微型涡喷发动机喷油环优化设计
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  • 英文篇名:Optimum Design of Injection Ring for Micro-turbojet Engine
  • 作者:谭锟 ; 王云 ; 张飞 ; 张洋洋 ; 李俊杰
  • 英文作者:Tan Kun;Wang Yun;Zhang Fei;Zhang Yangyang;Li Junjie;School of Aircraft Engineering,Nanchang Hangkong University;
  • 关键词:航空 ; 微型涡喷发动机 ; 喷油环 ; 燃油流量 ; 数值模拟
  • 英文关键词:aerospace;;micro-turbojet engine;;nozzle-loop;;fuel flow;;numerical simulation
  • 中文刊名:HKGC
  • 英文刊名:Advances in Aeronautical Science and Engineering
  • 机构:南昌航空大学飞行器工程学院;
  • 出版日期:2018-08-28
  • 出版单位:航空工程进展
  • 年:2018
  • 期:v.9;No.35
  • 基金:国家自然科学基金(51266012)
  • 语种:中文;
  • 页:HKGC201803014
  • 页数:6
  • CN:03
  • ISSN:61-1479/V
  • 分类号:90-95
摘要
喷油环是微型涡喷发动机的重要组成部分,其喷油量的均匀性决定了燃烧室温度场的均匀性。针对微型涡喷发动机喷油环喷油量不均匀问题,采用不等径喷油针结构方案来补偿压力损失影响;运用CFX软件数值模拟实验时喷油环内部的三维流场,并计算喷油环环体上各喷油针的出口流量值、出口速度以及喷油环整个内部流场的压力变化情况,最后与实验结果对比。结果表明:不等径喷油针结构方案可以较好的改善喷油环喷油量不均匀问题,可为研究喷油环内部流场奠定基础。
        The fuel injection ring is an important part of the micro-turbojet engine.The uniformity of fuel injection quantity determines the uniformity of the temperature field in the combustion chamber.Aiming at microturbojet injection ring uneven fuel injection problems,the influence of pressure loss is compensated through the use of unequal-diameter needle structure.By using CFX software,the experiment of three-dimensional flow field inside the fuel injection ring is simulated and the outlet flow rate,outlet velocity and the pressure change of the entire internal flow field of injection needle on the injection ring body are calculated and compared with the experimental results.Results show that the scheme of unequal injection nozzle can improve the problem of nonuniform injection of fuel injection ring.According to the calculated results,we can lay the foundation for the study of the internal flow field of the injection ring.
引文
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