DEVELOPMENT OF ION-PLASMA REFRACTORY METALLIC LAYERS OF HEAT-INSULATING COATINGS FOR COOLED TURBINE ROTOR BLADES

摘要

Alloys ZhS32 and ZhS36 with heat-protection coatings (HPC) consisting of external ceramic layers and internal refractory metallic layers are studied. The coated alloys are tested for heat fastness and high-temperature strength at 1100 - 1150°C. The HPC with a metallic layer of the (Ni - Cr - Al - Hf) + Al system are shown to be more advantageous than similar HPC based on an SPD-2 + VSDP-16 commercial refractory coating. The effect of the HPC on the characteristics of high-temperature strength and fatigue resistance of alloys ZhS32 and ZhS36 is investigated.