Non-destructive Inspection of Composite Aileron during Fatigue Test

The operational safety and reliability of an airplane must be an integral part of its design. The use of suitable materials that pass material certification tests is very important for a new aircraft design. The next part is testing specific samples, sub-components, and components such as the ailero...

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Autores principales: Podstawka Michal, Snop Vladimír, Bělský Petr, Kutiová Kristýna
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FR
Publicado: EDP Sciences 2021
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Acceso en línea:https://doaj.org/article/a1f8c858765348d8aee0411a32c226b9
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spelling oai:doaj.org-article:a1f8c858765348d8aee0411a32c226b92021-12-02T17:13:46ZNon-destructive Inspection of Composite Aileron during Fatigue Test2261-236X10.1051/matecconf/202134903016https://doaj.org/article/a1f8c858765348d8aee0411a32c226b92021-01-01T00:00:00Zhttps://www.matec-conferences.org/articles/matecconf/pdf/2021/18/matecconf_iceaf2021_03016.pdfhttps://doaj.org/toc/2261-236XThe operational safety and reliability of an airplane must be an integral part of its design. The use of suitable materials that pass material certification tests is very important for a new aircraft design. The next part is testing specific samples, sub-components, and components such as the aileron. The paper deals with a non-destructive evaluation of composite primary structural part fatigue tests in accordance with damage tolerance philosophy considering impact damage presence. NDT methods such as visual, eddy current, and ultrasonic testing included phased array technique, are used for the inspections. A schedule of inspections was created, and structural durability was verified.Podstawka MichalSnop VladimírBělský PetrKutiová KristýnaEDP SciencesarticleEngineering (General). Civil engineering (General)TA1-2040ENFRMATEC Web of Conferences, Vol 349, p 03016 (2021)
institution DOAJ
collection DOAJ
language EN
FR
topic Engineering (General). Civil engineering (General)
TA1-2040
spellingShingle Engineering (General). Civil engineering (General)
TA1-2040
Podstawka Michal
Snop Vladimír
Bělský Petr
Kutiová Kristýna
Non-destructive Inspection of Composite Aileron during Fatigue Test
description The operational safety and reliability of an airplane must be an integral part of its design. The use of suitable materials that pass material certification tests is very important for a new aircraft design. The next part is testing specific samples, sub-components, and components such as the aileron. The paper deals with a non-destructive evaluation of composite primary structural part fatigue tests in accordance with damage tolerance philosophy considering impact damage presence. NDT methods such as visual, eddy current, and ultrasonic testing included phased array technique, are used for the inspections. A schedule of inspections was created, and structural durability was verified.
format article
author Podstawka Michal
Snop Vladimír
Bělský Petr
Kutiová Kristýna
author_facet Podstawka Michal
Snop Vladimír
Bělský Petr
Kutiová Kristýna
author_sort Podstawka Michal
title Non-destructive Inspection of Composite Aileron during Fatigue Test
title_short Non-destructive Inspection of Composite Aileron during Fatigue Test
title_full Non-destructive Inspection of Composite Aileron during Fatigue Test
title_fullStr Non-destructive Inspection of Composite Aileron during Fatigue Test
title_full_unstemmed Non-destructive Inspection of Composite Aileron during Fatigue Test
title_sort non-destructive inspection of composite aileron during fatigue test
publisher EDP Sciences
publishDate 2021
url https://doaj.org/article/a1f8c858765348d8aee0411a32c226b9
work_keys_str_mv AT podstawkamichal nondestructiveinspectionofcompositeaileronduringfatiguetest
AT snopvladimir nondestructiveinspectionofcompositeaileronduringfatiguetest
AT belskypetr nondestructiveinspectionofcompositeaileronduringfatiguetest
AT kutiovakristyna nondestructiveinspectionofcompositeaileronduringfatiguetest
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