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公开(公告)号：US20160229547A1
公开(公告)日：2016-08-11
申请号：US15028611
申请日：2014-09-23
CPC分类号： B64D31/06 , B64C11/303 , B64C11/305 , F01D5/02 , F02C9/00 , F04D27/004 , F04D29/325 , F04D29/362 , F05D2220/324 , F05D2220/325 , F05D2220/36 , F05D2260/70 , F05D2270/02 , F05D2270/70
摘要： A turboprop control system 10 for use with a turboprop 2 having a turbine engine 12 operably coupled to and rotationally driving a propeller 14 having variable pitch blades 16 to control the engine speed, propeller speed, and propeller pitch. The pilot provides, by a single power control lever 30, the control input used to control the engine and propeller.
摘要翻译： 涡轮螺旋桨发动机控制系统10，其用于具有涡轮发动机12的涡轮螺旋桨发动机控制系统10，涡轮发动机12可操作地联接到旋转驱动具有可变桨距叶片16的螺旋桨14，以控制发动机速度，螺旋桨速度和螺旋桨桨距。 飞行员通过单个功率控制杆30提供用于控制发动机和螺旋桨的控制输入。
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公开(公告)号：US08751423B2
公开(公告)日：2014-06-10
申请号：US12956689
申请日：2010-11-30
IPC分类号： G06N5/00
CPC分类号： F02C9/00 , F05D2260/80 , F05D2270/44 , F05D2270/70 , F05D2270/71 , G06N7/005
摘要： A turbine performance diagnostic system creates a performance report for one or more turbines and includes an assessment module that receives operating data from at least one turbine and produces a performance report from the operating data. The assessment module includes a change detection module configured to determine when at least one parameter has changed beyond an associated threshold and generate an alarm and a root cause analyzer coupled to the change detection module that predicts a root cause of the alarm utilizing a Bayesian Belief Network (BBN). The performance report includes an indication of the predicted root cause.
摘要翻译： 涡轮机性能诊断系统为一个或多个涡轮机创建一个性能报告，并且包括一个评估模块，该评估模块从至少一个涡轮机接收运行数据，并从运行数据产生一个性能报告。 所述评估模块包括变化检测模块，所述变化检测模块被配置为确定何时至少一个参数已经改变超过相关联的阈值，并且生成警报，以及耦合到所述变化检测模块的根本原因分析器，所述变化检测模块使用贝叶斯信念网络预测所述警报的根本原因 （BBN）。 绩效报告包括预测根本原因的指示。
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公开(公告)号：US08126628B2
公开(公告)日：2012-02-28
申请号：US11833596
申请日：2007-08-03
申请人： John Erik Hershey , Brock Estel Osborn , Donald Lee Gardner , Rafael Jose Ruiz , William Lee Herron
发明人： John Erik Hershey , Brock Estel Osborn , Donald Lee Gardner , Rafael Jose Ruiz , William Lee Herron
CPC分类号： F01D11/24 , F02C9/00 , F02C9/26 , F02C9/48 , F05D2270/305 , F05D2270/44 , F05D2270/70
摘要： A method and system adjusts blade tip clearance between rotating aircraft gas turbine engine blade tips and a surrounding shroud in anticipation of and before an engine command that changes an engine rotational speed. The method may include determining when to begin adjusting the tip clearance by expanding or contracting the shroud before the engine command and may be based on monitored aircraft and/or aircraft crew data indicative of the engine. The aircraft and/or aircraft crew data may include communications between aircraft crew and air traffic control authorities or air traffic control surrogates. Determining when to begin adjusting the tip clearance may include using learning algorithms which may use the aircraft gas turbine engine's operating experience and/or operating experience of other jet engines on an aircraft containing the aircraft gas turbine engine and/or on other aircraft.
摘要翻译： 一种方法和系统预期在改变发动机转速的发动机命令之前和之前调整旋转飞机燃气涡轮发动机叶片尖端和周围罩之间的叶片顶端间隙。 该方法可以包括通过在发动机命令之前扩展或收缩护罩来确定何时开始调整顶端间隙，并且可以基于指示发动机的受监视的飞行器和/或飞机机组数据。 飞机和/或飞机机组数据可以包括飞机机组人员和空中交通管制机构或空中交通管制代理人之间的通信。 确定何时开始调整尖端间隙可以包括使用学习算法，其可以使用飞机燃气涡轮发动机在包含飞机燃气涡轮发动机的飞机和/或其它飞行器上的其它喷气发动机的操作经验和/或操作经验。
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公开(公告)号：US07647778B2
公开(公告)日：2010-01-19
申请号：US11591552
申请日：2006-11-02
申请人： Netsebrak T Zewde , Arthur L Rowe
发明人： Netsebrak T Zewde , Arthur L Rowe
IPC分类号： F02C9/18
CPC分类号： F02C9/18 , F05D2270/023 , F05D2270/06 , F05D2270/301 , F05D2270/64 , F05D2270/70
摘要： It is known that power is normally extracted within a gas turbine engine from a shaft in order to drive auxiliary devices such as electrical power generators. With high extraction rates from such shafts there is mismatching in rotational speeds between the shafts which must be adjusted through leakage taken from valves 8, 9. By measuring parameters and in particular pressure at a number of positions or parts within an engine arrangement 1 and comparing those parameters either through ratios or directly with reference values a controller can be configured in order to choose the correct sequence and scheduling of the valves 8, 9 opening to balance shaft speed. In such circumstances more efficient operation of the engine arrangement can be achieved over a wider range of engine speeds including idling.
摘要翻译： 众所周知，通常在燃气涡轮发动机内从轴提取动力，以驱动诸如发电机之类的辅助装置。 由于这种轴的提取速度很高，轴之间的转速不匹配，必须通过阀8,9的泄漏来调节。通过测量发动机装置1内的多个位置或部件上的参数，特别是压力，并比较 这些参数可以通过比例或直接与参考值配置，以便控制器可以被配置为选择正确的顺序和调节阀8,9打开以平衡轴速度。 在这种情况下，可以在更宽范围的发动机速度（包括空转）下实现发动机装置的更有效的操作。
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5.发明申请System and method for real-time detection of gas turbine or aircraft engine blade problems 审中-公开实时检测燃气轮机或飞机发动机叶片问题的系统和方法公开(公告)号：US20090228230A1
公开(公告)日：2009-09-10
申请号：US12075059
申请日：2008-03-06
申请人： Vinay Bhaskar Jammu , Sudhanshu Rai , Srihari Balasubramanian , Mandar Kalidas Chati , Omprakash Velagandula , Nirm Velumylum Nirmalan
发明人： Vinay Bhaskar Jammu , Sudhanshu Rai , Srihari Balasubramanian , Mandar Kalidas Chati , Omprakash Velagandula , Nirm Velumylum Nirmalan
CPC分类号： F01D21/003 , F01D17/085 , F05D2270/112 , F05D2270/70 , G01M15/14
摘要： A method and system are implemented to detect gas turbine blade problems in real time and provide more accurate prediction capabilities than known techniques due to inclusion of physics-based correction and temperature modeling methods for the hot gas path parts lifing. The system and method use pyrometer data and operational data to generate physics-based corrections of pyrometer data and physics-based bucket temperature estimations and failure signatures.
摘要翻译： 实现了一种方法和系统来实时检测燃气轮机叶片问题，并提供比已知技术更准确的预测能力，因为包括基于物理学的校正和温度建模方法用于热气路径部件升降。 系统和方法使用高温计数据和操作数据来生成基于物理学的高温计数据和基于物理的桶温度估计和故障签名的校正。
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公开(公告)号：US09932120B2
公开(公告)日：2018-04-03
申请号：US15028611
申请日：2014-09-23
CPC分类号： B64D31/06 , B64C11/303 , B64C11/305 , F01D5/02 , F02C9/00 , F04D27/004 , F04D29/325 , F04D29/362 , F05D2220/324 , F05D2220/325 , F05D2220/36 , F05D2260/70 , F05D2270/02 , F05D2270/70
摘要： A turboprop control system 10 for use with a turboprop 2 having a turbine engine 12 operably coupled to and rotationally driving a propeller 14 having variable pitch blades 16 to control the engine speed, propeller speed, and propeller pitch. The pilot provides, by a single power control lever 30, the control input used to control the engine and propeller.
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7.发明授权Asset-specific equipment health monitoring (EHM) for industrial equipment using standardized asset models 有权使用标准资产模型的工业设备的资产特定设备健康监测（EHM）公开(公告)号：US08896437B2
公开(公告)日：2014-11-25
申请号：US13012592
申请日：2011-01-24
申请人： Rajat Sadana
发明人： Rajat Sadana
CPC分类号： F02C9/00 , F01D21/003 , F05D2260/80 , F05D2270/70
摘要： A system includes at least one sensor and an equipment health monitoring (EHM) unit. The at least one sensor is configured to measure one or more characteristics of an asset, where the asset includes a piece of equipment. The EHM unit includes at least one sensor interface configured to receive at least one input signal associated with the asset from the sensor(s). The EHM unit also includes at least one processing unit operable to be pre-configured to identify a specified fault in the asset using the input signals and an asset-specific model that includes a combination of standard subsystem models. The EHM unit further includes at least one output interface configured to provide an indicator identifying the fault. The standard subsystem models could include standardized fault models configured to identify faults for standard assets.
摘要翻译： 系统包括至少一个传感器和设备健康监测（EHM）单元。 所述至少一个传感器被配置为测量资产的一个或多个特征，其中所述资产包括一件设备。 EHM单元包括至少一个传感器接口，被配置为从传感器接收与资产相关联的至少一个输入信号。 EHM单元还包括至少一个处理单元，其可操作以预先配置为使用输入信号来识别资产中的指定故障，以及包括标准子系统模型的组合的资产特定模型。 EHM单元还包括至少一个输出接口，其被配置为提供识别故障的指示符。 标准子系统模型可以包括配置为识别标准资产故障的标准化故障模型。
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公开(公告)号：US08707709B2
公开(公告)日：2014-04-29
申请号：US12415065
申请日：2009-03-31
IPC分类号： F02C6/08
CPC分类号： F02C7/16 , F01D25/12 , F02C7/18 , F02C9/18 , F02C9/28 , F05D2270/30 , F05D2270/301 , F05D2270/303 , F05D2270/70
摘要： Embodiments of methods and apparatus for providing compressor extraction cooling are provided. According to one example embodiment, a method is disclosed for controlling compressor extraction cooling. The method can include providing a cooling medium. The method can include extracting air from a compressor associated with a gas turbine. The method can also include introducing the cooling medium to the compressor extraction air, wherein the compressor extraction air is cooled by the cooling medium prior to or during introduction to the turbine section. Furthermore, method can include selectively controlling at least one of the compressor extraction air or the cooling medium based at least in part on a characteristic associated with the gas turbine.
摘要翻译： 提供了用于提供压缩机提取冷却的方法和装置的实施例。 根据一个示例性实施例，公开了一种用于控制压缩机提取冷却的方法。 该方法可以包括提供冷却介质。 该方法可以包括从与燃气轮机相关联的压缩机中提取空气。 该方法还可以包括将冷却介质引入到压缩机抽出空气中，其中压缩机抽出空气在引入涡轮部分之前或期间由冷却介质冷却。 此外，方法可以包括至少部分地基于与燃气轮机相关联的特性来选择性地控制压缩机提取空气或冷却介质中的至少一个。
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公开(公告)号：US20120136819A1
公开(公告)日：2012-05-31
申请号：US12956689
申请日：2010-11-30
CPC分类号： F02C9/00 , F05D2260/80 , F05D2270/44 , F05D2270/70 , F05D2270/71 , G06N7/005
摘要： A turbine performance diagnostic system creates a performance report for one or more turbines and includes an assessment module that receives operating data from at least one turbine and produces a performance report from the operating data. The assessment module includes a change detection module configured to determine when at least one parameter has changed beyond an associated threshold and generate an alarm and a root cause analyzer coupled to the change detection module that predicts a root cause of the alarm utilizing a Bayesian Belief Network (BBN). The performance report includes an indication of the predicted root cause.
摘要翻译： 涡轮机性能诊断系统为一个或多个涡轮机创建一个性能报告，并且包括一个评估模块，该评估模块从至少一个涡轮机接收运行数据，并从运行数据产生一个性能报告。 所述评估模块包括变化检测模块，所述变化检测模块被配置为确定何时至少一个参数已经改变超过相关联的阈值，并且生成警报，以及耦合到所述变化检测模块的根本原因分析器，所述变化检测模块使用贝叶斯信念网络预测所述警报的根本原因 （BBN）。 性能报告包括预测根本原因的指示。
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公开(公告)号：US07752833B2
公开(公告)日：2010-07-13
申请号：US11328942
申请日：2006-01-10
申请人： Majid Feiz
发明人： Majid Feiz
IPC分类号： F02C9/00
CPC分类号： F02C9/28 , F02C3/22 , F02C7/22 , F05D2260/96 , F05D2270/3011 , F05D2270/3013 , F05D2270/44 , F05D2270/56 , F05D2270/62 , F05D2270/70
摘要： A method for reducing or eliminating oscillations in a gas turbine fuel control system includes utilizing an engine model to regulate a gas supply pressure for a gas turbine, sensing the pressure of gas actually supplied, and applying integral state feedback plus gas supply pressure feedforward combined with integral plus state feedback to the engine model to control and reduce gas fuel supply variations.
摘要翻译： 一种用于减少或消除燃气轮机燃料控制系统中的振荡的方法包括利用发动机模型来调节燃气轮机的气体供应压力，感测实际供应的气体的压力，以及将积分状态反馈加气体供应压力前馈与 整体加状态反馈到发动机模型，以控制和减少燃气供应变化。
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