Evaluation of low power consumption and temperature drop potential in an aero-engine pre-swirl system for turbine performance improvement

Engineering

• Aero-Engines 100%
• Aerodynamics 20%
• Air Flow 20%
• Angle-of-Attack 40%
• Blade Cooling 20%
• Blade Turbine 20%
• Electric Power Utilization 20%
• Influencing Factor 20%
• Local Structure 20%
• Low Power Consumption 100%
• Performance Improvement 100%
• Rotor Blade 20%
• Specific Power 20%
• Subsystem 20%
• Systems Performance 40%
• Temperature Drop 100%
• Turbine 100%