Department of Applied Science, College of William and Mary, Williamsburg, VA, USA.
Ultrasonics. 2014 Jan;54(1):247-58. doi: 10.1016/j.ultras.2013.04.020. Epub 2013 May 16.
In this paper, the authors present a formal classification routine to characterize flaw severity in an aircraft-grade aluminum plate using Lamb waves. A rounded rectangle flat-bottom hole is incrementally introduced into the plate, and at each depth multi-mode Lamb wave signals are collected to study the changes in received signal due to mode conversion and scattering from the flaw. Lamb wave tomography reconstructions are used to locate and size the flaw at each depth, however information about the severity of the flaw is obscured when the flaw becomes severe enough that scattering effects dominate. The dynamic wavelet fingerprint is then used to extract features from the raw Lamb wave signals, and supervised pattern classification techniques are used to identify flaw severity with up to 80.7% accuracy for a training set and up to 51.7% accuracy on a series of validation data sets extracted from independent plate samples.
在本文中,作者提出了一种使用兰姆波对飞机级铝板缺陷严重程度进行特征化的正式分类程序。在板中逐渐引入一个圆角矩形平底孔,在每个深度采集多模态兰姆波信号,以研究由于模式转换和缺陷散射引起的接收信号的变化。兰姆波层析成像重建用于在每个深度定位和尺寸缺陷,但当缺陷变得足够严重以至于散射效应占主导地位时,缺陷严重程度的信息就会被掩盖。然后使用动态小波指纹从原始兰姆波信号中提取特征,并使用监督模式分类技术对缺陷严重程度进行识别,在训练集上的准确率高达 80.7%,在从独立板样本中提取的一系列验证数据集上的准确率高达 51.7%。