Technical and Economical Aspects of Current Thermal Barrier Coating Systems for Gas Turbine Engines by Thermal Spray and EBPVD: A Review

By A. Feuerstein, J. Knapp, T. Taylor, A. Ashary, A. Bolcavage, N. Hitchman. 2008

391 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Ceramics and Composites, Materials Chemistry

View Paper: https://www.semanticscholar.org/paper/0b329bbbe3a39fb967911fcfcd4802a4e0b61061

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. A. Vardelle
2. P. Fauchais
3. L. Anand
4. K. Loeffel

In Ceramics and Composites

1. P. Fauchais

In Materials Chemistry

1. K. Loeffel
2. P. Fauchais
3. L. Anand
4. A. Vardelle
5. T. P. G. Thamburaja

Citations in the corpus

• Thermal Sprayed Coatings Used Against Corrosion and Corrosive Wear (2012, background): “The second problem is the oxidation of bond coat with the formation of Thermally Grown Oxide (TGO) Feuerstein et al (2008) as well as the bond coat corrosion with oxides such as CMAS (calcium-magnesium-alumino- www.intechopen.com Advanced Plasma Spray Applications 26 silicate) Li et al (2010), Vasse”
• A chemo-thermo-mechanically coupled theory for elastic–viscoplastic deformation, diffusion, and volumetric swelling due to a chemical reaction (2011, background): “…two layers: (a) a metallic layer, or bond-coat (BC), deposited on the superalloy — the bond coat is typically an alloy based on Ni(Al) with various additions (such as Cr, Co, Pt, Y, and Hf); and (b) an yttria-stabilized-zirconia (YSZ) top-coat deposited on the bond-coat (Feuerstein et al., 2008).”