留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

回流环形燃烧室出口温度场的试验

刘富强 房爱兵 崔玉峰 徐纲 朱俊强 聂超群

刘富强, 房爱兵, 崔玉峰, 徐纲, 朱俊强, 聂超群. 回流环形燃烧室出口温度场的试验[J]. 航空动力学报, 2012, 27(1): 48-54.
引用本文: 刘富强, 房爱兵, 崔玉峰, 徐纲, 朱俊强, 聂超群. 回流环形燃烧室出口温度场的试验[J]. 航空动力学报, 2012, 27(1): 48-54.
LIU Fu-qiang, FANG Ai-bing, CUI Yu-feng, XU Gang, ZHU Jun-qiang, NIE Chao-qun. Experiment of outlet temperature distribution of a reverse-flow annular combustor[J]. Journal of Aerospace Power, 2012, 27(1): 48-54.
Citation: LIU Fu-qiang, FANG Ai-bing, CUI Yu-feng, XU Gang, ZHU Jun-qiang, NIE Chao-qun. Experiment of outlet temperature distribution of a reverse-flow annular combustor[J]. Journal of Aerospace Power, 2012, 27(1): 48-54.

回流环形燃烧室出口温度场的试验

基金项目: 国际科技合作项目(2010DFB70620); 国家重点基础研究发展计划项目(2007CB210109)

Experiment of outlet temperature distribution of a reverse-flow annular combustor

  • 摘要: 以某涡轮风扇发动机回流环形燃烧室为研究对象,采用试验的方法,研究了不同工况下该燃烧室出口温度分布特性.部件试验结果得到了出口温度沿周向分布和径向分布特性,重点详细分析了温度沿涡轮导叶叶高的分布特性,并在此基础上提出了局部扇形区域径向温度沿叶高的分布特性这一概念来考核燃烧室出口温度品质,为燃烧室出口温度分布的评估和改进优化提供了有益的参考价值.

     

  • [1] Lefebvre A H.Gas Turbine combustion[M].2nd ed.Philadelphia:Taylor & Francis,1998.
    [2] Eggels R L.Modelling of the combustion process of a premixed DLE gas turbine.ASME Paper GT2000-0130,2000.
    [3] Boudier G,Gicquel L Y M,Poinsot T,et al.Comparison of LES,RANS and experiments in an aeronautical gas turbine combustion chamber[J].Proceedings of the Combustion Institutes,2007,31(2):3075-3082.
    [4] Fureby C,Grinstein F F,Li G,et al.An experimental and computational study of a multi-swirl gas turbine combustor[J].Proceeding of the Combustion Institute,2007,31(2):3107-3114.
    [5] Noll B,Kessler R,Theisen P,et al.Flow field mixing characteristics of an aero-engine combustor Part Ⅱ:numerical simulations.AIAA 2002-3708,2002.
    [6] Clercq L P,Schlieper M,Noll B,et al.Liquid fuel flameless combustion RANS simulation.ASME Paper GT2008-50552,2008.
    [7] 蔡文祥,赵坚行,胡好生,等.环形燃烧室冷态流场数值模拟中的数学方法[J]. 航空动力学报,2010,25(4):748-753. CAI Wenxiang,ZHAO Jianxing,HU Haosheng,et al.Numerical methods in simulation of annular combustor cold flow field[J].Journal of Aerospace Power,2010,25(4):748-753.(in Chinese)
    [8] 彭云晖,林宇震,刘高恩.三旋流器燃烧室出口温度分布的初步试验研究 [J].航空动力学报,2007,22(4):554-558. PENG Yunhui,LIN Yuzhen,LIU Gaoen.A preliminary experimental study of pattern factor for a triple swirle combustor[J].Journal of Aerospace Power,2007,22(4):554-558.(in Chinese)
    [9] 郑严,沈倍毅.弹用涡喷发动机燃烧室出口温度场试验与分析[J].推进技术,2001,22(3):187-191,206. ZHENG Yan,SHEN Beiyi.Tests and analysis of exit temperature distribution of the combustor for mussile turbojet[J].Journal of Propulsion Technology,2001,22(3):187-190,206.(in Chinese)
    [10] 胡好生,赵坚行,钟建平,等.一种新颖的燃烧室出口温度场调试方法[J].航空动力学报,2007,22(8):1222-1226. HU Haosheng,ZHAO Jianxing,ZHONG Jianping,et al.A new adjustment method of combustor outlet temperature field[J].Journal of Aerospace Power,2007,22(8):1222-1226.(in Chinese)
    [11] Bishop C K,Allan W.Effects of fuel nozzle condition on gas turbine combustion chamber exit temperature distributions.ASME Paper GT2010-23441,2010.
    [12] Fu Y,Cai J,Elkady A,et al.Fuel and equivalence ratio effects on spary combustor of a counter-rotating swirler.AIAA 2005-0354,2005.
    [13] 董平, 郭兆元,王强,等.进口温度不均匀对气冷涡轮叶片传热的影响[J].工程热物理学报,2010,31(7):1109-1112. DONG Ping,GUO Zhaoyuan,WANG Qiang,et al.Effects of non-uniform inlet temperature distribution on air cooled gas turbine vane[J].Journal of Engineering Thermophysics ,2010,31(7):1109-1112.(in Chinese)
  • 加载中
计量
  • 文章访问数:  1384
  • HTML浏览量:  4
  • PDF量:  447
  • 被引次数: 0
出版历程
  • 收稿日期:  2011-03-08
  • 修回日期:  2011-06-09
  • 刊出日期:  2012-01-28

目录

    /

    返回文章
    返回