发明名称 Overlay metallic-cermet alloy coating systems
摘要 A substrate, such as a turbine blade, vane, or the like, which is subjected to high temperature use is coated with a base coating of an oxide dispersed, metallic alloy (cermet). A top coating of an oxidation, hot corrosion, erosion resistant alloy of nickel, cobalt, or iron is then deposited on the base coating. A heat treatment is used to improve the bonding. The base coating serves as an inhibitor to interdiffusion between the protective top coating and the substrate. Otherwise, the protective top coating would rapidly interact detrimentally with the substrate and degrade by spalling of the protective oxides formed on the outer surface at elevated temperatures.
申请公布号 US4446199(A) 申请公布日期 1984.05.01
申请号 US19820403378 申请日期 1982.07.30
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION 发明人 GEDWILL, MICHAEL A.;LEVINE, STANLEY R.;GLASGOW, THOMAS K.
分类号 B32B15/01;C23C4/02;C23C28/02;(IPC1-7):B32B15/00 主分类号 B32B15/01
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