授权Axial vibration monitoring for detecting shaft misalignments in turbomachinary trains 有权轴向振动监测，用于检测涡轮喷气火车中的轴不对准公开(公告)号：US08322223B2
公开(公告)日：2012-12-04
申请号：US12765974
申请日：2010-04-23
申请人： Malath Ibrahim Arar
发明人： Malath Ibrahim Arar
CPC分类号： G01B21/24
摘要： A system for determining a shaft misalignment in a turbomachinary train having a plurality of components with serially coupled rotating shafts. A disclosed system includes a sensor affixed to a component of the turbomachinary train proximate a rotating shaft, wherein the sensor collects vibration data along an axial direction of the rotating shaft. Also provided is a frequency analyzer for generating frequency domain data from the vibration data and an analysis system for analyzing a frequency component of the frequency domain data at one times a rotational frequency of the rotating shaft to identify a misalignment between the rotating shaft and an adjacently coupled rotating shaft.
摘要翻译： 一种用于确定具有多个具有串联连接的旋转轴的部件的涡轮机中的轴未对准的系统。 所公开的系统包括附接到旋转轴上的涡轮机的部件的传感器，其中传感器沿着旋转轴的轴向方向收集振动数据。 还提供了一种用于从振动数据产生频域数据的频率分析器和用于分析频域数据的频率分量的分析系统，该频率分量是旋转轴的旋转频率的一倍，以识别旋转轴和相邻之间的未对准 耦合旋转轴。
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公开(公告)号：US08973373B2
公开(公告)日：2015-03-10
申请号：US13285209
申请日：2011-10-31
申请人： Malath Ibrahim Arar
发明人： Malath Ibrahim Arar
CPC分类号： F02C9/18 , F01D11/24 , F02C6/08 , F02C7/185 , F05D2220/3218 , F05D2220/3219 , F05D2260/213
摘要： A method to provide clearance control for a gas turbine having a multi-stage compressor and a turbine having turbine buckets rotating within a turbine shell, the method includes: selecting a first compressor stage from which to extract compressed air; ducting the compressed air from the first compressor stage to the turbine shell; passing the compressed air from the first compressor stage to thermally contract the turbine shell; selecting a second compressor stage from which to extract compressed air and deselecting the first compressor stage; ducting the compressed air from the second compressor stage to the turbine shell, and passing the compressed air from the second compressor stage to thermal expand the turbine shell.
摘要翻译： 一种为具有多级压缩机和涡轮机的涡轮机提供间隙控制的方法，所述涡轮机具有在涡轮壳体内旋转的涡轮机叶片，所述方法包括：选择从其中提取压缩空气的第一压缩机级; 将压缩空气从第一压缩机级引导到涡轮壳; 使来自第一压缩机级的压缩空气使涡轮壳体热收缩; 选择第二压缩机级，从其中提取压缩空气并取消选择第一压缩机级; 将压缩空气从第二压缩机级引导到涡轮壳体，并且使来自第二压缩机级的压缩空气通过热膨胀涡轮壳体。
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公开(公告)号：US06519945B2
公开(公告)日：2003-02-18
申请号：US10167075
申请日：2002-06-12
IPC分类号： F02C328
摘要： A nitrogen compressor in an IGCC (integrated gasification, combined cycle) system provides gaseous nitrogen to be directly injected into the combustor of a gas turbine in the IGCC. The nitrogen is injected at substantially the same pressure as the output pressure from the nitrogen compressor. The compressor is controlled to adjust the output pressure of the nitrogen to match a nitrogen injection pressure for the combustor. By controlling the flow (pressure) of the nitrogen injected to a combustor of a gas turbine at the nitrogen compressor, the compressor is relieved of having to overcome the pressure loss through the nitrogen injection valves (which valves are run at or near full open throughout the operation of the nitrogen injection process), and does not need to provide nitrogen at a pressure substantially greater than the nitrogen pressure injected into the combustor.
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公开(公告)号：US06513317B2
公开(公告)日：2003-02-04
申请号：US09758718
申请日：2001-01-11
IPC分类号： F02C328
摘要： A nitrogen compressor in an IGCC (integrated gasification, combined cycle) system provides gaseous nitrogen to be directly injected into the combustor of a gas turbine in the IGCC. The nitrogen is injected at substantially the same pressure as the output pressure from the nitrogen compressor. The compressor is controlled to adjust the output pressure of the nitrogen to match a nitrogen injection pressure for the combustor. By controlling the flow (pressure) of the nitrogen injected to a combustor of a gas turbine at the nitrogen compressor, the compressor is relieved of having to overcome the pressure loss through the nitrogen injection valves (which valves are run at or near full open throughout the operation of the nitrogen injection process), and does not need to provide nitrogen at a pressure substantially greater than the nitrogen pressure injected into the combustor.
摘要翻译： IGCC（综合气化，联合循环）系统中的氮气压缩机提供气态氮气直接喷入IGCC燃气轮机的燃烧室。 以与来自氮压缩机的输出压力基本相同的压力注入氮气。 控制压缩机以调节氮气的输出压力以匹配用于燃烧器的氮气注入压力。 通过控制喷射到氮气压缩机上的燃气轮机的燃烧器的氮气的流量（压力），压缩机不需要通过氮气喷射阀克服压力损失（该阀门在全开或全部运行 氮气喷射过程的操作），并且不需要在基本上大于喷射到燃烧器中的氮气压力的压力下提供氮气。
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公开(公告)号：US6027304A
公开(公告)日：2000-02-22
申请号：US85910
申请日：1998-05-27
申请人： Malath Ibrahim Arar , Timothy Robert Kemp , George Raymond Hubschmitt , David Anthony DeAngelis , James Giles Eignor
发明人： Malath Ibrahim Arar , Timothy Robert Kemp , George Raymond Hubschmitt , David Anthony DeAngelis , James Giles Eignor
摘要： The high pressure inlet bleed heat system includes a plurality of tubes which receive heated compressed air from the compressor extraction discharge manifold. The tubes extend into the inlet duct of the compressor, are uniformly spaced one from the other and have a uniform distribution of laterally opening apertures along their lengths in registration with the apertures of next laterally adjacent tubes. The tubes are located downstream of the silencer baffles. By providing choked flow through the apertures and lateral registration of the apertures of adjacent tubes, complete mixing of the heated air with the inlet air vortices behind the silencer baffles is achieved, affording a uniform temperature distribution across the inlet duct with minimum pressure loss. The tubes are constructed to accommodate thermal expansion of the manifold receiving compressor discharge air, the manifold also being supported to accommodate thermal expansion and contraction.
摘要翻译： 高压入口放气加热系统包括从压缩机排气歧管接收加热的压缩空气的多个管。 管延伸到压缩机的入口管道中，彼此均匀地间隔开，并且沿着它们的长度具有与下一个横向相邻管的孔对准的横向开口孔的均匀分布。 管位于消声器挡板的下游。 通过提供通过孔的扼流和相邻管的孔的横向对准，实现了加热的空气与消声器挡板后面的入口空气涡流的完全混合，从而以最小的压力损失在入口管道上提供均匀的温度分布。 管被构造成适应接收压缩机排放空气的歧管的热膨胀，歧管也被支撑以适应热膨胀和收缩。
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公开(公告)号：US08904747B2
公开(公告)日：2014-12-09
申请号：US13175006
申请日：2011-07-01
摘要： A gas turbine inlet heating system is disclosed. In one embodiment, the system includes: a compressor having: an inlet bellmouth adjacent to a set of inlet guide vanes (IGVs); and an outlet fluidly connected to the inlet bellmouth; and a conduit coupled to an outlet of the compressor, the conduit including a control valve, the conduit for diverting a first portion of compressed air from the outlet of the compressor to the inlet bellmouth.
摘要翻译： 公开了一种燃气轮机进气加热系统。 在一个实施例中，系统包括：压缩机，其具有：与一组入口导叶（IGV）相邻的入口喇叭口; 和与入口喇叭口流体连接的出口; 以及连接到压缩机的出口的导管，所述导管包括控制阀，所述导管用于将压缩空气的第一部分从压缩机的出口转向入口喇叭口。
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公开(公告)号：US20130000321A1
公开(公告)日：2013-01-03
申请号：US13175006
申请日：2011-07-01
摘要： A gas turbine inlet heating system is disclosed. In one embodiment, the system includes: a compressor having: an inlet bellmouth adjacent to a set of inlet guide vanes (IGVs); and an outlet fluidly connected to the inlet bellmouth; and a conduit coupled to an outlet of the compressor, the conduit including a control valve, the conduit for diverting a first portion of compressed air from the outlet of the compressor to the inlet bellmouth.
摘要翻译： 公开了一种燃气轮机进气加热系统。 在一个实施例中，系统包括：压缩机，其具有：与一组入口导叶（IGV）相邻的入口喇叭口; 和与入口喇叭口流体连接的出口; 以及连接到压缩机的出口的导管，所述导管包括控制阀，所述导管用于将压缩空气的第一部分从压缩机的出口转向入口喇叭口。
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8.发明申请AXIAL VIBRATION MONITORING FOR DETECTING SHAFT MISALIGNMENTS IN TURBOMACHINARY TRAINS 有权用于检测涡轮机火箭中的扭矩的轴向振动监测公开(公告)号：US20110259103A1
公开(公告)日：2011-10-27
申请号：US12765974
申请日：2010-04-23
申请人： Malath Ibrahim Arar
发明人： Malath Ibrahim Arar
IPC分类号： G01N29/12
CPC分类号： G01B21/24
摘要： A system for determining a shaft misalignment in a turbomachinary train having a plurality of components with serially coupled rotating shafts. A disclosed system includes a sensor affixed to a component of the turbomachinary train proximate a rotating shaft, wherein the sensor collects vibration data along an axial direction of the rotating shaft. Also provided is a frequency analyzer for generating frequency domain data from the vibration data and an analysis system for analyzing a frequency component of the frequency domain data at one times a rotational frequency of the rotating shaft to identify a misalignment between the rotating shaft and an adjacently coupled rotating shaft.
摘要翻译： 一种用于确定具有多个具有串联连接的旋转轴的部件的涡轮机中的轴未对准的系统。 所公开的系统包括附接到旋转轴上的涡轮机的部件的传感器，其中传感器沿着旋转轴的轴向方向收集振动数据。 还提供了一种用于从振动数据产生频域数据的频率分析器和用于分析频域数据的频率分量的分析系统，该频率分量是旋转轴的旋转频率的一倍，以识别旋转轴和相邻之间的未对准 耦合旋转轴。
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公开(公告)号：US07269952B2
公开(公告)日：2007-09-18
申请号：US10906689
申请日：2005-03-02
IPC分类号： F02C9/28
CPC分类号： F23N5/00 , F02C9/28 , F02C9/50 , F05D2270/082 , F05D2270/083 , F23L7/007 , F23N1/022 , F23N3/002 , F23N5/006 , F23N2025/04 , F23N2025/30 , F23N2035/06 , F23N2037/24 , F23N2037/26 , Y02E20/344
摘要： A method for controlling a combustor of an engine, the combustor having a fuel to oxidant ratio, the fuel to oxidant ratio being defined as a ratio of an amount of fuel supplied to the combustor divided by an amount of oxygen in an oxidant stream supplied to the combustor includes controlling the fuel to oxidant ratio of the combustor as a function of the amount of oxygen in the oxidant stream.
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10.发明授权Method and apparatus for gas turbine dry low NOx combustor corrected parameter control 失效燃气轮机干式低NOx燃烧器校正参数控制方法及装置公开(公告)号：US07237377B2
公开(公告)日：2007-07-03
申请号：US11650255
申请日：2007-01-05
IPC分类号： F02C9/00
CPC分类号： F23N5/00 , F02C9/28 , F02C9/50 , F05D2270/082 , F05D2270/083 , F23L7/007 , F23N1/022 , F23N3/002 , F23N5/006 , F23N2025/04 , F23N2025/30 , F23N2035/06 , F23N2037/24 , F23N2037/26 , Y02E20/344
摘要： A method for controlling a combustor of an engine, the combustor having a fuel to oxidant ratio, the fuel to oxidant ratio being defined as a ratio of an amount of fuel supplied to the combustor divided by an amount of oxygen in an oxidant stream supplied to the combustor includes controlling the fuel to oxidant ratio of the combustor as a function of the amount of oxygen in the oxidant stream.
摘要翻译： 一种用于控制发动机的燃烧器的方法，所述燃烧器具有燃料与氧化剂的比例，所述燃料与氧化剂的比率被定义为供应到所述燃烧器的燃料量除以提供给燃烧器的氧化剂流中的氧气的量的比率 燃烧器包括将燃烧器的燃料与氧化剂的比例控制为氧化剂流中氧的量的函数。
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