作者: T.N. Rhys-Jones
DOI: 10.1016/0010-938X(89)90104-2
关键词:
摘要: Abstract The variety of surface coatings and deposition processes available for the protection blade vane components in aero gas turbines is reviewed. Diffusion, overlay thermal barrier are described such as pack vapour metallizing, plasma spraying PVD techniques outlined. performance various coating systems discussed, where possible, with reference to behaviour engine-tested components.