Journal of Aeronautical Materials (Aug 2017)

Optimal Design for Hybrid Ratio of Carbon/Basalt Hybrid Fiber Reinforced Resin Matrix Composites

  • XU Hong,
  • LU Yan,
  • ZHANG Ke,
  • LIU Shuan,
  • WANG Xianghui,
  • DOU Yanli

DOI
https://doi.org/10.11868/j.issn.1005-5053.2017.000047
Journal volume & issue
Vol. 37, no. 4
pp. 7 – 13

Abstract

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The optimum hybrid ratio range of carbon/basalt hybrid fiber reinforced resin composites was studied. Hybrid fiber composites with nine different hybrid ratios were prepared before tensile test.According to the structural features of plain weave, the unit cell's performance parameters were calculated. Finite element model was established by using SHELL181 in ANSYS. The simulated values of the sample stiffness in the model were approximately similar to the experimental ones. The stress nephogram shows that there is a critical hybrid ratio which divides the failure mechanism of HFRP into single failure state and multiple failure state. The tensile modulus, strength and limit tensile strain of HFRP with 45% resin are simulated by finite element method. The result shows that the tensile modulus of HFRP with 60% hybrid ratio increases by 93.4% compared with basalt fiber composites (BFRP), and the limit tensile strain increases by 11.3% compared with carbon fiber composites(CFRP).

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