Title of article
Ti–N multilayer systems for compressor airfoil sand erosion protection
Author/Authors
Feuerstein، نويسنده , , A. and Kleyman، نويسنده , , A.، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2009
Pages
5
From page
1092
To page
1096
Abstract
Frequently aircraft, tank and helicopter gas turbine engines are operated in a desert environment where the gas turbine compressor rotor blades and vanes are exposed to erosive media such as sand and dust. Base metal erosion leads to increased fuel consumption, efficiency loss, and can cause damage to compressor and turbine hardware. Erosion resistant coatings such as Ti–N, Ti–C–N, Ti–Zr–N, Ti–Zr–C–N, Ti–Al–N, and Ti–Al–C–N applied by cathodic arc physical vapor deposition or other PVD processes can be used to prolong the life of compressor airfoils in a sand erosion environment. Praxair Surface Technologies, Inc. has developed unique multilayered Ti–N coating systems with optimized erosion resistance compared to conventional single layers. The multilayer structure can be tailored to the erosion media particle size distribution. The key features of two selected coating architectures are outlined. Selected erosion performance data with different erosion media are presented. And finally the aspects to ensure high quality mass production are addressed.
Keywords
Erosion coating , TIN , Helicopter compressor blade erosion , Cathodic arc
Journal title
Surface and Coatings Technology
Serial Year
2009
Journal title
Surface and Coatings Technology
Record number
1821728
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