Volume 30 Issue 2
Feb.  2015
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HAN Ji-ang, LI Xiao-dong, ZHONG Jing-jun. Comparison of trapped vortex cavity with/without injection in annular central bluff-body trapped vortex combustor[J]. Journal of Aerospace Power, 2015, 30(2): 331-340. doi: 10.13224/j.cnki.jasp.2015.02.010
Citation: HAN Ji-ang, LI Xiao-dong, ZHONG Jing-jun. Comparison of trapped vortex cavity with/without injection in annular central bluff-body trapped vortex combustor[J]. Journal of Aerospace Power, 2015, 30(2): 331-340. doi: 10.13224/j.cnki.jasp.2015.02.010

Comparison of trapped vortex cavity with/without injection in annular central bluff-body trapped vortex combustor

doi: 10.13224/j.cnki.jasp.2015.02.010
  • Received Date: 2013-09-16
  • Publish Date: 2015-02-28
  • The three dimensional Reynolds-averaged Navier-Stokes (N-S) equations, renormalization group (RNG) k-ε turbulent model and standard wall functions were adopted to numerically simulate the cold flow field of annular central bluff-body trapped vortex combustor under trapped vortex cavity with/without injection. The effects of trapped vortex cavity with/without injection on the vortex structure, flow parameters in the trapped vortex cavity and the overall performance of the annular central bluff-body trapped vortex combustor were analyzed. Results show that a relatively stable double vortex structure can be formed in the trapped vortex cavity with trapped vortex cavity injection compared to trapped vortex cavity without injection. With the existence of trapped vortex cavity injection, the total pressure loss coefficient of the annular central bluff-body trapped vortex combustor is reduced about 9.2% at the exit section and the average flow parameters of the trapped vortex cavity also increase. The trapped vortex cavity injection has little influence on changing trend of flow parameters along flow-path height direction at the exit section of the annular central bluff-body trapped vortex combustor.

     

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  • [1]
    张津,洪杰,陈光.现代航空发动机技术与发展[M].北京:北京航空航天大学出版社,2006.
    [2]
    尚守堂,程明,李锋,等.低排放长寿命燃烧室关键技术分析[J].航空制造技术,2009(2):32-37. SHANG Shoutang,CHENG Ming,LI Feng,et al.Analysis on key technologies of low-emission and long-life combustion chamber[J].Aeronautical Manufacturing Technology,2009(2):32-37.(in Chinese)
    [3]
    金捷,岳明.燃气涡轮发动机低污染燃烧室的发展趋势及思考[C]//大型飞机关键技术高层论坛暨中国航空学会2007年学术年会论文集.深圳:中国航空学会,2007:1836-1846.
    [4]
    林宇震,许全宏,刘高恩.燃气轮机燃烧室[M].北京:国防工业出版社,2008.
    [5]
    Hsu K Y.Gross L P.Characteristics of a trapped vortex combustor[J].Journal of Propulsion and Power,1998,14(1):57-65.
    [6]
    于达仁,刘金福,徐基豫.面向21世纪的燃气轮机技术的发展[J].燃气轮机技术,2001,14(1):14-21,53. YU Daren,LIU Jinfu,XU Jiyu.Facing the development of GT technology in the 21th century[J].Gas Turbine Technology,2001,14(1):14-21,53.(in Chinese)
    [7]
    Hsu K Y,Goss L P,Trump D D,et al.Performance of a trapped vortex combustor[R].AIAA 95-0810,1995.
    [8]
    Roquemore W M,Shouse D,Burrus D,et al.Trapped vortex combustor concept for gas turbine engines[R].AIAA-2001-0483,2001.
    [9]
    Katta V R,Roquemore W M.Study on trapped-vortex combustor-effect of injection on dynamics of non-reacting and reacting flows in a cavity[R].AIAA 97-3256,1997.
    [10]
    Burrus D L,Johnson A W,Roquemore W M,et al.Performance assessment of a prototype trapped vortex combustor concept for gas turbine application[R].ASME Paper 2001-GT-0087,2001.
    [11]
    Mancilla P C,Chaka P,Acharya S.Performance of a trapped vortex spray combustor[R].ASME Paper 2001-GT-0058,2001.
    [12]
    Meyer T R,Brown M S,Fonov S,et al.Optical diagnostics and numerical characterization of a trapped vortex combustor[R].AIAA-2002-3863,2002.
    [13]
    樊未军,孔昭健,邢菲,等.凹腔驻涡模型燃烧室内涡的演化发展[J].航空动力学报,2007,22(6):888-892. FAN Weijun,KONG Zhaojian,XING Fei,et al.Vortexes evolvement and development in the model of trapped vortex combustor[J].Journal of Aerospace Power,2007,22(6):888-892.(in Chinese)
    [14]
    何小民,许金生,苏俊卿.驻涡区进口结构参数影响TVC燃烧性能的试验[J].航空动力学报,2007,22(11):1798-1802. HE Xiaomin,XU Jinsheng,SU Junqing.Effect of air and fuel injection patterns in pilot zone on trapped-vortex combustor performance[J].Journal of Aerospace Power,2007,22(11):1798-1802.(in Chinese)
    [15]
    邢菲,孟祥泰,李继保,等.凹腔双驻涡稳焰冷态流场初步研究[J].推进技术,2008,29(2):135-138. XING Fei,MENG Xiangtai,LI Jibao,et al.Elementary study on cool flow field of double vortex in cavity for flame stabilization[J].Journal of Propulsion Technology,2008,29(2):135-138.(in Chinese)
    [16]
    Kendrick D,Lawlor S P,Steele R C.Trapped vortex combustor:USA,US7003961B2[P].2006-02-28.
    [17]
    Edmonds R G,Steele R C,Williams J T,et al.Ultra-low NOx advanced vortex combustor[R].ASME Paper GT2006-90319,2006.
    [18]
    Bucher J,Edmonds R G,Steele R C,et al.The development of a lean-premixed trapped vortex combustor[R].ASME Paper GT2003-38236,2003.
    [19]
    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):488-493. 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):488-493.(in Chinese)
    [20]
    程平.驻涡燃烧室冷态流场气体喷射的研究[D].辽宁 大连:大连海事大学,2009. CHENG Ping.Study on the cool flow field in trapped vortex combustor with air injection[D].Dalian Liaoning:Dalian Maritime University,2009.(in Chinese)
    [21]
    刘世青.驻涡燃烧室流动特性的冷态数值研究[D].辽宁 大连:大连海事大学,2011. LIU Shiqing.The numerical study of the cold flow properties in the trapped vortex combustor[D].Dalian Liaoning:Dalian Maritime University,2011.(in Chinese)
    [22]
    Lawlor S P,Steele R C,Baldwin P.Advanced supersonic component engine for military application[R].ASME Paper GT2007-27336,2007.
    [23]
    Lawlor S P,Hinkey J B,Mackin S G,et al.Supersonic compression stage design and test results[R].International Mechanical Engineering Congress and Exposition,IMECE 2004-59914,2004.
    [24]
    姚征,陈康民.CFD通用软件综述[J].上海理工大学学报,2002,24(2):137-144. YAO Zheng,CHEN Kangmin.Review on the commercial CFD softwares[J].Journal of University of Shanghai for Science and Technology,2002,24(2):137-144.(in Chinese)
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