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涡轮叶片气膜孔超快激光加工超声速吹气流场机理研究 *

  • Zhiyuan Cao
  • , Qinpeng Gu
  • , Peng Li
  • , Xi Gao
  • , Bo Liu
  • Northwestern Polytechnical University Xian
  • Xi’an Micromach Technology Co.,Ltd.

科研成果: 期刊稿件 › 文章 › 同行评审

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

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