Inlet Fogging of Gas Turbine Engines—Part I: Fog Droplet Thermodynamics, Heat Transfer, and Practical Considerations

Author:

Chaker Mustapha,Meher-Homji Cyrus B.1,Mee Thomas1

Affiliation:

1. Gas Turbine Division, Mee Industries, Inc., 204 West Pomona Avenue, Monrovia, CA 91016

Abstract

The inlet fogging of gas turbine engines for power augmentation has seen increasing application over the past decade yet not a single technical paper treating the physics and engineering of the fogging process, droplet size measurement, droplet kinetics, or the duct behavior of droplets, from a gas turbine perspective, is available. This paper provides the results of extensive experimental and theoretical studies conducted over several years coupled with practical aspects learned in the implementation of nearly 500 inlet fogging systems on gas turbines ranging in power from 5 to 250 MW. Part I of the paper covers the underlying theory of droplet thermodynamics and heat transfer, and provides several practical pointers relating to the implementation and application of inlet fogging to gas turbine engines.

Publisher

ASME International

Subject

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

Reference25 articles.

1. Meher-Homji, C. B., and Mee, T. R., 1999, “Gas Turbine Power Augmentation by Fogging of Inlet Air,” Proceedings of the 28th Turbomachinery Symposium, Houston, TX, Sept.

2. Meher-Homji, C. B., and Mee, T. R., 2000, “Inlet Fogging of Gas Turbine Engines—Part II: Practical Considerations, Control and O&M Aspects,” ASME Paper No. 2000-GT-0308.

3. Bhargava, R., and Meher-Homji, C. B., 2002, “Parametric Analysis of Existing Gas Turbines With Inlet Evaporative and Overspray Fogging,” ASME Paper No. 2002-GT-30560.

4. Kleinschmidt, R. V., 1946, “The Value of Wet Compression in Gas Turbine Cycles,” Annual Meeting of the ASME, Dec. 2–6.

5. Wilcox, E. C., and Trout, A. M., 1951, “Analysis of Thrust Augmentation of Turbojet Engines by Water Injection at the Compressor Inlet Including Charts for Calculation Compression Processes With Water Injection,” NACA Report No. 1006.

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