Functionally gradient ceramic/metallic coatings for gas turbine components by high-energy beams for high-temperature applications

Keyphrases

• Turbine Components 100%
• Metallic Coating 100%
• Functionally Gradient Materials 100%
• High-energy Beams 100%
• Coatings for Gas Turbine Components 100%
• Thermal Spray Technology 100%
• High-temperature Applications 100%
• Electron Beam Physical Vapor Deposition (EB-PVD) 75%
• Thermal Barrier Coatings 75%
• Laser Surface Cladding 75%
• Laser Glazing 75%
• Laser Surface Alloying 75%
• Turbine Blade 50%
• Aerospace Industry 50%
• Turbine Industry 50%
• Substrate Surface 25%
• Mechanical Properties 25%
• High Temperature 25%
• Trailing Edge 25%
• Elevated Temperature 25%
• Fine-grained Microstructure 25%
• Laser Technique 25%
• Columnar Microstructure 25%
• Recent Advancements 25%
• Surface Material 25%
• Oxidation Resistance 25%
• High Temperature Oxidation 25%
• Corrosion Resistance 25%
• Increased Demand 25%
• Microstructural Evolution 25%
• Physical-chemical Properties 25%
• Amorphous Materials 25%
• Textured Coating 25%
• Unmelted Particles 25%
• Lifetime Enhancement 25%
• Engine Temperature 25%
• Erosion-corrosion 25%
• Fatigue Wear 25%
• Improved Surface Properties 25%
• Inhomogeneous Microstructure 25%
• Wear-resistant 25%
• Oxidation Corrosion 25%
• Metal Matrix Composite Coating 25%
• Laser Grooving 25%
• Corrosion Fatigue 25%
• Metastable Phase 25%

Material Science

• Thermal Spray 100%
• Alloying 75%
• Electron Beam Physical Vapor Deposition 75%
• Thermal Barrier Coating 75%
• Amorphous Material 25%
• Mechanical Property 25%
• Surface Property 25%
• Laser Technique 25%
• Metal Matrix Composite 25%
• Corrosion Resistance 25%
• Composite Coating 25%
• Microstructural Evolution 25%
• Erosion Corrosion 25%
• Elevated Temperature 25%