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地面燃气轮机单管燃烧室流量分配试验

何敏 刘云鹏 颜应文

何敏, 刘云鹏, 颜应文. 地面燃气轮机单管燃烧室流量分配试验[J]. 航空动力学报, 2018, 33(4): 919-927. doi: 10.13224/j.cnki.jasp.2018.04.018
引用本文: 何敏, 刘云鹏, 颜应文. 地面燃气轮机单管燃烧室流量分配试验[J]. 航空动力学报, 2018, 33(4): 919-927. doi: 10.13224/j.cnki.jasp.2018.04.018
Experiment on mass flow distribution of ground gas turbine single tube combustor[J]. Journal of Aerospace Power, 2018, 33(4): 919-927. doi: 10.13224/j.cnki.jasp.2018.04.018
Citation: Experiment on mass flow distribution of ground gas turbine single tube combustor[J]. Journal of Aerospace Power, 2018, 33(4): 919-927. doi: 10.13224/j.cnki.jasp.2018.04.018

地面燃气轮机单管燃烧室流量分配试验

doi: 10.13224/j.cnki.jasp.2018.04.018
基金项目: 国家自然科学基金(51676097)

Experiment on mass flow distribution of ground gas turbine single tube combustor

  • 摘要: 对设计的100kW地面燃气轮机单管燃烧室空气流量分配进行了试验研究。在常压环境下采用堵孔法分别得到了旋流器、主燃孔和掺混孔的流量特性曲线,分析得到燃烧室不同结构的流量系数;试验研究了不同进口流量条件下燃烧室的流量分配,测量得到了燃烧室总压损失。研究发现:随着进口空气流量的增加,燃烧室的流量分配比例基本保持稳定,并且与燃烧室的设计空气比例基本吻合;随着燃烧室进口流量(雷诺数)的增加,旋流器、主燃孔和掺混孔的流量系数呈线性降低;随着进口流量(雷诺数)的增加,燃烧室总压损失逐渐增大;对主燃孔和掺混孔的流量特性测量中,两种测量方法得到的试验结果稍有差别,总体上看两种测量方法的试验结果较为接近。通过对比分析证明两种试验测量方法真实可靠,该研究结果可为100kW地面燃气轮机燃烧室的设计与优化提供依据。

     

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出版历程
  • 收稿日期:  2016-10-09
  • 刊出日期:  2018-04-28

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