| Issue |
E3S Web Conf.
Volume 19, 2017
International Conference Energy, Environment and Material Systems (EEMS 2017)
|
|
|---|---|---|
| Article Number | 03018 | |
| Number of page(s) | 4 | |
| Section | Materials | |
| DOI | https://doi.org/10.1051/e3sconf/20171903018 | |
| Published online | 23 October 2017 | |
Determination of mechanical properties of carbon/epoxy plates by tensile stress test
1 Technical University of Cluj-Napoca, Faculty of Machine Building, B-dul Muncii 103 – 105, RO-400641 Cluj-Napoca, Romania
2 Opole University of Technology, Faculty of Mechanical Engineeing, Proszkowska 76, 45-758 Opole, Poland
⁎ Corresponding author: j.krolczyk@po.opole.pl
The polymeric composite materials used in aerospace, military, medical or racing cars manufacturing end up being used in our daily life Whether we refer to the performing vehicles, subassemblies or parts for aircrafts, wind, telegraph poles, or medical prostheses they all are present in our lives and they are made of composite materials (CM). This paper presents research regarding three different composite materials, plates by carbon fiber, in epoxy matrix. Starting with materials presentation, manufacturing methodology and determination of mechanical properties at carbon fiber/epoxy were done. Vacuum bag technology to obtain the composite structure offer opportunity to get a very compact and homogeny composite structure. For the moment this technology are adequate for high performances pieces. The mechanical characteristics of plates made of composite materials reinforced presented indicates closed value like metal materials. Based on the results, a comparative study between the reinforced materials typically used to manufacture the plates of CM is carried out.
© The authors, published by EDP Sciences, 2017
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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