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民用发动机污染排放及低污染燃烧技术发展趋势 被引量:84

Pollutant emission and development of low-emission combustion technology for civil aero engine
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摘要 针对民用发动机污染排放的现状,介绍了低污染燃烧技术发展概况及趋势,国际民航组织(ICAO)颁布的《航空发动机的排放》标准,以及中国民用航空局(CAAC)对排气污染物的规定,分析了排气污染物的生成机理和主要影响因素以及改善措施.对6种先进低污染燃烧室(分级、变几何、催化、贫油预混预蒸发燃烧室(LPP)、富油燃烧/淬熄/贫油燃烧技术(RQL)以及双环预混旋流(TAPS)等燃烧室)的工作原理与特点、以及应用状况作了简要分析.其中分级燃烧技术构成了先进低污染燃烧室设计的技术基础,而LPP,RQL与TAPS燃烧室为三种很有发展前途的低污染燃烧室.此外,还介绍了贫油直接喷射、燃料电池以及主动燃烧控制等三种新型的低污染燃烧技术,虽然实现这些技术难度较大,但有广阔的应用前景. Directed against the pollutant emission status of civil aero engine, the devel-opment of low-emissions combustion technology described is done. The standards for inter-national civil aviation organization (ICAO) aircraft engine emissions and regulations of civil aviation administration of China (CAAC) exhaust emission are given. The formation mecha-nisms of exhaust emissions are summarized. Various factors influencing pollutant formation and improved approaches decreasing exhaust emission are discussed. The key features, combustion concept and application of six advanced low-emissions combustors (staged, variable geometry, and catalytic combustor, lean premixed prevaporized (LPP), rich-burn, quick- mix,lean-burn (RQL) and twin annular premixing swirler (TAPS)) are detailed. In these low-emission combustors, staged combustor is the foundational design scheme LPP, RQL and TAPS combustors have widely developed perspective. Some novel low-emission combustion concept,such as lean direct injection, fuel cell and active combustor control are recom-mended. These new low-emissions technology are very useful, however many formidable problems remain to be solved before the systems can be applied to advanced aircraft engines.
作者 赵坚行
出处 《航空动力学报》 EI CAS CSCD 北大核心 2008年第6期986-996,共11页 Journal of Aerospace Power
关键词 航空 航天推进系统 民用发动机 排气污染物 低污染燃烧 分级燃烧室 aerospace propulsion system civil aero engine pollutant low-emissions combustion staged combustor
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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.
  • 4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
  • 5Marek C J, Smith T D. Low emission hydrogen combustots for gas turbines using lean direct injection[R]. AIAA 2005 3776,2005.
  • 6张彦仲.航空环境工程与科学[J].中国工程科学,2001,3(7):1-6. 被引量:7
  • 7Walker 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.
  • 8Rizk N K, Chin J S. Modeling of NOx formation in diffusion flame combustors[R]. AIAA 2002 3713, 2002.
  • 9Smith 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.
  • 10Rizk N K, Mongia H C. Three dimensional emission modeling for diffusion flame, rich/lean and lean gas turbine combustors[R]. AIAA 93-2338,1993.

二级参考文献18

  • 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.

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