Volume 27 Issue 12
Dec.  2012
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XUE Xin, LIN Yu-zhen, ZHANG Chi, XU Quan-hong, DU Jiang-yi. Effects of liner pressure loss on combustor lean blow-out and combustion efficienly performances[J]. Journal of Aerospace Power, 2012, 27(12): 2687-2691.
Citation: XUE Xin, LIN Yu-zhen, ZHANG Chi, XU Quan-hong, DU Jiang-yi. Effects of liner pressure loss on combustor lean blow-out and combustion efficienly performances[J]. Journal of Aerospace Power, 2012, 27(12): 2687-2691.

Effects of liner pressure loss on combustor lean blow-out and combustion efficienly performances

  • Received Date: 2011-12-17
  • Publish Date: 2012-12-28
  • Based on a liner with 3.0% pressure loss liner, two low pressure loss liners (2.5% and 2.0%) were designed.The light lean ignition experiments were conducted to study the effect of liner pressure loss on the combustor lean blow-out and combustion efficiency.Under the idle conditions, the lean blow-out fuel air ratios of low pressure loss liner were lower than that of the baseline liner, and 2.5% pressure loss liner had the lowest.Under the high pressure and high temperature connditions, the low pressure loss had no effect on the combustion efficiency.Compared with the results of ignition, it was acceptable to reduce the liner pressure to 2.5% without negative effect on the combustion characteristic of combustor.

     

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  • [1]
    沈维道,蒋智敏,童钧耕.工程热力学[M].北京:高等教育出版社,2001.
    [2]
    廉筱纯,吴虎.航空发动机原理[M].西安:西北工业大学出版社,2005.
    [3]
    金如山.航空燃气轮机燃烧室[M].北京:宇航出版社,1988.
    [4]
    Lefebvre A H.Gas turbine combustion[M].2nd ed.Philadelphia:Taylor & Francis,1999.
    [5]
    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.
    [6]
    胡正义.航空发动机设计手册:第9册[M].北京:航空工业出版社,2000.
    [7]
    彭云晖,林宇震,许全宏,等.双旋流空气雾化喷嘴喷雾、流动和燃烧性能[J].航空学报,2008,29(1):1-14.PENG Yunhui,LIN Yuzhen,XU Quanhong,et al.Atomization,aerodynamics and combustion performance of swirl cup[J].Acta Aeronautica et Astronautica Sinica,2008,29(1):1-14.(in Chinese)
    [8]
    Lefebvre A H,Ballal D R.Gas turbine combustion,alternative fuels and emission,third edition edition[M].Boca Raton:Taylor & Francis,2010.
    [9]
    Lefebvre A H.Fuel effects on gas turbine combustion-ignition,stability,and combustion efficiency[J].Journal of Engineering for Gas Turbine and Power,1985,107(24):23-37.
    [10]
    Meller A M.Design of modern turbin combustor[M].London:Academic Press,1995.
    [11]
    Rizk N K,Mongia H C.Gas turbine combustor design methodology[R].AIAA-1986-1531,1986.
    [12]
    Sturgess G J.Design and development of a rasearch combustor for lean blow-out studies[J].Journal of Engineering for Gas Turbine and Power,1992,114(1):13-19.
    [13]
    Sturgess G J,Shouse D T.A hybrid model for calculating lean blow-outs in practical combustor [R].AIAA-1996-3125,1996.
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