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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

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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