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脉动供燃料燃烧技术及火焰频率特征 被引量:3

Oscillating Combustion and Flame Modes in Different Oscillating Frequencies
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摘要 介绍了一种天然气的新型脉动供燃料燃烧技术,该技术能有效降低NOx,提高传热效率,节约能源,且改造简易,运行经济;阐述了其技术原理,综述了其发展状况,指出对我国燃烧技术改进的重要意义.利用直接摄像技术,对一个采用该燃烧方式的射流火焰在不同流量脉动频率下的火焰类型和结构特征进行了研究.结果发现,随脉动频率变化出现了丰富的火焰类型.燃气脉动与系统共振特性相耦合影响火焰脉动特性,在系统共振和谐振频率附近,火焰根部出现崩溃混合,且火焰湍动升起,火焰长度变短.在某些频率下火焰直长,具有清晰的贫富燃交替结构. Oscillating combustion was introduced as a new combustion technology for de-NOx applied in high temperature industrial process burning natural gas. Its principle and developing status were explained and reviewed. It is of significance for the innovation of combustion technology in China. A turbulent diffusion flame exploring this technique was investigated in various conditions of different oscillating frequency through direct photographs. Many various flame modes were observed and analyzed. Fuel flow rate oscillation coupled with system vibration properties strongly influences flame oscillation characteristics. Near resonant and syntonic frequency collapsible mixing occurs in the flame foot and the flame get lift-off and shortened. Under some frequency the flame get straight and long with regular alternative fuel-rich and fuel-lean structures.
出处 《燃烧科学与技术》 EI CAS CSCD 2004年第5期459-464,共6页 Journal of Combustion Science and Technology
关键词 脉动供燃料燃烧 火焰特征 交替火焰结构 Combustion Environmental protection Natural gas Photography Thermal diffusion
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参考文献10

  • 1Charon O, Jouvaud D, Genis B. Pulsated O2/fuel flame as a new technique for low NOx emission[J]. Combust Sci and Tech, 1993, 93(1-6): 211-222.
  • 2Drogue S, Breininger S, Ruiz R. Minimization of NOx emissions with improved oxy-fuel combustion: Controlled pulsated combustion[A]. In: Proceedings of 54th Conference on Glass Problems[C]. University of Illinois at Urbana Champaign, IL, 1993.
  • 3Drogue Sophie, Breininger Shannon, Ruiz Roberto. Minimizing NOx emissions through improved oxy-fuel[J]. Glass Industry, 1994,75(6): 13-20.
  • 4Kurek Harry S, Wagner John C. Oscillating Combustion on a High Temperature Forging Furnace[R]. Project Review Meeting at California Air Resources Board. Sacramento,CA,August 30, 2001.
  • 5Eric Streicher, Ovidiu Marin, Olivier Charon. Oscillating combustion technology boosts furnace efficiency[J]. Industrial Heating, 2001, 68(2): 35-39.
  • 6Kurek Harry S. Oscillating combustion technology being evaluated as method to reduce NOx emissions[J]. Industrial Heating, 2000, 67(8): 64-67.
  • 7Kathleen Tierney. Natural gas technology reduces NOx emissions [J]. Pollution Engineering, 2000,32 (8): 10.
  • 8Office of Industrial Technologies, U.S. Department of Energy. Oscillating combustion increases efficiency and reduces NOx emissions of industrial furnaces [ EB/OL]. http://www. oit. doe. gov/combustion/factsheets/ oscillcomb. pdf,Jan. 1999.
  • 9Kim Ki Seong, Park Sang Kyu, Zhao Hailiang. Flame characteristics of a pulse jet burner[A]. In: Proceedings of the KOSME 2002 Autumn Conference[C]. Changwon: Korean Society of Marine Engineering, 2002.
  • 10Kim T K, Park J, Shin H D. Mixing mechanism near the nozzle exit in a tone excited non-premixed jet flame[J].Combust Sci and Tech, 1993, 89(1-4): 83-100.

同被引文献30

  • 1张文普,丰镇平.微型燃气轮机环型燃烧室的设计研究[J].中国电机工程学报,2005,25(5):150-153. 被引量:27
  • 2周昊,岑可法,樊建人.分离涡方法模拟浓淡气固射流两相非稳态流动特性研究[J].中国电机工程学报,2005,25(7):1-6. 被引量:21
  • 3李熙,朱华庆.瑞利-泰勒不稳定性的实验研究及数值模拟[J].科技导报,2005,23(11):30-32. 被引量:3
  • 4徐旭常,周力行.燃烧技术手册[M].北京:化学工业出版,2007.
  • 5Ryder R C, Brankovic A, Bulzan D L, et al. CFD definition study of interstage burners in turbine engine transition duct[R]. ASME 2003-GT-38440.
  • 6Chiu Ya-tien. A performance study of a super-cruise engine with isothermal combustion inside the turbine [D]. Virginia: Virginia polytechnic institute & state university, 2004.
  • 7Sirignano W A, Delplanque J P, Liu F, Sected challenges in jet and rocket engine combustion research[R]. AIAA-97-2701.
  • 8Liu F, Sirignano W A. Turbojet and turbofan engine performance increases through turbine burners[J]. Journal of Propulsion and Power, 2001,17(3) :695-705.
  • 9Sirignano W A, Liu F. Performance increases for gas turbine engines through combustion inside the turbine [J]. Journal of Propulsion and Power, 1999,15 ( 1 ) : 111-118.
  • 10Zelina J, Shouse D T, Neuroth C. High-pressure tests of a high-g, ultra compact combustor[R]. AIAA-2005-3779.

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