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Use of computed tomography to assess quality and structure of curved CFRP laminate samples produced by autoclave technology

Helizanowicz Barbara, Helizanowicz Damian, Krzemiński Łukasz, Matula Grzegorz

Composites Theory and Practice

2024

R. 24, nr 1

72--77

Carbon fiber reinforced polymer (CFRP) composite laminates are widely used in parts with complex shapes with different curvatures. The curved regions are susceptible to the occurrence of manufacturing defects and premature in-service damage, thus the nondestructive inspection (NDI) of the curved regions is an important issue. X-ray computed tomography (CT) was used to assess the structure of CFRP composite laminate curved beams with different curvature geometry produced in the autoclave technology. The performed inspection allowed visualization of the structure of the curvatures on the ply level and the detection of defects such as foreign objects, voids, resin rich regions, wrinkles and changes in thickness. Also, the quantitative assessment of the defects and distances between the adjacent layers was carried out. The performed investigations show that X-ray CT is an adequate tool to visualize curved CFRP structures.

A Comparison of Composite Specimens Damage area Measurements Performed using Pulsed Thermography and Ultrasonic NDT Methods

Luziński Rafał, Ziemkiewicz Jarosław, Synaszko Piotr, Żyluk Andrzej, Dragan Krzysztof

Fatigue of Aircraft Structures

2019

Iss. 11

68--77

Carbon fiber reinforced plastics (CFRPs) are widely used in aerospace structures due to their high stiffness, strength and good fatigue properties. They are however vulnerable to loads perpendicular to their plane and, while impacted, can suffer significant internal damage decreasing their overall strength. Detecting and sizing such damage is an important task of the non-destructive inspection (NDI) methods. This study was conducted to detect and quantify damage in a set of six impacted even rectangular CFRP specimens designed from a MiG-29 vertical stabilizer’s skin. The inspection was done using the ultrasonic (UT) method (based on mobile scanner – MAUS V) and the pulsed infrared thermographic (IRT) method. Each specimen’s inside and outside (impacted) surface was inspected separately with IRT, while the outside surface was then inspected with UT. UT provided the most precise measurements of the damage area, while the IRT inspection of the outside surface (which would be accessible on a real aircraft structure) provided underestimated values due to the damage’s depth and geometry.