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Schulz, U., Leyans, C., Fritscher, K., Peters, M., Saruhan-Brings, M., Lavigne, O., Dorvaux, J.-M., Poulain, M., Mév- rel, R. and Caliez, M. (2003) Some Recent Trends in Research and Technology of Advanced Thermal Barrier Coatings. Aerospace Science and Technology, 7, 73-80. http://dx.doi.org/10.1016/S1270-9638(02)00003-2
has been cited by the following article:
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TITLE:
Effects of Syngas Particulate Fly Ash Deposition on the Mechanical Properties of Thermal Barrier Coatings on Simulated Film-Cooled Turbine Vane Components
AUTHORS:
Kevin Luo, Andrew C. Nix, Bruce S. Kang, Dumbi A. Otunyo
KEYWORDS:
IGCC Gas Turbine Thermal Barrier Coatings, Coal Syngas, Fly Ash Deposition, Micro-Indentation, Strain Tolerance
JOURNAL NAME:
International Journal of Clean Coal and Energy,
Vol.3 No.4,
November
26,
2014
ABSTRACT: Research is being conducted to study the effects of particulate deposition from contaminants in coal synthesis gas (syngas) on the mechanical properties of thermal barrier coatings (TBC) employed on integrated gasification combined cycle (IGCC) turbine hot section airfoils. West Virginia University (WVU) had been working with US Department of Energy, National Energy Technology Laboratory (NETL) to simulate deposition on the pressure side of an IGCC turbine first stage vane. To model the deposition, coal fly ash was injected into the flow of a combustor facility and deposited onto TBC coated, angled film-cooled test articles in a high pressure (approximately 4 atm) and a high temperature (1560 K) environment. To investigate the interaction between the deposition and the TBC, a load-based multiple-partial unloading micro-indentation technique was used to quantitatively evaluate the mechanical properties of materials. The indentation results showed the Young’s Modulus of the ceramic top coat was higher in areas with deposition formation due to the penetration of the fly ash. This corresponds with the reduction of strain tolerance of the 7% yttria-stabilized zirconia (7YSZ) coatings.