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A Long-Term Field Test of Advanced Gas Turbine Airfoil Coatings Under a Severe Industrial Environment FREE

[+] Author Affiliations
Kenneth G. Kubarych

Solar Turbines Inc., San Diego, CA

Donald H. Boone

University of California, Berkeley, CA

Richard L. Duncan

Electric Power Research Institute, Palo Alto, CA

Paper No. 84-GT-277, pp. V005T11A007; 9 pages
doi:10.1115/84-GT-277
From:
  • ASME 1984 International Gas Turbine Conference and Exhibit
  • Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; Process Industries; Technology Resources
  • Amsterdam, The Netherlands, June 4–7, 1984
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7950-4
  • Copyright © 1984 by ASME

abstract

Severe hot corrosion of gas turbine blades and vanes can result from the use of fuels contaminated with sodium and sulfur. A program has been initiated to survey currently available commercial as well as advanced developmental hot corrosion resistant coatings and select a list of coatings for application to Solar Centaur first-stage blades and vanes. A subsequent engine test program will be run on high-sulfur marine diesel fuel doped with sodium to produce severe hot corrosion conditions. The coatings will be tested in a rainbow fashion for a period up to 15,000 hours.

Copyright © 1984 by ASME
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