I3PS | Integration of Innovative Ice Protection Systems

Summary
This proposal fits within the framework of aircraft effectiveness constant improvement by reducing fuel and power consumptions. Its ultimate goal is to economically remove ice accreting on aircraft structure critical parts and thus increase reliability and mass saving on the global function. By comparison with the present existing solutions which are based on active pneumatic and electro-thermal means the targeted solutions will enable electrical power consumption, cost and mass reductions and ease the overall integration process.
The subject of this proposal is to integrate and test two innovative ice protection systems in aircraft structures. The first system is based on two-phase heat transport and will be tested in a turboprop metallic air intake. The second system is based on electromagnetic induction and will be tested on a wing fixed leading edge and on a flap leading edge.
Unfold all
/
Fold all
More information & hyperlinks
Web resources: https://cordis.europa.eu/project/id/785550
Start date: 01-03-2018
End date: 31-12-2020
Total budget - Public funding: 1 350 090,00 Euro - 1 349 900,00 Euro
Cordis data

Original description

This proposal fits within the framework of aircraft effectiveness constant improvement by reducing fuel and power consumptions. Its ultimate goal is to economically remove ice accreting on aircraft structure critical parts and thus increase reliability and mass saving on the global function. By comparison with the present existing solutions which are based on active pneumatic and electro-thermal means the targeted solutions will enable electrical power consumption, cost and mass reductions and ease the overall integration process.
The subject of this proposal is to integrate and test two innovative ice protection systems in aircraft structures. The first system is based on two-phase heat transport and will be tested in a turboprop metallic air intake. The second system is based on electromagnetic induction and will be tested on a wing fixed leading edge and on a flap leading edge.

Status

CLOSED

Call topic

JTI-CS2-2017-CFP06-AIR-02-39

Update Date

27-10-2022
Images
No images available.
Geographical location(s)
Structured mapping
Unfold all
/
Fold all
Horizon 2020
H2020-EU.3. SOCIETAL CHALLENGES
H2020-EU.3.4. SOCIETAL CHALLENGES - Smart, Green And Integrated Transport
H2020-EU.3.4.5. CLEANSKY2
H2020-EU.3.4.5.4. ITD Airframe
H2020-CS2-CFP06-2017-01
JTI-CS2-2017-CFP06-AIR-02-39 Integration of innovative ice protection systems into structure and their validation