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变弯度导叶对某高负荷双级风扇气动性能的影响

吴东 金东海 曹志鹏 安利平 桂幸民

吴东, 金东海, 曹志鹏, 安利平, 桂幸民. 变弯度导叶对某高负荷双级风扇气动性能的影响[J]. 航空动力学报, 2014, 29(12): 2973-2979. doi: 10.13224/j.cnki.jasp.2014.12.026
引用本文: 吴东, 金东海, 曹志鹏, 安利平, 桂幸民. 变弯度导叶对某高负荷双级风扇气动性能的影响[J]. 航空动力学报, 2014, 29(12): 2973-2979. doi: 10.13224/j.cnki.jasp.2014.12.026
WU Dong, JIN Dong-hai, CAO Zhi-peng, AN Li-ping, GUI Xing-min. Influence on aerodynamic performance of a highly loaded two-stage fan with variable inlet guide vane[J]. Journal of Aerospace Power, 2014, 29(12): 2973-2979. doi: 10.13224/j.cnki.jasp.2014.12.026
Citation: WU Dong, JIN Dong-hai, CAO Zhi-peng, AN Li-ping, GUI Xing-min. Influence on aerodynamic performance of a highly loaded two-stage fan with variable inlet guide vane[J]. Journal of Aerospace Power, 2014, 29(12): 2973-2979. doi: 10.13224/j.cnki.jasp.2014.12.026

变弯度导叶对某高负荷双级风扇气动性能的影响

doi: 10.13224/j.cnki.jasp.2014.12.026
基金项目: 

国家自然科学基金(51006005,50736007)

详细信息
    作者简介:

    吴东(1989-), 男, 重庆合川人, 硕士生, 主要从事叶轮机械气动热力学研究.

  • 中图分类号: V231.3

Influence on aerodynamic performance of a highly loaded two-stage fan with variable inlet guide vane

  • 摘要: 为了改善某高负荷双级风扇在非设计转速出现的裕度不足和转子攻角过大的问题,研究了变弯度导叶的调节对高负荷双级风扇气动性能和内部流场的影响,对比分析了不同形式变弯度导叶和传统可调导叶的性能差异.数值模拟结果表明:80%转速时高负荷双级风扇的绝热效率随着正预旋角度增加而显著增加,预旋角度为30°时的绝热效率提高了3.5%;传统可调导叶扩稳效果较优,受到大预旋角度下大损失的限制;变弯度导叶的开缝形式、开缝位置、导叶稠度均与气动性能密切相关,具体设计需要根据高负荷双级风扇工作情况进行探讨.

     

  • [1] 刘大响.航空发动机技术的发展和建议[J].中国工程科学,1999,1(2):24-29. LIU Daxiang.The development and proposals of aeroengine technology[J].Engineering Science,1999,1(2):24-29.(in Chinese)
    [2] Creason T L,Baghdadi S.Design and test of a low aspect ratio fan stage[R].AIAA 88-2816,1988.
    [3] Hasegawa H.Development of highly loaded fan with tandem cascade[R].AIAA-2003-1065,2003.
    [4] 单鹏,桂幸民.单级后掠风扇ATS-2设计与实验研究最终报告[R].北京:北京航空科技报告(HK-JB004024),2000.
    [5] 胡国荣,周亚峰,陈葆实,等.高速、高负荷跨音速单级风扇设计与试验[J].工程热物理学报,2001,22(1):40-43. HU Guorong,ZHOU Yafeng,CHEN Baoshi,et al.Design and test for single stage transonic fan with high speed,high load[J].Journal of Engineering Thermophysics,2001,22(1):40-43.(in Chinese)
    [6] 金海良,金东海,桂幸民.某高负荷跨音双级风扇气动设计与数值模拟[J].航空动力学报,2011,26(2):272-280. JIN Hailiang,JIN Donghai,GUI Xingmin.Aerodynamic design and numerical simulation of a highly loaded transonic two-stage fan[J].Journal of Aerospace Power,2011,26(2):272-280.(in Chinese)
    [7] 刘占民,赵凤声,惠兆森,等.新型变几何导叶试验研究[J].热能动力工程,1990,5(1):1-4. LIU Zhanmin,ZHAO Fengsheng,HUI Zhaosen,et al.An experimental study on a new type of variable-geometry guide vanes[J].Journal of Engineering for Thermal Energy and Power,1990,5(1):1-4.(in Chinese)
    [8] 刘占民,赵凤声,牟尚军,等.变弯度叶栅的试验研究[J].热能动力工程,1991,6(3):113-121. LIU Zhanmin,ZHAO Fengsheng,MU Shangjun,et al.An experimental study of variable camper cascades[J].Journal of Engineering for Thermal Energy and Power,1991,6(3):113-121.(in Chinese)
    [9] Seroy G K,Kavanagh P.Considerations in the design of variable geometry blading for axial compressor stages[R].Advisory Group for Aerospace Research and Development,AGARD CP-34,1968.
    [10] Bobula G A,Soeder R H,Burkarolt L A.Effect of a part-span variable inlet guide vane on the performance of a high- bypass turbofan engine[R].AIAA 81-1362,1981.
    [11] Woollett R R.Aerodynamic performance of a fan stage utilizing variable inlet guide vanes for thrust modulation[R].Washington:AIAA/SAE/ASME 19th Joint Propulsion Conference,1983.
    [12] Celis C,Pinto P M R,Barbosa R S,et al.Modeling of variable inlet guide vanes affects on a one shaft industrial gas turbine used in a combined cycle application[R].ASME Paper GT2008-50076,2008.
    [13] Hani M,Pascal C,David C,et al.Effect of casing treatment and variable axial guide vanes on a turbocharger compressor performance[R].ASME Paper GT2009-59190,2009.
    [14] Boehle M,Cagna M,Itter L.Compressible flow in inlet guide vanes with mechanical flaps[R].ASME Paper GT2004-53191,2004.
    [15] Tyner T M,Sullivan J P.Design and performance of a small,high speed axial compressor[R].AIAA 90-1911,1990.
    [16] Calvert W J,Emmerson P R,Moore J M.Design,test and analysis of a high-pressure-ratio transonic fan[R].ASME Paper GT2003-38302,2003.
    [17] 董玉玺,赵全春.带可变弯度零级导向叶片的风扇性能最佳化的试验研究[J].航空发动机,1996(3):27-29. DONG Yuxi,ZHAO Quanchun.An experimental study of optimization performance of fan with a variable inlet guide vane[J].Aeroengine,1996(3):27-29.(in Chinese)
    [18] 肖敏.压气机可变弯度静子叶片特性的试验研究[J].燃气涡轮试验与研究,2006,19(2):1-4. XIAO Min.Experimental investigation on performance of variable curvature vane of compressor stator[J].Gas Turbine Experiment and Research,2006,19(2):1-4.(in Chinese)
    [19] 刘红,朱俊强.可变弯度导叶及其后转子的性能研究[R].北京:中国工程热物理学会热机气动热力学学术会议,1999.
    [20] 楚武利,朱俊强.变几何叶片对压气机特性影响的实验研究及分析[J].应用力学学报,2003,20(1):78-80. CHU Wuli,ZHU Junqiang.Experiment research on effects of end curved of inlet guide vane to surge margin and performance of axial compressor[J].Chinese Journal of Applied Mechanics,2003,20(1):78-80.(in Chinese)
    [21] 金海良.周向平均方法在多级轴流风扇/压气机设计与分析中的应用[D].北京:北京航空航天大学,2011. JIN Hailiang.Application of circumferentional average method in multistage axial fan/compressor design and analysis[D].Beijing:Beijing University of Aeronautics and Astronautics,2011.(in Chinese)
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出版历程
  • 收稿日期:  2013-08-17
  • 刊出日期:  2014-12-28

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