ICE GENESIS SIGNED
Creating the next generation of 3D simulation means for icing
Total Cost €
0EC-Contrib. €
0Partnership
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0ICE GENESIS project word cloud
Explore the words cloud of the ICE GENESIS project. It provides you a very rough idea of what is the project "ICE GENESIS" about.
Project "ICE GENESIS" data sheet
The following table provides information about the project.
| Coordinator |
AIRBUS OPERATIONS SAS
Organization address contact info |
| 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
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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
| 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.