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Study on Remote Field Eddy Current Testing Technology for Crack-like Defects in Long Truss Structure of Aircraft

Detection of hidden defects of aircraft long truss structures (aluminum alloy) is a challenging problem. The shape of the aircraft truss structure is complex, and the crack defects are buried in a large depth. Without the restriction of skin effect, remote field eddy current (RFEC) has great advanta...

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Autores principales: Zhang, Lipan, Deng, Rui, Ning, Ning, Fan, Junling, Wang, Wentao, Song, Kai
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2022
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9330189/
https://www.ncbi.nlm.nih.gov/pubmed/35897527
http://dx.doi.org/10.3390/ma15155093
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author Zhang, Lipan
Deng, Rui
Ning, Ning
Fan, Junling
Wang, Wentao
Song, Kai
author_facet Zhang, Lipan
Deng, Rui
Ning, Ning
Fan, Junling
Wang, Wentao
Song, Kai
author_sort Zhang, Lipan
collection PubMed
description Detection of hidden defects of aircraft long truss structures (aluminum alloy) is a challenging problem. The shape of the aircraft truss structure is complex, and the crack defects are buried in a large depth. Without the restriction of skin effect, remote field eddy current (RFEC) has great advantages in detecting buried depth defects. In this paper, in order to detect the hidden defects of the aluminum alloy aircraft long truss structure, the remote field eddy current probe is improved from two aspects of magnetic field enhancement and near-field signal suppression using the finite element method. The results show that indirect coupling energy is greatly enhanced when the connected magnetic circuit is added to the excitation coil. By adding a composite shielding structure outside the excitation coil and the detection coil, respectively, the direct coupling energy is effectively restrained. As a result, the size of the probe is reduced. By optimizing the coil spacing and probe placement position, the detection sensitivity of the probe is improved. The simulation is verified by experiments, and the experimental results are consistent with the simulation conclusions.
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spelling pubmed-93301892022-07-29 Study on Remote Field Eddy Current Testing Technology for Crack-like Defects in Long Truss Structure of Aircraft Zhang, Lipan Deng, Rui Ning, Ning Fan, Junling Wang, Wentao Song, Kai Materials (Basel) Article Detection of hidden defects of aircraft long truss structures (aluminum alloy) is a challenging problem. The shape of the aircraft truss structure is complex, and the crack defects are buried in a large depth. Without the restriction of skin effect, remote field eddy current (RFEC) has great advantages in detecting buried depth defects. In this paper, in order to detect the hidden defects of the aluminum alloy aircraft long truss structure, the remote field eddy current probe is improved from two aspects of magnetic field enhancement and near-field signal suppression using the finite element method. The results show that indirect coupling energy is greatly enhanced when the connected magnetic circuit is added to the excitation coil. By adding a composite shielding structure outside the excitation coil and the detection coil, respectively, the direct coupling energy is effectively restrained. As a result, the size of the probe is reduced. By optimizing the coil spacing and probe placement position, the detection sensitivity of the probe is improved. The simulation is verified by experiments, and the experimental results are consistent with the simulation conclusions. MDPI 2022-07-22 /pmc/articles/PMC9330189/ /pubmed/35897527 http://dx.doi.org/10.3390/ma15155093 Text en © 2022 by the authors. https://creativecommons.org/licenses/by/4.0/Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/).
spellingShingle Article
Zhang, Lipan
Deng, Rui
Ning, Ning
Fan, Junling
Wang, Wentao
Song, Kai
Study on Remote Field Eddy Current Testing Technology for Crack-like Defects in Long Truss Structure of Aircraft
title Study on Remote Field Eddy Current Testing Technology for Crack-like Defects in Long Truss Structure of Aircraft
title_full Study on Remote Field Eddy Current Testing Technology for Crack-like Defects in Long Truss Structure of Aircraft
title_fullStr Study on Remote Field Eddy Current Testing Technology for Crack-like Defects in Long Truss Structure of Aircraft
title_full_unstemmed Study on Remote Field Eddy Current Testing Technology for Crack-like Defects in Long Truss Structure of Aircraft
title_short Study on Remote Field Eddy Current Testing Technology for Crack-like Defects in Long Truss Structure of Aircraft
title_sort study on remote field eddy current testing technology for crack-like defects in long truss structure of aircraft
topic Article
url https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9330189/
https://www.ncbi.nlm.nih.gov/pubmed/35897527
http://dx.doi.org/10.3390/ma15155093
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