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The Study of Turbo-Engine Early Fault Detection Technology Based PHM Sensor

机译:基于PHM传感器的涡轮发动机早期故障检测技术研究

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The electrostatic sensor can measure the level of engine exhaust electrostatic charge, based on electrostatic induction principle between the inducing charge and conductors. This paper proposes the basic design theory of the electrostatic sensor by building electrostatic sensor function and physical models. This study is significant for designing and manufacturing of a probe-type electrostatic sensor. In order to verify the effectiveness of the designed electrostatic sensor, there is a successful application in the aviation engine test process based on the aviation engine exhaust gas electrostatic monitoring principle and system. There were measured noise signals from electrostatic collection system, the electrostatic signals of an old engine starting process and a new engine for the first time test. These two types of signals reveal the basic form of the electrostatic signal changes and describe the levels of electrostatic charge in the Turbo-engine exhaust gas. The signal showed different characteristics conforming theoretical analysis for detecting early faults.
机译:基于诱导电荷和导体之间的静电感应原理,静电传感器可以测量发动机排气电荷的水平。本文通过建立静电传感器功能和物理模型提出了静电传感器的基本设计理论。该研究对于探测型静电传感器的设计和制造是很大的综合感。为了验证设计的静电传感器的有效性,基于航空发动机排气静电监测原理和系统,在航空发动机测试过程中存在成功应用。从静电收集系统中测量噪声信号,旧发动机启动过程的静电信号和第一次测试的新发动机。这两种类型的信号揭示了静电信号的基本形式改变,并描述了涡轮发动机废气中的静电电荷水平。该信号显示出不同特征,符合检测早期断层的理论分析。

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