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双环预混旋流与单、双环腔燃烧室性能对比

李锋 程明 尚守堂 刘殿春 张珊珊 宋博

李锋, 程明, 尚守堂, 刘殿春, 张珊珊, 宋博. 双环预混旋流与单、双环腔燃烧室性能对比[J]. 航空动力学报, 2012, 27(8): 1681-1687.
引用本文: 李锋, 程明, 尚守堂, 刘殿春, 张珊珊, 宋博. 双环预混旋流与单、双环腔燃烧室性能对比[J]. 航空动力学报, 2012, 27(8): 1681-1687.
LI Feng, CHENG Ming, SHANG Shou-tang, LIU Dian-chun, ZHANG Shan-shan, SONG Bo. Capability compare of twin annular premixing swirler with the single annular and dual annular combustor[J]. Journal of Aerospace Power, 2012, 27(8): 1681-1687.
Citation: LI Feng, CHENG Ming, SHANG Shou-tang, LIU Dian-chun, ZHANG Shan-shan, SONG Bo. Capability compare of twin annular premixing swirler with the single annular and dual annular combustor[J]. Journal of Aerospace Power, 2012, 27(8): 1681-1687.

双环预混旋流与单、双环腔燃烧室性能对比

基金项目: 航空重点基金(2010ZB06)

Capability compare of twin annular premixing swirler with the single annular and dual annular combustor

  • 摘要: 将中心分级的双环预混旋流(TAPS)燃烧室、单环腔燃烧室(SAC)及双环腔燃烧室(DAC)采用相同的扩压器尺寸、外机匣最大直径以及燃烧室出口尺寸,采用相同的数理模型,对TAPS燃烧室,SAC,DAC进行三维数值模拟.对比研究了TAPS燃烧室,SAC,DAC的总压恢复系数、燃烧效率、燃烧室出口温度分布系数、污染排放等性能参数.研究结果表明:采用TAPS燃烧室,可获得比SAC和DAC更高的总压恢复系数及燃烧效率;比SAC和DAC更低的燃烧室出口温度分布系数及NOx等污染的排放,尤其是设计工况下出口NOx排放.从研究结果来看中心分级的TAPS燃烧室的技术优势十分明显,是一种很有发展前景的高温升、低污染燃烧室.

     

  • [1] Turner M G,Ryder R,Norris A,et al.High fidelity 3D turbofan engine simulation with emphasis on turbomanchinery combustor coupling .AIAA-2002-3769,2002.
    [2] Zelina J,Cardena M,Tomondi C,et al.Low-emissions gas turbine combustor development using sector and full annular rigs .AIAA-1998-3528,1998.
    [3] Fuller E J,Smith C E.CFD analysis of a research gas turbine combustor primary zone .AIAA-1994-2768,1994.
    [4] Cline M C,Deur J M,Micklow G J,et al.Computation of the flow field in an annular gas turbine combustor .AIAA-1993-2074,1993.
    [5] 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):986-995. ZHAO Jianxing.Pollutant emission and development of low-emission combustion technology for civil aero engine[J].Journal of Aerospace Power,2008,23(6):986-995.(in Chinese)
    [6] Hukam C,Mogia H C.Aero-hermal design and analysis of gas turbine combustion systems:current status and future direction .AIAA-1998-3982,1998.
    [7] Rizk N K,Mongia H C.Three-dimensional emission modeling for diffusion flame,rich/lean,and lean gas turbine combustors .AIAA-1993-2338,1993.
    [8] 李杰.TAPS燃烧室燃油喷嘴结构设计特点分析及思考[J].航空科学技术,2010(1):8-10. LI Jie.Analysis of fuel nozzle configuration characteristic of TAPS combustor[J].Aeronautical Manufacturing Technology,2010(1):8-10.(in Chinese)
    [9] 梁春华,尚守堂.大飞机发动机先进低排放燃烧室技术[J].航空制造技术,2010(14):40-43. LIANG Chunhua,SHANG Shoutang.Advanced low emission combustor technologies for large commercial aircraft engine[J].Aeronautical Manufacturing Technology,2010,(14):40-43.(in Chinese)
    [10] 李锋,孙佰刚,彭浪青,等.大发动机双环腔燃烧室设计及性能分析[J].航空科学技术,2008(2):17-21. LI Feng,SUN Baigang,PENG Langqing,et al.Design and capability analysis of dual annular combustor[J].Aeronautical Science and Technology,2008(2):17-21.(in Chinese)
    [11] 李锋,尚守堂,程明,等.双环腔燃烧室置换单环腔燃烧室可行性研究[J].航空动力学报,2008,23(1):145-149. LI Feng,SHANG Shoutang,CHENG Ming,et al.Research on the feasibility of displacing the single annular combustor with a dual annular combustor[J].Journal of Aerospace Power,2008,23(1):145-149.
    [12] 宋博.发动机燃烧室的参数化建模和数值模拟 .北京:北京航空航天大学,2009. SONG Bo.Parametric modeling and numerical analysis of aero-engine combustor .Beijing:Beijing University of Aeronautics and Astronautics,2009.(in Chinese)
    [13] 刘殿春,董玉玺,尚守堂,等.单环腔中心分级燃烧室流畅数值模拟[J].航空动力学报,2010,25(6):1251-1257. LIU Dianchun,DONG Yuxi,SHANG Shoutang,et al.Numerical simulation of the flow field in a single annular concentric staged combustor[J].Journal of Aerospace Power,2010,25(6):1251-1257.(in Chinese)
    [14] 张珊珊.双环预混旋流燃烧室优化设计 .北京:北京航空航天大学,2010. ZHANG Shanshan.Optimization design of twin annular premixing swirler combustor .Beijing:Beijing University of Aeronautics and Astronautics,2010.(in Chinese)
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出版历程
  • 收稿日期:  2011-09-29
  • 刊出日期:  2012-08-28

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