作者: Werner Stamm
DOI:
关键词: Process (computing) 、 Turbine 、 Substrate (building) 、 Turbine blade 、 Oxide 、 Marine engineering 、 Operating temperature 、 Composite material 、 Engineering 、 Metal 、 Layer (electronics)
摘要: A process for producing a component of gas turbine having substrate with metallic layer is provided. The MCrAlX which treated at temperatures elevated above the operating temperature, by least 50° C., so that oxidation and corrosion behavior are improved. In particular type, NiCoCrAlX used.