The Basic Thermodynamics of Turbine Cooling

Author:

Horlock J. H.1

Affiliation:

1. Whittle Laboratory, Engineering Department, Cambridge University, United Kingdom

Abstract

Analyses of gas turbine plant performance, including the effects of turbine cooling, are presented. The thermal efficiencies are determined theoretically, assuming air standard (a/s) cycles, and the reductions in efficiency due to cooling are established; it is shown that these are small, unless large cooling flows are required. The theoretical estimates of efficiency reduction are compared with calculations, assuming that real gases form the working fluid in the gas turbine cycles. It is shown from a/s analysis that there are diminishing returns on efficiency as combustion temperature is increased; for real gases there appears to be a limit on this maximum temperature for maximum thermal efficiency.

Publisher

ASME International

Subject

Mechanical Engineering

Reference18 articles.

1. Hawthorne, W. R., and Davis, G. de V., 1956, “Calculating Gas Turbine Performance,” Engineering, 181, p. 361361.

2. Elmasri, M. A. , 1987, “Energy Analysis of Combined Cycles: Part 1—Air-Cooled Brayton-Cycle Gas Turbines,” ASME J. Eng. Gas Turbines Power, 109, pp. 228–235.

3. Chiesa, P., Consonni, S., Lozza, G., and Macchi, E., 1993, “Predicting the Ultimate Performance of Advanced Power Cycles Based on Very High Temperatures,” ASME Paper No. 93-GT-223.

4. MacArthur, C. D., 1999, “Advanced Aero-engine Turbine Technologies and Their Application to Industrial Gas Turbines,” ISABE Paper No. 99-7151, 14th International Symposium on Air-Breathing Engines, Florence, Italy.

5. Horlock, J. H., Watson, D. E., and Jones, T. V., 2000, “Limitations on Gas Turbine Performance Imposed by Large Turbine Cooling Flows,” ASME Paper No. 2000-GT-0635.

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