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Smart radiation thermometry system for real time gas turbine control and prognosis

机译:用于燃气轮机实时控制和预测的智能辐射测温系统

摘要

A smart radiation thermometry system including a turbine component is provided. The smart radiation thermometry system includes an optical imaging sub-system configured to receive a continuous broad wavelength band radiation signal emitted by the turbine component. The thermometry system also includes a wavelength splitting sub-system in optical communication with the optical transmission sub-system, wherein the wavelength splitting sub-system receives the continuous broad wavelength band radiation signal, and splits the radiation signal into multiple sub-wavelength band signals. The thermometry system further includes at least one detector array in optical communication with the wavelength-splitting sub-system, wherein the at least one detector array receives the multiple sub-wavelength band signals, and outputs respective analog voltage signals for each of the signals. The thermometry system further includes at least one high-speed multi-channel analog-to-digital converter (ADC) electrically coupled to the at least one detector array, wherein the ADC digitizes respective analog voltage signals and outputs digital voltage signals. The thermometry system also includes at least one smart real time processing sub-system electrically coupled to the at least one detector array via the at least one high-speed multi-channel ADC. The at least one smart real time processing sub-system calculates temperature and emissivity of the turbine component based upon a computed radiance temperature, reflection correction and multi-wavelength algorithm. The smart real time processing sub-system also transmits data indicative of the temperature, emissivity and other plurality of parameters within a pre-determined time period to a communication unit. The smart real time processing sub-system also outputs emergency alarm signals and controls either directly or via a controller one or more actuators coupled to the gas turbine based upon the data to ensure optimum operation of the gas turbine within safe operating limits.
机译:提供了一种包括涡轮机部件的智能辐射测温系统。智能辐射测温系统包括光学成像子系统,该光学成像子系统被配置为接收由涡轮机部件发射的连续的宽带波段辐射信号。测温系统还包括与光传输子系统进行光通信的波长分离子系统,其中该波长分离子系统接收连续的宽波段辐射信号,并将辐射信号分成多个子波段信号。该测温系统还包括至少一个与波长分离子系统光学通信的检测器阵列,其中该至少一个检测器阵列接收多个子波长带信号,并为每个信号输出各自的模拟电压信号。测温系统还包括至少一个电耦合到至少一个检测器阵列的高速多通道模数转换器(ADC),其中,ADC将相应的模拟电压信号数字化并输出数字电压信号。测温系统还包括至少一个经由至少一个高速多通道ADC电耦合到至少一个检测器阵列的智能实时处理子系统。至少一个智能实时处理子系统基于计算出的辐射温度,反射校正和多波长算法来计算涡轮机部件的温度和发射率。智能实时处理子系统还将在预定时间段内指示温度,发射率和其他多个参数的数据发送到通信单元。智能实时处理子系统还输出紧急警报信号,并根据数据直接或通过控制器控制一个或多个与燃气轮机相连的执行器,以确保燃气轮机在安全运行范围内达到最佳运行。

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