Gas turbine firing temperature control system and method

    公开(公告)号:US09665077B2

    公开(公告)日:2017-05-30

    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.

    Systems and methods for control of operating life of a gas turbine
    38.
    发明授权
    Systems and methods for control of operating life of a gas turbine 有权
    控制燃气轮机运行寿命的系统和方法

    公开(公告)号:US09476361B2

    公开(公告)日:2016-10-25

    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。

    APPLICATION OF PROBABILISTIC CONTROL IN GAS TURBINE TUNING FOR EMISSIONS-EXHAUST ENERGY PARAMETERS, RELATED CONTROL SYSTEMS, COMPUTER PROGRAM PRODUCTS AND METHODS
    39.
    发明申请
    APPLICATION OF PROBABILISTIC CONTROL IN GAS TURBINE TUNING FOR EMISSIONS-EXHAUST ENERGY PARAMETERS, RELATED CONTROL SYSTEMS, COMPUTER PROGRAM PRODUCTS AND METHODS 有权
    气体排放控制在排气排放能量参数,相关控制系统,计算机程序产品和方法中的应用

    公开(公告)号:US20160305335A1

    公开(公告)日:2016-10-20

    申请号:US14686193

    申请日:2015-04-14

    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 emissions value to match a nominal emissions value, and subsequently measuring an actual exhaust energy 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 exhaust energy value and a nominal exhaust energy 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集合中的每个GT来调整相应的排放值以匹配名义排放值,然后测量每个GT的实际排气能量值; 并且基于各个测量的实际排气能量值和在环境条件下的标称排气能量值之间的差异来调整GT组中的每个GT的操作条件。

    Systems and methods for gas turbine tuning and control
    40.
    发明授权
    Systems and methods for gas turbine tuning and control 有权
    燃气轮机调节和控制的系统和方法

    公开(公告)号:US09422869B2

    公开(公告)日:2016-08-23

    申请号:US13801259

    申请日:2013-03-13

    Abstract: A method of tuning a gas turbine includes receiving a first plurality of operating parameters as the gas turbine engine is operated at a first operating state. Further, the method includes operating the gas turbine engine at a second operating state to measure a second plurality of operating parameters at the second operating state. In addition, the method includes operating the gas turbine engine at a third operating state to measure a third plurality of operating parameters at the third operating state, wherein the first, second, and third operating states are different from each other. Additionally, the method includes generating a correction factor based on the first, second, and third plurality of operating parameters. The method also includes adjusting the operation of the gas turbine engine based on the correction factor.

    Abstract translation: 调节燃气轮机的方法包括当燃气涡轮发动机在第一操作状态下操作时接收第一多个操作参数。 此外,该方法包括在第二操作状态下操作燃气涡轮发动机,以在第二操作状态下测量第二多个操作参数。 此外,该方法包括在第三操作状态下操作燃气涡轮发动机,以在第三操作状态下测量第三多个操作参数,其中第一,第二和第三操作状态彼此不同。 另外,该方法包括基于第一,第二和第三多个操作参数产生校正因子。 该方法还包括基于校正因子调整燃气涡轮发动机的运行。

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