A number of commercially available chemical additives for utilization in modern high temperature gas turbines were evaluated for their corrosion and deposit inhibiting characteristics. The evaluation was made in pressurized passages which simulate conditions of operating gas turbines. Initial screening tests of 10 hr each were made with a contaminant level of 50 ppm vanadium, and promising additives were further tested for times up to 300 hr at the more realistic contaminant level of a No. 3 GT fuel. Characteristics of the deposits were studied with x-ray diffraction and ash fusion tests. Corrosion rates for various alloys tested with treated fuel were measured and compared to test results obtained with untreated fuel. Conclusions were drawn as to the type of elements most effective in reducing corrosion caused by combinations of vanadium and sodium. The role of elements in preventing deposit buildup is also assessed.
Skip Nav Destination
Article navigation
October 1973
This article was originally published in
Journal of Engineering for Power
Research Papers
Evaluation of Additives for Prevention of High Temperature Corrosion of Superalloys in Gas Turbines
S. Y. Lee,
S. Y. Lee
Westinghouse Research Laboratories, Pittsburgh, Pa.
Search for other works by this author on:
W. E. Young,
W. E. Young
Westinghouse Research Laboratories, Pittsburgh, Pa.
Search for other works by this author on:
G. Vermes
G. Vermes
Westinghouse Gas Turbine Systems Division, Lester, Pa.
Search for other works by this author on:
S. Y. Lee
Westinghouse Research Laboratories, Pittsburgh, Pa.
W. E. Young
Westinghouse Research Laboratories, Pittsburgh, Pa.
G. Vermes
Westinghouse Gas Turbine Systems Division, Lester, Pa.
J. Eng. Power. Oct 1973, 95(4): 333-339 (7 pages)
Published Online: October 1, 1973
Article history
Received:
November 16, 1972
Online:
July 14, 2010
Article
Article discussed|
View article
Connected Content
Citation
Lee, S. Y., Young, W. E., and Vermes, G. (October 1, 1973). "Evaluation of Additives for Prevention of High Temperature Corrosion of Superalloys in Gas Turbines." ASME. J. Eng. Power. October 1973; 95(4): 333–339. https://doi.org/10.1115/1.3445740
Download citation file:
Get Email Alerts
Cited By
Experimental Characterization of Superheated Ammonia Spray From a Single-Hole Spray M Injector
J. Eng. Gas Turbines Power (August 2025)
Foreign Object Damage of Environmental Barrier Coatings Subjected to CMAS Attack
J. Eng. Gas Turbines Power (October 2025)
Related Articles
Hot Corrosion of Gas Turbine Components
J. Eng. Power (January,1979)
Environmental Effects on the High-Temperature Corrosion of Superalloys in Present and Future Gas Turbines
J. Eng. Power (April,1972)
Case Studies of Fatigue Life Improvement Using Low Plasticity Burnishing in Gas Turbine Engine Applications
J. Eng. Gas Turbines Power (October,2006)
Influence of Carbon Content in Cobalt-Based Superalloys on Mechanical and Wear Properties
J. Eng. Mater. Technol (April,2004)
Related Proceedings Papers
Related Chapters
Operation of Gas Turbines on ASTM 3-GT Fuel
Manual on Requirements, Handling, and Quality Control of Gas Turbine Fuel
Chemical Redistribution of Alloying Elements in Growing Oxides Formed on Irradiated Zr-Nb-Fe Alloys and Its Implication on Corrosion
Zirconium in the Nuclear Industry: 20th International Symposium
E110opt Fuel Cladding Corrosion under PWR Conditions
Zirconium in the Nuclear Industry: 20th International Symposium