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多孔介质结构参数对表面火焰熄火特性的影响

张龙 许全宏 张弛 林培华 林宇震

张龙, 许全宏, 张弛, 林培华, 林宇震. 多孔介质结构参数对表面火焰熄火特性的影响[J]. 航空动力学报, 2014, (7): 1654-1659. doi: 10.13224/j.cnki.jasp.2014.07.019
引用本文: 张龙, 许全宏, 张弛, 林培华, 林宇震. 多孔介质结构参数对表面火焰熄火特性的影响[J]. 航空动力学报, 2014, (7): 1654-1659. doi: 10.13224/j.cnki.jasp.2014.07.019
ZHANG Long, XU Quan-hong, ZHANG Chi, LIN Pei-hua, LIN Yu-zhen. Effect of porous media structure parameters on surface flame blow-out performance[J]. Journal of Aerospace Power, 2014, (7): 1654-1659. doi: 10.13224/j.cnki.jasp.2014.07.019
Citation: ZHANG Long, XU Quan-hong, ZHANG Chi, LIN Pei-hua, LIN Yu-zhen. Effect of porous media structure parameters on surface flame blow-out performance[J]. Journal of Aerospace Power, 2014, (7): 1654-1659. doi: 10.13224/j.cnki.jasp.2014.07.019

多孔介质结构参数对表面火焰熄火特性的影响

doi: 10.13224/j.cnki.jasp.2014.07.019
详细信息
    作者简介:

    张龙(1989-),男,山东烟台人,硕士生,主要从事航空发动机燃烧室研究。

  • 中图分类号: V23

Effect of porous media structure parameters on surface flame blow-out performance

  • 摘要: 为优化基于多孔介质头部的微型燃烧室,以甲烷/空气预混气为燃料,针对多孔介质结构参数(当量孔径、孔隙率)在不同预混气初始温度下,对表面火焰熄火特性进行实验研究.研究表明:当量孔径为120 μm的多孔介质表面火焰两侧同时发生脱火,当量孔径为80 μm时先发生一侧脱火.随孔隙率或当量孔径的减小,熄火速度提升.当量孔径为80 μm,孔隙率为0.55,0.50,0.45的多孔介质在当量比为1.0,预混气初始温度为300K时的熄火速度分别为1.11,1.22,1.31 m/s.孔隙率为0.50,孔径为120,80 μm的多孔介质在当量比为1.0,预混气温度为300K时的熄火速度分别为0.73,1.22 m/s.预混气初始温度的升高对当量孔径为120 μm或孔隙率为0.45的多孔介质影响更加明显,预混气初始温度从300 K升至500 K时,熄火速度分别增加了120%,76%.

     

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出版历程
  • 收稿日期:  2013-04-08
  • 刊出日期:  2014-07-28

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