Disk design methodology for reducing blade vibration in turbine engine rotors

Keyphrases

• Design Methodology 100%
• Turbine Engine 100%
• Stress Level 100%
• Rotor 100%
• Blade Vibration 100%
• Disc Design 100%
• Blade Mistuning 100%
• Modeling Techniques 50%
• Design Optimization 50%
• Process Optimization 50%
• Safe Level 50%
• Metric Basis 50%
• Reduced Order Model 50%
• Reduced Order Modeling 50%
• Comprehensive Design 50%
• Design Configuration 50%
• Rotational Effects 50%
• High Cycle Fatigue 50%
• Fatigue Failure 50%
• Maximum Stress 50%
• Dynamic Stress 50%
• Cross-sectional Profile 50%
• Minimum Weight 50%
• Vibration Response 50%
• Vibration Energy 50%
• Vibration Level 50%
• Mistuned Bladed Disk 50%
• Bladed Disk 50%
• Goodman Diagram 50%
• Blade Stress 50%
• Centrifugal Load 50%

Engineering

• Stress Level 100%
• Rotors 100%
• Blade Vibration 100%
• Turbine 100%
• Metrics 50%
• Optimal Design 50%
• Design Optimization 50%
• Reduced Order Model 50%
• Centrifugal 50%
• Fatigue Failure 50%
• High Cycle Fatigue 50%
• Maximum Stress 50%
• Dynamic Stress 50%
• Safe Level 50%
• Rotational Effect 50%
• Goodman Diagram 50%