In this paper, a calculation code, developed in house by the authors, able to evaluate the performance of a gas turbine with all possible fogging strategies (high pressure fogging, overspray, and interstage injection) is presented and discussed. The code has a flexible structure and can be applied to evaluate the performance of every commercial gas turbine model. The aim of the calculation code is to overcome the limits of the most widespread commercial software, especially with regard to the two phase flow compression process simulation. The calculation code was validated on results available in the literature showing a good agreement with experimental and theoretical results.
Issue Section:
Gas Turbines: Industrial & Cogeneration
Topics:
Compression,
Compressors,
Gas turbines,
Water,
Pressure,
Temperature,
Drops,
Flow (Dynamics),
Turbines
1.
Tawney
, R.
, Pearson
, C.
, and Brown
, M.
, 2001, “Options to Maximize Power Output for Merchant Plants in Combined Cycle Applications
,” ASME Paper No. 2001-GT-0409.2.
Bianchi
, M.
, Melino
, F.
, Peretto
, A.
, Bhargava
, R. K.
, Chaker
, M. C.
, Ingistov
, S.
, and Meher-Homji
, C. B.
, 2005, “Gas Turbine Fogging Technology: A State of the Art Review, Part I: Inlet and Evaporative Fogging—Analytical and Experimental Aspects
,” ASME Paper No. GT2005-68336.3.
Kleinschmidt
, R. V.
, 1947, “Value of Wet Compression in Gas-Turbine Cycles
,” Mech. Eng. (Am. Soc. Mech. Eng.)
0025-6501, 69
(2
), pp. 115
–116
.4.
Wilcox
, E. C.
, and Trout
, A. M.
, 1951, “Analysis of Thrust Augmentation of Turbojet Engines by Water Injection at Compressor Inlet Including Charts for Calculating Compression Process with Water Injection
,” NACA Report No. 1006.5.
Hill
, P. G.
, 1963, “Aerodynamic and Thermodynamic Effects of Coolant Injection on Axial Compressors
,” Aeronaut. Q.
0001-9259, 1
, pp. 331
–348
.6.
Utamura
, M.
, Kuwahara
, T.
, Murata
, H.
, and Horii
, N.
, 1999, “Effects of Intensive Evaporative Cooling on Performance Characteristics of Land-Based Gas Turbine
,” Proceedings Joint Power Generation Conference
, p. 34
.7.
Horlock
, J. H.
, 2001, “Compressor Performance with Water Injection
,” ASME Paper No. 2001-GT-0343.8.
Zheng
, Q.
, Sun
, Y.
, Li
, S.
, and Wang
, Y.
, 2002, “Thermodynamic Analysis of Wet Compression Process in the Compressor of Gas Turbine
,” ASME Paper No. GT-2002-30590.9.
Hartel
, C.
, and Pfeiffer
, P.
, 2003, “Model Analysis of High-Fogging Effects on the Work of Compression
,” ASME Paper No. GT-2003-38117.10.
White
, A. J.
, and Meacock
, A. J.
, 2003, “An Evaluation of the Effects of Water Injection on Compressor Performance
,” ASME Paper No. GT-2003-38237.11.
Cataldi
, G.
, Gunter
, H.
, Matz
, C.
, McKay
, T.
, Hoffman
, J.
, Nemet
, A.
, Lecheler
, S.
, and Braun
, J.
, 2004, “Influence of High Fogging Systems on Gas Turbine Engine Operation and Performance
,” ASME Paper No. GT2004-53788.12.
Bagnoli
, M.
, Bianchi
, M.
, Melino
, F.
, Peretto
, A.
, Spina
, P. R.
, Bhargava
, R.
, and Ingistov
, S.
, 2004, “A Parametric Study of Interstage Injection on GE Frame 7 EA Gas Turbine
,” ASME Paper No. GT-2004-53042.13.
Ingistov
, S.
, 2001, “Interstage Injection System for Heavy Duty Industrial Gas Turbine Model 7EA
,” ASME Paper No. 2001-GT-407.14.
Ingistov
, S.
, 2002, “Interstage Injection into Axial Compressor, Gas Turbine Model 7EA
,” ASME Paper No. GT-2002-30656.15.
Sparrow
, E. M.
, and Gregg
, J. L.
, 1958, “The Variable Fluid Property Problem in Free Convection
,” Trans. ASME
0097-6822, 80
, 879
–886
.16.
Eckert
, E. R. G.
, and Drake
, R. M.
, Jr., 1959, Heat and Mass Transfer
, 2nd ed., McGraw-Hill
, New York
.17.
Spina
, P. R.
, 2002, “Gas Turbine Performance Prediction by Using Generalized Performance Curves of Compressor and Turbine Stages
,” ASME Paper No. GT-2002-30275.18.
Muir
, D. E.
, Saravanamuttoo
, H. I. H.
, and Marshall
, D. J.
, 1989, “Health Monitoring of Variable Geometry Gas Turbines for the Canadian Navy
,” ASME J. Eng. Gas Turbines Power
0742-4795, 111
, pp. 244
–250
.19.
Howell
, A. R.
, and Bonham
, R. P.
, 1950, “Overall and Stage Characteristics of Axial Flow Compressors
,” Proc. Inst. Mech. Eng.
0020-3483, 163
, pp. 235
–248
.20.
Csanady
, G. T.
, 1964, Theory of Turbomachines
, McGraw-Hill
, New York
.21.
Thermoflow 15, release 1, 2005, Thermoflow Inc., Sudbury, MA.
22.
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
, Vol. 8
, pp. 327
–337
.23.
Bettocchi
, R.
, and Spina
, P. R.
, 1997, “Influence of the Control Logic on Gas Turbine Operation
,” ASME Paper No. 97-AA-127.Copyright © 2008
by American Society of Mechanical Engineers
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