A Preliminary Design System for Turbine Discs

Keyphrases

• Aircraft Engine 50%
• Batch Mode 50%
• Computer-aided Design 50%
• Configuration Optimization 50%
• Cycle Design 50%
• Design Analysis 50%
• Design Elements 50%
• Design Engineers 50%
• Disc Design 50%
• Disc Geometry 50%
• Finite Element Analysis Software 50%
• High Pressure Turbine Disk 50%
• Integrated Architecture 50%
• Integrated Simulation Environment 50%
• Mechanical Performance 50%
• Minimum Weight 50%
• Multidisciplinary Analysis 50%
• Optimal Curves 50%
• Optimization Algorithm 50%
• Parameterized Model 50%
• Phase Duration 50%
• Platform Analysis 50%
• Platform Design 50%
• Potential Improvement 50%
• Preliminary Design Stage 100%
• Product Development Cycle 50%
• Reference Charts 50%
• Rotor Disc 50%
• Single Platform 50%
• Software Processing 50%
• System Design 100%
• Time Reduction 50%
• Turbine Disk 100%

Engineering

• Aircraft Engine 50%
• Computer Aided Design 50%
• Cycle Design 50%
• Design Analysis 50%
• Design Element 50%
• Design Engineer 50%
• Design System 100%
• Disc Turbine 100%
• Finite Element Analysis 50%
• High-Pressure Turbine 50%
• Improvement Potential 50%
• Limited Design 50%
• Mechanical Performance 50%
• Parameterized Model 50%
• Platform Design 50%
• Preliminary Design 100%
• Preliminary Design Phase 100%
• Processing Software 50%
• Product Development Cycle 50%
• Rotor Disc 50%
• Simulation Environment 50%
• Supporting Disk 50%