THE USE OF THERMALLY SPRAYED COATINGS FOR COMPRESSOR AND TURBINE APPLICATIONS IN AERO ENGINES

被引：40

作者：

RHYSJONES, TN

机构：

来源：

SURFACE & COATINGS TECHNOLOGY | 1990年 / 42卷 / 01期

关键词：

D O I：

10.1016/0257-8972(90)90109-P

中图分类号：

TB3 [工程材料学];

学科分类号：

0805 ; 080502 ;

摘要：

The range of thermal spraying processes available for the deposition of surface coatings for compressor, combustion chamber and turbine section components in aero engines are described, and typical coating applications discussed. Combustion flame, arc wire, high velocity combustion and plasma spraying techniques are described, and coatings for wear, oxidation and corrosion resistance, clearance control and thermal barrier applications are discussed. © 1989.

引用

页码：1 / 11

页数：11