摘要
Thermal fatigue test was conducted to study the failure process and failure mode of the plasma sprayed thermal barrier coating structures. The controlling factors for failure were also analyzed. A viscoplastic constitutive model was introduced for the ceramic coat. Moreover, the thermal fatigue behavior of the coating layer was studied numerically. The analysis indicates that: Mode I crack is easily initiated at the peak position, and mode II crack at above middle position of interfaces when TGO (thermally growth oxides) thickness is 2μm; the extension of transverse crack is dominated by normal stress when TGO thickness is 8μm; high strain energy density is formed within TGO of different thickness. The process and mechanisms of crack coalescence within PS-TBC (plasma sprayed thermal grown oxides) were presented.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 270-275 |
| 页数 | 6 |
| 期刊 | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| 卷 | 23 |
| 期 | 2 |
| 出版状态 | 已出版 - 2月 2008 |
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