Volume 29 Issue 7
Jul.  2014
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SUN Hai-jun, ZENG Zhuo-xiong, XU Yi-hua, HU Chun-bo. Influence of improved structure of bluff-body on combustion flow characteristics in advanced vortex combustor[J]. Journal of Aerospace Power, 2014, (7): 1639-1646. doi: 10.13224/j.cnki.jasp.2014.07.017
Citation: SUN Hai-jun, ZENG Zhuo-xiong, XU Yi-hua, HU Chun-bo. Influence of improved structure of bluff-body on combustion flow characteristics in advanced vortex combustor[J]. Journal of Aerospace Power, 2014, (7): 1639-1646. doi: 10.13224/j.cnki.jasp.2014.07.017

Influence of improved structure of bluff-body on combustion flow characteristics in advanced vortex combustor

doi: 10.13224/j.cnki.jasp.2014.07.017
  • Received Date: 2013-04-17
  • Publish Date: 2014-07-28
  • In order to study the mechanism of flame stabilization in cavity of advanced vortex combustor, an improvement program of after bluff-body structure was introduced, and the combustion characteristics of improved combustor under the conditions of premixed and non-premixed combustion were numerically simulated. The results show that under the condition of premixed combustion, the improved bluff-body structure can enhance the intensity and temperature of vortex flow in cavity, and make the temperature distribution more evenly no matter if equivalence ratio is 0.6 or equal to 1.0. In addition, the cavity temperature increases with the increasing premixed inlet velocity, and changes little when the velocity reaches a certain value. Under the condition of non-premixed combustion, the improved bluff-body structure ameliorates the vortex flow and temperature distribution in cavity, and the cavity maintains relatively high temperature under the condition of lean burning. The improved lightweight combustor can provide certain reference for engineering application.

     

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  • [1]
    Komerath N M,Ahuja K K.Chambers F W.Prediction and measurement of flow over cavities:a survey[R].AIAA 87-0166,1987.
    [2]
    Hsu K Y,Goss L P,Trump D D,et al.Performance of a trapped vortex combustor[R].AIAA 95-0810,1995.
    [3]
    樊未军,易琪,严明,等.驻涡燃烧室凹腔双涡结构研究[J].中国电机工程学报,2006,26(9):66-70. FAN Weijun,YI Qi,YAN Ming,et al.A study of double vortex structure in the trapped vortex combustor[J].Proceedings of the CSEE,2006,26(9):66-70.(in Chinese)
    [4]
    何小民,许金生,苏俊卿.驻涡燃烧室燃烧性能试验[J].航空动力学报,2009,24(2):318-323. HE Xiaomin,XU Jinsheng,SU Junqing.Experimental research of the performance of the trapped vortex combustor[J].Journal of Aerospace Power,2009,24(2):318-323.(in Chinese)
    [5]
    Ben-Yakar A,Hanson R K.Cavity flame-holders for ignition and flame stabilization in scramjets:an overview[J].Journal of Propulsion and Power,2001,17(4):869-877.
    [6]
    刘娟,潘余,刘卫东,等. 超燃冲压发动机双凹腔燃烧室氢气燃烧流场分析[J].航空动力学报,2009,24(11):2501-2505. LIU Juan,PAN Yu,LIU Weidong,et al.Analysis of the hydrogen combustion field in scramjet dual cavity combustor[J].Journal of Aerospace power,2009,24(11):2501-2505.(in Chinese)
    [7]
    耿辉,周进,翟振辰,等.凹腔结构对超声速燃烧室中横向燃料喷流流动与燃烧的影响[J].推进技术,2007,28(6):599-606. GENG Hui,ZHOU Jin,ZHAI Zhenchen,et al.Influence of cavity geometry on flow and combustion of transverse fuel jets in a supesonic combustor[J].Journal of Propulsion Technology,2007,28(6):599-606.(in Chinese)
    [8]
    Kendrick D W,Chenevert B C,Trueblood B,et al.Combustion system development for the ramgen engine[J].Journal of Engineering for Gas Turbines and Power,2003,125(4):885-894.
    [9]
    Edmonds R G,Steele R C,Williams J T,et al.Ultra-low NOx advanced vortex combustor[C]//Proceedings of the ASME Turbo Expo Power for Land,Sea and Air.Barcelona,Spain:ASME,2006,255-262.
    [10]
    Edmonds R G,Williams J T,Steele R C,et al.Low NOx advanced vortex combustor[J].Journal of Engineering for Gas Tu rbines and Power,2008,130(3):034502.1-034502.4.
    [11]
    邓洋波,刘世青,钟兢军.AVC中钝体布置与燃烧室流动特性研究[J].工程热物理学报,2008,29(8):1416-1418. DENG Yangbo,LIU Shiqing,ZHONG Jingjun.Research of the flow characteristics of cold state flow of advanced vortex combustor[J].Journal of Engineering Thermophysics,2008,29(8):1416-1418.(in Chinese)
    [12]
    邓洋波,刘世青,钟兢军.先进旋涡燃烧室燃烧特性数值模拟[J].大连海事大学学报,2008,34(3):21-24. DENG Yangbo,LIU Shiqing,ZHONG Jingjun.Numerical simulation for combustion characteristics of advanced vortex combustor[J].Journal of Dalian Maritime University,2008,34(3):21-24.(in Chinese)
    [13]
    邓洋波,刘世青,钟兢军.先进旋涡燃烧室流动与燃烧特性分析[J].航空动力学报,2009,24(3):1416-1418. DENG Yangbo,LIU Shiqing,ZHONG Jingjun.Analysis of the combustion and flow field characteristics of advanced vortex combustor[J].Journal of Aerospace Power,2009,24(3):1416-1418.(in Chinese)
    [14]
    邓洋波,孙海涛,王玉龙,等.氢燃料先进旋涡燃烧室流动和燃烧特性[J].航空动力学报,2013,28(1):120-128. DENG Yangbo,SUN Haitao,WANG Yulong,et al.Flow and combustion characteristics of advanced vortex combustor with hydrogen fuel[J].Journal of Aerospace Power,2013,28(1):120-128.(in Chinese)
    [15]
    钟兢军,刘世青.后驻体喷孔位置影响驻涡腔流动冷态数值研究[J].上海海事大学学报,2011,32(1):44-48. ZHONG Jingjun,LIU Shiqing.Impact of nozzle position on after body on cold flow field values in trapped vortex chamber[J].Journal of Shanghai Maritime University,2011,32(1):44-48.(in Chinese)
    [16]
    刘世青,钟兢军.后驻体喷射角度对驻涡燃烧室影响冷态数值研究[J].哈尔滨工程大学学报,2010,31(8):1065-1072. LIU Shiqing,ZHONG Jingjun.Numerical investigation on the influence of injection angle from afterbody in cold field of the trapped vortex combustor[J].Journal of Harbin Engineering University,2010,31(8):1065-1072.(in Chinese)
    [17]
    刘世青,钟兢军.驻涡燃烧室后驻体形状选择冷态数值研究[J].工程热物理学报,2010,31(9):1480-1483. LIU Shiqing,ZHONG Jingjun.Numerical investigation of cool flow field in trapped vortex combustor in after body selection[J].Journal of Engineering Thermophysics,2010,31(9):1480-1483.(in Chinese)
    [18]
    孙海俊,曾卓雄,徐义华.先进旋涡燃烧室钝体结构参数选择的数值分析[J].弹箭与制导学报,2012,32(6):99-102. SUN Haijun,ZENG Zhuoxiong,XU Yihua.Numerical simulation of bluff-body structural parameters in advanced vortex combustor[J].Journal of Projectiles,Rockets,Missiles and Guidance,2012,32(6):99-102.(in Chinese)
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