230 VAC/28 VDC high‐power density power supply for more electric aircraft applications

Reliability Analysis to Design Electric Power Systems for More - Electric Aircraft

Title of Document: APPLYING RELIABILITY ANALYSIS TO DESIGN ELECTRIC POWER SYSTEMS FOR MORE-ELECTRIC AIRCRAFT Baozhu Zhang, Master of Science, 2014 Directed By: Research Assistant Professor Huan Xu, Aerospace Engineering and Institute for Systems Research The More-Electric Aircraft (MEA) is a type of aircraft that replaces conventional hydraulic and pneumatic systems with electrically powered co...

Reactive Protocols for Aircraft Electric Power Distribution

The increasing complexity of electric power systems leads to integration and verification challenges. We consider the problem of designing a control protocol for the aircraft electric power system that meets these system requirements and reacts dynamically to changes in internal system states. We formalize these requirements by translating them into a temporal logic specification language descr...

A Review of More-Electric Aircraft

The More-Electric Aircraft (MEA) underlines the utilization of the electrical power to power the non-propulsive aircraft systems. Adopting the MEA achieves numerous advantages such as optimizing the aircraft performance and decreasing operating and maintenance costs. Moreover, the MEA reduces the emission of the air pollutant gases from the aircraft, which can contribute in solving the problem ...

Power Generation and Distribution System for a More Electric Aircraft - A Review

Stability Analysis and Control Design for Hybrid Ac-dc More- Electric Aircraft Power Systems