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TECHNICAL PAPERS: Gas Turbines: Pipelines and Applications

Degradation in Gas Turbine Systems

[+] Author and Article Information
R. Kurz, K. Brun

Solar Turbines Incorporated, San Diego, CA 92123

J. Eng. Gas Turbines Power 123(1), 70-77 (Nov 01, 2000) (8 pages) doi:10.1115/1.1340629 History: Received February 01, 2000; Revised November 01, 2000
Copyright © 2001 by ASME
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References

Diakunchak, I. S., 1991, “Performance Degradation in Industrial Gas Turbines,” ASME Report No. 91-GT-228.
Brun, K., and Kurz, R., 1998, “Measurement Uncertainties Encountered During Gas Turbine Driven Compressor Field Testing,” ASME Report No. 98-GT-1.
Bakken, L. E., and Skorping, R., 1996, “Optimum Operation and Maintenance of Gas Turbines Offshore,” ASME Report No. 96-GT-273.
Bammert,  K., and Sonnenschein,  H., 1967, “Der Einfluss verdickter und verduennter Turbinenschaufeln auf die Gittereigenschaften,” Arch. Eisenhuettenwes., 38, Heft 4, pp. 287–299.
Bammert, K. et al., 1965, “Ueber Korrosion, Erosion and Verschmutzung bei Gichtgasturbinen,” VIK Bericht No. 164, Essen.
Kind, R. J., Serjak, P. J., and Abbott, M. W. P., 1996, “Measurements and Predictions of the Effects of Surface Roughness on Profile Losses and Deviation in a Turbine Cascade,” ASME Report No. 96-GT-203.
Boelcs,  A., and Sari,  O., 1988, “Influence of Deposit on the Flow in a Turbine Cascade,” ASME J. Turbomach., 110, pp. 512–519.
Kurz,  R., 1995, “Effects of Nonuniform Blade Pitch on the Flow Through an Annular Turbine Nozzle,” Int. Rotating Machinery, 2, No. 1, pp. 59–65.
Kurz, R., 1991, “Transonic Flow Through Turbine Cascades With 3 Different Pitch-to-Chord Ratios,” Proc. 10. ISABE, Nottingham.
Schmidt, K. J., 1992, “Experimentelle und theoretische Untersuchungen zum instattionaeren Betriebsverhalten von Gasturbinentriebwerken,” VDI, Duesseldorf.
Milsch, R., 1971, “Systematische Untersuchung ueber den Einfluss der Rauhigkeit von Verdichterschaufeln auf den Gitterwirkungsgrad,” Ph.D. thesis, University of Hannover.
Pinson, M., and Wang, T., 1994, “Effects of Leading-Edge Roughness on Fluid Flow and Heat Transfer in the Transitional Boundary Layer of a Flat Plate,” ASME Report No. 94-GT-326.
Shabbir, A., Celestina, M. L., Adamczyk, J. J., and Strazisar, A. J., 1997, “The Effect of Hub Leakage on Two High Speed Axial Flow Compressor Rotors,” ASME Report No. 97-GT-346.
Khalid, S. A., Khalsa, A. S., Waitz, I. A., Tan, S. C., Greitzer, E. M., Cumpsty, N. A., Adamczyk, J. J., and Marble, F. E., 1998, “Endwall Blockage in Axial Compressors,” ASME Report No. 98-GT-188.
Frith, P. C., 1992, “The Effect of Compressor Rotor Tip Crops on Turboshaft Engine Performance,” ASME Report No. 92-GT-83.
Singh, D., Hamed, A., and Tabakoff, W., 1996, “Simulation of Performance Deterioration in Eroded Compressors,” ASME Report No. 96-GT-422.
Elrod, W. C., King, P. I., and Poniatowsky, E. M., 1990, “Effects of Roughness, Freestream Turbulence, and Incidence Angle on the Performance of a 2-D Compressor Cascade,” ASME Report No. 90-GT-208.
Stalder, J. P., 1998, “Gas Turbine Compressor Washing State of the Art Field Experiences,” ASME Report No. 98-GT-420.
Spakovszky, Z. S., Gertz, J. B., Sharma, O. P., Paduano, J. D., Epstein, A. H., and Greitzer, E. M., 1999, “Influence of Compressor Deterioration on Engine Dynamic Behavior and Transient Stall Margin,” ASME Report No. 99-GT-439.
Boyle,  R. J., 1994, “Prediction of Surface Roughness and Incidence Effects on Turbine Performance,” ASME J. Turbomach., 116, pp. 745–751.
Traupel, W., 1988, Thermische Turbomaschinen, Springer, Berlin.
Radtke, F., and Dibelius, G., 1980, “Reynoldszahleinfluss bei hochbelasteten axialen Turbinenbeschaufelungen,” VDI-Berichte No. 361.
Haq, I. U., Bu-Hazza, A. L., and Al-Baz, K., 1998, “Multistage Centrifugal Compressor Fouling Evaluation at High Power Settings,” ASME Report No. 98-GT-53.
Cohen, H., Rogers, G. F. C., and Saravanamuttoo, H. I. H., 1996, Gas Turbine Theory, Longman, Harlow.
Tarabrin, A. P., Schurovsky, V. A., Bodrov, A. I., and Stalder, J. P., 1998, “Influence of Axial Compressor Fouling on Gas Turbine Unit Performance Based on Different Schemes and With Different Initial Parameters,” ASME Report No. 98-GT-416.
MacLeod, J. D., Taylor, V., and Laflamme, J. C. G., 1991, “Implanted Component Faults and Their Effects on Gas Turbine Engine Performance,” ASME Report No. 91-GT-41.
Aker, G. F., and Saravanamuttoo, H. I. H., 1988, “Predicting the Gas Turbine Performance Degradation due to Compressor Fouling Using Computer Simulation Techniques,” ASME Report No. 88-GT-206.

Figures

Grahic Jump Location
Gas turbine cross section
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Effect of fouling on an axial compressor, comparing a new compressor, a compressor with 0.5 percent fouling on head and efficiency, and a compressor with additionally 1 percent blockage: Pressure ratio
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Effect of fouling on an axial compressor comparing a new compressor, a compressor with 0.5 percent fouling on head and efficiency, and a compressor with additionally 1 percent blockage: Efficiency
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Effect of probe location on the measured average temperature
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Degradation of engine efficiency at full load
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Degradation of engine power output
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Degradation of engine efficiency at constant load
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Effect of detergent washing
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Simulation of effects of detergent washing
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Effect of system degradation on a gas turbine driven pipeline compressor

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