Low Power De-Icing System suitable for Small Aircrafts

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(JTI-CS2-2016-CFP03-SYS-03-04) - LOW POWER DE-ICING SYSTEM SUITABLE FOR SMALL AIRCRAFTS

Programme: Horizon 2020 Framework Programme
Call: Clean Sky 2 Call for Proposals 03 EU

Topic description

Specific Challenge:

To Design, Manufacture and Test up to TRL 5 a Low Power De-Icing System suitable for Small Aircraft applications. A mixed solution Electro-Thermal and Electro–Expulsive is preferred. The idea is to design the system on the icing requirement of a modified P180 aircraft Main Wing and test a section of the Main Wing Leading edge in an IWT. For the full topic description see the Call Text Document (Annex of Workplan) published with this call.

Keywords

Aircraft Avionics, Systems & Equipment AVS

Tags

Electro-Expulsive Electro-Thermal De-Icing

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