This paper describes the manufacturing method and properties of a superalloy as a gas
turbine blade material and a thermal barrier coating to protect it. The development process …

Modern gas turbines rely on ceramic coatings to protect structural components along the hot
gas path. These coatings are susceptible to accelerated degradation caused by silicate …

Abstract Calcium-magnesium-alumino-silicate (CMAS) corrosion is a critical factor which
causes the failure of thermal barrier coating (TBC). CMAS attack significantly alters the …

This review critically examines the current understanding of calcia–magnesia–alumina–
silicate (CMAS) degradation mechanisms and mitigation approaches in thermal and …

Developing new systems with excellent properties is of great significance to the progress of
TBC. We herein study the CMAS corrosion behavior of four A 6 B 2 O 17 ceramics to …

Thermal barrier coatings (TBCs) used in marine condition recently suffer from a new
degradation mainly induced by the coupling effect of calcium-magnesium-aluminum-silicate …

Gadolinium zirconate (GZ) is a promising candidate for next-generation thermal barrier
coating (TBC) materials. Its corrosion resistance against calcium-magnesium-alumino …

Abstract Ta 2 O 5 doped Hf 6 Ta 2 O 17 system (Hf 6 Ta 2 O 17/Ta 2 O 5) is considered to
have potential application prospect in the field of aero-engine. We herein focus on the …

This study investigates the effect of CMAS (CaO-MgO-Al 2 O 3-SiO 2) penetration with
different dosages on TBCs applied by the APS/APS method. For this purpose, CMAS …

Considerable efforts are being invested to explore alternative ceramic materials to yttria
stabilized zirconia (YSZ) for thermal barrier coating (TBC) applications. In this work, 18 mol …