期刊文献+

基于二次燃料喷射的预混燃烧室热声振荡主动控制方法

Active control of thermoacoustic oscillations in premixed combustor based on secondary fuel injection
下载PDF
导出
摘要 为了实现热声振荡的主动控制,基于燃气轮机模型燃烧室,实验研究了二次燃料喷射对热声振荡的影响。采用高频压力传感器和光电倍增管同步测量了燃烧室内压力振荡和CH*表征的释热脉动,采用高速相机捕捉了火焰结构,通过对实验数据的分析获得了热声振荡的产生机理和二次燃料喷射解耦热声耦合的作用机制。结果表明:涡流效应会引起火焰的周期性卷曲,导致火焰面积的变化,引发释热率的脉动,激发并维持热声振荡。二次燃料喷射可以显著降低热声振荡水平,当二次燃料占比5.0%时,声压幅值和均方根压力幅值分别降低了32%和35%;当二次燃料占比10%时,声压幅值和均方根压力幅值降低到噪声水平。二次燃料喷射可以改变火焰形态,随着二次燃料占比的增加,火焰抬升高度和火焰宽度相应增加,释热区域向燃烧室下游延展,火焰的非定常特性减弱。二次燃料喷射可以打破燃烧室压力和释热率之间的相位耦合,实现对热声振荡的主动控制。 To achieve active control of thermoacoustic oscillations,the effects of secondary fuel injection on thermoacoustic oscillations were experimentally investigated based on a gas turbine model combustor.Highfrequency pressure transducers and photomultiplier tubes were used to synchronously measure the pressure oscil⁃lations and heat release rate(HRR)disturbances characterised by CH*.High-speed camera was used to capture the flame structure.The mechanisms of the thermoacoustic oscillations and secondary fuel injection decoupling thermoacoustic process were obtained through theanalysis of the experimental data.The results show that the vor⁃tex effect causes the periodic flame roll-up,which leads to the change of the flame area and makes HRR distur⁃bances,and further induces and maintains the thermoacoustic oscillations.The level of thermoacoustic oscilla⁃tions can be significantly weakened by the secondary fuel injection.The peaks of sound pressure level and root mean square pressure are reduced by 32%and 35%,respectively,at 5.0%proportion of secondary fuel,and drop to noise levels at 10%proportion of secondary fuel.The flame structure can be changed by the secondary fu⁃el injection.As the proportion of secondary fuel increases,the lift height and width of the flame increase accord⁃ingly.The heat release area extends downstream of the combustor,and the unsteady characteristics of the flame are weakened.The secondary fuel injection can break the phase coupling between pressure and HRR in the com⁃bustor,and achieve the active control of thermoacoustic oscillations.
作者 曹炜 杨凯淇 任永杰 郭康康 仝毅恒 黄卫东 聂万胜 CAO Wei;YANG Kaiqi;REN Yongjie;GUO Kangkang;TONG Yiheng;HUANG Weidong;NIE Wansheng(Department of Aerospace Science and Technology,Space Engineering University,Beijing 101416,China)
出处 《推进技术》 EI CAS CSCD 北大核心 2024年第12期194-204,共11页 Journal of Propulsion Technology
基金 国家自然科学基金(12002386)。
关键词 热声振荡 二次燃料喷射 主动控制 预混燃烧 旋流火焰 Thermoacoustic oscillations Secondary fuel injection Active control Premixed combus⁃tion Swirling flame
  • 相关文献

参考文献3

二级参考文献27

  • 1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):2637-2642. 被引量:18
  • 2李卓毅,张会强.甲烷一维层流预混火焰的详细和单步反应机理模拟[J].清华大学学报(自然科学版),2005,45(11):1510-1512. 被引量:3
  • 3李祥晟,丰镇平.贫油预混燃烧室燃烧稳定性的数值研究[J].西安交通大学学报,2006,40(5):502-505. 被引量:12
  • 4焦树建.燃气轮机燃烧室[M].北京:机械工业出版社,1988.
  • 5Yang V,Anderson W E.液体火箭发动机燃烧稳定性CFD分析.张宝炯,洪鑫,陈杰,译.北京:科学出版社,2001.121-293
  • 6Lieuwen T,Torres H,Zinn B T,et al.A Mechanism for Combustion Instabilities in Premixed Gas Turbine Engines.Journal of Engineering for Gas Turbines and Power,2001,123(1):182-189
  • 7Ju H C,Lieuwen T.Laminar Premixed Flame Response to Equivalence Ratio Oscillations.Combustion and Flame,2005,140(1):116-129
  • 8Brookes S J,Cant R S,Dowling A P.Modeling Combustion Instabilities Using Computational Fluid Dynamics.In:ASME Turbo Expo.Indianapolls Indiana,1999
  • 9Chae H S,Han C C.Numerical Analysis of Combustion Instability and its Suppression in Gas Turbine Combustor with Swirlers Modeled on EV Premix Burners.In:ASME Turbo Expo.Nevada USA,2005
  • 10Westbrook C K,Driyer F L.Simplified Reaction Mechanisms for the Oxidation of Hydrocarbon Fuels in Flames.Combustion Science and Technology,1981,27(1-2):31-43

共引文献20

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