Temperatures in a Gas Turbine Vaporizer at Near Idle Engine Conditions-Reference-Cited by-同舟云学术

Temperatures in a Gas Turbine Vaporizer at Near Idle Engine Conditions

Published:1995-04-01 Issue:2 Volume:117 Page:302-306
ISSN:0742-4795
Container-title:Journal of Engineering for Gas Turbines and Power
language:en
Short-container-title:

Author:

Vaskopulos T.¹,Polymeropoulos C. E.¹,Sernas V.¹

Affiliation:

1. Department of Mechanical and Aerospace Engineering, Rutgers University, Piscataway, NJ 08855

Abstract

The work is a laboratory investigation of the effect of different liquids and liquid flow rates on the metal temperature of a gas turbine T vaporizer. Most of the experimentation was carried out using JP5. A limited number of runs using Diesel Fuel Marine and calibration runs using water provided additional data for different fluids. Conditions that approach local liquid depletion inside the vaporizer were identified by monitoring local overheating of the vaporizer metal. Because of apparatus limitations, testing was carried out only at vaporizer pressure and liquid flow rates approaching idle engine operation. An experimental correlation was developed allowing estimation of the mean vaporizer temperature as a function of input conditions and fluid properties.

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/117/2/302/5747526/302_1.pdf

Reference13 articles.

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2. CRC Inc., 1983, Aviation Fuel Properties, 3rd ed., Atlanta, GA.

3. Hewitt, G. F., 1982, “Burnout,” Handbook of Multiphase Systems, G. Hestroni. ed., Hemisphere, Washington, DC, pp. 6–66.

4. Jasuja, A. K., and Low, H. C., 1988, “Spray Performance of a Vaporizing Fuel Injector,” AGARD Conference on Combustion and Fuels in Gas Turbine Engines, CP 422.

5. Lefebvre, A., 1983, Gas Turbine Combustion, McGraw-Hill, Washington, DC.