Comparison and choice of a fault tolerant inverter topology for the traction drive of an electrical helicopter

Keyphrases

• Inverter Topology 100%
• Traction Drive 100%
• Power Electronic Inverters 100%
• Electrical Helicopter 100%
• Fault-tolerant Inverter 100%
• Fault Tolerance 50%
• System Analysis 50%
• Inverter 50%
• Design Requirements 50%
• Electric Energy 50%
• Design Futures 50%
• Permanent Magnet Synchronous Motor 50%
• Operation Conditions 50%
• Markov Model 50%
• Multi-state System Reliability 50%
• System Reliability Evaluation 50%
• Future Operations 50%

Engineering

• Inverter 100%
• Fits and Tolerances 25%
• System Reliability 25%
• Design Requirement 25%
• Reliability Evaluation 25%
• Permanent Magnet Synchronous Motor 25%
• State System 25%
• Systems Analysis 25%
• Electric Energy 25%