Abstract
In this work, four different carbon fiber reinforced SiC-based matrix composites (C/SiC) were prepared, and microstructure evolution during laser ablation process was characterized. Laser irradiation provided a special high-temperature environment up to 3500 °C. For all four composites, different morphologies can be obtained in the transition region due to the oxidation of different matrices. While only needle-shaped carbon fiber and nanolayered carbon without any matrix remained in the central region, indicating that graphitization process occurred in the center, resulting from the high-temperature and low-oxygen environment in the laser process. Therefore, the laser ablation of C/SiC composites is controlled by chemical and physical erosion, and mainly by the physical erosion in the center.
| Original language | English |
|---|---|
| Pages (from-to) | 2919-2925 |
| Number of pages | 7 |
| Journal | Journal of Materials Science and Technology |
| Volume | 35 |
| Issue number | 12 |
| DOIs | |
| State | Published - Dec 2019 |
Keywords
- Ablation performance
- C/SiC composite
- Laser ablation
- Mechanism
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