Abstract
The current work reports on the oxidation behavior and residual flexural strength of carbon fiber-reinforced silicon carbide composites (C/SiC) after induction of thermal crack damage by heat treatment (HT) at 1900. °C and the effect, therein, of a repair process involving recoating by SiC. As-prepared, heat-treated and heat-treated/recoated specimens, were subjected to static oxidation tests in air at a temperature range of 500-1500. °C for 10. h and then tested in three-point bending. It was found that composite weight of heat-treated samples decreased dramatically with increasing oxidation temperature with weight loss values of ~30% being systematically observed for oxidation temperatures above 800. °C. On the other hand, as-prepared and heat-treated/SiC-recoated specimens reached almost their original weight after oxidation. The residual flexural strength of C/SiC composites with thermally-induced crack damage decreased significantly compared to as-prepared specimens, while SiC recoating was found to efficiently enable strength enhancement. Microstructural analysis showed that HT was associated with increased population and dimensions of micro-cracks on the C/SiC surface while SiC recoating enabled repair of HT-induced thermal crack damage hence leading to oxidation resistance recovery of the material.
Original language | English |
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Pages (from-to) | 33-37 |
Number of pages | 5 |
Journal | Materials Science and Engineering: A |
Volume | 631 |
DOIs | |
State | Published - 7 Apr 2015 |
Keywords
- C/SiC composite
- Coating repair
- Heat treatment
- Oxidation resistance