The invention relates to the field of
ceramic materials for thermal barrier / environmental barrier integrated
coating layers of advanced aero-engines, and in particular, relates to gamma-type high-entropy
rare earth disilicate with ultrahigh-temperature stability and a preparation method thereof. The
chemical formula of the gamma-type high-entropy
rare earth disilicate
ceramic material is defined in the specification, wherein n is more than or equal to 5, and REn is one of
rare earth elements Y, Sc, La, Ce, Pr, Nd, Pm, Sm, Eu, Gd, Tb, Dy, Ho, Er, Tm, Yb and Lu respectively. The preparation method specifically comprises the preparation processes: by taking corresponding rare earth
oxide powder and
silicon oxide powder as raw materials, performing wet mixing, and performing
pressureless sintering synthesis in an
air atmosphere, and thus obtaining the gamma-type high-entropy rare earth disilicate
ceramic powder material; and further hot-pressing and
sintering in a hot-pressing furnace witha protective
atmosphere to obtain the gamma-type high-entropy rare earth disilicate ceramic block material with excellent high-temperature
phase stability. According to the invention, the gamma-typehigh-entropy ceramic material with high purity,
high density and excellent high-temperature
phase stability can be prepared.