DOI QR코드

DOI QR Code

A Study on Impact Fracture on CFRP Sandwich Composite and CFRP Sandwich Composite with Aluminum Foam Core

CFRP 샌드위치 복합재와 알루미늄 폼 코어 CFRP 샌드위치 복합재에 대한 충격 파괴 연구

  • Lee, Jung-Ho (Mechanical Engineering Dept. Graduate School, Kongju National University) ;
  • Cho, Jae-Ung (Division of Mechanical & Automotive Engineering, Kongju National University)
  • Received : 2016.03.15
  • Accepted : 2016.04.07
  • Published : 2016.04.30

Abstract

In this study, the fracture property of impact absorption is investigated using the carbon fiber composite material. And this property is compared with the carbon fiber composite material with aluminum foam. Carbon fiber composite material has the high specific strength and rigidity and the superior durability and fatigue life and light weight. On the ground of these properties, this material has been used widely at the fields of airplane, national defence industry, vehicle and the various industrial areas. Aluminum foam can also be applied at the various areas as it is the material with the superior properties. And this foam is the material which can solve the problem on the light weight of particular product. At the condition of the impact energy of 20J, the maximum loads of CFRP sandwich composite and CFRP sandwich composite with aluminum foam core are shown to be 5.7 kN and 6.5 kN respectively. In case of maximum energies, these values are shown to be 19 J and 17.5 J respectively. At the impact energy of 50 J, the maximum loads of CFRP sandwich composite and CFRP sandwich composite with aluminum foam core are shown to be 7 kN and 8.8 kN respectively. In case of maximum energies, these values are shown to be 43 J and 48 J respectively. At the impact energy of 80 J, the maximum loads of CFRP sandwich composite and CFRP sandwich composite with aluminum foam core are shown to be 9.2 kN and 11 kN respectively. In case of maximum energies, these values are shown to be 70 J and 63 J respectively. As the result of this study, the mechanical properties are investigated through the impact experiments on the composites composed of the closed aluminum foam and the carbon fiber reinforced plastic used frequently as absorbents.

Keywords

Acknowledgement

Supported by : 한국연구재단

References

  1. B. R. K. Blackman, J. P. Dear, A. J. Kinloch, H. MacGillivray, Y. Wang, J. G. Williams, and P. Yayla, "The Failure of Fibre Composites and Adhesively Bonded Fibre Composites under High Rates of Test Part III Mixed-mode I/II and Mode II Loadings", Journal of Materials Science, Vol. 31, No. 17, pp. 4467-4477, 1996 https://doi.org/10.1007/BF00366342
  2. B. R. K. Blackman, H. Hadavinia, A. J. Kinloch, M. Paraschi and J. G. Williams, "The Calculation of Adhesive Fracture Energies in Mode I: Revisiting the Tapered Double Cantilever Beam (TDCB) Test", Engineering Fracture Mechanics, Vol. 70, No. 2, pp. 233-248, 2003 https://doi.org/10.1016/S0013-7944(02)00031-0
  3. T. W. Kim, B. J. Kim, y. Kim, H. I. Kim, "Density and Geometric Characteristic of Aluminum Foam for Shock Absorption Performance", Transactions of the Korean Society Mechanical Engineers, pp. 11-14, 2007
  4. K. B. Shin and D. H. Koo, "A Study on the Evaluation of the Failure for Carbody Structures Made of Laminated Fiber-reinforced Composite Materials Using Total Laminate Approach", Korean Society for Composite Materials, Vol. 17, No. 1, pp. 18-28, 2004
  5. H. K. Choi and J. U. Cho, "Study on the Fatigue Analysis of DCB Model with Aluminum Foam", Journal of Korean Society of Mechanical Technology, Vol. 14, No. 6, pp. 39-43, 2012.
  6. H. S. Yang and K. H. Kim, "A Study on the Impact Characteristics in the absence of Aircraft Laminated Shell for CF/Epoxy composite", Journal of Korean Society of Mechanical Technology, Vol. 14, No. 6, pp.17-24, 2012.

Cited by

  1. Evaluation on Strength and Durability of Tensile Specimens of CFRP and Metal with Notches vol.18, pp.6, 2016, https://doi.org/10.17958/ksmt.18.6.201612.867
  2. An Analysis Study on the Compact Tension Composite Specimen of Unidirectional CFRP Sandwich Type with SM45C vol.19, pp.3, 2017, https://doi.org/10.17958/ksmt.19.3.201706.360