TY - JOUR
T1 - High-temperature effects on the compressive behaviors of SiC-coated carbon-bonded carbon fiber composites
T2 - Insights into mechanical properties and cyclic deformation recovery
AU - Li, Zhinan
AU - Li, Tongqi
AU - Xia, Tong
AU - Qian, Yixing
AU - Yang, Zhenyu
AU - Lu, Zixing
N1 - Publisher Copyright:
© 2025 The Authors.
PY - 2025/5/1
Y1 - 2025/5/1
N2 - Porous SiC-coated carbon-bonded carbon fiber composites (SiC-coated CBCFs) are fabricated via chemical vapor deposition (CVD) method, where silicon carbide coatings are uniformly applied to carbon fibers bonded by pyrolytic carbon while preserving their three-dimensional interconnected pore structure. The mechanical responses of SiC-coated CBCFs under elevated temperatures are systematically characterized through quasi-static compression testing coupled with multiscale microstructural analysis. The results demonstrate a monotonic decrease in elastic moduli as temperature increases to 2000 °C. In contrast, compressive strengths initially rise and then experience a slight fluctuation before the significant decrease. Under stepwise cyclic compressive loading, both the deformation recovery ability and load-bearing stiffness exhibit notable degradation at elevated temperatures, highlighting the need for larger safety margins in realistic thermal insulation scenarios. These findings establish quantitative correlations between thermomechanical degradation mechanisms and operational limits, offering valuable insights for their design and application in reusable high-performance systems.
AB - Porous SiC-coated carbon-bonded carbon fiber composites (SiC-coated CBCFs) are fabricated via chemical vapor deposition (CVD) method, where silicon carbide coatings are uniformly applied to carbon fibers bonded by pyrolytic carbon while preserving their three-dimensional interconnected pore structure. The mechanical responses of SiC-coated CBCFs under elevated temperatures are systematically characterized through quasi-static compression testing coupled with multiscale microstructural analysis. The results demonstrate a monotonic decrease in elastic moduli as temperature increases to 2000 °C. In contrast, compressive strengths initially rise and then experience a slight fluctuation before the significant decrease. Under stepwise cyclic compressive loading, both the deformation recovery ability and load-bearing stiffness exhibit notable degradation at elevated temperatures, highlighting the need for larger safety margins in realistic thermal insulation scenarios. These findings establish quantitative correlations between thermomechanical degradation mechanisms and operational limits, offering valuable insights for their design and application in reusable high-performance systems.
KW - Carbon-bonded carbon fiber composites (CBCFs)
KW - Compressive mechanical properties
KW - Deformation recovery ability
KW - High temperature
KW - SiC coatings
UR - https://www.scopus.com/pages/publications/105025420336
U2 - 10.1016/j.jmrt.2025.05.081
DO - 10.1016/j.jmrt.2025.05.081
M3 - 文章
AN - SCOPUS:105025420336
SN - 2238-7854
VL - 36
SP - 8264
EP - 8276
JO - Journal of Materials Research and Technology
JF - Journal of Materials Research and Technology
ER -