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

机译:结构健康监测系统中使用声发射传感器的裂纹扩展分析

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摘要

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:航空航天系统有望在其设计使用寿命之外继续保持服役状态。因此,维护是重要的问题。这项研究的重点是实现人工神经网络和声发射传感器以形成用于航天检查程序的结构健康监测(SHM)系统的新方法。由AL 2024-T3的扁平铝板组成的简单结构元件承受的静态拉伸载荷不断增加。随着载荷的增加,设计裂纹的长度会增加,从而在此过程中释放出应变波。由声发射传感器测量的应变波信号在人工神经网络(ANN)的后处理中进一步分析。进行了几次实验,以确定结构中裂纹扩展的严重程度和位置。在传感器获取的部分数据上对人工神经网络进行了训练,然后用剩余的数据对人工神经网络进行了验证。声发射传感器系统和ANN的组合可以准确确定裂纹扩展。确定的预测裂纹扩展与实际裂纹扩展之间的差异在0.004英寸至0.015英寸之间,置信度为95%。这些人工神经网络与声发射传感器相结合,显示出为航空航天系统创建SHM系统的希望。

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