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叶顶间隙流动是导致涡轮动叶中产生流动损失的主要原因之一.对某动力涡轮第一级内三维流动的数值计算结果表明,流体在经过动叶叶顶间隙以后在约25%叶顶轴向弦长处(τ=3mm)在叶顶与吸力边夹角处卷起形成间隙涡,造成流动阻塞,同时在间隙内叶片顶部10%叶顶轴向弦长处(τ=3mm)开始在压力边出现叶顶分离涡,使得间隙流动损失增加.随着间隙高度增大,通过间隙的流量增加,间隙涡形成位置后移,间隙涡、叶顶分离涡尺寸变大,在流道内影响范围增大,导致流动损失变大.

参考文献

[1] Bindon J P .The Measurement and Formation of Tip Clearance Loss[J].Journal of Turbomachinery,Transactions of the ASME,1989,111(07):257-263.
[2] Schaub U W;Vlasic E;Moustapha S H.Effect of Tip Clearance on the Performance of a Highly Loaded Turbine Stage[A].Montreal,Canada:North Atlantic Treaty Organization,1993:29-1-29-11.
[3] Xiao Xinwen .Investigation of Tip Clearance Flow Physics in Axial Flow Turbine Rotors[D].Pennsylvania:Pennsylvania State University,2001.
[4] Shin S .Reynolds-Averaged Navier-Stokes Computation of Tip Clearance Flow in a Compressor Cascade Using an Unstructured Grid[D].Virgina Polytechnic Institute and State University,2001.
[5] S. A. Sjolander;D. Cao .Measurements of the flow in an idealized turbine tip gap[J].Journal of turbomachinery,1995(4):578-584.
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