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Crack Propagation Analysis Using Acoustic Emission Sensors for Structural Health Monitoring Systems

机译:用于结构健康监测系统声发射传感器的裂纹传播分析

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Aerospace systems are expected to remain in service well beyond their designed life. Consequently, maintenance is an important issue. A novel method of implementing artificial neural networks and acoustic emission sensors to form a structural health monitoring (SHM) system for aerospace inspection routines was the focus of this research. Simple structural elements, consisting of flat aluminum plates of AL 2024-T3, were subjected to increasing static tensile loading. As the loading increased, designed cracks extended in length, releasing strain waves in the process. Strain wave signals, measured by acoustic emission sensors, were further analyzed in post-processing by artificial neural networks (ANN). Several experiments were performed to determine the severity and location of the crack extensions in the structure. ANNs were trained on a portion of the data acquired by the sensors and the ANNs were then validated with the remaining data. The combination of a system of acoustic emission sensors, and an ANN could determine crack extension accurately. The difference between predicted and actual crack extensions was determined to be between 0.004 in. and 0.015 in. with 95% confidence. These ANNs, coupled with acoustic emission sensors, showed promise for the creation of an SHM system for aerospace systems.
机译:预计航空航天系统将远远超出其所设计的寿命。因此,维护是一个重要问题。一种实施人工神经网络和声发射传感器的新方法,以形成用于航空航天检验惯例的结构健康监测(SHM)系统是该研究的重点。由Al 2024-T3的扁平铝板组成的简单结构元件进行静态拉伸载荷。随着装载的增加,设计的设计裂缝长度,在该过程中释放应变波。通过声发射传感器测量的应变波信号在人工神经网络(ANN)后处理中进一步分析。进行了几个实验以确定结构中裂缝延伸的严重程度和位置。 ANNS在由传感器获取的一部分数据上培训,然后用剩余数据验证ANN。声发射传感器系统的组合和ANN可以准确地确定裂缝延伸。预测和实际裂缝延伸之间的差异确定为0.004英寸和0.015英寸。置信95%。与声发射传感器相结合的这些ANNS向航空系统创建了SHM系统的承诺。

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