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Characteristics analysis and experiment verification of electrostatic sensor for aero-engine exhaust gas monitoring

机译:航空发动机尾气监测用静电传感器的特性分析与实验验证

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摘要

An electrostatic sensor is a critical component of the electrostatic monitoring system for an aero-engine gas path. In this paper, the basic principles of the electrostatic sensor are described and the materials selection process for sensor electrodes and an isolation medium is introduced. The finite element method was adopted to calculate the sensitivity distribution, and the influence of relevant structural parameters on the sensitivity distribution characteristic is analyzed. The data fitting method was employed to acquire the unified spatial sensitivity distribution functions for a given structure sensor, which provides a useful reference for the sensor's installation location. Based on the unified function, the sensitivity distribution function along the particle moving direction and the frequency characteristic of the electrostatic sensor were acquired. Then the corresponding influence factors of the frequency properties were analyzed. An experiment platform was established to verify the model and the theoretical analysis results. Then, simulated experiments were applied to verify the feasibility and validity of the electrostatic sensor, and the experiment results provided a useful reference for the identification of abnormal particles as a characteristic of aero-engine faults.
机译:静电传感器是用于航空发动机气路的静电监控系统的关键组件。本文介绍了静电传感器的基本原理,介绍了传感器电极和隔离介质的材料选择过程。采用有限元法计算了敏感度分布,分析了相关结构参数对敏感度分布特性的影响。数据拟合方法用于获取给定结构传感器的统一空间灵敏度分布函数,这为传感器的安装位置提供了有用的参考。基于统一函数,获得了沿粒子运动方向的灵敏度分布函数和静电传感器的频率特性。然后分析了频率特性的相应影响因素。建立了实验平台,对模型和理论分析结果进行了验证。然后,通过仿真实验验证了静电传感器的可行性和有效性,实验结果为航空发动机故障特征异常颗粒的识别提供了有益的参考。

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