摘要
Due to high precision and non-contact advantages,ultrafast laser drilling is widely applied in precision hole machining. During drilling process,assist gas is used to enhance machining quality and efficiency. Regarding the blowing flow field during ultrafast laser processing of film cooling holes in turbine blades,the im⁃ pacts of parameters such as gas assisted methods,inlet pressure,and modified nozzles on the shock wave struc⁃ ture were investigated. The results indicate that:both coaxial and paraxial gas assistance have normal shock wave,coaxial also has shock diamonds,paraxial flow yields higher hole velocity,benefiting machining. Increas⁃ ing inlet pressure strengthens shock wave,expands affected area,and raises peak Mach number. Larger nozzle diameters extend shock wave expansion,lower normal shock and diamond positions,and shrink the second nor⁃ mal shock and diamond scopes. When the nozzle is modified into an elliptical shape,the shock wave structure no longer distributes symmetrically. As the aspect ratio of the ellipse increases,the shock wave affected area ex⁃ pands,Ma=1.95 equivalent surface shift from inverted bell to conical,and shock diamonds vanish. Modified noz⁃ zles introduce swirling flow to weaken shocks,improving fluid mixing and hole velocity. The swirl nozzle with four vortex generators ejects metal residues better,enhancing drilling quality and efficiency. In comparison,varia⁃ tions in inlet pressure and nozzle diameter mainly influence the shock wave intensity and range,while the nozzle shape exerts the most prominent impact on the shock wave shape and structure.
| 投稿的翻译标题 | Mechanism of supersonic blowing flow field in ultra-fast laser drilling film cooling hole in turbine blade |
|---|---|
| 源语言 | 繁体中文 |
| 期刊论文编号 | 202503032 |
| 期刊 | Tuijin Jishu/Journal of Propulsion Technology |
| 卷 | 47 |
| 期 | 1 |
| DOI | |
| 出版状态 | 已出版 - 10 1月 2026 |
关键词
- Assisted blowing
- Film cooling hole
- Shock wave structure
- Supersonic
- Turbine blade
- Ultra-fast laser drilling
学术指纹
探究 '涡轮叶片气膜孔超快激光加工超声速吹气流场机理研究 *' 的科研主题。它们共同构成独一无二的学术指纹。引用此
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