Thermophysical Properties of Silicon-Carbide-Based Ceramic Composite Materials Obtained by Spark Plasma Sintering (SPS)
- Authors: Loshchinin Y.V.1, Lebedeva Y.E.1, Slavin A.V.1
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Affiliations:
- All-Russia Scientific-Research Institute of Aviation Materials (VIAM)
- Issue: Vol 75, No 9-10 (2019)
- Pages: 340-344
- Section: Science for Ceramic Production
- URL: https://journals.rcsi.science/0361-7610/article/view/245291
- DOI: https://doi.org/10.1007/s10717-019-00082-w
- ID: 245291
Cite item
Abstract
The factors influencing the thermal conductivity of SiC-based ceramic composite materials obtained by the spark plasma sintering technology with relative density 99% and B4C, AlN, Si3N4, Y2O3, Al2O3, and HfB2 as additives are examined. The thermophysical properties were determined in the temperature range 20 – 1300°C: specific heat, thermal diffusivity, and thermal conductivity of composites. The thermal diffusivity and specific heat were measured by the laser-spark method. The measurements of specific heat are supplemented by measurements performed with a DSC and adiabatic calorimeter. The thermal conductivity is calculated using data on the thermal diffusivity, specific heat, and density.
About the authors
Yu. V. Loshchinin
All-Russia Scientific-Research Institute of Aviation Materials (VIAM)
Email: yulia.ananieva@gmail.com
Russian Federation, Moscow
Yu. E. Lebedeva
All-Russia Scientific-Research Institute of Aviation Materials (VIAM)
Author for correspondence.
Email: yulia.ananieva@gmail.com
Russian Federation, Moscow
A. V. Slavin
All-Russia Scientific-Research Institute of Aviation Materials (VIAM)
Email: yulia.ananieva@gmail.com
Russian Federation, Moscow
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