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旋流强度对氢气预混火焰CIVB回火的影响 被引量:2

Effects of Swirl Strength on CIVB Flashback in Hydrogen Premixed Flames
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摘要 为了研究旋流强度对氢气预混火焰燃烧诱导涡破碎(CIVB)回火的影响,以便深入理解氢气的CIVB回火特点进而减弱回火,首先采用二维轴对称模型,并使用用户自定义函数(UDF)修改动量守恒方程来模拟旋流,得到了不同旋流数下氢气预混火焰的CIVB回火极限,然后从旋流强度对流场特性和火焰特性两方面的影响进行深入分析。结果表明:对于无中心体旋流预混喷嘴中氢气火焰的CIVB回火,旋流数从0.409增加到0.432,从流场条件分析,旋流数增加使负切向涡量增加,对回火起促进作用;从火焰条件分析,旋流数增加使氢气湍流火焰速度先增加后减小,最后趋于猝熄,对回火先起促进作用后起抑制作用。流场和火焰条件共同决定了旋流数对氢气预混火焰CIVB回火的影响趋势,即旋流数增加先促进回火后抑制回火。 In order to deepen understanding the flashback due to combustion induced vortex breakdown(CIVB)and prevent it,the effects of swirl strength on CIVB flashback in hydrogen premixed flames were investigated. Flashback limits of hydrogen premixed flames were obtained by numerical simulation with two-dimensional axisymmetric model and implementing user defined function(UDF)to simulate swirl by modifying the momentum conservation equations. Effects of swirl strength on flow aerodynamic characteristics and flame characteristics were analyzed in detail. The results are as follows: for hydrogen flames in the swirl-premixed nozzle without a centerbody,increase of swirl number from 0.409 to 0.432 enhances flashback due to the increase of negative azimuthal vorticity from the aspect of the flow conditions. From the aspect of the flame conditions,increase in swirl strength firstly enhances flashback and then prevents it,because the turbulent flame speed of hydrogen flame firstly increases with increasing swirl strength and then decreases,finally toward quenching. Both aspects together determine the effects of swirl strength on CIVB flashback in hydrogen premixed flames. That is,flashback is firstly enhanced and then prevented with increasing swirl strength.
出处 《推进技术》 EI CAS CSCD 北大核心 2018年第4期819-826,共8页 Journal of Propulsion Technology
基金 国家自然科学基金(51406203)
关键词 燃烧诱导涡破碎回火 旋流数 氢气预混火焰 负切向涡量 湍流火焰速度 Combustion induced vortex breakdown flashback Swirl number Hydrogen premixed flames Negative azimuthal vorticity Turbulent flame speed
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  • 1Satoshi TANIMURA,Masaharu KOMIYAMA,Kenichiro TAKEISHI,Yuji IWASAKI,Kiyonobu NAKAYAMA.Visualization of flashback in a premixed burner with swirling flow[J].Science China(Technological Sciences),2010,53(1):40-45. 被引量:4
  • 2张永生,周俊虎,杨卫娟,刘茂省,岑可法.T型微细管道内氢气空气预混燃烧实验研究[J].中国电机工程学报,2005,25(21):128-131. 被引量:28
  • 3Louis J,Jurgen J,Jim B W,et al. Modeling and Measurements of a 16 - kW Turbulent Nonadiabatic Syngas Diffusion Flame in a Cooled Cylindrical Combustion Chamber [ J]. Combustion and Flame ,2001,125 ( 1-2 ).
  • 4Giacomazzi E,Piccia F E. Unsteady Simulation of a CO/ H2/N2/Air Non-Premixed Flame[ C ]. Moscow :29th Meeting on Combustion, 2005 : 1-5.
  • 5Chung S H, Williams F A. Asymptotic Structure and Extinction of CO-H2 Diffusion Flames with Reduced Kinetic Mechanisms [ J ]. Combustion and Flame, 1990,82 ( 3-4 ).
  • 6Mogia H C. Gas Turbine Combustion Design,Technology and Research:Current Status and Future Direction [ C ]. Seattle: 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 1997.
  • 7Prakash S, Lieuwen T, Zinn B T, et al. Acoustic Based Rapid Blowout Mitigation in a Swirl Stabilized Combustor [ C ]. Nevada : Proceedings of ASME Turbo. Expo. , 2005.
  • 8Poinsot T J, Trouve A C, Candel S, et al. Vortex-driving Acoustically Coupled Combustion Instabilities [ J ]. Journal of Fluid Mechanics, 1987, 177:165-292.
  • 9Ying Huang, Vigor Yang. Bifurcation of Flame Structure in a Lean-premixed Swirl-stabilized Combustor: Transition from Stable to Unstable Flame [ J ]. Combustion and Flame, 2004(136) :383-389.
  • 10Ying Huang,Vigor Yang. Effect of Swirl on Combustion Dynamics in a Lean-premixed Swirl-stabilized Combustor [ J ]. Proceedings of the Combustion Institute, 2005, (30) : 1775-1782.

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