期刊文献+

基于凹腔驻涡的无焰燃烧室数值模拟 被引量:5

Numerical Simulation of Flameless Combustor Based on Trapped-Vortex
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摘要 无焰燃烧的关键在于高温烟气与新鲜空气燃料的充分掺混。本文设计了一种基于凹腔驻涡的无焰燃烧室,并对其进行了零维和三维数值计算。零维数值计算运用简单的化学反应网络模型预测了燃烧室NO_x排放,凹腔当量比为0.5时,NO_x排放低于5 mg/m^3(@15%O_2)。凹腔产生的高温烟气,可以使燃烧室后部温度分布均匀,消除了温度峰值,燃烧室实现了无焰燃烧。双凹腔结构有利于改善燃烧室出口温度分布。 Flameless combustion can be obtained by mixing a large amount of high-temperature burnt gas with fresh air and fuel. This paper designed a flameless model combustor based on trapped-vortex, and zero-dimensional and three-dimensional numerical simulation of the model was taken. Chemical Reactor Network(CNR) method was used in zero-dimension calculation to predict NOx emission of the combustor. When cavity equivalence ratio is 0.5, NOx emission is lower than 5 rag/m3(@15% 02). The temperature distribution becomes uniformity because of the high-temperature burnt gas, and temperature peak was eliminated, so the combustor had possibility to reach flameless combustion. The temperature profile of the outlet is perfect with doublecavity.
出处 《工程热物理学报》 EI CAS CSCD 北大核心 2012年第9期1615-1618,共4页 Journal of Engineering Thermophysics
基金 国家自然科学基金资助项目(No.50706054)
关键词 无焰燃烧 数值模拟 双凹腔结构 flameless combustion numerical simulation double-cavity structure
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参考文献6

  • 1Wunning J A, Wunning J G. Flameless Oxidation to Re- duce Thermal NO-Formation [J]. Prog Energy Combust Sci, 1997, 23:81-94.
  • 2Erwann Guillou, Michael Cornwell, Ephraim Gutmark. Application of "Flameless" Combustion for Gas Turbine Engines [R]. AIAA 2009-225, 2009.
  • 3Nicholas Overman, Michael Cornwell, Ephrain J Gut- mark. Application of Flameless Combustion in Gas Tur- bine Engines JR]. AIAA 2006-4920, 2006.
  • 4Li Guoqiang, Gutmark E J. Experimental Study of Flame- less Combustion in Gas Thrbine Combustors [R]. AIAA 2006-546, 2006.
  • 5杨小龙,崔玉峰,徐纲,黄伟光.燃气轮机燃烧室化学反应器网络模型研究[J].工程热物理学报,2009,30(9):1585-1588. 被引量:12
  • 6Eliseo Ranzi, Tiziano Faravelli, Roberto Grana, et al. Creck Modeling Group [DB/OL]. [2011-04-11]. http:// creckmod-eling.chem.polimi.it/kinetic.ht ml.

二级参考文献7

  • 1Igor V Novosselov, Philip C. Malte, Development and Application of an Eight-Step Global Mechanism for CFD and CRN Simulations of Lean-Premixed Combustor. ASME GT2007-27990, 2007.
  • 2Novosselov I V. Chemical Reactor Network Modeling of Combustion Systems: [Ph.D. Dissertation]. University of Washington, Seattle, WA, 2006.
  • 3Novosselov I V, Malte PC, Yuan S, et al. Chemical Reactor Network Application to Emissions Prediction for Industrial DLE Gas Turbine. ASME GT2006-90282, 2006.
  • 4Carmine Russo, Giulio Mori, Joao Parente. Micro Gas Turbine Combustor Emissions Evaluation Using The Chemical Reactor Modelling Approach. ASME GT2007- 27687, 2007.
  • 5Rutar T, Malte P C. NOx Formation in High-Pressure Jet-Stirred Reactors with Significance to Lean-Premixed Combustion Turbines. ASME Journal of Engineering for Gas Turbines and Power, 2002, 124:776-783.
  • 6Yu Lei, Yufeng Cui, Gang Xu, et al. The Effects of Fuel Dillution with Steam on Gas Turbine Combustor Performance. ASME GT2007-27681, 2007.
  • 7崔玉峰.合成气燃气轮机燃烧室数值模拟与试验研尧[博士论文].北京:中国科学院工程热物理研究所,2005.

共引文献11

同被引文献53

  • 1樊未军,易琪,严明,杨茂林.驻涡燃烧室凹腔双涡结构研究[J].中国电机工程学报,2006,26(9):66-70. 被引量:47
  • 2王爱华,蔡九菊,王连勇,田红,高广轶.高温空气燃烧技术进展与应用[J].中国冶金,2006,16(8):1-5. 被引量:9
  • 3林宇震,许全宏,刘高恩,等.燃气轮机燃烧室[M].国防工业出版社,2008:189-250.
  • 4Maier G, Wittig S. Fuel Preparation and Emission Characteristics of a Pressure Loaded LPP Combustor[ J ]. AIAA - 99 - 3774.
  • 5Miehou Y, Chauvear C, Gokalp I. Experimental Study of Loan Premixed and Prevaporised Turbulent Spray Combustion [ J ]. AIAA - 99 - 0332.
  • 6Micklow G J, Royehoudhury S, Nguyen H L, Cline M C. Emis- sion Reduction by Varying the Swirler Airflow Split in Advanced Gas Turbine Combustors [ J ]. Journal of English Gas Turbines Power,117 (4) :617 -654.
  • 7Zarzalis N, Joos F, Glaes B. NOX-Reduction by Rich-Lean Com- bustion [ J ]. AIAA - 92 - 3339.
  • 8Colantonio R O. The Applicability of Jet-Shear-Layer Mixing and Effervescent Atomization for Low-NOX Combustors[ J]. Journal of Engineering for Gas Turbines and Power, 1998,120 : 17 - 23.
  • 9Bahr D W, Gleason C C. Experimental Clean Combustor Program Phase I Final Report[ C]. NASA CR- 134732, June 1975.
  • 10Mongia H C, Held T J, Hsiao, G C. Challenges and Progress in Controling Dynamics in Gas Turbine Combustors [ J ]. Journal of Propulsion and Power,2003,19 (5) :822 - 829.

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