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Ablation Mechanism of HfC-HfO2Protective Coating for SiC-Coated C/C Composites in an Oxyacetylene Torch Environment 被引量:3

Ablation Mechanism of HfC-HfO_2Protective Coating for SiC-Coated C/C Composites in an Oxyacetylene Torch Environment
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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 Hf CxOy-HfO2 transitional layer was generated in the coating, which resulted from the active oxidation of Hf C. 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. 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 Hf CxOy-HfO2 transitional layer was generated in the coating, which resulted from the active oxidation of Hf C. 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.
出处 《Journal of Materials Science & Technology》 SCIE EI CAS CSCD 2017年第10期1195-1202,共8页 材料科学技术(英文版)
基金 supported by the National Natural Science Foundation of China under Grant Nos. U1435202 and 51521061 the “111” Project under Grant No. 08040 the Research Fund of the State Key Laboratory of Solidification Processing (Northwestern Polytechnical University), China (Grant No. 142-TZ-2016)
关键词 Carbon/carbon composites Supersonic atmospheric plasma spraying Protective coating Ablation property Carbon/carbon composites Supersonic atmospheric plasma spraying Protective coating Ablation property
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