High-temperature resistant gas turbine component

摘要

A high-temperature resistant component for a gas turbine hot part and so on is provided, which has durability and reliability enough to withstand a corrosive environment with use of the low-grade oil. The high-temperature resistant component includes an alloy substrate (10) containing Ni, Co, or Fe as the principal component, and a thermal barrier coating formed over the surface of the substrate (10) via a bond coat. The thermal barrier coating includes a porous thermal-barrier layer (12) made of ceramic and an environmental barrier layer (13) with corrosion resistance. An impregnated layer (14) is provided between the environmental barrier layer (13) and the thermal barrier layer (12). In the impregnated layer (14), the thermal barrier layer (12) is impregnated with a part of the environmental barrier layer (13). The thermal barrier layer (12) is made of a porous zirconia layer, and the environmental barrier layer (13) includes silica as the principal component. The porous zirconia layer has pores (16) impregnated with the part of the environmental barrier layer (13). As a result, the high-temperature resistant component has excellent corrosion resistance and excellent heat resistance.