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ICE GENESIS SIGNED

Creating the next generation of 3D simulation means for icing

Total Cost €

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EC-Contrib. €

0

Partnership

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Project "ICE GENESIS" data sheet

The following table provides information about the project.

Coordinator
AIRBUS OPERATIONS SAS 

Organization address
address: ROUTE DE BAYONNE 316
city: TOULOUSE
postcode: 31060
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.

 Coordinator Country France [FR]
 Total cost 21˙980˙549 €
 EC max contribution 11˙964˙300 € (54%)
 Programme 1. H2020-EU.3.4. (SOCIETAL CHALLENGES - Smart, Green And Integrated Transport)
 Code Call H2020-MG-2018-SingleStage-INEA
 Funding Scheme RIA
 Starting year 2019
 Duration (year-month-day) from 2019-01-01   to  2022-12-31

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    AIRBUS OPERATIONS SAS FR (TOULOUSE) coordinator 974˙136.00
2    CENTRO ITALIANO RICERCHE AEROSPAZIALI SCPA IT (CAPUA - CASERTA) participant 1˙509˙900.00
3    OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES FR (PALAISEAU) participant 1˙081˙788.00
4    RTA RAIL TEC ARSENAL FAHRZEUGVERSUCHSANLAGE GMBH AT (WIEN) participant 882˙607.00
5    TECHNISCHE UNIVERSITAT DARMSTADT DE (DARMSTADT) participant 642˙050.00
6    CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE CNRS FR (PARIS) participant 627˙046.00
7    SAFRAN AIRCRAFT ENGINES FR (PARIS) participant 596˙297.00
8    OSTERREICHISCHES INSTITUT FUR VEREISUNGSWISSENSCHAFTEN IN DER LUFTFAHRT AT (KOFLACH) participant 504˙375.00
9    TECHNISCHE UNIVERSITAET BRAUNSCHWEIG DE (BRAUNSCHWEIG) participant 497˙125.00
10    DASSAULT AVIATION FR (PARIS) participant 474˙875.00
11    AIRBUS HELICOPTERS FR (MARIGNANE) participant 384˙082.00
12    DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV DE (KOELN) participant 378˙675.00
13    IAG INDUSTRIE AUTOMATISIERUNGS GMBH AT (WEIKERSDORF) participant 372˙370.00
14    ARTTIC FR (PARIS) participant 359˙672.00
15    CRANFIELD UNIVERSITY UK (CRANFIELD - BEDFORDSHIRE) participant 324˙555.00
16    MINISTERE DE LA DEFENSE FR (PARIS) participant 313˙125.00
17    LEONARDO - SOCIETA PER AZIONI IT (ROMA) participant 285˙585.00
18    RAINBOWVISION FR (ROUEN) participant 240˙625.00
19    POLITECNICO DI MILANO IT (MILANO) participant 238˙000.00
20    ECOLE POLYTECHNIQUE FEDERALE DE LAUSANNE CH (LAUSANNE) participant 228˙410.00
21    AVIONS DE TRANSPORT REGIONAL FR (BLAGNAC) participant 205˙750.00
22    SOCIETE NATIONALE DE CONSTRUCTION AEROSPATIALE SONACA SA BE (GOSSELIES) participant 201˙587.00
23    LIEBHERR AEROSPACE TOULOUSE SAS FR (TOULOUSE) participant 191˙875.00
24    ROLLS-ROYCE PLC UK (LONDON) participant 184˙875.00
25    GENERAL ELECTRIC DEUTSCHLAND HOLDING GMBH DE (FRANKFURT AM MAIN) participant 160˙625.00
26    AIT AUSTRIAN INSTITUTE OF TECHNOLOGY GMBH AT (WIEN) participant 104˙286.00
27    BOMBARDIER INC. CA (MONTREAL) participant 0.00
28    CENTRAL AEROLOGICAL OBSERVATORY RU (DOLGOPRUDNY) participant 0.00
29    CORPORATION DE L ECOLE POLYTECHNIQUE DE MONTREAL ASSOCIATION CA (MONTREAL) participant 0.00
30    FEDERAL STATE UNITARY ENTERPRISE THE CENTRAL AEROHYDRODYNAMIC INSTITUTE NAMED AFTER PROF. N.E. ZHUKOVSKY RU (ZHUKOVSKY) participant 0.00
31    FEDERALNOE GOSUDARSTVENNOE UNITARNOE PREDPRIYATIE CENTRALNII INSTITUTAVIACIONOGO MOTOROSTROENIYA IMENI PI BARANOVA RU (MOSKVA) participant 0.00
32    MOSCOW INSTITUTE OF PHYSICS AND TECHNOLOGY (STATE UNIVERSITY) RU (MOSCOW) participant 0.00
33    TOKYO UNIVERSITY OF SCIENCE FOUNDATION JP (TOKYO) participant 0.00

Map

 Project objective

Current design methodologies used to characterise ice accretion and its effects on air vehicle components and power plant systems are mainly based on empirical methods, comparative analysis, 2D simulation tools and past experience gained on in-service products. Due to the associated uncertainties, cautious design margins are used, leading to conservative and non-optimised solutions. As future air vehicle and propulsive system architectures introduce radical design changes, it will no longer be possible to rely on the existing design methodologies, making future development extremely difficult to accomplish efficiently and within short development cycles that are demanded by customers and desired by industry. These difficulties are increased by the recent changes in certification regulations, in particular for Supercooled Large Droplets (SLD), which require manufacturers to certify their products against more stringent requirements. Snow also remains a challenge, especially for turbine engines and APUs. ICE GENESIS will provide the European aeronautical industry with a validated new generation of 3D icing engineering tools (numerical simulation tools and upgraded test capabilities), addressing App C, O and snow conditions, for safe, efficient, right first time, and cost effective design and certification of future regional, business and large aircraft, rotorcraft and engines. ICE GENESIS will permit weather hazards to be more precisely evaluated and properly mitigated thanks to adapted design or optimised protection through either active or passive means. Furthermore, ICE GENESIS will pave the way for 3D digital tools to be used in the future as acceptable means of compliance by the regulation authorities. Overall, ICE GENESIS will contribute to flight safety, reduced certification costs and increased operability.

 Deliverables

List of deliverables.
Calibration methodology for snow test facility Documents, reports 2020-04-02 08:53:05
Definition of the target requirements for test facilities operating envelopes for snow Documents, reports 2020-04-01 20:06:41
Definition of numerical capability requirements for snow Documents, reports 2020-04-01 20:06:41
Definition of the target requirements for test facilities operating envelopes for App O Documents, reports 2020-04-01 20:06:41
Selection of most suitable instrumentation for IWT/T calibration Documents, reports 2020-04-01 20:06:41
Selection of most suitable instrumentation for F/T Documents, reports 2020-04-01 20:06:40
Definition of numerical capability requirements for liquid icing conditions Documents, reports 2020-04-01 20:06:40
Initial communication kit with information about project structure and goals Other 2020-04-01 20:06:40
ICE GENESIS Public Website Websites, patent fillings, videos etc. 2020-04-01 20:06:41

Take a look to the deliverables list in detail:  detailed list of ICE GENESIS deliverables.

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

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