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TECHNICAL PAPERS: Gas Turbines: Industrial and Cogeneration

A Feasibility Study of Existing Gas Turbines for Recuperated, Intercooled, and Reheat Cycle

[+] Author and Article Information
R. Bhargava

Universal Ensco, Inc., 1811 Bering Drive, Houston, TX 77057

M. Bianchi, A. Peretto

P. R. Spina

DIEM–University of Bologna, Viale Risorgimento 2, 40136 Bologna, Italy

J. Eng. Gas Turbines Power 126(3), 531-544 (Aug 11, 2004) (14 pages) doi:10.1115/1.1707033 History: Received December 01, 2001; Revised March 01, 2002; Online August 11, 2004
Copyright © 2004 by ASME
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References

Oganowski, G., 1990, “GE LM-6000 Development of the First 40% Thermal Efficiency Gas Turbine,” GE Marine & Industrial Engines Publication GE817.
Imwinkelried, B., 1994, “ABB’s Advanced Gas Turbines GT-24/GT-26: How the Most Efficient Gas Turbine Family was Tested and Validated in a 4-Year Program,” Technical Paper Presented at PowerGen ’94 AMERICAS, Dec. 7–9, Orlando, FL.
Michael,  V., 1995, “A Turbine for Tomorrow’s Navy,” Mech. Eng. (Am. Soc. Mech. Eng.), Sept. pp. 70–73.
El-Masri, M. A., 1987, “Thermodynamics and Performance Projections for Intercooled/Reheat/Recuperated Gas Turbine Systems,” ASME Paper No. 87-GT-108.
Macchi, E., Bombarda, P., Chiesa, P., Consonni, S., and Lozza, G., 1991, “Gas Turbine Based Advanced Cycles for Power Generation. Part B: Performance Analysis of Selected Configurations,” International Gas Turbine Congress, Yokohama, Oct.
Bhargava, R., Bianchi, M., Negri di Montenegro, G., and Peretto, A., 2000, “Thermo-Economic Analysis of an Intercooled, Reheat and Recuperated Gas Turbine for Cogenerative Applications: Part I—Base Load Operation,” ASME Paper No. 2000-GT-0316.
Bhargava, R., Negri di Montenegro, G., and Peretto, A., 2001, “Thermo-economic Analysis of an Intercooled, Reheat and Recuperated Gas Turbine for Cogeneration Applications—Part II: Part-Load,” ASME Paper No. 2001-GT-0207.
Bhargava, R., and Peretto, A., 2001, “A Unique Approach for Thermo-Economic Optimization of an Intercooled, Reheat and Recuperated Gas Turbine for Cogeneration Applications,” ASME Paper No. 2001-GT-0206.
Thermoflex 6 Release 2, 2001, Thermoflow, Inc., Sudbury, MA.
Saravanamuttoo,  H. I. H., and Mac Isaac,  B. D., 1983, “Thermodynamic Models for Pipeline Gas Turbine Diagnostics,” ASME J. Eng. Gas Turbines Power, 105, pp. 875–884.
Kurzke, J., and Riegler, C., 2000, “A New Map Scaling Procedure for Preliminary Conceptional Design of Gas Turbines,” ASME Paper No. 2000-GT-0006.
Cumpsty, N. A., 1989, Compressor Aerodynamics, Longman, London.
Cohen, H., Rogers, G. F. C., and Saravanamuttoo, H. I. H., 1999, Gas Turbine Theory, 4th Ed., Longman, London.
Freeman, C., and Dawson, R. E., 1983, “Core Compressor Developments for Large Civil Jet Engines,” Proceedings, International Gas Turbine Congress, Tokyo, Japan, Oct., Paper No. 83-Tokyo-IGTC-46.
Wisler, D. C., 1988, “Advanced Compressor and Fan Systems,” GE Aircraft Engines, Cincinnati, OH.
Howell,  A. R., and Bonham,  R. P., 1950, “Overall and Stage Characteristics of Axial Flow Compressors,” Proc. Inst. Mech. Eng., 163, pp. 235–248.
Benvenuti, E., Bettocchi, R., Cantore, G., Negri di Montenegro, G., and Spina, P. R., 1993, “Gas Turbine Cycle Modeling Oriented to Component Performance Evaluation From Limited Design or Test Data,” Proceedings, 7th ASME COGEN–TURBO, Bournemouth, UK, IGTI, Atlanta, 8 , pp. 327–337.
Benvenuti, E., and Gusso, R., 1985, “Design and Development of the PGT10 Heavy-Duty Advanced Gas Turbine,” ASME Paper No. 85-IGT-21.
Bianchi, D., Noccioni, P., and Silvestri, C. J., 2000, “The New PGT5B/2, a State-of-the-Art 6MW Two-Shaft Gas Turbine,” ASME Paper No. 2000-GT-0561.
Smith,  S. F., 1965, “A Simple Correlation of Turbine Efficiency,” J. R. Aeronaut. Soc.,69, pp. 467–470.
Ainley, D. G., and Mathieson, G. C. R., 1951, “A Method of Performance Estimation for Axial Flow Turbines,” Aeronautical Research Council, R&M 2974.

Figures

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Schematic layout of the Alstom GT-24 gas turbine
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Schematic layout of the GE LM-6000 gas turbine
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Schematic layout of the Mitsubishi-Rolls-Royce WR-21 gas turbine
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Smith diagram, 20, with points representative of GE-Nuovo Pignone gas turbine stages, 1819
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Schematic layouts of modified Alstom GT-24 compressors: (a) nonrecuperated case with LPC redesigned; (b) recuperated case with LPC redesigned; (c) nonrecuperated case with HPC redesigned; (d) recuperated case with HPC redesigned
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(a) Schematic layout of the modified GE LM-6000 GT (nonrecuperated ICRH cycle); (b) Schematic layout of the modified GE LM-6000 GT (recuperated ICRH cycle)
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LM-6000 HP compressor maps and modification of its working point, 9
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Schematic layouts of modified Mitsubishi-Rolls-Royce WR-21 with reheat combustor inserted between LPT and PT
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Schematic layouts of modified Mitsubishi-Rolls-Royce WR-21 with reheat combustor inserted between HPT and LPT
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Compressor stage schematic layout and corresponding velocity triangles
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Turbine stage schematic layout and corresponding velocity triangles

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