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1.发明申请公开(公告)号：US20150192912A1
公开(公告)日：2015-07-09
申请号：US14149349
申请日：2014-01-07
发明人： Prabhanjana Kalya , Steven William Backman , Laura Lea Boes , David Spencer Ewens , Trevor Valder Jones
IPC分类号： G05B15/00
CPC分类号： G05B15/00 , F02C7/228 , F02C9/00 , F02C9/28 , F02C9/34 , F05D2270/08 , F05D2270/082 , F23N2037/02 , F23N2041/20 , F23R3/34
摘要： A method and system for transferring between combustion modes in a gas turbine engine is provided. A processor generates data representative of an initial set of splits for providing at least one of fuel and air to at least one combustor in the gas turbine engine. A gas turbine engine model module generates data representative of at least one engine operating condition. A first split calculation module generates data representative of at least one set of active control splits to control the engine in a first combustion mode, using as an input the initial split data. A second split calculation module generates data representative of at least one set of passive control splits to control the engine in at least a second combustion mode. Transfer between combustion modes may be accomplished via use of at least one of the active control splits and the passive control splits.
摘要翻译： 提供了一种用于在燃气涡轮发动机中的燃烧模式之间进行转换的方法和系统。 处理器产生代表初始分组集合的数据，用于将燃料和空气中的至少一个提供给燃气涡轮发动机中的至少一个燃烧器。 燃气涡轮发动机模型模块生成代表至少一个发动机运行状态的数据。 第一分割计算模块生成代表至少一组主动控制分段的数据，以使用初始分割数据作为输入来控制处于第一燃烧模式的发动机。 第二分割计算模块生成表示至少一组无源控制分段的数据，以在至少第二燃烧模式中控制发动机。 燃烧模式之间的转换可以通过使用至少一个主动控制分流器和被动控制分流器来完成。
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公开(公告)号：US20160025596A1
公开(公告)日：2016-01-28
申请号：US14340289
申请日：2014-07-24
发明人： Sanjeev Shyam Heda , Steven William Backman , Matthew John Mckeever , Scott Alan Wood , Carlo Angelo Yon , Robert Joseph Iasillo , Christopher Childs
CPC分类号： G01M15/14 , F01D21/003 , G05B23/0232 , G05B23/0235
摘要： A system for remote detection of surge in a fleet of turbine engines includes an on-site monitoring device coupled to each turbine engine of the fleet of turbine engines. The on-site monitoring device is configured to continuously receive operating parameter measurements indicative of operational and thermodynamic conditions of the turbine engine. The operational condition includes a compressor exit condition of the turbine engine compressor. The on-site monitoring device is configured to compile and transmit a snapshot of the operating parameter measurements to a remote monitoring unit. The remote monitoring unit is positioned remote from each turbine engine of the fleet of turbine engines. The remote monitoring unit is configured to receive the snapshot of operating parameter measurements from the on-site monitoring device. The remote monitoring unit is further configured to detect surge in the turbine engine based on analysis of the snapshot of operating parameter measurements.
摘要翻译： 用于远程检测涡轮发动机的浪涌的系统包括耦合到涡轮发动机车队的每个涡轮发动机的现场监测装置。 现场监控装置被配置为连续接收指示涡轮发动机的操作和热力学条件的操作参数测量。 操作条件包括涡轮发动机压缩机的压缩机出口状态。 现场监控设备被配置为将操作参数测量的快照编译并发送到远程监控单元。 远程监控单元位于远离涡轮发动机车队的每个涡轮发动机的位置。 远程监控单元被配置为从现场监控设备接收操作参数测量的快照。 远程监视单元还被配置为基于对操作参数测量的快照的分析来检测涡轮发动机中的浪涌。
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公开(公告)号：US10180107B2
公开(公告)日：2019-01-15
申请号：US15453399
申请日：2017-03-08
发明人： Steven William Backman , Trevor Valder Jones , Daniel Joseph Flavin , Scott Michael Schaberg , Kelly Marie Kurylo
IPC分类号： F02C9/26 , F02C3/04 , F02C7/228 , G05B19/042
摘要： A non-transitory computer readable storage medium storing one or more processor-executable instructions wherein the one or more instructions when executed by a processor of a controller, cause acts to be performed is provided. The acts to be performed include controlling a fuel split to a combustor of a gas turbine utilizing automatic tuning and switching control of the fuel split to the combustor of the gas turbine to utilizing an adjusted fixed fuel split schedule instead of automatic tuning. The adjusted fixed fuel split schedule includes a fixed fuel split schedule adjusted via a biasing value, and the biasing value is based on both the fixed fuel split schedule and an automatic tuning based fuel split.
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公开(公告)号：US09639071B2
公开(公告)日：2017-05-02
申请号：US14149349
申请日：2014-01-07
发明人： Prabhanjana Kalya , Steven William Backman , Laura Lea Boes , David Spencer Ewens , Trevor Valder Jones
CPC分类号： G05B15/00 , F02C7/228 , F02C9/00 , F02C9/28 , F02C9/34 , F05D2270/08 , F05D2270/082 , F23N2037/02 , F23N2041/20 , F23R3/34
摘要： A method and system for transferring between combustion modes in a gas turbine engine is provided. A processor generates data representative of an initial set of splits for providing at least one of fuel and air to at least one combustor in the gas turbine engine. A gas turbine engine model module generates data representative of at least one engine operating condition. A first split calculation module generates data representative of at least one set of active control splits to control the engine in a first combustion mode, using as an input the initial split data. A second split calculation module generates data representative of at least one set of passive control splits to control the engine in at least a second combustion mode. Transfer between combustion modes may be accomplished via use of at least one of the active control splits and the passive control splits.
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公开(公告)号：US20180258863A1
公开(公告)日：2018-09-13
申请号：US15453399
申请日：2017-03-08
发明人： Steven William Backman , Trevor Valder Jones , Daniel Joseph Flavin , Scott Michael Schaberg , Kelly Marie Kurylo
IPC分类号： F02C9/26 , F02C3/04 , F02C7/228 , G05B19/042
CPC分类号： F02C9/26 , F02C3/04 , F02C7/228 , F02C9/34 , F05D2220/32 , F05D2240/35 , F05D2270/082 , F05D2270/31 , F05D2270/54 , F05D2270/70 , G05B19/042
摘要： A non-transitory computer readable storage medium storing one or more processor-executable instructions wherein the one or more instructions when executed by a processor of a controller, cause acts to be performed is provided. The acts to be performed include controlling a fuel split to a combustor of a gas turbine utilizing automatic tuning and switching control of the fuel split to the combustor of the gas turbine to utilizing an adjusted fixed fuel split schedule instead of automatic tuning. The adjusted fixed fuel split schedule includes a fixed fuel split schedule adjusted via a biasing value, and the biasing value is based on both the fixed fuel split schedule and an automatic tuning based fuel split.
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公开(公告)号：US20170248036A1
公开(公告)日：2017-08-31
申请号：US15056409
申请日：2016-02-29
发明人： Daniel Joseph Flavin, II , Steven William Backman , Scott Michael Schaberg , Trevor Valder Jones
CPC分类号： F01K11/02 , F01K13/003 , F01K13/02 , F01K23/101 , Y02E20/16
摘要： A system may include a gas turbine system. The gas turbine system may include a compressor, such that the gas turbine system may produce exhaust gas in an exhaust outlet when generating electricity. The system may also include a heat recovery steam generator (HRSG) that may use the exhaust gas to create steam, a manifold system configured to couple compressed air in the compressor to the exhaust outlet, and a controller configured to send a command to the manifold system to couple the compressed air to the exhaust outlet when a temperature of the exhaust gas is above a threshold.
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公开(公告)号：US09528913B2
公开(公告)日：2016-12-27
申请号：US14340289
申请日：2014-07-24
发明人： Sanjeev Shyam Heda , Steven William Backman , Matthew John Mckeever , Scott Alan Wood , Carlo Angelo Yon , Robert Joseph Iasillo , Christopher Childs
CPC分类号： G01M15/14 , F01D21/003 , G05B23/0232 , G05B23/0235
摘要： A system for remote detection of surge in a fleet of turbine engines includes an on-site monitoring device coupled to each turbine engine of the fleet of turbine engines. The on-site monitoring device is configured to continuously receive operating parameter measurements indicative of operational and thermodynamic conditions of the turbine engine. The operational condition includes a compressor exit condition of the turbine engine compressor. The on-site monitoring device is configured to compile and transmit a snapshot of the operating parameter measurements to a remote monitoring unit. The remote monitoring unit is positioned remote from each turbine engine of the fleet of turbine engines. The remote monitoring unit is configured to receive the snapshot of operating parameter measurements from the on-site monitoring device. The remote monitoring unit is further configured to detect surge in the turbine engine based on analysis of the snapshot of operating parameter measurements.
摘要翻译： 用于远程检测涡轮发动机的浪涌的系统包括耦合到涡轮发动机车队的每个涡轮发动机的现场监测装置。 现场监控装置被配置为连续接收指示涡轮发动机的操作和热力学条件的操作参数测量。 操作条件包括涡轮发动机压缩机的压缩机出口状态。 现场监控设备被配置为将操作参数测量的快照编译并发送到远程监控单元。 远程监控单元位于远离涡轮发动机车队的每个涡轮发动机的位置。 远程监控单元被配置为从现场监控设备接收操作参数测量的快照。 远程监视单元还被配置为基于对操作参数测量的快照的分析来检测涡轮发动机中的浪涌。
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