Results 291 to 300 of about 268,967 (357)
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The hydrogenation mechanism of PtAl and IrAl thermal barrier coatings from first-principles investigations

, 2020
In addition to oxidation resistance, the improvement of hydrogen embrittlement is also a big challenge for the noble metal thermal barrier coating. Unfortunately, the hydrogenation mechanism of noble metal thermal barrier coating is unknown.
Yong Pan, W. Guan
semanticscholar   +1 more source

Ceramic thermal barrier coatings

Industrial & Engineering Chemistry Product Research and Development, 1984
Revue des recherches entreprises depuis les annees 50. Le developpement, dans les turbines a gaz, de ces revetements est du a l'amelioration des procedes d'utilisation et a l'analyse de leurs proprietes.
Curt H. Liebert, Robert A. Miller
openaire   +1 more source

CMAS corrosion of YSZ thermal barrier coatings obtained by different thermal spray processes

, 2020
Degradation of yttria-stabilized zirconia (YSZ) layers by molten CaO-MgO-Al2O3-SiO2 (CMAS)-based deposits is an important failure mode of thermal barrier coating (TBC) systems in modern gas turbines.
S. Morelli   +6 more
semanticscholar   +1 more source

Calcia–magnesia–alumina–silicate (CMAS) attack mechanisms and roadmap towards Sandphobic thermal and environmental barrier coatings

International Materials Reviews, 2020
This review critically examines the current understanding of calcia–magnesia–alumina–silicate (CMAS) degradation mechanisms and mitigation approaches in thermal and environmental barrier coatings.
A. Nieto   +5 more
semanticscholar   +1 more source

Thermal barrier coatings for high temperature applications – A short review

Materials Today: Proceedings, 2020
This review paper aims to portray the work done by various researchers in the domain of thermal barrier coatings. Thermal barrier coatings (TBCs) are provided to minimize the temperature of components in the field of aviation and power generation sector ...
D. Chellaganesh, M. A. Khan, J. Jappes
semanticscholar   +1 more source

Latest Advancements in Thermal Barrier Coatings

Canadian Aeronautics and Space Journal, 2004
As gas turbine engine designers strive to increase engine efficiency, thrust, and higher turbine inlet temperatures, the substrate superalloys are pushed to their upper limits of thermal stability. For this reason, thermal barrier coatings, with a typical composition of ZrO2-7%Y2O3, were developed and applied to the metallic substrate for added ...
Patnaik, P. C., Wang, D., Huang, X.
openaire   +2 more sources

A novel strategy to control the microstructure of plasma-sprayed YSZ thermal barrier coatings

, 2020
The properties of coating materials can be improved via microstructural design. This study proposed a structure control strategy for plasma sprayed YSZ coatings.
Ji Bo Huang   +6 more
semanticscholar   +1 more source

Composition, mechanical properties and thermal cycling performance of YSZ toughened La2Ce2O7 composite thermal barrier coatings

, 2020
Poor fracture toughness of La2Ce2O7 (LC) seriously prevents its practical applications as thermal barrier coatings. In this study, 8 wt% yttria stabilized zirconia (YSZ) was introduced to toughen the plasma-sprayed LC coatings. The mechanical performance,
Hao Zhang   +11 more
semanticscholar   +1 more source

Thermal conductivity of thermal barrier coatings

Materials Science and Engineering: A, 1998
Abstract In thermal barrier coatings and other ceramic oxides, heat is conducted by lattice waves, and also by a radiative component which becomes significant at high temperatures. The theory of heat conduction by lattice waves is reviewed in the equipartition limit (above room temperature).
P.G. Klemens, M. Gell
openaire   +1 more source

Thermal Strain-Tolerant Abradable Thermal Barrier Coatings

Journal of Engineering for Gas Turbines and Power, 1991
Thermal barrier coatings (TBCs) are applied to hot gas path surfaces to reduce metal temperatures and thermal stresses for improved turbine component durability. Improvements in engine performance are achieved when TBCs enable reductions in cooling air usage and turbine blade tip-shroud clearances.
openaire   +1 more source

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