Nanoindentation Experiment and Properties Analysis of C/C Composites
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Xi’an Aerospace Composites Research Institute, Xi’an 710025

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TB332

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    Abstract:

    The properties of C/C composites with different graphitization temperatures and mixed matrix carbon were investigated by nanoindentation. The results show that the nanoindentation modulus of C/C composites with graphitization temperature of 2 500 ℃ was 10% lower than that of C/C composites with graphitization temperature of 2 300 ℃. The highest modulus of resin carbon is measured by nanoindentation in C/C composites with mixed matrix of pyrolytic carbon, resin carbon and asphalt carbon, followed by pyrolytic carbon and the lowest by asphalt carbon. The surface fracture toughness of the C/C composite micro-component was finally obtained as 0.492 MPa•m1/2 by nonlinear fitting of the nanoindentation load displacement curve after finite element calculations.

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History
  • Received:August 26,2021
  • Revised:September 02,2021
  • Adopted:August 27,2021
  • Online: September 29,2021
  • Published: