对微型燃机向心透平叶轮顶部间隙流动在级环境下进行了全三维粘性数值模拟.研究结果表明:顶部间隙小于2%时,间隙每增加1%,级效率降低1.5%,而级通流能力有所降低;径向与轴向间隙变化对级性能影响有很大差别,径向间隙增加对级效率降低的影响是轴向间隙增加的8.3倍,径向间隙增加使通流能力增强的程度是轴向间隙增加使通流能力减弱的4.2倍.此外,将间隙流场与文献报道试验结果进行了比较,差别主要在工作轮顶部区域.
参考文献
[1] | Yaras M I;Sjolander S A .Effects of Simulated Rotation on Tip Leakage in a Planar Cascade of Turbine Blades:Part Ⅰ-Tip Gap Flow[J].Transactions of the ASME Journal of Heat Transfer,1992,114(04):652-660. |
[2] | Yaras M I;Sjolander S A .Prediction of Tip-Leakage Losses in Axial Turbines[J].Journal of Turbomachinery,Transactions of the ASME,1992,114(02):204-210. |
[3] | Dambach R .Tip Leakage Flow in a Radial Inflow Turbine[D].Cambridge University Engineering Department,1999. |
[4] | 邓清华,牛久芳,丰镇平.微型燃机向心透平叶轮顶部间隙流动的数值模拟[J].西安交通大学学报,2005(07):685-688. |
[5] | 邓清华 .100 kW微型燃气轮机向心透平气动设计与特性分析的研究[D].西安:西安交通大学,2004. |
[6] | Feng Zhenping;Deng Qinghua;Li Jun .Aerothermodynamic Design and Numerical Simulation of Radial Inflow Turbine Impeller for a 100 kW Microturbine[R].ASME Paper GT2005-68276,2005. |
[7] | 邓清华,丰镇平.微型燃气轮机向心透平导向器的流场分析与设计研究[J].西安交通大学学报,2005(09):962-965. |
[8] | Moustapha H;Zelesky M F;Baines N C.Axial and Radial Turbines[J].Concepts NREC,2004 |
[9] | Futral S M;Holeski D E.Experimental Results of Varying the Blade-Shroud Clearance in a 6.02-Inch Radial Inflow Turbine.NASA Technical Note D-5513[M].Washington,DC:NASA,1970 |
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