Abstract
C/C-ZrC-SiC composites were prepared by thermal gradient chemical vapor infiltration (TCVI) and precursor infiltration and pyrolysis (PIP) process. The microstructures and phase compositions of C/C-ZrC-SiC composites after oxidation were analyzed by scanning electron microscopy and X-ray diffraction, respectively. Isothermal oxidation behavior at 1500 ℃, dynamic oxidation behavior from room temperature to 1400 ℃ and long-term ablation resistance of the composites were investigated. The results show that dynamic oxidation behavior from room temperature to 1 400 ℃ can be divided into four stages: mass gain, slow mass loss, severe mass loss and constant. While the isothermal oxidation behavior of C/C-ZrC-SiC at 1500 ℃ can be divided into five stages: mass gain, slow mass loss, constant, severe mass loss and constant. ZrC and SiC trend to be oxidized preferentially and generate ZrO2and SiO2, which wrap and protect C/C matrix and fibers partly. After ablated for 1200 s by oxyacetylene flame, the linear and mass ablation rates of composites are 9.27×10-4 mm·s-1 and 6.67×10-4 g·s-1, respectively. ZrO2 and SiO2 are formed by the oxidation of ZrC and SiC, respectively. ZrO2 can alleviate the thermal-physical and thermal-chemical erosion caused by the oxyacetylene torch, and dense SiO2 glassy film can seal the defects such as cracks and holes, leading to a good ablation resistance of C/C-ZrC-SiC composites.
| Original language | English |
|---|---|
| Pages (from-to) | 425-431 |
| Number of pages | 7 |
| Journal | Materials China |
| Volume | 34 |
| Issue number | 6 |
| DOIs | |
| State | Published - 1 Jun 2015 |
Keywords
- Ablation resistance
- C/C-ZrC-SiC composites
- Oxidation
- Thermogravimetric analysis
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