Abstract:With the increasing service temperature of aeroengines, the development of thermal/environmental barrier coatings (T/EBCs) has been considered to be a great challenge, which requires high‐temperature stability and excellent thermal and mechanical properties. In this work, high‐entropy design was adopted to change the crystal structure of rare‐earth monosilicates used for T/EBCs. The microstructure evolution, thermal and mechanical properties of the plasma‐sprayed (Lu0.25Yb0.25Er0.25Y0.25)2SiO5 and (Lu0.2Yb0.2E… Show more
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