Abstract
Hot pressed ZrB2-SiC-graphite ultra high temperature ceramic composites were prepared for the fracture toughness tests in vacuum up to 1800 °C and in air up to 1300 °C. Measured results show that a brittle-ductile transition temperature of ZrB2-SiC-graphite composite is deduced to be 1300 °C, and ZrB2-SiC-graphite composite exhibits a linear behavior below 1300 °C. Fracture toughness in vacuum linearly decreases with the increase of temperature below 1300 °C, increases from 1300 °C to 1600 °C, and has a rapid reduction at 1800 °C. The phenomenon can be attributed to the relaxation of thermal residual stress under 1300 °C, the existence of plastic flow from 1300 °C to 1600 °C, and the degeneration of graphite flakes and cavitation formation at 1800 °C. In comparison to vacuum, the fracture toughness in air improves by the healing effect of pre-oxidation below 1300 °C. The microstructure observations further reveal the great effects of temperature and pre-oxidation on the fracture behavior of ZrB2-SiC-graphite composite.
Original language | English |
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Pages (from-to) | 145-150 |
Number of pages | 6 |
Journal | Journal of Alloys and Compounds |
Volume | 619 |
DOIs | |
Publication status | Published - 15 Jan 2015 |
Externally published | Yes |
Keywords
- Fracture toughness
- High temperature
- Microstructure
- ZrB-SiC-graphite composite