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带同轴引气激光制孔中的气动特性分析

崔子健 张庆才 谭晓茗 张靖周

南京航空航天大学学报2024,Vol.56Issue(4):658-667,10.
南京航空航天大学学报2024,Vol.56Issue(4):658-667,10.DOI:10.16356/j.1005-2615.2024.04.008

带同轴引气激光制孔中的气动特性分析

Aerodynamic Characterization in Laser Hole Making with Coaxial Air Induction

崔子健 1张庆才 1谭晓茗 1张靖周1

作者信息

  • 1. 南京航空航天大学能源与动力学院,南京 210016
  • 折叠

摘要

Abstract

For the slag-blowing effect of a conical laser processor in the cooling hole machining process of aeroengine hot parts,the flow field characteristics near the jet impinging on the aperture plate and its influencing factors are investigated.For the jet structure of coaxial high-pressure gas impinging on a flat plate with blind holes,numerical simulation methods are used to analyze the comprehensive effects of different inlet pressures pint(0.2-1.5 MPa),jet spacing H/De(3.6,5.6,7.6)and impact angle α(30°,45°,60°,90°)on the gas dynamics performance near the blind holes.The results show that when H/De is 3.6,with the increase of inlet pressure,the gas dynamics performance near the blind orifice shows a tendency of gradual improvement followed by a drastic decrease,and the better working pressure is 1 MPa;when the jet spacing H/De reaches 5.6 and above,the aerodynamic level of the gas flow near the blind orifice can be improved by appropriately increasing the nozzle pressure,but the enhancement is limited.As the impact angle α decreases,the outflow mass flow rate in the blind hole gradually increases,and when α is 30°,it is about 11 times higher than that of the vertical jet,but the shear flow of the gas on the impact surface becomes weaker as the impact angle decreases.

关键词

航空发动机/激光制孔/同轴引气/冲击射流/计算流体动力学

Key words

aeroengine/laser hole making/coaxial air induction/shock jet/computational fluid dynamics

分类

矿业与冶金

引用本文复制引用

崔子健,张庆才,谭晓茗,张靖周..带同轴引气激光制孔中的气动特性分析[J].南京航空航天大学学报,2024,56(4):658-667,10.

南京航空航天大学学报

OA北大核心CSTPCD

1005-2615

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