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I3PS SIGNED

Integration of Innovative Ice Protection Systems

Total Cost €

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EC-Contrib. €

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Partnership

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Project "I3PS" data sheet

The following table provides information about the project.

Coordinator
SOCIETE NATIONALE DE CONSTRUCTION AEROSPATIALE SONACA SA 

Organization address
address: ROUTE NATIONALE CINQ PARK INDUSTRIEL
city: GOSSELIES
postcode: 6041
website: www.sonaca.com

contact info
title: n.a.
name: n.a.
surname: n.a.
function: n.a.
email: n.a.
telephone: n.a.
fax: n.a.

 Coordinator Country Belgium [BE]
 Project website http://www.sonaca.com
 Total cost 1˙350˙090 €
 EC max contribution 1˙349˙900 € (100%)
 Programme 1. H2020-EU.3.4.5.4. (ITD Airframe)
 Code Call H2020-CS2-CFP06-2017-01
 Funding Scheme CS2-RIA
 Starting year 2018
 Duration (year-month-day) from 2018-03-01   to  2020-06-30

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    SOCIETE NATIONALE DE CONSTRUCTION AEROSPATIALE SONACA SA BE (GOSSELIES) coordinator 574˙900.00
2    RTA RAIL TEC ARSENAL FAHRZEUGVERSUCHSANLAGE GMBH AT (WIEN) participant 355˙600.00
3    EURO HEAT PIPES SA BE (NIVELLES) participant 202˙700.00
4    IKERLAN S. COOP ES (MONDRAGON) participant 116˙700.00
5    CRANFIELD UNIVERSITY UK (CRANFIELD - BEDFORDSHIRE) participant 100˙000.00

Map

 Project objective

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.

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The information about "I3PS" are provided by the European Opendata Portal: CORDIS opendata.

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