Preliminary Assessment of the Influence of the Type of a Curing Agent upon Impact Loading of a Multi-Layered Composite

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Abstract:

The properties of a multi-layered composite can be moulded through a selection of type, shape, and the number of layers of reinforcement material as well as powder fillers. Furthermore, the type and share of the matrix as well as the kind of hardeners also exert a significant influence on mechanical properties of composites. We attempted to experimentally establish the influence of the type of hardeners on mechanical properties. The test used Charpy’s hammer, and it was performed in the configuration of impact loading parallel to the edge. We prepared specimens of the materials. The specimens contained 12 layers of different fibre reinforcement: aramid (kevlar) fibre of 230 g/m2 basis weight, glass fibre of 150 g /m2, and carbon fibre of 160 g/m2 basis weight. The base was epoxy resin – Epidian 52, which was cured at room temperature by means of the following curing agents: PAC, TFF or Z-1, manufactured by Z. Ch. Organika-Sarzyna S.A. in Nowa Sarzyna. The experiments proved the tremendous influence of the type of the hardeners on toughness KC. It can be increased even by 25% for glass fibre reinforcement, about 20% for carbon fibre reinforcement and about 10% for aramid fibre reinforcement due to the use of an appropriate type of hardener.

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Solid State Phenomena (Volume 223)

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19-26

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November 2014

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© 2015 Trans Tech Publications Ltd. All Rights Reserved

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[1] S. Ochelski, Metody doświadczalne mechaniki kompozytów konstrukcyjnych, first ed., WNT, Warszawa, (2004).

Google Scholar

[2] A.P. Wilczyński, Polimerowe kompozyty włókniste, first ed., WNT, Warszawa, (1996).

Google Scholar

[3] J. Zhang, K. He S. Chaisombat, C.H. Wang, Hybrid composite laminates reinforced with glass/carbon woven fabrics for lightweight load bearing structures, Mater. Design 36 (2012) 75–80.

DOI: 10.1016/j.matdes.2011.11.006

Google Scholar

[4] A.P. Mouritz, J. Gallagher, A.A. Goodwin, Flexural strength and interlaminar shear strength of stitched GRP laminates following repeated impacts, Compos. Sci. Technol. 57 (1997) 509-522.

DOI: 10.1016/s0266-3538(96)00164-9

Google Scholar

[5] V.P.W. Shim, L.M. Yang, Characterization of the residual mechanical properties of woven fabric reinforced composites after low-velocity impact, Int. J. Mech. Sci. 47 (2005) 647-665.

DOI: 10.1016/j.ijmecsci.2005.01.014

Google Scholar

[6] Z.Y. Zhang, M.O.W. Richardson, Low velocity impact induced damage evaluation and its effect on the residual flexural properties of pultruded GRP composites, Compos. Struc. 81 (2007) 195-201.

DOI: 10.1016/j.compstruct.2006.08.019

Google Scholar

[7] P.N.B. Reis , J.A.M. Ferreira , P. Santos, Richardson  M.O.W., J.B. Santos, Impact response of Kevlar composites with filled epoxy matrix, Compos. Struc. 94 (2012) 3520-3528.

DOI: 10.1016/j.compstruct.2012.05.025

Google Scholar

[8] A. Komorek, P. Przybyłek, Examination of the influence of cross-impact load on bend strength properties of composite materials, used in aviation, Eksploat. Niezawod. 14 (2012) 265-269.

Google Scholar

[9] M. Kozioł, The effect of reinforcing fabric type on mechanical performance of laminar FR epoxy composite, Composites 12: 1 (2012) 60-65.

Google Scholar