化学气相渗透
材料科学
相间
复合材料
烧蚀
等温过程
抗弯强度
热解
复合数
化学工程
遗传学
生物
热力学
物理
工程类
航空航天工程
作者
Rida Zhao,Chenglong Hu,Yuanhong Wang,Shengyang Pang,Jian Li,Sufang Tang,Hui‐Ming Cheng
标识
DOI:10.1016/j.jeurceramsoc.2021.12.006
摘要
Four kinds of sandwich-structured C/C-SiC and C/C-SiC-ZrC composites with or without a SiC interphase deposited by isothermal chemical vapor infiltration (ICVI), were designed and fabricated by a joint process of electromagnetic coupling chemical vapor infiltration (ECVI) and precursor infiltration and pyrolysis (PIP). The fabricated composites are macroscopically nonhomogeneous materials with low density, high strength and low ablation rate. The interphase and matrix constituents had remarkable effects on the mechanical and ablation properties of these composites. The C/C-SiC composites with an ICVI-SiC interphase exhibited the highest flexural strength of 306.5 MPa. While the C/C-SiC-ZrC composites with the interphase showed the best anti-ablation performance with low linear and mass ablation rates of 0.37 μm/s and 0.04 mg/cm2·s, respectively, after the ablation for 500 s under an oxyacetylene flame test at around 2000 °C.
科研通智能强力驱动
Strongly Powered by AbleSci AI