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Ablation Mechanism of HfC-HfO2 Protective Coating for SiC-Coated C/C Composites in an Oxyacetylene Torch Environment
被引:45
|作者:
Yang, Yang
[1
]
Li, Kezhi
[1
]
Liu, Guanxi
[1
]
Zhao, Zhigang
[1
]
机构:
[1] Northwestern Polytech Univ, Carbon Carbon Composites Res Ctr, State Key Lab Solidificat Proc, Xian 710072, Shaanxi, Peoples R China
基金:
中国国家自然科学基金;
关键词:
Carbon/carbon composites;
Supersonic atmospheric plasma spraying;
Protective coating;
Ablation property;
HIGH-TEMPERATURE OXIDATION;
THERMAL-SHOCK RESISTANCE;
CARBON/CARBON COMPOSITES;
HAFNIUM CARBIDE;
HFC NANOWIRES;
BEHAVIOR;
ENHANCE;
CARBON;
MODEL;
HFO2;
D O I:
10.1016/j.jmst.2016.11.010
中图分类号:
T [工业技术];
学科分类号:
08 ;
摘要:
To prevent the C/C composites from ablation, HfC-HfO2 protective coating was prepared by supersonic atmospheric plasma spraying. The morphology and microstructure of HfC-HfO2 coating were characterized by X-ray diffraction and scanning electron microscopy. The ablation resistance test was carried out by an oxyacetylene torch. The results show that the as-prepared coating is dense with little pinholes and crack free. The elements Hf, C and O were uniformly distributed in the cross-section. After ablation for different time, the mass ablation rate fluctuated along with the change of ablation time. The ablation process of the surface coating could be divided into rapid oxidation and solid state sintering stages. During ablation, an HfCxOy-HfO2 transitional layer was generated in the coating, which resulted from the active oxidation of HfC. After cooling, some microcracks were observed on the surface of coating, and the structure of cross-section was broken, which were due to the phase transition of HfO2. (C) 2016 Published by Elsevier Ltd on behalf of The editorial office of Journal of Materials Science & Technology.
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页码:1195 / 1202
页数:8
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