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燃机预旋喷嘴流动特性的数值研究 被引量:3

Numerical Investigation on the Flow of Preswirl Nozzle in Gas Turbine
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摘要 为了降低燃机透平叶片的温度,进一步提高透平叶片的使用寿命和燃机的功率,对燃机预旋喷嘴的流动特性进行了数值研究,研究了预旋喷嘴的长径比对喷嘴流量系数、出气角度和流场均匀性的影响。通过研究发现随着预旋喷嘴长径比的增加,预旋喷嘴的出气角度先减小后增加,最后趋近于预旋角度;出气角度的均匀性和出气速度的均匀性都有很大的提高;预旋喷嘴流量系数随着长径比的增加先减小后增加。 Numerical investigation of the flow of preswirl nozzle was carried out to reduce the temperature of gas turbine blade and further improve the service life and the power of gas turbine. The influence of length-to-diameter ratio on the discharge coefficient, outflow angle and flow field uniformity of a preswirl nozzle was studied extensively. The results showed that outflow angle first decreased and then increased with the increase of length-to-diameter ratio, finally approaching the preswirl angle, outflow angle and flow field uniformity were greatly improved, the discharge coefficient of preswirl nozzle first raised and then reduced with increasing of length-to-diameter ratio of the preswirl nozzle.
出处 《东方汽轮机》 2012年第1期53-60,共8页 Dongfang Turbine
关键词 预旋喷嘴 长径比 流量系数:均匀性 preswirl nozzle, length-to-diameter ratio, discharge coefficient, uniformity
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参考文献8

  • 1Dittman M. Discharge Coefficients of a Preswirl System in Secondary Air System.[ASME 2001-GT-0122][R].
  • 2Benim A.C. Investigation into the Computational Analysis of Direct-Transfer Preswirl System for Gas Turbine Blade Cooling.[ASME GT2004-54151,][R].2004.
  • 3Geis T. Cooling Air Temperature Reduction in a Direct Transfer Preswirl System.[GT2003-38231][R].
  • 4Pilbrow A. Heat Transfer in a Cover-Plate Preswirl Rotor-Stator System[J].Jour Turbomachinery,1999.
  • 5Wilson M. Flow and Heat Transfer in a Preswirl Rotor-Stator System.[ASME 95-GT-239][R].
  • 6Fabio Ciampoli,John W.Chew,Shahrokh Shahpar,Elisabeth Willocq. Automatic optimisation of preswirl nozzle design.[ASME GT2006-90249,][R].2006.
  • 7王锁芳,朱强华,张羽,栾海峰,黄爱霞.预旋进气位置对转静盘腔换热影响的数值研究[J].航空动力学报,2007,22(8):1227-1232. 被引量:25
  • 8Ciampoli F,Hills N.J,Chew J.w. Unsteady numerical simulation of the flow in a direct transfer pre-swirl system.[ASME Paper GT-2008-51198][R]..doi:10.1007/s10729-007-9044-5.

二级参考文献12

  • 1冶萍,张靖周.有预旋进气转静盘腔中的流动和换热特性数值研究[J].航空动力学报,2004,19(3):370-374. 被引量:16
  • 2陶文铨.数值传热学[M].西安:西安交通大学出版社,1998..
  • 3Karabay H,Pilbrow R,Wilson M,et al.Performance of pre-swirl rotating-disc systems[J].ASME Journal of Gas Turbines and Power,2000,122:442-450.
  • 4Karabay H,Owen J M,Wilson M.Approximate solutions for flow and heat Transfer in pre-swirl rotating-disc systems[R].ASME Paper 2001-GT-0200,2001.
  • 5Wilson M,Pilbrow R,Owen J M.Flow and heat transfer in a preswirl rotor-stator system[J].ASME Journal of Turbomachinery,1997,119:364-373.
  • 6Wilson M,Owen J M,Lock G.Influence of fluid-dynamics on heat transfer in a preswirl rotating-disc system[R].ASME Paper 2004-GT-53158.
  • 7栾海峰.带有预旋孔的旋转盘腔传热实验研究[D].南京:南京航空航天大学,2005.
  • 8El-oun Z B,Owen J M.Pre-swirl blade-cooling effectiveness in an adiabatic rotor-stator system[R].ASME Paper No.88-GT-276,1988.
  • 9丁水汀,陶智,徐国强,袁怡祥,邱绪光.带进气预旋的旋转空腔平均换热特性研究[J].航空动力学报,1998,13(3):277-280. 被引量:15
  • 10徐国强,詹治国,丁水汀,陶智,罗翔.中心进气和高位垂直进气转静系旋转盘冷却品质比较[J].推进技术,2000,21(5):42-44. 被引量:6

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