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Evaluation of Eddy Current Array Performance in Detecting Aircraft Component Defects Cover

Evaluation of Eddy Current Array Performance in Detecting Aircraft Component Defects

Open Access
|Jun 2024

Figures & Tables

Fig. 1.

Sample made of AD31T5 alloy (1–8: defects of various types and sizes)
Sample made of AD31T5 alloy (1–8: defects of various types and sizes)

Fig. 2.

Airplane in a steady-state turn
Airplane in a steady-state turn

Fig. 3.

Scanning results in the form of C-scans for sample sections
Scanning results in the form of C-scans for sample sections

Experimental data of the test specimen investigation_

No. of defectThe number of holes n (length in mm)Signal amplitude from the defect (V)
80 kHz160 kHz320 kHz
19 (2.9)4.610.610.6
27 (1.7)2.77.97.9
319 (2.9)5.710.710.8
437 (4.1)7.510.910.9
51 (0.5)-1.11.6
63 (1.1)1.02.74.3
75 (1.7)2.06.210.3
87 (2.3)3.48.310.5
Language: English
Page range: 1 - 9
Submitted on: Dec 9, 2023
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Accepted on: Mar 20, 2024
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Published on: Jun 12, 2024
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year

© 2024 Iuliia Lysenko, Yurii Kuts, Valentyn Uchanin, Yordan Mirchev, Oleksandr Levchenko, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.