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81. 发明申请

US20160283647A1 METHOD OF MODELLING AT LEAST A PART OF A GAS TURBINE ENGINE 审中-公开
标题翻译：至少建立一个气体涡轮发动机的一部分的方法
公开(公告)号：US20160283647A1
公开(公告)日：2016-09-29
申请号：US15072842
申请日：2016-03-17
申请人： ROLLS-ROYCE PLC
发明人： Luca DI MARE , Davendu Y. KULKARNI , Gan LU
IPC分类号： G06F17/50 , F02C9/24
CPC分类号： G06F17/5086 , F02C9/24 , F05D2260/81 , F05D2270/71 , G06F17/5095 , Y02T90/50
摘要： A method of modelling at least a part of a gas turbine engine, the method comprising: preparing a model of at least a part of the gas turbine engine using a data structure including: a first set of data entities representing geometrical shapes of physical features; and a second set of data entities representing geometrical shapes of aerodynamic boundaries, the second set of data entities being used to preserve aerodynamic design intent during preparation of the model.
摘要翻译：一种对燃气涡轮发动机的至少一部分进行建模的方法，所述方法包括：使用数据结构来准备所述燃气涡轮发动机的至少一部分的模型，所述数据结构包括：表示物理特征的几何形状的第一组数据实体; 以及表示空气动力学边界的几何形状的第二组数据实体，第二组数据实体用于在模型准备期间保持空气动力学设计意图。

82. 发明申请

US20160010494A1 SHAFT STIFFNESS 审中-公开
标题翻译：轴强度
公开(公告)号：US20160010494A1
公开(公告)日：2016-01-14
申请号：US14743701
申请日：2015-06-18
申请人： ROLLS-ROYCE PLC
发明人： Mark Nicholas ERLUND , Arthur Laurence ROWE
IPC分类号： F01D21/00 , G01H1/00 , G01H1/10 , F02C9/28
CPC分类号： F01D21/003 , F02C9/28 , F05D2220/32 , F05D2260/83 , F05D2270/05 , F05D2270/331 , F05D2270/334 , F05D2270/335 , F05D2270/44 , F05D2270/71 , G01H1/006 , G01H1/10 , G01L3/04 , G01M15/14
摘要： A method to determine shaft stiffness of a rotating shaft, the shaft coupling a turbine to drive the rotation and a load to be driven by the rotation. For a given operational temperature and rotational speed of the shaft, the method including steps to determine polar moments of inertia of the load and the turbine. Determine natural torsional vibration frequency of the shaft. Determine the shaft stiffness by calculation using the inertias and vibration frequency.
摘要翻译：一种确定旋转轴的轴刚度的方法，所述轴联接涡轮以驱动旋转和由旋转驱动的负载。对于给定的轴的工作温度和转速，该方法包括确定负载和涡轮的极坐标惯性矩的步骤。确定轴的自然扭转振动频率。通过使用惯性和振动频率计算确定轴刚度。

83. 发明申请

US20150016949A1 TIP CLEARANCE CONTROL METHOD 审中-公开
标题翻译：提示间隙控制方法
公开(公告)号：US20150016949A1
公开(公告)日：2015-01-15
申请号：US14305437
申请日：2014-06-16
申请人： ROLLS-ROYCE PLC
发明人： Marcus Donegan Wood SMITH
IPC分类号： F01D11/24 , F01D21/00
CPC分类号： F01D11/24 , F01D21/003 , F01D25/14 , F05D2270/303 , F05D2270/71 , F05D2270/80 , F05D2300/5021 , Y02T50/675
摘要： A method of controlling tip clearance of rotor blades from a surrounding casing in a gas turbine engine. The method comprising the steps of performing a first run of the gas turbine engine, shutting down the gas turbine engine and starting the gas turbine engine for a second run. The method further comprises measuring at least one performance parameter during or after the first engine run but before a time selected at which air within the gas turbine engine, soaked to the approximate temperature of one or more surrounding engine components, is substantially displaced as a consequence of the second run. The thermal condition of at least part of the engine in accordance with the measured performance parameters is then recorded. Finally the recorded thermal condition is retrieved and the temperature of the casing is controlled during at least part of the second run in a manner dependent on it.
摘要翻译：一种控制燃气涡轮发动机中的周围壳体的转子叶片的顶端间隙的方法。该方法包括以下步骤：执行燃气涡轮发动机的第一次运行，关闭燃气涡轮发动机并启动燃气涡轮发动机进行第二次运行。该方法还包括在第一发动机运行期间或之后但在被选择的时间之前测量至少一个性能参数，该时间被选定为燃烧在一个或多个周围发动机部件的大致温度内的燃气涡轮发动机内的空气被大大地移位的第二次跑步。然后记录根据测量的性能参数的至少部分发动机的热条件。最后，记录的热条件被检索，并且壳体的温度在第二次运行的至少部分期间以取决于其的方式被控制。

84. 发明申请

US20140321985A1 ROTOR TIP CLEARANCE 有权
标题翻译：转子间隙
公开(公告)号：US20140321985A1
公开(公告)日：2014-10-30
申请号：US14223447
申请日：2014-03-24
申请人： ROLLS-ROYCE PLC
发明人： Leo Vivian LEWIS
IPC分类号： F01D11/24 , G01N25/16 , G05B15/02
CPC分类号： F01D11/24 , F01D11/18 , F01D11/20 , F05D2260/81 , F05D2270/44 , F05D2270/71 , G01N25/16 , G05B15/02
摘要： A method of characterising mechanical and thermal growth of a rotor tip clearance arrangement and a method of controlling such an arrangement. The characterisation method comprising constructing a finite element model and calibration cases; run the model for the calibration cases to obtain displacements; and calculating component growth therefrom. The growth is characterised and scaled for the operating conditions. The clearance is calculated in a time step from the growths and input to a control arrangement for subsequent time steps.
摘要翻译：表征转子顶端间隙布置的机械和热生长的方法和控制这种布置的方法。表征方法包括构建有限元模型和校准案例; 运行校准案例的模型以获得位移; 并计算其成分。增长的特点和规模的运行条件。间隔在从增长和输入到随后的时间步长的控制装置的时间步长中计算。

85. 发明申请

US20140244051A1 DIRECT DRIVE FAN SYSTEM WITH VARIABLE PROCESS CONTROL 审中-公开
标题翻译：具有可变过程控制的直接驱动风扇系统
公开(公告)号：US20140244051A1
公开(公告)日：2014-08-28
申请号：US14352050
申请日：2012-10-21
申请人： PRIME DATUM, INC.
发明人： Patrick Rollins , George Lucas , Joseph Costello
IPC分类号： G05D27/02
CPC分类号： G05D27/02 , B01F3/04078 , F04D19/002 , F04D25/0606 , F04D27/004 , F05D2220/766 , F05D2220/768 , F05D2260/20 , F05D2260/70 , F05D2260/821 , F05D2260/96 , F05D2270/3011 , F05D2270/306 , F05D2270/44 , F05D2270/71 , F28C1/00 , Y02B30/748 , Y02P80/156 , Y02T50/675
摘要： The present invention is directed to a direct-drive fan system and a variable process control system for efficiently managing the operation of fans in a cooling system such a as wet-cooling tower or air-cooled heat exchanger (ACHE), HVAC systems, mechanical towers or chiller systems. The present invention is based on the integration of key features and characteristics such as tower thermal performance, fan speed and airflow, motor torque, fan pitch, fan speed, fan aerodynamic properties, and pump flow. The variable process control system processes feedback signals from multiple locations in order control a high torque, variable speed, permanent magnet motor to drive the fan. Such feedback signals represent certain operating conditions including motor temperature, basin temperature, vibrations, and pump flow rates. Other data processed by the variable process control system in order to control the motor include turbine back pressure set-point, condenser temperature set-point and plant part-load setting. The variable process control system processes this data and the aforesaid feedback signals to optimize the operation of the cooling system in order to prevent disruption of the industrial process and prevent equipment (turbine) failure or trip. The variable process control system alerts the operators for the need to conduct maintenance actions to remedy deficient operating conditions such as condenser fouling. The variable process control system increases cooling for cracking crude and also adjusts the motor RPM, and hence the fan RPM, accordingly during plant part-load conditions in order to save energy.
摘要翻译：本发明涉及一种直接驱动风扇系统和可变过程控制系统，用于有效地管理诸如湿式冷却塔或风冷式热交换器（ACHE），HVAC系统，机械式塔或冷却器系统。本发明基于塔式热性能，风扇速度和气流，电机转矩，风扇间距，风扇转速，风扇空气动力特性和泵流量等关键特性和特点的集成。可变过程控制系统处理来自多个位置的反馈信号，以便控制高扭矩，可变速度的永磁电动机来驱动风扇。这种反馈信号表示某些操作条件，包括电机温度，盆温度，振动和泵流量。由可变过程控制系统处理以控制电动机的其他数据包括涡轮机背压设定点，冷凝器温度设定点和设备部分负载设置。可变过程控制系统处理这些数据和上述反馈信号，以优化冷却系统的运行，以防止工业过程中断，并防止设备（涡轮）故障或跳闸。可变过程控制系统警告操作者需要进行维护操作以补救诸如冷凝器结垢的不良操作条件。可变过程控制系统增加了用于裂解原油的冷却，并且在工厂部分负载条件下相应地调节电动机RPM，并因此调整风扇RPM，以节省能源。

86. 发明申请

US20130173231A1 SYSTEM AND METHOD FOR FORMING FAILURE ESTIMATES FOR A HEAT RECOVERY STEAM GENERATOR 有权
标题翻译：用于形成热回收蒸汽发生器的故障估计的系统和方法
公开(公告)号：US20130173231A1
公开(公告)日：2013-07-04
申请号：US13343341
申请日：2012-01-04
申请人： Achalesh Kumar Pandey , Deepali Nitin Bhate , Shivappa Ningappa Goravar , David Lee Rogers
发明人： Achalesh Kumar Pandey , Deepali Nitin Bhate , Shivappa Ningappa Goravar , David Lee Rogers
IPC分类号： G06F17/10
CPC分类号： G05B17/02 , F05D2270/71 , F22B35/00 , F22B35/18 , G05B13/04 , G07C3/00
摘要： A method of forming a failure estimate for one or more components of a heat recovery steam generator (HRSG) includes forming from failure models and at least one of fired hours and fired starts, factored hours and factored starts. The factored hours and/or starts are applied to failure equations for the one or more components to form the failure estimate.
摘要翻译：形成热回收蒸汽发生器（HRSG）的一个或多个部件的故障估计的方法包括从故障模型形成，以及至少一个点火时间和点火开始，因子小时和因子开始。将因子小时数和/或起始值应用于一个或多个组件的失效方程以形成故障估计。

87. 发明授权

US08321118B2 Operations support systems and methods with power assurance 有权
标题翻译：运行支持系统和方法与功率保证
公开(公告)号：US08321118B2
公开(公告)日：2012-11-27
申请号：US12342633
申请日：2008-12-23
申请人： Kevin Moeckly , Jan Goericke , Andy Stramiello , Richard Ling
发明人： Kevin Moeckly , Jan Goericke , Andy Stramiello , Richard Ling
IPC分类号： G06F19/00 , G06G7/70
CPC分类号： G05B23/0254 , F02C9/00 , F05D2270/71 , G05B23/0281
摘要： An operations support system for an engine includes an engine prediction unit configured to receive an engine rating condition and scalars associated with the engine, and to generate condition indicators based on the engine rating condition and the scalars; and a power assurance algorithm unit coupled to the engine prediction unit and configured to generate health indicators based on the condition indicators. The health indicators include a power assurance number.
摘要翻译：用于发动机的操作支持系统包括：发动机预测单元，被配置为接收与发动机相关联的发动机额定值条件和标量，并且基于发动机额定值条件和标量来生成状况指示器; 以及功率保证算法单元，其耦合到所述引擎预测单元并且被配置为基于所述条件指示符生成健康指示符。健康指标包括电力保证号码。

88. 发明申请

US20120285174A1 Systems and Methods for Optimized Gas Turbine Shutdown 有权
标题翻译：优化燃气轮机关闭的系统和方法
公开(公告)号：US20120285174A1
公开(公告)日：2012-11-15
申请号：US13103164
申请日：2011-05-09
申请人： Scott Victor Hannula
发明人： Scott Victor Hannula
IPC分类号： F02C9/26
CPC分类号： F01D21/06 , F01D21/02 , F02C9/26 , F05D2220/323 , F05D2270/11 , F05D2270/304 , F05D2270/31 , F05D2270/705 , F05D2270/71
摘要： The present application and the resultant patent provide a gas turbine engine. The gas turbine engine may include a compressor for compressing a flow of air, a combustor for combusting the flow of air and a flow of fuel to create a flow of combustion gases, a turbine driven by the flow of combustion gases, a rotor driven by the turbine and driving the compressor, a rotor speed sensor, and a gas turbine shut down controller. The gas turbine shut down controller varies the flow of fuel to the combustor based upon a rotational speed of the rotor as determined by a dynamic target trajectory schedule.
摘要翻译：本申请和所得专利提供了一种燃气涡轮发动机。燃气涡轮发动机可以包括用于压缩空气流的压缩机，用于燃烧空气流的燃烧器和燃料流以产生燃烧气体流，由燃烧气体驱动的涡轮，由涡轮机和驱动压缩机，转子速度传感器和燃气轮机关闭控制器。燃气轮机关闭控制器基于由动态目标轨迹调度确定的转子的转速来改变燃料到燃烧器的流动。

89. 发明授权

US08260523B2 Method for detecting gas turbine engine flashback 有权
标题翻译：燃气涡轮发动机回火检测方法
公开(公告)号：US08260523B2
公开(公告)日：2012-09-04
申请号：US12434695
申请日：2009-05-04
申请人： Kapil Kumar Singh , Balachandar Varatharajan , Gilbert Otto Kraemer , Ertan Yilmaz , Benjamin Paul Lacy
发明人： Kapil Kumar Singh , Balachandar Varatharajan , Gilbert Otto Kraemer , Ertan Yilmaz , Benjamin Paul Lacy
IPC分类号： G06F17/00 , G06G7/70
CPC分类号： F02C9/00 , F05D2260/80 , F05D2270/71 , F23N5/082 , F23N5/242 , F23N2041/20 , Y02T50/677
摘要： A method for monitoring and controlling a gas turbine, comprises predicting frequencies of combustion dynamics in a combustor using operating conditions of a gas turbine, receiving a signal from a sensor that is indicative of combustion dynamics in the combustor, and detecting a flashback if a frequency of the received signal does not correspond to the predicted frequencies.
摘要翻译：一种用于监测和控制燃气轮机的方法，包括使用燃气轮机的操作条件来预测燃烧器中的燃烧动态的频率，从传感器接收指示燃烧器中的燃烧动力学的信号，以及如果频率的接收信号不对应于预测的频率。

90. 发明申请

US20120136819A1 TURBINE PERFORMANCE DIAGNOSTIC SYSTEM AND METHODS 有权
标题翻译：涡轮性能诊断系统及方法
公开(公告)号：US20120136819A1
公开(公告)日：2012-05-31
申请号：US12956689
申请日：2010-11-30
申请人： Achalesh Kumar Pandey , Subrat Nanda , Maria Cecilia Mazzaro , Atanu Talukdar
发明人： Achalesh Kumar Pandey , Subrat Nanda , Maria Cecilia Mazzaro , Atanu Talukdar
IPC分类号： G06F15/18 , G06F15/00 , G06N5/02
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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