Kral Zachary, Horn Walter, Steck James
Wichita State University, Wichita, KS 67260, USA ; Department of Aerospace Engineering, 1845 Fairmount, Wichita, KS 67226, USA.
ScientificWorldJournal. 2013 Aug 20;2013:823603. doi: 10.1155/2013/823603. eCollection 2013.
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.
航空航天系统预计将在远超其设计寿命的时间内持续服役。因此,维护是一个重要问题。本研究的重点是一种实施人工神经网络和声学发射传感器以形成用于航空航天检查程序的结构健康监测(SHM)系统的新方法。由AL 2024-T3铝板组成的简单结构元件承受逐渐增加的静态拉伸载荷。随着载荷增加,设计的裂纹长度扩展,在此过程中释放应变波。由声学发射传感器测量的应变波信号在后期处理中通过人工神经网络(ANN)进一步分析。进行了多项实验以确定结构中裂纹扩展的严重程度和位置。人工神经网络在传感器获取的一部分数据上进行训练,然后用其余数据进行验证。声学发射传感器系统与人工神经网络的组合能够准确确定裂纹扩展情况。预测的裂纹扩展与实际裂纹扩展之间的差异在95%置信度下确定为0.004英寸至0.015英寸之间。这些人工神经网络与声学发射传感器相结合,为创建航空航天系统的结构健康监测系统展现出了前景