Effects of Cooling Air on Performance of Turbine Blade Based on CHT Simulation

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Abstract:

A numerical model for conjugate heat transfer (CHT) simulation is established for a turbine blade with air cooling, and 3D heat transfer simulation is accomplished. Effects of different amount of cooling air on the surface temperature distribution, work, efficiency of turbine blade is studied. The results show that the surface temperature drops quickly with the increase of cooling air at beginning and then become mild, the blade work goes up, the efficiency goes down.

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184-187

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June 2012

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© 2012 Trans Tech Publications Ltd. All Rights Reserved

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[1] C. Tadeusz, W. Wlodzimierz, N. Grzegorz, et ac, Coupled analysis of cooled gas turbine blades [R], ASME GT-2003- 38657.

Google Scholar

[2] K. Karsten, B. Dieter, S. Takao, et al, Conjugate calculations for a film-cooled blade under different operating conditions[R]. ASME GT-2004- 53719.

Google Scholar

[3] K. Karsten, B. Dieter, S. Takao, et al, Improvement of a film-cooled blade by application of the conjugate calculation technique[R], ASME GT-2005- 68555.

Google Scholar

[4] A. Sergio, V. Tom, R. Braembussche, et al, Desigh and optimization of the internal cooling channels of a high pressure turbin blade –partⅠ: methodology, J. Turbomachinery. 132(2010) 0201013-1-0201013-7.

Google Scholar

[5] D. Sushant, Y. Savas, Film cooling calculations with an iterative conjugate heat transfer approach using empirical heat transfer coefficient corrections [R], ASME GT-2010-22958.

DOI: 10.1115/gt2010-22958

Google Scholar

[6] L. D. Hylton, M. S. Milhec, Turner E R, eta . Analytical and experimental evaluation of the heat transfer distribution over the surface of turbine vanes[R], NASA-CR-168015, (1983).

Google Scholar

[7] D. Bohn, T. Heuer. Conjugate flow and heat transfer calculations of a high-pressure turbine nozzle guide vane[R], AIAA-2001-3304.

DOI: 10.2514/6.2001-3304

Google Scholar

[8] J. William, Three-dimensional conjugate heat transfer simulation of an internally-cooled gas turbine vane [R], ASME GT-2003- 38551.

DOI: 10.1115/gt2003-38551

Google Scholar