期刊文献+

Effect of dilution holes on the performance of a triple swirler combustor 被引量:13

Effect of dilution holes on the performance of a triple swirler combustor
原文传递
导出
摘要 A triple swirler combustor is considered to be a promising solution for future high temperature rise combustors. The present paper aims to study dilution holes including primary dilution holes and secondary dilution holes on the performance of a triple swirler combustor. Experimental investigations are conducted at different inlet airflow velocities(40–70 m/s) and combustor overall fuel–air ratio with fixed inlet airflow temperature(473 K) and atmospheric pressure. The experimental results show that the ignition is very difficult with specific performance of high ignition fuel–air ratio when the primary dilution holes are located 0.6H(where H is the liner dome height)downstream the dome, while the other four cases have almost the same ignition performance. The position of primary dilution holes has an effect on lean blowout stability and has a large influence on combustion efficiency. The combustion efficiency is the highest when the primary dilution holes are placed 0.9H downstream the dome among the five different locations.For the secondary dilution holes, the pattern factor of Design A is better than that of Design B. A triple swirler combustor is considered to be a promising solution for future high temperature rise combustors. The present paper aims to study dilution holes including primary dilution holes and secondary dilution holes on the performance of a triple swirler combustor. Experimental investigations are conducted at different inlet airflow velocities(40–70 m/s) and combustor overall fuel–air ratio with fixed inlet airflow temperature(473 K) and atmospheric pressure. The experimental results show that the ignition is very difficult with specific performance of high ignition fuel–air ratio when the primary dilution holes are located 0.6H(where H is the liner dome height)downstream the dome, while the other four cases have almost the same ignition performance. The position of primary dilution holes has an effect on lean blowout stability and has a large influence on combustion efficiency. The combustion efficiency is the highest when the primary dilution holes are placed 0.9H downstream the dome among the five different locations.For the secondary dilution holes, the pattern factor of Design A is better than that of Design B.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2014年第6期1421-1429,共9页 中国航空学报(英文版)
基金 supported by Funding for Outstanding Doctoral Dissertation in NUAA (No. BCXJ 14-01) Funding of Jiangsu Innovation Program for Graduate Education (No. CXLX12_0169)
关键词 Combustor performance Fuel–air ratio Primary dilution holes Secondary dilution holes Triple swirler combustor Combustor performance Fuel–air ratio Primary dilution holes Secondary dilution holes Triple swirler combustor
  • 相关文献

参考文献3

二级参考文献13

  • 1Sikorski R L. An Overview of Some Combustion System Development Programs[R]. AIAA Paper 98-3267.
  • 2Bahr D W. Technology for the Design of High Temperature Rise Combustor[R]. AIAA Paper 85-12925.
  • 3Baxter M R,Lefebvre A H. Weak Extinction Limits of Large Scale Flameholders[J]. Journal of Engineering for Power, 114(4) :776-782,1992.
  • 4Lefebvre A H. Gas Turbine Combustion, Second Edition[M]. Taylor and Franeis, USA, 1999.
  • 5李概奇,严传俊.小发直流燃烧室扩压器和火焰筒匹配的数值模拟[J].航空动力学报,1997,12(3):299-302. 被引量:2
  • 6Rizk N K,Mongia H C. Performance of Hybrid Airblast Atomizers Under Low Power Condition [R]. AIAA- 920463,1992.
  • 7Adel Mansour,et al. A New Hybrid Air Blast Nozzle For Advanced Gas Turbine Combustion[R]. ASME Paper 2000-GT- 113,2000.
  • 8liao Y,et al. On The Mechanism of Pressure-swirl Airblast Atomization[R]. AIAA- 2001 - 3571,2001.
  • 9Lefebvre A H. Gas Turbine Combustion[M]. Taylor & Francis Press, 1999.
  • 10Jasuja A K. Atomization of Crude and Residual Fuel Oils[J].Journal of Engineering for Power, 1979,101 ( 2 ): 250 - 258.

共引文献44

同被引文献85

引证文献13

二级引证文献47

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