The protection of hot structures in modern turbine engines significantly relies on thermal
barrier coatings (TBCs). Considering the growing demand for enhanced gas turbine …

This work focuses on phase, thermo-physical property, microstructure, lifetime, and failure
behaviour of GdZrPrO/YSZ/NiCoCrAlYHf TBCs by EB-PVD. The thermal property of GdZrPrO …

Today's competitive world economy is creating an indispensable demand for increased
efficiency of engineering components that operate in harsh environments (ie, very high …

Abstract Thermal Barrier Coatings (TBCs) are generally used in both industrial gas turbines
and aircraft engines. In this study, metal powders with CoNiCrAlY content were coated on …

Hot corrosion and oxidation cause very destructive damage in thermal barrier coatings
(TBCs) during service conditions. In hot corrosion, TBCs exposed to molten salts lose their …

La 2 Zr 2 O 7 coatings are promising candidates to substitute YSZ coatings in advanced gas
turbine engines. In this work, Sm-doped La 2 Zr 2 O 7 coatings were deposited by physical …

A high temperature aggressive environment is a great challenge for the long lifetime of
thermal barrier coatings (TBCs). In this study, the hot corrosion and isothermal oxidation …

This study employs cold spraying technology to introduce supersonic-YSZ ceramic particle
impacts onto the bond coat, enabling control the coating structure and interface morphology …

The durability and service performance of thermal barrier coatings (TBCs) is influenced by
its microstructure. One type of yttria stabilized zirconia coating containing irregular …

Abstract The Gd 2 Zr 2 O 7 ceramic material is a promising candidate for thermal barrier
coatings. In this work, Sm-doped Gd 2 Zr 2 O 7 coating was deposited by electron beam …