Method for detecting compressor stall precursors
    1.
    发明授权
    Method for detecting compressor stall precursors 失效
    检测压缩机失速前体的方法

    公开(公告)号:US07596953B2

    公开(公告)日:2009-10-06

    申请号:US10744617

    申请日:2003-12-23

    CPC classification number: F04D27/001 F05D2270/101

    Abstract: A method of detecting onset of a gas turbine condition, such as compressor stall, includes receiving data indicative of an operating parameter of a compressor of the gas turbine. The method also includes performing a wavelet transformation on the data to generate wavelet transformed data. The wavelet transformation is configured to affect a processing characteristic regarding a performance of the wavelet transformation. Features indicative of onset of the gas turbine condition in the wavelet transformed data are then identified to provide an indication for controlling the gas turbine to prevent compressor stall from occurring. A system for detecting onset of compressor stall in a gas turbine includes a sensor for providing data indicative of an operating parameter of the compressor and a processor for performing a wavelet transform on the data to identify features of the optimized wavelet transformed data indicative of onset of stall.

    Abstract translation: 检测诸如压缩机失速的燃气轮机状态的发生的方法包括接收表示燃气轮机的压缩机的运行参数的数据。 该方法还包括对数据执行小波变换以产生小波变换数据。 小波变换被配置为影响关于小波变换的性能的处理特性。 然后识别表示小波变换数据中的燃气轮机状况的特征的特征,以提供用于控制燃气涡轮机以防止压缩机失速发生的指示。 用于检测燃气涡轮机中的压缩机失速开始的系统包括用于提供指示压缩机的操作参数的数据的传感器和用于对数据执行小波变换的处理器,以识别指示发生的最佳化的小波变换数据的特征 摊位

    Method and system for detecting precursors to compressor stall and surge
    2.
    发明授权
    Method and system for detecting precursors to compressor stall and surge 失效
    用于检测压缩机失速和喘振的前体的方法和系统

    公开(公告)号:US07003426B2

    公开(公告)日:2006-02-21

    申请号:US10065331

    申请日:2002-10-04

    CPC classification number: F04D27/001 Y02E20/16

    Abstract: A method and system for detecting precursors to compressor stall and surge in which at least one compressor parameter is monitored to obtain raw data representative of said at least one compressor parameter. The raw data is pre-processed using a frequency demodulator to produce pre-processed data, and the pre-processed raw data is post-processed using a Kalman filter to obtain stall precursors.

    Abstract translation: 一种用于检测压缩机失速和喘振的前体的方法和系统,其中监测至少一个压缩机参数以获得表示所述至少一个压缩机参数的原始数据。 使用频率解调器预处理原始数据以产生预处理的数据,并且使用卡尔曼滤波器对预处理的原始数据进行后处理以获得失速前体。

    Method and apparatus for monitoring the performance of a gas turbine system
    3.
    发明授权
    Method and apparatus for monitoring the performance of a gas turbine system 有权
    用于监测燃气轮机系统的性能的方法和装置

    公开(公告)号:US06962043B2

    公开(公告)日:2005-11-08

    申请号:US10354824

    申请日:2003-01-30

    CPC classification number: F01D17/085

    Abstract: A method for monitoring performance of a gas turbine system comprises providing a plurality of combustor cans; placing a plurality of temperature sensors circumferentially around an exhaust plane of the plurality of combustor cans; operating the plurality of combustor cans while varying a plurality of gas turbine operating parameters, where exhaust gas issues from each combustor can of the plurality of combustor cans during operation; measuring temperature of the exhaust gas in the exhaust plane using the plurality of temperature sensors to obtain a plurality of individual temperature measurements; determining a correlation of the individual temperature measurements of exhaust gas temperature with corresponding individual combustor cans of the plurality of combustor cans issuing the exhaust gas; and developing a swirl model, where the model uses the correlation to predict swirl values in the exhaust plane as a function of the operating parameters.

    Abstract translation: 一种用于监测燃气轮机系统的性能的方法包括提供多个燃烧器罐; 将多个温度传感器周向地围绕多个燃烧器罐的排气平面放置; 在改变多个燃气轮机操作参数的同时操作多个燃烧器罐,其中在操作期间废气从多个燃烧器罐的每个燃烧器罐发出; 使用所述多个温度传感器测量排气平面中的废气的温度,以获得多个单独的温度测量值; 确定废气温度的各个温度测量值与排放废气的多个燃烧室的相应单独燃烧器罐的相关性; 并开发涡流模型,其中模型使用相关性来预测排气平面中的涡流值作为运行参数的函数。

    SYSTEM AND A METHOD FOR CONTROL AND AUTOMATION SERVICE
    5.
    发明申请
    SYSTEM AND A METHOD FOR CONTROL AND AUTOMATION SERVICE 审中-公开
    系统和控制和自动化服务的方法

    公开(公告)号:US20110257766A1

    公开(公告)日:2011-10-20

    申请号:US13110172

    申请日:2011-05-18

    CPC classification number: G05B19/4185 Y02P90/18 Y02P90/86

    Abstract: The present disclosure relates to exemplary systems for providing control and expert services over a communication network by specialized service providers to various kinds of automation needs and methods thereof. The arrangement allows sharing of automated control system components among one or multiple users. Methods to configure and use control and automation service are also described. Exemplary systems for control and automation service as disclosed herein can have greater flexibility and simplicity from the plant user perspective.

    Abstract translation: 本公开涉及用于通过专业服务提供商通过通信网络提供各种自动化需求的控制和专家服务的示例性系统及其方法。 该安排允许在一个或多个用户之间共享自动化控制系统组件。 还描述了配置和使用控制和自动化服务的方法。 如本文所公开的用于控制和自动化服务的示例性系统可以具有来自植物用户观点的更大的灵活性和简单性。

    Method and apparatus for detecting compressor stall precursors
    6.
    发明申请
    Method and apparatus for detecting compressor stall precursors 失效
    用于检测压缩机失速前体的方法和装置

    公开(公告)号:US20050132712A1

    公开(公告)日:2005-06-23

    申请号:US10744617

    申请日:2003-12-23

    CPC classification number: F04D27/001 F05D2270/101

    Abstract: A method of detecting onset of a gas turbine condition, such as compressor stall, includes receiving data indicative of an operating parameter of a compressor of the gas turbine. The method also includes performing a wavelet transformation on the data to generate wavelet transformed data. The wavelet transformation is configured to affect a processing characteristic regarding a performance of the wavelet transformation. Features indicative of onset of the gas turbine condition in the wavelet transformed data are then identified to provide an indication for controlling the gas turbine to prevent compressor stall from occurring. A system for detecting onset of compressor stall in a gas turbine includes a sensor for providing data indicative of an operating parameter of the compressor and a processor for performing a wavelet transform on the data to identify features of the optimized wavelet transformed data indicative of onset of stall.

    Abstract translation: 检测诸如压缩机失速的燃气轮机状态的发生的方法包括接收表示燃气轮机的压缩机的运行参数的数据。 该方法还包括对数据执行小波变换以产生小波变换数据。 小波变换被配置为影响关于小波变换的性能的处理特性。 然后识别表示小波变换数据中的燃气轮机状况的特征的特征,以提供用于控制燃气涡轮机以防止压缩机失速发生的指示。 用于检测燃气涡轮机中的压缩机失速开始的系统包括用于提供指示压缩机的操作参数的数据的传感器和用于对数据执行小波变换的处理器,以识别指示发生的最佳化的小波变换数据的特征 摊位

    Method and apparatus for monitoring the performance of a gas turbine system
    7.
    发明授权
    Method and apparatus for monitoring the performance of a gas turbine system 有权
    用于监测燃气轮机系统的性能的方法和装置

    公开(公告)号:US07140186B2

    公开(公告)日:2006-11-28

    申请号:US11195323

    申请日:2005-08-02

    CPC classification number: F01D17/085

    Abstract: A method for monitoring performance of a gas turbine system comprises providing a plurality of combustor cans; placing a plurality of temperature sensors circumferentially around an exhaust plane of the plurality of combustor cans; operating the plurality of combustor cans while varying a plurality of gas turbine operating parameters, where exhaust gas issues from each combustor can of the plurality of combustor cans during operation; measuring temperature of the exhaust gas in the exhaust plane using the plurality of temperature sensors to obtain a plurality of individual temperature measurements; determining a correlation of the individual temperature measurements of exhaust gas temperature with corresponding individual combustor cans of the plurality of combustor cans issuing the exhaust gas; and developing a swirl model, where the model uses the correlation to predict swirl values in the exhaust plane as a function of the operating parameters.

    Abstract translation: 一种用于监测燃气轮机系统的性能的方法包括提供多个燃烧器罐; 将多个温度传感器周向地围绕多个燃烧器罐的排气平面放置; 在改变多个燃气轮机操作参数的同时操作多个燃烧器罐,其中在操作期间废气从多个燃烧器罐的每个燃烧器罐发出; 使用所述多个温度传感器测量排气平面中的废气的温度,以获得多个单独的温度测量值; 确定废气温度的各个温度测量值与排放废气的多个燃烧室的相应单独燃烧器罐的相关性; 并开发涡流模型,其中模型使用相关性来预测排气平面中的涡流值作为运行参数的函数。

    METHOD AND APPARATUS FOR MONITORING THE PERFORMANCE OF A GAS TURBINE SYSTEM
    8.
    发明申请
    METHOD AND APPARATUS FOR MONITORING THE PERFORMANCE OF A GAS TURBINE SYSTEM 有权
    用于监测气体涡轮机系统性能的方法和装置

    公开(公告)号:US20060201158A1

    公开(公告)日:2006-09-14

    申请号:US11195323

    申请日:2005-08-02

    CPC classification number: F01D17/085

    Abstract: A method for monitoring performance of a gas turbine system comprises providing a plurality of combustor cans; placing a plurality of temperature sensors circumferentially around an exhaust plane of the plurality of combustor cans; operating the plurality of combustor cans while varying a plurality of gas turbine operating parameters, where exhaust gas issues from each combustor can of the plurality of combustor cans during operation; measuring temperature of the exhaust gas in the exhaust plane using the plurality of temperature sensors to obtain a plurality of individual temperature measurements; determining a correlation of the individual temperature measurements of exhaust gas temperature with corresponding individual combustor cans of the plurality of combustor cans issuing the exhaust gas; and developing a swirl model, where the model uses the correlation to predict swirl values in the exhaust plane as a function of the operating parameters.

    Abstract translation: 一种用于监测燃气轮机系统的性能的方法包括提供多个燃烧器罐; 将多个温度传感器周向地围绕多个燃烧器罐的排气平面放置; 在改变多个燃气轮机操作参数的同时操作多个燃烧器罐,其中在操作期间废气从多个燃烧器罐的每个燃烧器罐发出; 使用所述多个温度传感器测量排气平面中的废气的温度,以获得多个单独的温度测量值; 确定废气温度的各个温度测量值与排放废气的多个燃烧室的相应单独燃烧器罐的相关性; 并开发涡流模型,其中模型使用相关性来预测排气平面中的涡流值作为运行参数的函数。

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