CORDIS Project
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This project investigates the integration of hybrid ice protection systems for aircraft wing slats, combining electro-thermal and electro-expulsive technologies. The goal is to enhance energy efficiency and functionality for larger aircraft platforms.
There are presently two principle alternatives to engine bleed air Ice Protection on mid to large size aircraft; these are known as ‘electro-expulsive’ low power and ‘electro-thermal’ systems.Whilst electro-thermal systems can perform very
successfully when provided with adequate electrical power, an electro-expulsive system can be highly energy efficient and therefore extremely attractive on platforms where generator sizing is critical or less power is available for the ice
protection system.Ne…
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