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Sensors and methodology for improved turbine exhaust gas temperature measurements

机译:用于改善涡轮废气温度测量的传感器和方法

摘要

A method for characterizing the parameters of a normally occurring turbine exhaust gas temperature profile is provided. From that characterization the characteristics of a filter function to eliminate or significantly reduce the strength of aliased signals from that normally occurring pattern are established. Sensors to provide filtering functions for that purpose include a distributed gradient thermocouple system and a resistance thermometer system. Examples of such sensor systems are disclosed. The method and related sensors improve the detection limits associated with exhaust gas temperature profiles used to monitor, diagnose, and control gas turbines.
机译:提供了一种用于表征正常出现的涡轮机排气温度曲线的参数的方法。根据该特征,建立了消除或显着降低来自通常发生的模式的混叠信号的强度的滤波器功能的特征。为此目的提供滤波功能的传感器包括分布式梯度热电偶系统和电阻温度计系统。公开了这种传感器系统的示例。该方法和相关传感器提高了与用于监测,诊断和控制燃气轮机的排气温度曲线相关的检测极限。

著录项

  • 公开/公告号US6565255B2

    专利类型

  • 公开/公告日2003-05-20

    原文格式PDF

  • 申请/专利权人 GENERAL ELECTRIC COMPANY;

    申请/专利号US20010948439

  • 发明设计人 SIMON RALPH SANDERSON;

    申请日2001-09-10

  • 分类号G01K70/20;G01K71/60;G01K130/00;

  • 国家 US

  • 入库时间 2022-08-22 00:07:34

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