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重型燃气轮机先进低NO_x燃烧技术分析 被引量:19

Advanced Low NO_x Combustion Technologies for Heavy-Duty Gas Turbine
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摘要 对重型燃气轮机领域中的低NO x燃烧技术进行介绍与说明,首先简要论述了重型燃气轮机燃烧室中氮氧化物的产生机理及抑制方法,其次,介绍了贫预混多喷嘴分级燃烧技术、富油/焠熄/贫油燃烧技术和贫预混低旋流燃烧技术等7种可用于重型燃气轮机燃烧室的先进低NO x燃烧技术,并详细论述了这7种低NO x燃烧技术的作用原理及应用进展,可为国内重型燃气轮机低污染燃烧室的设计与研制提供技术参考。 Low NOx combustion technologies used in modern heavy-duty gas tt, rbine are introduced. Firstly, the formation mechanisms of NO emissions in heavy-duty gas turbine are summarized, and the methods of NOx suppression are put forward. Secondly, the key features,combustion concepts and applications of seven advanced low NOx combustion technologies for heavy-duty gas turbine are presented in detail. The seven low NOx combustion technolngies include Lean premixed muti-nozzle co,nbnstion, Rich burn, Quick-lean combustion, Low swirl lean premixed combustion, Humid fuel/air combustion, Exhaust gas recirculation combustion, Catalytic combustion and Sequential combustion. The valuable reference for the design and development of low emission combustor of domestic heavy-duty gas turbine is provided.
出处 《热力透平》 2013年第4期251-259,共9页 Thermal Turbine
基金 自然科学基金(51206109)
关键词 低NOX燃烧 燃烧室 重型燃气轮机 low NOx combustion combustor heavy-duty gas turbine
作者简介 葛冰(1977-),男,汉族,江苏沭阳县人,毕业于上海交通大学.讲师,研究方向为:燃气轮机燃烧室低污染燃烧技术。
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参考文献22

  • 1赵坚行.民用发动机污染排放及低污染燃烧技术发展趋势[J].航空动力学报,2008,23(6):986-996. 被引量:90
  • 2FEITELBERG AS,LACEY M A.The GE Rich-Quench-Lean Gas Turbine Combustor[J].J.Eng.Gas Turbines Power,1998,120(3):502-508.
  • 3姚强,李水情,王宇.燃烧学导论:概念与应用[M].2版.北京:清华大学出版社,2009.
  • 4STRAUB DOUGLASL.,CASLETON Kent H,LEWISROBIE E,et al.Assessment of RQL Trapped Vortex Combustor for Stationary Gas Turbines[C]//Proceedings of ASME Turbo Expo 2003.Atlanta Georgia,USA:American Society of Mechanical Engineers,2003:GT2003-38569.
  • 5STEELE Robert Charles.The Gas Turbine Handbook[M].USA:Department of Energy,Office of Fossil Energy,National Energy Technology Laboratory,2006:237.
  • 6CARRERA Arturo Manrique,ANDERSSON Mats,N(A)SVALL Henrik.Experimental Investigation of the 4th Generation Dle Burner Concept:Emissions and Fuel Flexibility Performance at Atmospheric Conditions[C]// Proceedings of ASME Turbo Expo 2011.Vancouver,Canada:American Society of Mechanical Engineers,2011:GT2011-46387.
  • 7YEGIAN D T,CHENG R K.Development of a Lean Premixed Low Swirl Burner for Low NOxPractical Applications[J].Combustion Science and Technology,1998,139 (16):207-227.
  • 8LITTLE JOHN D,CHENG R K.Fuel Effects on a Low-Swirl Iujector For Lean Premixed Gas Turbines[C]// Proceedings of the Combustion Institute.[S.l.]:Proceedings of the Combustion Institute,2007:3155-3162.
  • 9CHENG RK,Littlejohn D,STRAKEY P and SIDWELL T.Laboratory Investigations of Low-Swirl Injectors with H2 and CH4 at Gas Turbine Conditions[J].Proc.Comb.Inst.,2009,32(1):3001-3009.
  • 10BHARGAVA A,COLKET M,SOWA W,et al.A Experiment and Modeling Study of Humid Air Premixed Flame[J].J.Eng.Gas Turbine Pwr.,2000,122(3):405-411.

二级参考文献15

  • 1Bahr W W, Gleason C C. Experiment clean combustor program, Phase I: Final reportERS. NACA-CR-134737, 1975.
  • 2Lew L H, Carl D R, Dezubay E A. Low NOx heavy fuel combustor concept program Phase I: Combustion technology generation[R]. NASA-CR-165482, 1981.
  • 3Mongia H C. TAPS-A4^th generation propulsion comhustor technology for low emissions [R]. AIAA 2003-2657, 2003.
  • 4Marek C J, Smith T D. Low emission hydrogen combustots for gas turbines using lean direct injection[R]. AIAA 2005 3776,2005.
  • 5Walker A D, Denman P A, McGuirk J J. Experimental and computational study of hybrid diffusers for gas turbine combustors[J]. ASME J. of Engineering Gas Tur hines and Power,2004, 126:717 725.
  • 6Rizk N K, Chin J S. Modeling of NOx formation in diffusion flame combustors[R]. AIAA 2002 3713, 2002.
  • 7Smith L L, Karim H, Castaldi M J. Rich-catalytic leanburn combustion for low-singht-digit NOx gas turbines[J]. ASME J. of Engineering for Gas Turbines and Pow er, 2005, 127: 27.
  • 8Rizk N K, Mongia H C. Three dimensional emission modeling for diffusion flame, rich/lean and lean gas turbine combustors[R]. AIAA 93-2338,1993.
  • 9Imamura A ,Yoshida M. Research and development of a LPP combustor with swirling flow for low NOx [R]. AIAA 2001 3311, 2001.
  • 10Douglas L, Straub K H. Assessment of rich burn, quick mix, lean-burn trapped vortex combustor for stationary gas turbines[J]. ASME J. of Engineering for GasTurhines and Power, 2005, 127: 36-41.

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