Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
1574404 | Materials Science and Engineering: A | 2015 | 5 Pages |
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.
Related Topics
Physical Sciences and Engineering
Materials Science
Materials Science (General)
Authors
Hui Mei, Tianming Ji, Xi Chen, Qianglai Bai, Laifei Cheng,