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NO-ICE-ROTOR SIGNED

Development and demonstration of materials and manufacturing process for ultra high reliability electric Anti-ice/De-ice thermal layers for high strain rotor blades and helicopter airframe sections

Total Cost €

EC-Contrib. €

Partnership

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Outcomes and
results

NO-ICE-ROTOR project word cloud

Explore the words cloud of the NO-ICE-ROTOR project. It provides you a very rough idea of what is the project "NO-ICE-ROTOR" about.

airframe sections conventional rotor frc tests establishment synthesis tilt pieces manufacturing layers composite functional outcome structures fast fixed realization emission rotorcraft gas productivity ips blade civil helicopter substantiation speed certification lift structural sky environmental reliability noise technologies layer clean icing materials matrix operators sustainable aircraft rig de anti heater adaptations fuel ice performance consumption rotors strain community representative suitable coupon ultra consisting items vertical criteria compound capability safety protection dictate prop wing intended realisation tested configuration combines cruise vibration

Project "NO-ICE-ROTOR" data sheet

The following table provides information about the project.

Coordinator	VILLINGER GMBH Organization address address: GEWERBEPARK 6 city: MIEDERS postcode: 6142 website: www.villinger.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	Austria [AT]
Total cost	985˙000 €
EC max contribution	749˙987 € (76%)
Programme	1. H2020-EU.3.4.5.3. (IADP Fast Rotorcraft)
Code Call	H2020-CS2-CFP02-2015-01
Funding Scheme	CS2-IA
Starting year	2017
Duration (year-month-day)	from 2017-01-01 to 2020-12-31

Partnership

Take a look of project's partnership.

#	participants	country	role	EC contrib. [€]
1	VILLINGER GMBH VILLINGER GMBH Organization address address: GEWERBEPARK 6 city: MIEDERS postcode: 6142 website: www.villinger.com contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	AT (MIEDERS)	coordinator	189˙525.00
2	AIT AUSTRIAN INSTITUTE OF TECHNOLOGY GMBH AIT AUSTRIAN INSTITUTE OF TECHNOLOGY GMBH Organization address address: GIEFINGGASSE 4 city: WIEN postcode: 1210 website: http://www.ait.ac.at/ contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	AT (WIEN)	participant	201˙624.00
3	RTA RAIL TEC ARSENAL FAHRZEUGVERSUCHSANLAGE GMBH RTA RAIL TEC ARSENAL FAHRZEUGVERSUCHSANLAGE GMBH Organization address address: PAUKERWERKSTRASSE 3 city: WIEN postcode: 1210 website: www.rta.eu contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	AT (WIEN)	participant	124˙337.00
4	SIA AVIATEST LTD SIA AVIATEST LTD Organization address address: REZEKNES IELA 1 city: RIGA postcode: 1073 website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	LV (RIGA)	participant	119˙700.00
5	CEST KOMPETENZZENTRUM FUR ELEKTROCHEMISCHE OBERFLACHENTECHNOLOGIE GMBH CEST KOMPETENZZENTRUM FUR ELEKTROCHEMISCHE OBERFLACHENTECHNOLOGIE GMBH Organization address address: VIKTOR KAPLAN STRASSE 2 city: WIENER NEUSTADT postcode: 2700 website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	AT (WIENER NEUSTADT)	participant	114˙800.00

Map

Project objective

The expected outcome of the NO-ICE-ROTOR project is structural and environmental test substantiation of ultra high reliability heater layers which are capable to be integrated into an advanced tilt civil rotorcraft configuration with high cruise speed, low fuel consumption and gas emission, low community noise impact, and high productivity for operators.

The realisation of such an advanced tilt civil rotorcraft is the objective of the Clean sky Fast Rotorcraft Project (FRC). It is the aim of this project to use technologies developed through the Clean Sky Programme to demonstrate a compound rotorcraft configuration that combines the vertical lift capability of the conventional helicopter with the speed capability of a fixed wing aircraft in a sustainable way.

The overall objectives of the NO-ICE-ROTOR project are: â€¨ - Design and development of heater layer for application in tilt rotors - Establishment of test criteria and test matrix project - Manufacturing of suitable test pieces for ice protection system (IPS) testing - Structural and environmental rig test adaptations for IPS testing - IPS rig and coupon test realization and tests results - Synthesis of results: comparison of performance of materials and of technologies tested The specific objective of the NO-ICE-ROTOR project is to develop heater layers to be embedded in composite structures to provide anti-icing and de-icing capability where safety requirements dictate ultra high reliability, while operating in high strain and vibration conditions. Structural and environmental testing will be conducted on representative test items consisting of functional heater layers embedded in the prop-rotor blade and airframe sections of a tilt-rotor configuration intended for civil certification.

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The information about "NO-ICE-ROTOR" are provided by the European Opendata Portal: CORDIS opendata.