摘要

The thermal shock behavior of ZrB2-SiC-graphite (ZSG) composites was investigated in this study using a novel method of simulating complex thermal stress states that involved electric resistance heating followed by dynamic water cooling. The ZSG composites were heated and cooled to 1020-2020 degrees C at a constant heating rate of similar to 134 degrees C/s and a constant cooling rate of 536 degrees C/s. The residual strength of the composites decreased at temperature difference of 1000-1400 degrees C. This weakening in strength was attributed to the multiple microcracks and flaws that were created by the two-dimensional thermal stresses and by the expanding and shrinking in the volume of the composites, attributed to chemical/physical reactions. Next, it was found that the residual strength of the composites increased at temperature difference of 1400-1700 degrees C, due to the formation of a liquid SiO2 glass and the increase in the quantity of oxides both of which were favorable to healing the flaws and cracks. Finally, the residual strength decreased slowly at temperature difference above 1700 degrees C, which was attributed to the ZrO2-induced crack healing. It was found that the thermal shock behavior of the ZSG composites depended on both the temperature difference and the mode of the thermal shock loading. The material was particular sensitivity to the regime of alternating heating and cooling, which would be similar to actual flight conditions.