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贫燃预混旋流火焰燃烧不稳定性的实验
引用本文:郭志辉,王帅,李磊,张澄宇,孙晓峰.贫燃预混旋流火焰燃烧不稳定性的实验[J].航空动力学报,2009,24(12):2367-2642.
作者姓名:郭志辉  王帅  李磊  张澄宇  孙晓峰
作者单位:北京航空航天大学能源与动力工程学院,航空发动机气动热力科技重点实验室,北京100191
摘    要:实验研究了常温常压条件下贫燃预混旋流火焰的燃烧不稳定性.结果表明:不稳定燃烧时,火焰结构发生显著变化,呈现大尺度运动的特点,燃烧室所发生的燃烧不稳定件是纵向自激式振荡,是燃烧室与预混段之间的耦合,振荡频率由整个系统决定,随着当量比的提高,燃烧经历了由稳定到不稳定,并达到有限循环脉动的过程,流动脉动和火焰的相互作用,是激发和维持振荡的主要原因,需要深入研究不稳定燃烧性产生和得以维持的机理.

关 键 词:燃烧不稳定性  贫油预混火焰  旋流
收稿时间:12/1/2008 4:17:20 PM
修稿时间:2009/2/26 0:00:00

Experimental study on combustion instability of lean premixed swirl flame
GUO Zhi-hui,WANG Shuai,LI Lei,ZHANG Cheng-yu and SUN Xiao-feng.Experimental study on combustion instability of lean premixed swirl flame[J].Journal of Aerospace Power,2009,24(12):2367-2642.
Authors:GUO Zhi-hui  WANG Shuai  LI Lei  ZHANG Cheng-yu and SUN Xiao-feng
Institution:Beijing University of Aeronautics and Astronautics
Abstract:An experimental study was conducted on combustion instabilities in a lean-premixed swirl-stabilized combustor at atmospheric pressure and temperature.The result shows that the combustion instability occurred in the model combustor is self-excited under longitudinal oscillation mode,the premixing section resonates with the combustor at the unstable mode of the system,and the oscillation frequency depends on the whole system.The equivalence ratio was identified to have major impact on the onset of instabilities.With equivalence ratio increase,the combustion was transited from stable to unstable states,and reached a limit cycle at last.In the occurrence of instability,the flame became much shorter and penetrated into the corner recirculation.The instability mechanism probably stems from the strong interaction between flame dynamics and flow oscillations inside the combustor,but more work is needed to provide an in-depth physical understanding of the mechanisms to initiate and sustain combustion instabilities.
Keywords:combustion instabilities  lcan premixed flame  swirl flow
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