Gas Turbine Fogging Technology: A State-of-the-Art Review—Part II: Overspray Fogging—Analytical and Experimental Aspects-Reference-Cited by-同舟云学术

Gas Turbine Fogging Technology: A State-of-the-Art Review—Part II: Overspray Fogging—Analytical and Experimental Aspects

Published:2006-02-01 Issue:2 Volume:129 Page:454-460
ISSN:0742-4795
Container-title:Journal of Engineering for Gas Turbines and Power
language:en
Short-container-title:

Author:

Bhargava R. K.¹,Meher-Homji C. B.²,Chaker M. A.²,Bianchi M.³,Melino F.³,Peretto A.³,Ingistov S.⁴

Affiliation:

1. 22515 Holly Lake Drive, Katy, TX 77450

2. Bechtel Corporation, 3000 Post Oak Boulevard, Houston, TX 77056

3. University of Bologna, DIEM, Facolta di Ingegneria, Viale Risorgimento 2, Bologna 40136, Italy

4. Watson Cogeneration Co./BP, 11850 S. Wilmington Avenue, P. O. Box 6203, Carson, CA 90749

Abstract

The strong influence of ambient temperature on the output and heat rate on a gas turbine has popularized the application of inlet fogging and overspray for power augmentation. One of the main advantages of overspray fogging is that it enhances power output as a result of decrease in compression work associated with the continuous evaporation of water within the compressor due to fog intercooling. A comprehensive review on the current understanding of the analytical and experimental aspects of overspray fogging technology as applied to gas turbines is presented in this paper.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Link

http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/129/2/454/5586852/454_1.pdf

Reference24 articles.

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2. Gas Turbine Fogging Technology: A State-of-the-Art Review—Part III: Practical Considerations and Operational Experience;Bhargava;ASME J. Eng. Gas Turbines Power

3. Value of Wet Compression in Gas-Turbine Cycles;Kleinschmidt;Mech. Eng. (Am. Soc. Mech. Eng.)

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 Processes With Water Injection,” NACA Report No. 1006.

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