AE Monitoring During Aircraft Flight Loading Conditions Fatigue Test
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摘要: 介绍了某型飞机全尺寸机体飞行载荷疲劳试验过程中对关键部件(包括不可接近部件)疲劳损伤的声发射(AE)实时监测技术。在强冲击、高振动背景下,利用基于时间、空间、幅度或能量滤波等多种信号处理方式,对预处理后的AE信号以趋势分析为主,多参数分析综合验证,另辅以其它方法(包括波形分析),对一些关键部位的健康状态进行AE实时在线监测。成功预报了机翼对接区域某螺栓孔夹层裂纹的萌生,为保证机体飞行载荷疲劳试验顺利进行起到了重要作用。Abstract: The technology of acoustic emission(AE) real time monitoring the critical structures (including inaccessible components) during aircraft flight loading conditions fatigue test was introduced. In a noise background due to severe shock and vibration, first of all, AE signals were pre-processed based on time filtering, amplitude filtering, and energy filtering as well as based on spatial filtering techniques. After acquiring the pre-processed AE signal, we adopted a new AE signal analysis principle that gave priority to AE diagnostic parameter trend analysis, multi-parameter analysis identifications and further looked for others(including waveform analysis) as assistant method. Real time monitoring of these critical structures was realized, and was successful in predicting a crack initiation in an interlayer of a bolt hole. The mean of AE monitoring played a key role for the fulfillment of the flight loading conditions fatigue test(FLCFT).
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Keywords:
- Acoustic emission testing /
- Aircraft /
- Flight load /
- Fatigue test /
- Trend analysis
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