推进技术 ›› 2000, Vol. 21 ›› Issue (5): 61-65.

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模型燃烧室冷态喷雾场的实验研究

邢小军,徐行,郭志辉,李继保,徐华胜   

  1. 北京航空航天大学热动力研究所!北京100083;北京航空航天大学热动力研究所!北京100083;北京航空航天大学热动力研究所!北京100083;中国航空燃气涡轮研究院!四川成都610500;中国航空燃气涡轮研究院!四川成都610500
  • 发布日期:2021-08-15
  • 基金资助:
    国家重点实验室基金资助项目

Experimental study on spray field in combustor by phase dopplor analyzer

  1. Inst of Thermo power Engineering,Beijing Univ.of Aeronautics and Astronautics,Beijing 100083,China;Inst of Thermo power Engineering,Beijing Univ.of Aeronautics and Astronautics,Beijing 100083,China;Inst of Thermo power Engineering,Beijing Univ.of Aeronautics and Astronautics,Beijing 100083,China;China Aero Gas Turbine Establishment,Chengdu 610500,China;China Aero Gas Turbine Establishment,Chengdu 610500,China
  • Published:2021-08-15

摘要: 使用相位多普勒分析仪PDA (PhaseDopplorAnalyzer)对模型燃烧室内的喷雾场进行了实验研究 ,测量了喷雾场不同工况下的喷雾特性 ,分析了喷雾压力和旋流器对喷雾场的影响 .证明喷嘴压力提高可以增大喷雾场中粒子速度、通量及降低平均直径 ;空气流则可以改变喷雾分布型 ,形成回流区并扩大喷雾场范围。

关键词: 航空发动机;燃烧室;喷雾;燃油雾化

Abstract: PDA (Phase Dopplor Analyzer ) was employed to study the structure of spray in model combustor The measured parameters include the three dimensional velocity, mean diameter and flux of liquid particles The relation between spray parameters and operating conditions (the airflow mass and liquid pressure) was studied It is proved that water pressure can accelerate the droplets and reduce the Sauter mean diameter(SMD) The air flow can enlarge and change the shape of the spray

Key words: Aircraft engine;Combustron chember;Spraging;Fule pulverization