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A Novel Data Fusion Method for Incipient Fault Detection in TRU of Aircraft Electrical System

机译:飞机电气系统TRU中早期故障检测的数据融合新方法

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摘要

Incipient fault detection in the Transformer Rectifier Unit (TRU) can prompt early preparedness for replacement of Line Replaceable Units (LRUs) thereby reducing the downtime of the aircraft. This paper describes a novel incipient fault detection and fault localization method of TRU in the context of an aircraft electrical system. Results from Failure Mode and Effects Analysis (FMEA) study identified diode failure as the primary reason for failure of TRU. The incipient fault detection of TRU is done by applying data fusion algorithm. The algorithm uses Hilbert transform as one of the computing tools to derive Health Index Parameter (HIP). Fast Fourier Transforms (FFT) and wavelet transforms were used for fault localization of the component within the TRU. The developed incipient fault detection method is validated on a TRU test rig. Though the test rig is configured on 50Hz supply the results can be read across on 400Hz supply. A scheme of communicating the fault status integrating through 1553B network is also addressed.
机译:变压器整流器单元(TRU)的早期故障检测可以促使人们为更换线路可更换单元(LRU)的早期准备做好准备,从而减少飞机的停机时间。本文介绍了一种在飞机电气系统环境下TRU的早期故障检测和故障定位的新方法。失效模式和影响分析(FMEA)研究的结果确定二极管故障是TRU失效的主要原因。 TRU的早期故障检测是通过应用数据融合算法完成的。该算法使用希尔伯特变换作为计算工具之一,以得出健康指数参数(HIP)。快速傅里叶变换(FFT)和小波变换用于TRU中组件的故障定位。在TRU测试台上验证了开发的早期故障检测方法。尽管测试台配置为50Hz电源,但可以在400Hz电源上读取结果。还提出了一种通过1553B网络传送故障状态积分的方案。

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