| Citation: | KANG Yao, LIN Yu-zhen, JIANG Yao, WANG Xiao-feng. Effects of sleeve mixing length of swirl cup on the ignition characteristics[J]. Journal of Aerospace Power, 2016, 31(9): 2095-2103. doi: 10.13224/j.cnki.jasp.2016.09.007
|
| [1] |
彭泽琰,刘刚.航空燃气轮机原理[M].北京:国防工业出版社,2000.
|
| [2] |
Peters J E,Mellor A M. An ignition model for quiescent fuel sprays[J].Combustion and Flame,1980,38(80):65-74.
|
| [3] |
Ballal D R,Lefebvre A H.A general model of spark ignition for gaseous and liquid fuel-air mixture[C]//18th Symposium (International) on Combustion.Waterloo:Combustion Institute,1981:1737-1746.
|
| [4] |
Lefebvre A H.Gas turbine combustion[M].Phiadelphia,PA,USA:Taylor & Francis Press,1999.
|
| [5] |
Mellor A M.Design of modern turbine combustors[M].London:Academic Press,1990.
|
| [6] |
Read R W.Experimental investigations into high-altitude relight of a gas turbine[D].Cambridge:University of Cambridge,2008.
|
| [7] |
Mosbach T,Sadanandan R,Meier W,et al.Experimental analysis of altitude relight under realistic conditions using laser and high-speed video techniques[R].ASME Paper 2010-GT-22625,2010.
|
| [8] |
Linassier G,Viguier C,Verdier H,et al.,Experimental investigations of the ignition performances on a multi-sector combustor under high altitude conditions[R].AIAA-2012-0934,2012.
|
| [9] |
Marchione T,Ahmed S F,Mastorakos E.Ignition of turbulent swirling n-heptane spray flames using single and multiple sparks[J].Combustion and Flame,2009,156(1):166-180.
|
| [10] |
Ahmed S F,Mastorakos E.Spark ignition of lifted turbulent jet flames[J].Combustion and Flame,2006,146(1/2):215-231.
|
| [11] |
Letty C,Mastorakos E,Masri A R,et al.Structure of igniting ethanol and n-heptane spray flames with and without swirl[J].Experimental Thermal and Fluid Science,2012,43:47-54.
|
| [12] |
Mastorakos E.Ignition of turbulent non-premixed flames[J].Progress in Energy and Combustion Science,2009,35(1):57-97.
|
| [13] |
程波,徐华胜,史家荣.某环形燃烧室地面起动点火试验研究[C]//中国航空学会第十四届燃烧与传热传质学术交流会论文集.沈阳:中国航空学会,2007:201-206.
|
| [14] |
史家荣.短环燃烧室点火和燃烧稳定性能研究[C]//中国航空学会青年科技论坛文集.银川:中国航空学会,2005:268-273.
|
| [15] |
薛鑫,林宇震,张弛,等.火焰筒压力损失对点火特性的影响[J].航空动力学报,2012,27(10):2229-2235. XUE Xin,LIN Yuzhen,ZHANG Chi,et al.Effects of liner pressure loss on combustor ignition performances[J].Journal of Aerospace Power,2012,27(10):2229-2235.(in Chinese)
|
| [16] |
张弛,王建臣,覃清钦,等.微型燃气轮机乙醇燃烧室点火与熄火试验[J].航空动力学报,2009, 24(9):1930-1936. ZHANG Chi,WANG Jianchen,QIN Qingqin,et al.Experimental research on ignition and lean blowout for micro gas turbine ethanol combustor[J].Journal of Aerospace Power,2009,24(9):1930-1936.(in Chinese)
|
| [17] |
方昌德.世界航空发动机手册[M].北京:航空工业出版,1996.
|
| [18] |
WANG Xiaofeng,LIN Yuzhen,HU Haosheng,et al.Effect of swirl cup's venturi shape on spray structure and ignition process[R].ASME Paper 2014-GT-25216,2014.
|
| [19] |
Kobayashi M,Ogata H,Oda T,et al.Improvement on ignition performance for a lean staged low NOx combustor[R].ASME Paper 2011-GT-46187,2011.
|
| [20] |
KANG Yao,LIN Yuzhen,SONG Shuangwen,et al. Effects of sleeve divergence angle of dual-stage swirl cup on the ignition performance[R].ASME Paper 2014-GT-25782,2014.
|
| [21] |
于锦峰,郭志辉,张君锋,等.套筒长度对火焰筒流场和雾化特性的影响[J].航空动力学报,2009,24(11):2506-2513. YU Jinfeng,GUO Zhihui,ZHANG Junfeng,et al.Experimental study the effect of flare sleeve length on the flowfield and spray characterization of a combustor swirl cup[J].Journal of Aerospace Power,2009,24(11):2506-2513.(in Chinese)
|
| [22] |
夏立峰,刁瑶朋,郭志辉.套筒结构参数对头部流场和喷雾场的影响[C]//中国航空学会第十四届燃烧与传热传质学术交流会论文集.沈阳:中国航空学会,2007:472-478.
|
| [23] |
康尧,林宇震,霍伟业,等.双级旋流杯结构变化对点火特性的影响研究[J].推进技术,2014,35(5):675-680. KANG Yao,LIN Yuzhen,HUO Weiye,et al.Effects of hardware geometry of dual-stage swirl cup on ignition performance[J].Journal of Propulsion Technology,2014,35(5):675-680.(in Chinese)
|
| [24] |
罗国良,宋双文,胡好生,等.旋流杯空气雾化喷嘴套筒出口形状对小型燃烧室点火性能的影响[J].航空动力学报,2011,26(8):1708-1712. LUO Guoliang,SONG Shuangwen,HU Haosheng,et al.Influences of the swirl cup flares design on the small combustor ignition performances[J].Journal of Aerospace Power,2011,26(8):1708-1712.(in Chinese)
|
| [25] |
林宇震,林培华,许全宏,等.复合式收扩套筒空气雾化喷嘴燃烧室点火研究[J].航空动力学报,2007,22(3):342-346. LIN Yuzhen,LIN Peihua,XU Quanhong,et al.Research on ignition performance of a hybrid airblast atomizer combustor with convergent-divergent[J].Journal of Aerospace Power,2007,22(3):342-346.(in Chinese)
|
DownLoad: