Skip to main content

Advertisement

Log in

Numerical simulation of tip clearance flow passive control in axial turbine

  • Published:
Journal of Thermal Science Aims and scope Submit manuscript

Abstract

This paper focuses on the effects of five different passive turbine tip clearance flow control methods on the tip clearance flow physics, which consists of a partial suction side squealer tip, a double squealer tip, a pressure side tip shelf with inclined squealer tip on a double squealer tip, a tip platform extension edge in pressure side and in suction side respectively. A pressure-correction based, 3D Reynolds-averaged Navier-Stokes equations CFD code with Reynolds Stress Model was adopted. The variable specific heat was considered. The detailed tip clearance flow field with different squealer rims was described with the streamline and the velocity vector. Accordingly, the mechanisms of five passive controls were elucidated; the effects of the passive controls on turbine efficiency and tip clearance flow field were illuminated. The results showed that the secondary flow loss near the outer casing including the tip leakage losses and the passage vortex losses could be reduced in all the five passive control methods. The turbine efficiency could be increased via the rational passive turbine tip clearance flow control. The Improved PS Squealer had the best effect on turbine efficiency, and the efficiency increased by 0.215%.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

References

  1. Huitao Yang, Hamn-Ching Chen, Je-Chin Han. Flow and Heat Transfer Prediction on Turbine Rotor with Various Tip Configurations. AIAA 2005-573.

  2. Huitao Yang, Sumanta Acharya, Srinath V. Ekkad. Numerical Simulation of Flow and Heat Transfer past a Turbine Blade with a Squealer-Tip. ASME GT-2002-30193.

  3. Ameri, A.A., Steinthorsson, E., Rigby, D.L., 1999, Effects of Tip Clearance and Casing Recess on Heat Transfer and Stage Efficiency in Axial Turbines. Journal of Turbomachinery, 121, pp. 683–693.

    Article  Google Scholar 

  4. Ameri, A.A., 2001, Heat Transfer and Flow on the Blade Tip of a Gas Turbine Equipped with a Mean-Camberline Strip. Journal of Turbomachinery, 123, pp. 704–708.

    Article  Google Scholar 

  5. Azad, GM S., Han, J.C., Bunker, R.S., Lee, C.P., 2002, Effect of Squealer Geometry Arrangement on a Gas Turbine Blade Tip Heat Transfer. Journal of Heat Transfer, 124, pp. 452–459.

    Article  Google Scholar 

  6. Papa, M., Goldstein, R.J., Gori, F., 2002, Effects of Tip Geometry and Tip Clearance on the Mass/Heat Transfer From a Large-Scale Gas Turbine Blade. ASME GT-2002-30192.

  7. Kwak, J.S., Ahn J., Han, J.C., Lee, C.P., Boyle, R., Gaugler, R., 2003, Heat Transfer Coefficient on the Squealer Tip and Near Tip Region of a Gas Turbine Blade with Single Squealer. ASME GT2003-38907.

  8. Kwak, J.S., Ahn J., Han, 2002, Heat Transfer Coefficient on a Gas Turbine Blade Tip and Near Tip Regions. AIAA-2002-3012.

  9. Kwak, J.S., Ahn J., Han, 2002, Heat Transfer Coefficient on the Squealer Tip and Near Squealer Tip Regions of a Gas Turbine Blade. IMECE 2002-31109.

  10. Cengiz Camci, Debashis Dey, Levent Kavurmacioglu. 2003 Tip Leakage Flows near Partial Squealer Rims in an Axial Flow Turbine Stage. ASME GT2003-38979.

  11. Azad, Gm.S., Han, J.C., Boyle, R.J. 2000 Heat Transfer and Flow on the Squealer Tip of a Gas Turbine Blade. ASME 2000-GT-195.

  12. Debashis Dey, Cengiz Camci. 2001 Aerodynamic Tip Desensitization of an Axial Turbine Rotor using Tip Platform Extensions. ASME 2001-GT-0484.

  13. C. Prakash, C.P. Lee, D.G. Cherry, R. Doughty, A.R. Wadia. Analysis of Some Improved Blade Tip Concepts. Journal of Turbomachinery. 2006, Vol.128, 639–642.

    Article  Google Scholar 

  14. Xinwen Xiao, Andrew A. McCarter, Budugur Lakshminarayana. 2000 Tip clearance effects in a turbine rotor. Part: I Pressure field and loss. ASME 2000-GT-0476.

  15. D.J.L. Smith, I.H. Johnston. Investigations on an Experimental Single-stage Turbine of Conservative Design[R]. Reports and Memoranda No.3541. 1967.

  16. LI Wei, QIAO Wei-yang, XU Kai-fu, LUO Hua-ling. Numerical simulation of tip leakage flows for different Reynolds numbers in turbine. Journal of Propulsion Technology, 2007, Vol.28, 4.

    Google Scholar 

  17. Wu Yan-hui. Numerical Investigation on End-wall Secondary Flows in Axial Flow Compressors. PhD Dissertation, 2003, Northwestern Polytechnical University. pp.51–52.

Download references

Author information

Authors and Affiliations

Authors

Rights and permissions

Reprints and permissions

About this article

Cite this article

Li, W., Qiao, Wy., Xu, Kf. et al. Numerical simulation of tip clearance flow passive control in axial turbine. J. Therm. Sci. 17, 147–155 (2008). https://doi.org/10.1007/s11630-008-0147-1

Download citation

  • Received:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s11630-008-0147-1

Keywords

Navigation