期刊文献+

燃油周向分级对贫油熄火油气比的影响 被引量:9

The Effect of Fuel-Circumferential-Staging on Lean Blowout Limit at Idle Condition
下载PDF
导出
摘要 为降低贫油熄火油气比,对双头部燃烧室进行了燃油周向分级贫油熄火模拟实验研究。实验考虑了进气速度、进气温度对贫油熄火油气比的影响。采用了三种不同长度的隔板来研究减少两个头部之间相互影响。试验结果表明:与不分级燃烧相比,燃油周向分级燃烧能够显著降低贫油熄火油气比。当燃烧室进气温度低于400K,贫油熄火油气比随燃烧室进气空气流速的上升而明显下降,当进气温度大于400K,贫油熄火油气比对燃烧室进气温度和速度不敏感;采取加在头部之间插入隔板的措施来降低燃烧室贫油熄火比,效果并不显著。 The experimental investigation was conducted for the fuelcircumferentialstaging combustor with two domes to improve the lean blowout fuel air ratio.The effects of inlet temperature and inlet velocity were taken into account.Three pieces of clapboard with different length were placed between two domes to eliminate their mutual effects.Results showed that the combustor with fuelcircumferentialstaging could obviously improve fuel air ratio at lean blowout.When the inlet temperature was lower than 400 K,fuel air ratio at lean blowout would decrease obviously with the rising of inlet velocity.When the inlet temperature was higher than 400 K,it wouldn't be sensitive to the inlet temperature and inlet velocity.However,the method was not so good in respect of reducing fuel air ratio at lean blowout by inserting clapboard into two domes.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2003年第5期639-644,共6页 Journal of Aerospace Power
关键词 贫油熄火 油气比 燃烧室 航空发动机 影响 燃油周向分级 aerospace propulsion system combustor aircraft engine fuel-circumferential-staging lean blowout
  • 相关文献

参考文献4

  • 1Sikorski R L. An Overview of Some Combustion System Development Programs[R]. AIAA Paper 98-3267.
  • 2Lefebvre A H. Gas Turbine Combustion, Second Edition[M ].Taylor & Francis, 19 9 9.
  • 3Mellor A M. Design of Modern Turbine Combustor[M]. Academic Press, 19 9 0.
  • 4Bahr D W. Technology for the Design of High Temperature Rise Combustor[R]. AIAA Paper 85-12925.

同被引文献108

引证文献9

二级引证文献65

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部