APPLICATION OF PROBABILISTIC CONTROL IN GAS TURBINE TUNING WITH MEASUREMENT ERROR, RELATED CONTROL SYSTEMS, COMPUTER PROGRAM PRODUCTS AND METHODS
    6.
    发明申请
    APPLICATION OF PROBABILISTIC CONTROL IN GAS TURBINE TUNING WITH MEASUREMENT ERROR, RELATED CONTROL SYSTEMS, COMPUTER PROGRAM PRODUCTS AND METHODS 有权
    在测量误差的气体涡轮调谐中应用概率控制,相关控制系统,计算机程序产品和方法

    公开(公告)号:US20160138482A1

    公开(公告)日:2016-05-19

    申请号:US14546491

    申请日:2014-11-18

    CPC classification number: F02C9/56 F02C9/28 F02C9/42 F05D2270/0831

    Abstract: Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective output to match a nominal mega-watt power output value, and subsequently measuring an actual emissions value for each GT; adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual emissions value and a nominal emissions value at the ambient condition; and further adjusting an operating condition of each GT in the set of GTs based upon a determined emissions measurement error.

    Abstract translation: 各种实施例包括一种系统,其具有:至少一个计算装置,其配置成通过执行动作来调节一组燃气轮机(GT),所述动作包括:基于每个所测量的环境条件,将所述GT组中的每个GT命令为基本负载水平 GT 指挥GT中的每个GT调整相应的输出以匹配标称兆瓦功率输出值,然后测量每个GT的实际排放值; 基于相应测量的实际发射值与环境条件下的标称发射值之间的差异来调整GT组中的每个GT的操作条件; 并且基于所确定的排放测量误差来进一步调整GT组中的每个GT的操作条件。

    APPLICATION OF PROBABILISTIC CONTROL IN GAS TURBINE TUNING, RELATED CONTROL SYSTEMS, COMPUTER PROGRAM PRODUCTS AND METHODS
    7.
    发明申请
    APPLICATION OF PROBABILISTIC CONTROL IN GAS TURBINE TUNING, RELATED CONTROL SYSTEMS, COMPUTER PROGRAM PRODUCTS AND METHODS 有权
    气体涡轮调谐中的概率控制应用,相关控制系统,计算机程序产品及方法

    公开(公告)号:US20160138480A1

    公开(公告)日:2016-05-19

    申请号:US14546525

    申请日:2014-11-18

    CPC classification number: F02C9/28 F02C3/04 F02C9/42 F05D2260/821 F05D2270/44

    Abstract: Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective output to match a nominal mega-watt power output value, and subsequently measuring an actual emissions value for each GT; and adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual emissions value and a nominal emissions value at the ambient condition.

    Abstract translation: 各种实施例包括一种系统,其具有:至少一个计算装置,其配置成通过执行动作来调节一组燃气轮机(GT),所述动作包括:基于每个所测量的环境条件,将所述GT组中的每个GT命令为基本负载水平 GT 指挥GT中的每个GT调整相应的输出以匹配标称兆瓦功率输出值,然后测量每个GT的实际排放值; 并且基于各个测量的实际排放值和环境条件下的标称排放值之间的差异来调整GT组中的每个GT的运行状况。

    GAS TURBINE FIRING TEMPERATURE CONTROL SYSTEM AND METHOD
    8.
    发明申请
    GAS TURBINE FIRING TEMPERATURE CONTROL SYSTEM AND METHOD 有权
    燃气涡轮机温度控制系统及方法

    公开(公告)号:US20150168927A1

    公开(公告)日:2015-06-18

    申请号:US14133611

    申请日:2013-12-18

    CPC classification number: G05B15/02 F02C9/28 F05D2270/303 F05D2270/311

    Abstract: A non-transitory computer-readable medium storing computer executable code that includes instructions to receive a signal representative of a gas turbine firing temperature. The code further includes instructions to convert the signal to an actuator signal to actuate a fuel valve supplying fuel to the gas turbine by following a first reference function. The first reference function includes a first boundary function, a second boundary function, or a combination thereof. The first boundary function maps a first value to a first temperature and the second boundary function maps a second value to a second temperature.

    Abstract translation: 一种存储计算机可执行代码的非暂时计算机可读介质,其包括接收代表燃气轮机燃烧温度的信号的指令。 代码还包括将信号转换为致动器信号以通过跟随第一参考功能致动向燃气涡轮机供应燃料的燃料阀的指令。 第一参考函数包括第一边界函数,第二边界函数或其组合。 第一边界函数将第一值映射到第一温度,而第二边界函数将第二值映射到第二温度。

    SYSTEMS AND METHODS FOR CONTROL OF A GAS TURBINE
    9.
    发明申请
    SYSTEMS AND METHODS FOR CONTROL OF A GAS TURBINE 有权
    用于控制气体涡轮机的系统和方法

    公开(公告)号:US20150007574A1

    公开(公告)日:2015-01-08

    申请号:US13937078

    申请日:2013-07-08

    Abstract: A system includes a gas turbine system including a compressor, a combustor, and a turbine. The system also includes a controller communicatively coupled to the gas turbine system and configured to control operations of the gas turbine system. The system further includes a life consumption model configured to determine an operating life of the gas turbine system based on both a health status of one or more components of the gas turbine system and operating conditions of the gas turbine system. The controller is configured to utilize at least the life consumption model to derive a control action for the gas turbine system.

    Abstract translation: 一种系统包括包括压缩机,燃烧器和涡轮机的燃气轮机系统。 该系统还包括通信地耦合到燃气涡轮机系统并被配置为控制燃气轮机系统的操作的控制器。 该系统还包括寿命模型,其构造成基于燃气轮机系统的一个或多个部件的健康状况和燃气轮机系统的运行状况来确定燃气轮机系统的运行寿命。 控制器被配置为利用至少寿命模型来导出燃气轮机系统的控制动作。

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