0
TECHNICAL PAPERS: Gas Turbines: Controls, Diagnostics, and Instrumentation

Model Development and Simulation of Transient Behavior of Heavy Duty Gas Turbines

[+] Author and Article Information
J. H. Kim

Turbo and Power Machinery Research Center, Seoul National University, Seoul 151-742, Korea

T. W. Song, S. T. Ro

School of Mechanical Engineering, Seoul National University, Seoul 151-742, Korea

T. S. Kim

Department of Mechanical Engineering, Inha University, Inchon 402-751, Korea

J. Eng. Gas Turbines Power 123(3), 589-594 (Oct 01, 2000) (6 pages) doi:10.1115/1.1370973 History: Received October 01, 1999; Revised October 01, 2000
Copyright © 2001 by ASME
Your Session has timed out. Please sign back in to continue.

References

Fawke, A. J., and Saravanamuttoo, H. I. H., 1971, “Digital Computer Methods for Prediction of Gas Turbine Dynamic Response,” SAE Paper 710550.
Rowen,  W. I., 1983, “Simplified Mathematical Representations of Heavy-Duty Gas Turbines,” ASME J. Eng. Power, 105, pp. 865–869.
Crosa, G., Ferrari, G., and Trucco, A., 1995, “Modeling and Recoupling the Control Loops in a Heavy-Duty Gas Turbine Plant,” ASME Paper 95-GT-61.
Korakianitis, T., Hochstein, J. I., and Zou, D., 1993, “Prediction of the Transient Thermodynamic Response of a Closed-Cycle Regenerative Gas Turbine,” ASME Paper 93-GT-136.
Schobeiri,  M. T., Attia,  M., and Lippke,  C., 1994, “GETRAN: A Generic, Modularly Structured Computer Code for Simulation of Dynamic Behavior of Aero- and Power Generation Gas Turbine Engines,” ASME J. Eng. Gas Turbines Power, 116, pp. 483–494.
Crosa,  G., Pittaluga,  F., Trucco,  A., Beltrami,  F., Torelli,  A., and Traverso,  F., 1998, “Heavy-Duty Gas Turbine Plant Aerothermodynamic Simulation Using Simulink,” ASME J. Eng. Gas Turbines Power, 120, pp. 550–556.
Badmus,  O. O., Eveker,  K. M., and Nett,  C. N., 1995, “Control-Oriented High-Frequency Turbomachinery Modeling: General One-Dimensional Model Development,” ASME J. Turbomach., 117, pp. 320–335.
Cohen, H., Rogers, G. F. C., and Saravanamutto, H. I. H., 1996, Gas Turbine Theory, 4th Ed., Longman Group Limited, U.K.
Stone,  A., 1958, “Effects of Stage Characteristics and Matching on Axial-Flow-Compressor Performance,” Trans. ASME, 80, pp. 1273–1293.
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, 111, pp. 244–250.
Klapproth, J. F., 1958, discussion in Stone, 9.
Kim, T. S., and Ro, S. T., 1995, “Comparative Evaluation of the Effect of Turbine Configuration on the Performance of Heavy-Duty Gas Turbines,” ASME Paper 95-GT-334.
Kim, J. H., Kim, T. S., Lee, J. S., and Ro, S. T., 1996, “Performance Analysis of a Turbine Stage Having Cooled Nozzle Blades with Trailing Edge Ejection,” ASME Paper 96-TA-12.
Rowen, W. I., 1992, “Simplified Mathematical Representations of Single Shaft Gas Turbines in Mechanical Drive Service,” ASME Paper 92-GT-22.
Hannett,  L. N., and Khan,  A., 1993, “Combustion Turbine Dynamic Model Validation from Tests,” IEEE Trans. On Power Systems,8, No. 1, pp. 152–158.
Cyrus, V., 1994, “Separated Flows in Axial Flow Compressor with Variable Stator Vanes at Positive Incidence Angles,” ASME Paper 94-GT-480.
Iwamoto, T., Ikesawa, K., Kanayama, T., Nagai, K., Yukinari, A., and Nakagawa, T., 1991, “Development of a High-Pressure Ratio Axial Flow Compressor,” Proceedings of the 1991 Yokohama International Gas Turbine Congress, Vol. II, Gas Turbine Society of Japan (GTSJ), pp. 79–86.
Kashiwabara,  Y., Matsuura,  Y., Katoh,  Y., Hagiwara,  N., Hattori,  T., and Tokunaga,  K., 1986, “Development of a High-Pressure-Ratio Axial Flow Compressor for a Medium-Size Gas Turbine,” ASME J. Turbomach., 108, pp. 233–239.
Jansen,  M., Schulenberg,  T., and Waldinger,  D., 1992, “Shop Test Result of the V64.3 Gas Turbine,” ASME J. Eng. Gas Turbines Power, 114, pp. 676–681.

Figures

Grahic Jump Location
Comparison of corrected stage characteristics by Eq. (10) with experimental data (lines: prediction, marks: experimental data from 16)
Grahic Jump Location
Predicted characteristics of an axial flow compressor with fixed geometry (data from 17)
Grahic Jump Location
Predicted characteristics of an axial flow compressor with variable geometry (data from 18)
Grahic Jump Location
Block diagram for the speed and target temperature control
Grahic Jump Location
Predicted off-design performance data compared with engine data for part-load operation of V64.3 (lines: prediction, marks: data from 19)
Grahic Jump Location
Predicted off-design performance data of GE 7F engine
Grahic Jump Location
Comparison of simulated transient behavior of GE 7F engine with real operation data: (a) developed power, (b) rpm deviation, (c) fuel flow rate, (d) firing temperature, (e) turbine exhaust temperature, (f) VIGV angle

Tables

Errata

Discussions

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In