Thermal Spray Processes for the Repair of Gas Turbine Components

被引:17
|
作者
Fiebig, Jochen [1 ]
Bakan, Emine [1 ]
Kalfhaus, Tobias [1 ]
Mauer, Georg [1 ]
Guillon, Olivier [1 ]
Vassen, Robert [1 ]
机构
[1] Forschungszentrum Julich, Inst Energy & Climate Res IEK 1, D-52428 Julich, Germany
关键词
cold gas spraying; nickel-based superalloys; repair; titanium aluminide; vacuum plasma spraying; ADIABATIC SHEAR INSTABILITY; IN-FLIGHT CHARACTERISTICS; COLD SPRAY; BONDING MECHANISM; PARTICLE-VELOCITY; RESIDUAL-STRESS; DYNAMIC-SPRAY; SUBSTRATE ROUGHNESS; ADHESION-STRENGTH; DEPOSITION;
D O I
10.1002/adem.201901237
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Gas turbine components are often operated in harsh conditions, which can lead to severe damage. As it is highly desirable from both an economical and an ecological point of view to restore these worn areas instead of manufacturing new components, repair technologies are of huge interest for companies supplying maintenance and overhaul of gas turbines. In this article, two thermal techniques are described that can be used for this application: cold gas spraying (CGS) and vacuum plasma spraying (VPS). The CGS process allows the deposition of metallic coatings with excellent mechanical properties; several examples including gamma-TiAl, Inconel (IN) 718, and IN 738 are given. Essential for the deposition of high-performance coatings in CGS is to exceed the so-called critical velocity. This is discussed also with experimental findings. As a final topic, experiments that use VPS for the repair of single-crystal alloys are described.
引用
收藏
页数:11
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