Pulsed eddy current technique for defect detection in aircraft riveted structures

被引:160
作者
He, Yunze [1 ]
Luo, Feilu [1 ]
Pan, Mengchun [1 ]
Weng, Feibing [1 ]
Hu, Xiangchao [1 ]
Gao, Junzhe [1 ]
Liu, Bo [1 ]
机构
[1] Natl Univ Def Technol, Coll Mechatron & Automat, Changsha 410073, Hunan, Peoples R China
关键词
Nondestructive testing; Pulsed eddy current; Differential probe; Defect detection; Riveted structure; CURRENT SIGNALS; AGING AIRCRAFT; CURRENT NDT; LAP-JOINTS; CLASSIFICATION; SENSORS;
D O I
10.1016/j.ndteint.2009.10.010
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
The Pulsed Eddy Current (PEC) technique is an effective method of quantifying defects in multi-layer structures. It is difficult to detect defects in riveted structures of aging aircraft. Based on theoretical analysis of PEC technique, three different probes, including a differential hall probe, a differential coil probe, and a two-stage differential coil probe are designed to detect this kind of defects. The averaging method and wavelet analysis method are used to de-noise the hall response signals. By selecting peak amplitude and zero-crossing time of response signal in time domain as key features, defects in riveted structures can be detected effectively. The experimental results indicated that the differential coil probe acted as effectively as the differential hall probe. The defects between third layer and fourth layer in riveted structures can be detected by utilizing the two-stage differential coil probe. The PEC technique has a promising application foreground in the field of aeronautical nondestructive testing. Crown Copyright (C) 2009 Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:176 / 181
页数:6
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