The sensitivity of Ni-based superalloy to hole making operations: Influence of process parameters on subsurface damage and residual stress

Keyphrases

• Residual Stress 100%
• Ni-based Superalloy 100%
• Process Parameters Influence 100%
• Subsurface Damage 100%
• Plunge Milling 100%
• Hole-making Operations 100%
• Stress Damage 100%
• RR1000 66%
• Aero-engine 66%
• Free Surface 66%
• Hoop 66%
• Gas Turbine 66%
• Material Removal Rate 66%
• Mechanical Properties 33%
• Working Surface 33%
• Nickel-based Superalloy 33%
• High Strength 33%
• High Temperature 33%
• Material Properties 33%
• Tool-workpiece Interaction 33%
• Cutting Speed 33%
• Thermal Properties 33%
• Feed Rate 33%
• Residual Stress Distribution 33%
• Drilling Process 33%
• Safety-critical 33%
• Ni-based Alloy 33%
• Machining Conditions 33%
• Damage-free 33%
• Difficult-to-machine 33%
• Flank Wear 33%
• Operational Efficiency 33%
• Finishing Process 33%
• Hole Making 33%
• Waspaloy 33%
• Inconel 33%
• Tensile Residual Stress 33%
• Cooling Conditions 33%
• High Temperature Operation 33%
• Proclivity 33%
• Drill Hole 33%
• Surface Sensitivity 33%
• Residual Stress Profile 33%
• Cutting Edge Quality 33%
• Material Deformation 33%
• Malformation 33%
• Hole Surface 33%
• Surface Hardening 33%

Engineering

• Material Removal Rate 100%
• Process Parameter 100%
• Residual Stress 100%
• Subsurface 100%
• Aeroengine 100%
• Free Surface 100%
• Gas Turbine 100%
• Cutting Edge 50%
• Cutting Speed 50%
• Tensile Residual Stress 50%
• Feed Rate 50%
• Residual Stress Distribution 50%
• Experimental Trial 50%
• Flank Wear 50%
• Operational Efficiency 50%
• Cooling Condition 50%
• High Operating Temperature 50%
• Finishing Operation 50%
• Drilled Hole 50%
• Produce Hole 50%
• Residual Stress Profile 50%