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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EDP Sciences
2021
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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) |
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Engineering (General). Civil engineering (General) TA1-2040 |
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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 |
_version_ |
1718381335973724160 |