期刊文献+

一种离心喷嘴多孔蒸发管的蒸发率实验 被引量:2

Experimental study of evaporation rate for multihole vaporizer with pressure swirl atomizer
原文传递
导出
摘要 发展了一种用于微小型燃气轮机燃烧室的多孔蒸发管,燃油通过离心喷嘴供入蒸发管上游,空气经喷嘴下游的多个离散小孔进入蒸发管,燃油在蒸发管内与空气混合并蒸发.测试了离心喷嘴的喷雾特性,并主要对该多孔蒸发管的燃油蒸发率进行了实验.结果表明:对于这种多孔蒸发管,影响蒸发率的主要因素是进气温度和离心喷嘴的喷雾特性,当进气温度超过480K,煤油接近完全蒸发,雾化颗粒度越小,相对流速越大,蒸发完全程度越高. A design multihole vaporizer was developed for micro gas turbine combu stor.Pressure swirl atomizer was used to atomize kerosene first and was fitted a t entrance of multihole vaporizer.A lap of holes were distributed around multiho le vaporizer wall of nozzle downstream,which were used to mix and vaporize keros ene.Spray characteristics of pressure swirl atomizer was measured,and vaporizati on rate of the multihole vaporizer was studied experimentally.The experimental r esults show that the air temperature and spray characteristics of pressure swirl atomizer are major influence factor to vaporization rate for multihole vaporize r.Kerosene is completely vaporized when the vaporizer inlet temperature exceeds 480 K.The smaller the kerosene particle size,the greater relative velocity,the h igher the level of evaporation achieved.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2011年第2期337-342,共6页 Journal of Aerospace Power
关键词 蒸发管 多孔 离心喷嘴 蒸发率 燃烧室 vaporizer multihole pressure swirl atomizer vaporization rate
  • 相关文献

参考文献11

  • 1Lefebvre A H. Gas turbine combustion[M]. Philadelphia, USA:Taylor & Francis, 1999.
  • 2Dobbeling K, Hellat J, Koch H. 25 years of bbc/abb/als tom lean premix combustion technologies[R]. ASME Paper 2005-GT-68269,2005.
  • 3Colibaba Evulet A, Bowman M J, Brand A R. Design and evaluation of the aims combustor[R]. ASME Paper 2004- GT-53150,2004.
  • 4Nakamura S, McDonell V, Samuelsen S. The effect of liquid-fuel preparation on gas turbine emissions[R]. ASME Paper 2006 GT 90730,2006.
  • 5Lee J C Y,Mahe P C,Benjarain M A. Low nox combustion for liquid fuels:atmospheric pressure experiments using a staged prevaporizer-premixer[R]. ASME Paper 2001-GT 0081,2001.
  • 6林宇震,彭云晖,刘高恩.分级/预混合预蒸发贫油燃烧低污染方案NO_X排放初步研究[J].航空动力学报,2003,18(4):492-497. 被引量:20
  • 7LIN Yuzhen, PENG Yunhui, LIU Gaoen. Investigation on nox of a low emission comhustor design with multihole premixer-prevaporizer[R]. ASME Paper 2004-GT-53203, 2004.
  • 8Gokulakrishnan P, Gaines G, Klassen M S, et al. Autoignition of aviation fuels: experimental and modeling study [R]. AIAA 2007 5701. 2007.
  • 9Suzuki T K, Oppata Y. A study of a fuel vaporizer for a gas turbine engine[R]. Tokyo, Japan ; Tokyo Joint International Gas Turbine Conference and Product Show, 1971: 135- 142.
  • 10朱菁,郭新华,林宇震,徐国强.微小“T”型蒸发管蒸发率实验[J].航空动力学报,2007,22(8):1273-1278. 被引量:4

二级参考文献25

  • 1刘高恩 林宇震.航空燃气轮机燃烧发展趋势及某些初步考虑[A]..中国航空学会21世纪航空动力发展研讨会[c].北京,2000..
  • 2Akira Imamura, Masanori Yoshida, Manabu Kawano, et al.Research and Development of a LPP Combustor with Swirling Flow for Low NOx[R]. AIAA 2001--3311,2001.
  • 3Yasuhiro Kinoshita, Takeo Oda, Juniehi Kttajima. Research on a Methane-Fueled Low NOx Combustor for a Mach 3 Supersonic Transporter Turbojet Engine[R]. ASME Paper 2000--GT-- 113,2000.
  • 4Takashi IKEZAKI, Jun HOSOI, Hidemi TOH, et al. The Performance of the Low NOX Aero Gas Trubine Combustor Under High Pressure [R]. ASME Paper 2001- GT-0084,2001.
  • 5Sturgess G J. Advanced Low Emissions Catalytic Combustor Program at Pratt & Whitney[R]. NASA CP 2078,1978.
  • 6Lefebvre A H. Gas Turbine Combustion [M]. Taylor & Francis Press, 1999.
  • 7Chin J S, Lefebvre A H. Steady-State Evaporation Characteristics of Hydrocarbon Fuel Drops[R]. AIAA Paper 82--1176,1982.
  • 8Chin J S,Durrett R,Lefebvre A. H. The Interdependence of Spray Characteristics and Evaporation History of Fuel Sprays[R]. ASME Paper 83-GT-7,1983.
  • 9Rink K K, Lefebvre A H. The Influence of Fuel Composition and Spray Characteristics on Nitric Oxide Formation [J].Combustion Science and Technology, 1989,68 : 1 -- 14.
  • 10Gleason C C, Oller M W, Bahr D W. Evaluation of Fuel Character Effects on F101 Engine Combustion System[R].AFAPL--TR-- 79-- 2018,1979.

共引文献34

同被引文献32

引证文献2

二级引证文献3

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