Meier, S.M. and Gupta, D.K. (1992) The Evolution of Thermal Barrier Coatings in Gas Turbine Engine Applications. Proceedings of the ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition, Cologne, 1-4 June 1992.
https://doi.org/10.1115/92-GT-203

has been cited by the following article:

• TITLE: Study on the Attack of Molten Silicates on Plasma-Sprayed Thermal Barrier Coatings

  AUTHORS: Roberto Fernando Martins, Karl Friehe, Cecília Chaves Guedes e Silva, Dolores Ribeiro Ricci Lazar, Antônio Augusto Couto, Carlos Roberto Camello Lima

  KEYWORDS: Thermal Barrier Coatings, Molten Silicates, Thermal Spray

  JOURNAL NAME: Journal of Minerals and Materials Characterization and Engineering, Vol.11 No.5, September 4, 2023

  ABSTRACT: Thermal barrier coating (TBC) revolutionized the industry by allowing higher operating temperatures for equipment, such as gas turbines in the aeronautical industry. However, at high temperatures, the TBC is exposed to the attack of molten silicates, known as CMAS (Calcium-Magnesium-Alumino-Silicate), which are particles from the environment that infiltrate the TBC, causing delamination. In this study, samples coated with TBC by thermal spray and covered with CMAS were evaluated at temperatures of 1200˚C and 1250˚C. For each temperature, exposure times of 1 h and 5 h were used. Samples with longer exposure time had a considerable volume increase. The main contribution of this work was to demonstrate the non-wettability of the CMAS, even in the 5-h heat treatments, which prevented its infiltration in the deeper regions. The conditions to guarantee the formation of the silicate and its consequent wettability are also discussed.