摘要
The arrangement of film cooling holes (FCHs) in nickel-based single crystal turbine blades directly affects the creep life of the structure. To investigate the effects of hole arrangement on the creep behavior and failure mechanism of a nickel-based single crystal superalloy, creep tests were carried out on specimens containing square and rhombus arrays of film cooling holes. The post-fracture morphology and microstructural evolution were then characterized. The results show that the inter-hole interference induced by the hole arrangement has a significant effect on the creep-fracture path. To analyze the deformation behavior around the holes under different arrangements, a crystallographic-slip-based creep-damage framework was used. The simulations indicate that the difference in fracture mode between the two arrangements is closely associated with the difference in inter-hole interference intensity and the resulting distributions of local resolved shear stress and resolved shear strain, slip-band evolution, and damage accumulation pathways. The simulation results show good agreement with the experimental observations, supporting the proposed interpretation of arrangement-dependent creep rupture behavior in film cooling hole structures.
| 源语言 | 英语 |
|---|---|
| 期刊论文编号 | 111330 |
| 期刊 | Engineering Failure Analysis |
| 卷 | 197 |
| DOI | |
| 出版状态 | 已出版 - 1 11月 2026 |
学术指纹
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