Simulation Analysis of Eddy Current Testing Parameters for Surface and Subsurface Defect Detection of Aviation Aluminum Alloy Plate

Author:

Deng Weiquan1ORCID,Bao Jun2ORCID,Luo Siqi3ORCID,Xiong Xin3ORCID

Affiliation:

1. Faculty of Mechanical and Electrical Engineering, Kunming University of Science and Technology, Kunming 650500, China

2. Faculty of Civil Aviation and Aeronautics, Kunming University of Science and Technology, Kunming 650500, China

3. Faculty of Information Engineering and Automation, Kunming University of Science and Technology, Kunming 650500, China

Abstract

In the process of eddy current testing (ECT) of surface and subsurface defects of aviation aluminum alloy plates, the setting of parameters is important to the test results. Inappropriate test parameters can cause false detection or even missed detection of defects. To address this problem, the effects of probe type, coil size, and excitation frequency on the accurate identification and quantitative evaluation of surface and subsurface defect detection were studied and analyzed in this study to determine the best testing parameters. The experimental results show that the absolute probe with an outer radius of 3.3 mm has better detection performance for aviation aluminum alloy plate defects. There are different optimal excitation frequency ranges for the surface and subsurface defects. An excitation frequency of 80 kHz to 90 kHz can be used for the detection of unknown defects.

Funder

Applied Basic Research Programs of Science and Technology Commission Foundation of Yunnan Province

Publisher

Hindawi Limited

Subject

Electrical and Electronic Engineering,Instrumentation,Control and Systems Engineering

Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. PECT Composite Defect Detection Algorithm Based on DualGAN;International Journal of Image and Graphics;2024-04-09

2. A novel defect identification design of gas pipeline based on inverse heat conduction problem;Journal of Thermal Analysis and Calorimetry;2023-02-01

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