| CPC C04B 35/22 (2013.01) [C04B 35/62222 (2013.01); C04B 35/657 (2013.01); C23C 4/11 (2016.01); C23C 4/134 (2016.01); F01D 5/18 (2013.01); C04B 2235/3234 (2013.01); C04B 2235/3454 (2013.01); C04B 2235/767 (2013.01); C04B 2235/9669 (2013.01)] | 14 Claims |

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1. A turbine part, comprising a substrate, an environmental barrier and at least one reactive layer,
the environmental barrier comprising a thermal insulation layer, a sublayer suitable for promoting adhesion between the substrate and the thermal insulation layer, and a protective layer suitable for protecting the substrate from oxidation and/or corrosion,
the environmental barrier at least partially covering the substrate,
the at least one reactive layer being suitable for reacting with at least one CMAS compound selected from a calcium oxide, a magnesium oxide, an aluminum oxide and a silicon oxide,
the at least one reactive layer covering at least a portion of the environmental barrier,
wherein a material of the at least one reactive layer comprises an oxide of formula A′A″BO5+δ, A′ being selected from a rare-earth element and yttrium, A″ being selected from a rare-earth element, yttrium and aluminum, B being selected from zirconium, hafnium, tantalum and niobium, δ being a real number comprised between 0 and 0.5,
wherein the oxide of formula A′A″BO5+δ has a rare-earth element atomic fraction comprised between 18% and 25%.
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