| Issue |
MATEC Web Conf.
Volume 349, 2021
6th International Conference of Engineering Against Failure (ICEAF-VI 2021)
|
|
|---|---|---|
| Article Number | 03016 | |
| Number of page(s) | 6 | |
| Section | Components and Structural Elements in Engineering Applications: Design, Detections of Defects, Structural Health Monitoring | |
| DOI | https://doi.org/10.1051/matecconf/202134903016 | |
| Published online | 15 November 2021 | |
Non-destructive Inspection of Composite Aileron during Fatigue Test
1 VZLU – Czech Aerospace Research Centre, Strength of Structures Department, Beranovych 130, Prague 9, 199 05, Czech Republic
2 VSB TUO – Technical University of Ostrava, Faculty of Mechanical Engineering, Department of Machine and Industrial Design, 17. Listopadu 2172/15, Ostrava-Poruba, 708 00, Czech Republic
* Corresponding author: podstawka@vzlu.cz
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.
© The Authors, published by EDP Sciences, 2021
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