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Methods for Preliminary Data Processing in a System for Measuring of Radial Clearances with Self-Compensation of Temperature Effects on the Sensor in Flow Section of Gas-Turbine Engine

机译:一种用于测量径向间隙的系统中的初步数据处理,其自补偿气体涡轮发动机流动部分的温度效应的自补偿

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摘要

The descriptions of innovative methods for preliminary data processing in a system for measuring of radial clearances, including the difference method for average extreme codes detection of blade-to-blade gaps, the difference method for extreme codes detection at the output of measuring circuit during one period of impeller rotation that is not dependent on temperature effect on the sensor, and the method for averaging of difference of extreme codes over several periods of impeller rotation, are considered. Methods provide processing speed and measurement accuracy increase. The quantitative estimates of methods speed and accuracy confirming their efficiency and application in gas-turbine engines diagnostic systems are given.
机译:关于测量径向间隙的系统中初步数据处理的创新方法的描述,包括用于平均极端代码检测的叶片到叶片间隙的差分方法,是一个测量电路输出的极端代码检测的差异方法考虑了叶轮旋转的周期,其不依赖于对传感器的温度效应,以及用于在几个叶轮旋转周期内进行极端代码的差异的平均方法。方法提供处理速度和测量精度的增加。给出了方法速度和准确性的定量估计,确认其在燃气 - 涡轮发动机诊断系统中的效率和应用。

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