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弯曲叶片对压气机轮毂-角区失速的影响 被引量:2

Bowed Blade Effect on Hub-Corner Stall
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摘要 为了数值模拟弯曲静子对某两级低速轴流压气机总体性能及轮毂-角区失速的影响,选取了第1级静子进行弯曲。弯曲静子积叠线为贝塞尔曲线-直线-贝塞尔曲线(Bezier-line-Bezier,BLB)形式,弯高为20%叶片高度,弯角为10,15,20,25和30°。结果表明,弯曲叶片能有效抑制小流量范围内的轮毂-角区失速,从而改善压气机的性能。过度的弯曲会带来较大的叶型损失,从而导致大流量工况下压气机效率有所下降。扩散因子不能作为判断轮毂-角区失速是否存在的主要依据。 A numerical simulation is performed to analyze the effect of first stage bowed stator with different bowed angles on the total performance and the hub-corner stall for a two-stage low speed axial compressor.Bezier-line-Bezier(BLB) curve is chosen as the stacking line.The bowed height of BLB is 20% of blade height and the bowed angles are 10,15,20,25 and 30°.The result shows that bowed blade can suppress the hub-corner stall at low flow rate,thus increaing the efficiency.Moreover,excessive bow can cause bigger profile loss,which decreases the efficiency at high flow rate.Diffusion factor based on the two-dimensional airfoil separation data cannot be used as the criterion to predict the hub-corner stall.
出处 《南京航空航天大学学报》 EI CAS CSCD 北大核心 2012年第2期139-145,共7页 Journal of Nanjing University of Aeronautics & Astronautics
关键词 弯曲叶片 数值模拟 轮毂-角区失速 bowed blade numerical simulation hub-corner stall
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参考文献9

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二级参考文献4

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共引文献38

同被引文献22

  • 1李美林,林峰,陈静宜,童志庭,聂超群.周向进口畸变对压气机失速过程的影响[J].工程热物理学报,2005,26(6):931-934. 被引量:11
  • 2黄健,吴虎,杜文海.45°周向压力畸变对轴流压气机影响的实验研究和机理分析[J].航空动力学报,2007,22(3):460-464. 被引量:3
  • 3李传鹏,胡骏,王英锋,赵勇.进气畸变对压气机稳定性的影响[J].工程热物理学报,2006,27(5):778-780. 被引量:4
  • 4Roy B,Chouhan M,Kaudinya K V.Experimental study of boundary layer control through tip injection on straight and swept compressor blades[R].ASME Paper GT2005-68304,2005.
  • 5Roy B,Veraarapu S.Stability enhancement and hysteresis improvement of axial flow fan by discrete and distributed tip injection schemes[R].ASME Paper GT2008-50075,2008.
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  • 9Gummer V,Wenger U,Kau H P.Using sweep and dihedral to control three-dimensional flow in transonic stators of axial compressors[J].Journal of Turbomachinery,2001,123(1):40-48.
  • 10Gallimore S J,Bolger J J,Cumpsty N A,et al.The use of sweep and dihedral in multistage axial flow compressor blading:Part Ⅱ low and high speed designs and test verification[J].Journal of Turbomachinery,2002,124(4):533-541.

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