Experimental and numerical analysis of a classical bleed slot system for a turbocharger compressor

This paper presents an insight into the performance and inducer flow field of a turbocharger centrifugal compressor incorporating a classical bleed slot system with various slot positions. The bleed slot is popular widely used map width enhancement method in the turbocharger industry. Even though the technique has been used for a long time, further study is still required to gain a better understanding of the flow structures inside the compressor stage due to the bleed slot. Therefore, this detailed study of the bleed slot system has been performed through a careful CFD analysis validated against experimental data. Three different positions of the bleed slot opening on the impeller shroud have been analysed and discussed in terms of their impact on the map width of the compressor. Discussion focuses on the slot flow variation throughout the speedline, the inducer inlet swirl near the surge flow condition and its impact on map width enhancement. The paper also demonstrates the capability of CFD analyses to predict the surge point.

[1]  M. L. Mansour,et al.  Numerical Optimization of a Vaned Shroud Design for Increased Operability Margin in Modern Centrifugal Compressors , 2006 .

[2]  Stephen Spence,et al.  An Impact Of Various Shroud Bleed Slot Configurations And Cavity Vanes On Compressor Map Width And The Inducer Flow Field , 2013 .

[3]  F. B. Fisher,et al.  Application of Map Width Enhancement Devices to Turbocharger Compressor Stages , 1988 .

[4]  Masahiro Ishida,et al.  Effect of Pre-Whirl on Unstable Flow Suppression in a Centrifugal Impeller With Ring Groove Arrangement , 2006 .

[5]  H. Mohtar,et al.  Effect of a map width enhancement system on turbocharger centrifugal compressor performance and surge margin , 2011 .

[6]  Abraham Engeda The unsteady performance of a centrifugal compressor with different diffusers , 2001 .

[7]  M Coppinger,et al.  Performance prediction of an industrial centrifugal compressor inlet guide vane system , 2000 .

[8]  R. Emmrich,et al.  Numerical and experimental investigation of a centrifugal compressor with an inducer casing bleed system , 2001 .

[9]  D. Japikse Centrifugal compressor design and performance , 1996 .

[10]  Hideaki Tamaki,et al.  Stability Improvement of High-Pressure-Ratio Turbocharger Centrifugal Compressor by Asymmetrical Flow Control-Part II: Nonaxisymmetrical Self-Recirculation Casing Treatment. , 2013, Journal of turbomachinery.

[11]  Naresh K. Amineni,et al.  A centrifugal compressor stage with wide flow range vaned diffusers and different inlet configurations , 2002 .