摘要
A novelty technique, namely, pre-oxidation, has been proposed to improve the strength and thermal shock behavior of ZrB 2-SiC-graphite ceramic composites, which is a promising candidate for ultra-high temperature ceramics (UHTCs) in aerospace engineering. The composite is pre-oxidized at temperatures of 900°C and 1100°C for 1 h and 3 h in air. A theoretical model considering surface heat transfer has been given and analyzed. A water-quenching technique is adopted at different temperatures from 300°C to 600°C in order to investigate the thermal shock behavior of pre-oxidized composites. The critical thermal shock temperature improves more than 40% after pre-oxidizing at 1100°C for 3 h. However, the composites strength is not improved as a result of the insensitivity to surface defects.
源语言 | 英语 |
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页(从-至) | 12-16 |
页数 | 5 |
期刊 | Journal of Harbin Institute of Technology (New Series) |
卷 | 19 |
期 | 1 |
出版状态 | 已出版 - 2月 2012 |
已对外发布 | 是 |