Progress in Thermal Barrier Coatings (Progress in Ceramic by The) ACerS (American Ceramics Society

By The) ACerS (American Ceramics Society

This version of the development in Ceramic know-how sequence compiles articles released on thermal barrier coatings (TBCs) through the yankee Ceramic Society (ACerS). It collects in a single source the present examine papers on materials-related points of thermal barrier coatings and linked applied sciences.

Logically equipped and thoroughly chosen, the papers during this version divide into six categories:

  • Applications
  • Material advancements and Novel Compositions
  • Developments in Processing
  • Mechanical Properties
  • Thermal Properties

Citations stick to each one name within the desk of contents, making this a key source for execs and academia.

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Additional info for Progress in Thermal Barrier Coatings (Progress in Ceramic Technology)

Example text

T h e design surface temperature for selected components is expected to exceed the 1414oC (2577°F) melting point of silicon, a key CMC constituent, and thus protective coatings are required. This paper discusses challenges in developing the coating system, specifically addressing issues related to the selection of materials, designing the coating architecture, and the test methodology. Introduction terial technology into turbine engines has been studied at GE Aircraft Engines over the last 10 years.

New chemistries for TBC a p plicattons need to meet the following requirements: - Thermal stability and chemical inertia at high temperature. - Chemical and mechanical compatibility with a metallic bond coat layer. - Manufacturability, best by use of existing coating technologies. g. by increasing the total amo~nlof stabikizer). - Partial (or total) substitution of‘Y and/or Zr ions with ions of different mass andor different ionic radius (mainly rare-earth metals). Based on these considerations new zirconia based TBC compositions manufactured by EBPVD were chosen as the prime candidate materials in this study.

Leger and P, Bengtsson (volvo Aero), F. Jansen and R. Damani (Sulzer Innotec), G. Marijnisen (Sulzer Coatings). Funding from the European commission within the 4th FWP under guidance of R. Simonini is highly acknowledged. References [ I ] 0. , "Microstructural charactenisation of plasma sprayed thermal barrier coatings by qunntitstlve image analysis", Quantitative Microscopy of High Tcmperaturc Materials, ed. J. Cawley, Shefield, UK,: 10M Communications L@ (2001), 131-44. 121 U. Schulz, J. MUnzer.

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