4th International Conference More Electric Aircraft

Hybrid-electric distributed propulsion system - Optimal electric systems - High temperature power electronics - Thermal management - Superconducting machines

More Electric Aircraft (MEA) applications demand high reliability, high availability, and high power density while aiming to reduce weight, complexity, fuel consumption, operational costs, and environmental impact. New electric driven systems can meet these requirements and also provide significant technical and economic improvements over conventional mechanical, hydraulic, or pneumatic systems.

However, the MEA puts some challenges on the aircraft electrical system, both in the amount of the required power and the processing and management of this power.

Join us to share ideas, problems and solutions relating to technological developments as well as future concepts associated to more electricalircraft.

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Reasons to Attend

Optimal design of electric systems for MEA

Move to More Electric Aircraft – results and upcoming projects

Power Electronics: High temperature PE

Potentials, challenges and limits of intelligent and effective thermal management

Hybrid-electric distributed propulsion system

Energy storage as the key to MEA design success

Superconducting Machines and Power Systems


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