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PEC Frequency Band Selection for Locating Defects in Two-Layer Aircraft Structures With Air Gap Variations

机译:PEC频带选择,用于确定气隙变化的两层飞机结构中的缺陷

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摘要

Multilayer structures are widely used in aircraft fuselage. Because of the interlayer air gap caused by deformation or disbonding, conventional single-frequency eddy current cannot discriminate between second-layer defect signals and gap signals. In this paper, several defects at varied locations (i.e., first-layer surface, first-layer subsurface, second-layer surface, and second-layer subsurface) are manufactured into two-layer Al–Mn 3003 alloy specimen with various air gaps. Pulsed eddy current (PEC) is investigated in combination with principal component analysis (PCA) to classify and locate defects in the specimen. The new feature named differential frequency to zero is proposed, and the frequency responses of selected frequency band are processed through PCA. The principal components are used for locating defects. The experimental results show that first-layer surface defects, first-layer subsurface defects, second-layer surface defects, and second-layer subsurface defects can be classified when air gap is varied from 0 to 1.4 mm through the proposed methods. In conclusion, PEC testing with the help of PCA can eliminate the interlayer air gap and liftoff effect, which has potential for defect characterization in multilayer aircraft structures.
机译:多层结构广泛用于飞机机身。由于由变形或剥离引起的层间气隙,常规的单频涡流不能在第二层缺陷信号和间隙信号之间进行区分。在本文中,将不同位置(即第一层表面,第一层次表面,第二层表面和第二层次表面)的几个缺陷制成具有不同气隙的两层Al-Mn 3003合金试样。结合主要成分分析(PCA)对脉冲涡流(PEC)进行了研究,以对样品中的缺陷进行分类和定位。提出了差分频率为零的新特性,并通过PCA处理了选定频段的频率响应。主要组件用于定位缺陷。实验结果表明,当气隙在0到1.4 mm之间变化时,可以对第一层表面缺陷,第一层次表面缺陷,第二层表面缺陷和第二层次表面缺陷进行分类。总而言之,借助PCA进行的PEC测试可以消除层间气隙和升空效应,这有可能在多层飞机结构中表征缺陷。

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