DAMAGE OF CARBON PLASTICS FROM LOW-VELOCITY IMPACT AND THEIR RELAXATION
DOI:
https://doi.org/10.18372/0370-2197.2(107).20169Keywords:
damage, carbon fiber, low-velocity impact, epoxy matrix, dent, relaxation degreeAbstract
The damage assessment of carbon plastics with different filler structures based on the same epoxy matrix HexPly M 21 from low-velocity impact was carried out. The purpose of the research was to determine the difference between the depths of dents and the diameters of damage of carbon plastics that had two different fillers, namely bidirectional fabric and unidirectional carbon tape. Low-velocity impact tests were carried out with the same energy of 6.7 J per 1 mm of sample thickness. Immediately after the impact, damage parameters such as the depth of the dent and the maximum size (diameter) were measured, with the latter being determined from both the front and back sides. The depth of the dent was measured immediately after impact and after 7 days to determine the degree of damage relaxation, which reached 17%. The results of the studies are presented in the form of histograms of dent depths and damage diameters on both sides of the samples. It was found that the damage diameters for carbon plastics of both performances on the back side are significantly larger than on the front side.
References
Deformation and damage of modern composites at low velocity impact event / Astanin V.V., Shevchenko O.A., Dydenko О.V. // Proceedings the Seventh World Congress “Aviation in the XXI-st Century” Safety in Aviation and Space Technologies. September 19-21, 2016, Theses of the Report – К.: NAU, 2016. – P. 1.3.6 –1.3.10.
Standart ASTM D7136/D7136 M – 05 the Impact Properties of Fiber Reinforced Com-posite Laminated Plates. Journal of Reinforced Plastics and Composites. 2000. V.19. N 06.
Rolls-Royce starts manufacture of world's largest fan blades, made with composites, for UltraFan demonstrator. // CompositesWorld. Published. 2/11/2020.
Wagner H., Bansemir H., Drechsler K., Weimer C. Impact Behavior and Residual Strength of Carbon Fiber Textile Based Materials. SAMPE Europe, SETEC 2007.–P.15–25.
Erber A., Gittel D., Geiger O., Chandhari R., Henning F., Drechsler K. Edvanced Damage tolerance of CFRP Laminates Using in-SITU Polymerised Thermoplastics. SAMPE Europe, SETEC 2009. – P. 15 – 25.
Damage of fiber reinforced polymer matrix composites from a drop weight impact event / Shevchenko O.A., Olefir О.I., Skrypnikov О.E. // Proceedings the Sixth World Congress “Aviation in the XXI-st Century” Safety in Aviation and Space Technologies. September 23 –25, 2014, Theses of the Report – К.: NAU, 2014. – Т. І. – P. 1.3.23 – 1.3.27.
Satkar A.R., Mache A., Kulkarni A. Numerical investigation on perforation resistance of glass-carbon/epoxy hybrid composite laminate under ballistic impact. Materials Today: Proceedings. Vol. 59, Part 1, 2022, – P. 734-741.
Zwick / Roell Intelligent Testing. Corporate Presentation Composites. XIX International Forum “testXpo”. 10 / 2010.
Mala hirnycha entsyklopediya: u 3 t./ za red. V. S. Biletsʹkoho. – D. Donbas, 2007. – Т.2. – 670 s. — ISBN 57740-0828-2