Automated Eddy Current System for Aircraft Structure Inspection

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dc.contributor.authorKuts, Yurii
dc.contributor.authorLysenko, Iuliia
dc.contributor.authorPetryk, Valentyn
dc.contributor.authorMalko, Volodymyr
dc.contributor.authorMelnyk, Andrii
dc.date.accessioned2023-12-09T16:14:56Z
dc.date.available2023-12-09T16:14:56Z
dc.date.issued2023
dc.description.abstractAircraft part diagnostics are crucial during both production and maintenance, with eddy current non-destructive testing (ECNDT) being the method of choice due to its cost-effectiveness, informativeness,productivity, and reliability. ECNDT excels regardless of surface condition or coatings. It’s employed fordiagnosing various aircraft components, necessitating diverse transducer types, excitation modes, andadvanced signal processing. To improve ECNDT, this article explores integrating harmonic and impulseexcitation modes in a single tool to enhance informativeness. Building upon a wireless eddy current system,the authors propose a comprehensive method for processing and displaying information suitable for objectcondition monitoring systems. The system includes automated transducer mode control and experimentaldata processing algorithms. The constant expansion of tested objects and new materials underscoresthe need to enhance the theoretical foundations of eddy current non-destructive testing, refine signalprocessing techniques, and identify informative signs. This demands the development of new automatedECNDT tools, and this article offers a promising avenue for improvement. The results include model andexperimental tests of system components, showcasing the potential of this approach to enhance ECNDTeffectiveness, automation, and informativeness in the realm of aircraft part diagnostics.uk
dc.format.pagerangeP. 33-40uk
dc.identifier.citationLysenko, I. Automated Eddy Current System for Aircraft Structure Inspection / I. Lysenko, Y. Kuts, V. Petryk, V. Malko, A. Melnyk // Transactions on Aerospace Research. - Institute of Aviation : Poland, 2023. - Volume 4/2023 (273). - P. 33-40.uk
dc.identifier.doihttps://doi.org/10.2478/tar-2023-0021
dc.identifier.issn545-2835
dc.identifier.orcid0000-0002-8493-9474uk
dc.identifier.orcid0000-0001-9110-6684uk
dc.identifier.orcid0000-0003-2301-0722uk
dc.identifier.orcid0000-0003-2879-7915uk
dc.identifier.orcid0009-0000-7572-6840uk
dc.identifier.urihttps://ela.kpi.ua/handle/123456789/62894
dc.language.isoenuk
dc.publisherSciendouk
dc.publisher.placePolanduk
dc.relation.ispartofTransactions on Aerospace Researchuk
dc.subjectscanninguk
dc.subjectinformation parametersuk
dc.subjectaviation material inspectionuk
dc.subjecteddy currentuk
dc.subjectsignal characteristics
dc.titleAutomated Eddy Current System for Aircraft Structure Inspectionuk
dc.typeArticleuk

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