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. |
上一张
下一张
上一张
下一张
计量
- 下载量()
- 访问量()
文章评分
- 您的评分:
-
10%
-
20%
-
30%
-
40%
-
50%