Volume 32 Issue 7
Jul.  2017
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Performance evaluation methods of two-stage axial swirler:Ⅰ influence of total swirling intensity[J]. Journal of Aerospace Power, 2017, 32(7): 1592-1598. doi: 10.13224/j.cnki.jasp.2017.07.008
Citation: Performance evaluation methods of two-stage axial swirler:Ⅰ influence of total swirling intensity[J]. Journal of Aerospace Power, 2017, 32(7): 1592-1598. doi: 10.13224/j.cnki.jasp.2017.07.008

Performance evaluation methods of two-stage axial swirler:Ⅰ influence of total swirling intensity

doi: 10.13224/j.cnki.jasp.2017.07.008
  • Received Date: 2015-11-02
  • Publish Date: 2017-07-28
  • Theoretical and numerical studies on the reaction flow field and combustion performance of two-stage axial swirler combustors were carried out. A performance evaluation method of multi-stage swirlers was developed. In addition, the total swirl intensity and energy utilization efficiency were put forward to evaluate the swirler performance. It was found that the total swirl intensity and flow resistance coefficient were the main influential factors to the swirler energy utilization efficiency. The interaction between the two stage swirlers was investigated numerically. And the results indicate that the inner swirl intensity has a greater impact on the width of central toroidal recirculation zone (CTRZ). The total swirl intensity plays a most important effect on combustor overall performance. When the total swirl intensity is less than 0.43, weak swirling flows will be produced; when the total swirl intensity is between 0.43 and 0.6, medium strength swirling flows will be produced and weak CTRZs are presented; when the total swirl intensity is more than 0.6, strong swirling flows will be produced and moderate CTRZs are presented at the same time; when the total swirl intensity is more than 1.03, very strong swirling flows will be generated. If the total swirl intensity is constant, a two-stage axial swirler will get better energy utilization efficiency than a single stage axial swirler. The results by the evaluation method are compared with the experimental and numerical results. Its found that the evaluation method for multi-stage axial swirler performance can accurately evaluate the performance of swirlers, providing a practical and effective method for the design of multi-stage swirlers in the future.

     

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  • [1]
    严传俊,范玮.燃烧学[M].西安:西北工业大学出版社,2008.
    [2]
    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.
    [3]
    MEHTA J M.Mean velocity and turbulent flow-field characteristics inside an advanced combustor swirl cup[R].AIAA 89-0215,1989.
    [4]
    MONGIA H C,AL-ROUB M,DANIS A.Swirl cup modeling:Part Ⅰ[R].AIAA-2001-3576,2001.
    [5]
    GIRIDHARAN M C,MONGIA H C,JENG S M.Swirl cup modeling:Part Ⅷ spray combustion in CFM-56 single cup flame tube[R].AIAA-2003-0319,2003.
    [6]
    JENG S M,FLOHRE N M.Air temperature effects on non-reacting spray characteristics issued from a counter-rotating swirler[R].AIAA-2005-355,2005.
    [7]
    EL-KADY A M,JENG S M,MONGIA H C.The influence of primary air jets on flow and pollutant emissions characteristics within a model gas turbine combustor[R].AIAA-2006-544,2006.
    [8]
    LIU Y,HAYASHI S.Experimental and numerical investigations on flow characteristics in a double-swirler combustor[R].AIAA 97-0708,1997.
    [9]
    LINCK M,GUPTA A K.Effect of swirl and combustion on flow dynamics in luminous kerosene sprayflames[R].AIAA-2003-1345,2003.
    [10]
    FU Y,CAI J,JENG S M,et al.Confinement effects on the swirling flow of a counter-rotating swirl cup[R].ASME Paper GT2005-469,2005.
    [11]
    ATESHKADI A,MCDONELL V G,SAMUELSEN G S.Effect of mixer geometry on fuel spray distribution,emission and stability[R].Reno,NV:The 36th AIAA Aerospace Sciences Meeting and Exhibit,Aerospace Sciences Meetings,1998.
    [12]
    MONGIA H C,GORE J P,GRINSTEIN F F,et al.Combustion research needs for helping development of next generation advanced combustors[R].Salt Lake City,US:The 37th Joint Propulsion Conference and Exhibit,Joint Propulsion Conferences,2001.
    [13]
    MCDONELL V G,SAMUELSEN G.Assessing the physics of spray behavior in complex combustion systems[R].Washington DC:American Institute of Aeronautics and Astronautics,1996.
    [14]
    WANG H,MCDONELL V G,SOWS W A,et al.Experimental study of a model gas turbine combustor swirl cup:Part Ⅱ droplet dynamics[J].Journal of Propulsion and Power,1994,10(4):446-452.
    [15]
    ARCHER S,GUPTA A K.The role of confinement on flow dynamics under fuel lean combustion conditions[R].AIAA-2004-5617,2004.
    [16]
    BEER J M,CHIGIER N A.Combustion aerodynamics[M].London:Applied Science Publishers Limited,1972.
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