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Horizon 2020 project information and now also report summaries are available on CORDIS. All H2020 projects can be downloaded from the EU Open Data Portal .

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Industrialisation of Jet Noise Prediction Methods
ID: 717228
Start date: 2016-07-01, End date: 2019-06-30
"The project, entitled "Industrialisation of Jet Noise Prediction Methods" (INSPiRE), addresses fully the scope outlined in Topic JTI-CS2-2015-CFP02-ENG-03-02 "Jet Noise Reduction Using Predictive Methods".Turbulence-resolving CFD coupled to efficient far-field integration...
Programme: H2020-EU.3.4.5.5.
Record Number: 204260
Last updated on: 2017-02-14
Engine Mount System for Ultra High Pass Engine
ID: 687023
Start date: 2016-03-15, End date: 2022-02-14
Our consortium is applying for the Engine Mounts System (EMS) of the Ultra High Propulsive Efficiency. Our 3 objectives are:1. Assist the Engine Manufacturer & the Airframer in the evaluation & selection of the most promising & suitable Engine Mounts System (EMS)...
Programme: H2020-EU.3.4.5.5.
Record Number: 202616
Last updated on: 2017-02-14
Engine INSTallation And INtegration
ID: 687132
Start date: 2016-01-01, End date: 2018-06-30
"Nowadays, almost all General Aviation piston-powered aircrafts are powered by Avgas fuel. For decades, piston engines like Lycoming and Continental were allowed to burn only this type of fuel, which is characterized by high-octane values, very low vapor pressure indexes and...
Programme: H2020-EU.3.4.5.5.
Record Number: 199571
Last updated on: 2015-12-23
Power Density improvement demonstrated on a certified engine
ID: 686533
Start date: 2016-01-01, End date: 2017-11-30
SMA currently manufacture a 4 cylinder air cooled diesel engine. It will render this product more competitive in the market place if it has a higher power output (+20%) and is lighter (10%). This proposal by Ilmor Engineering Ltd presents a program of work to achieve these...
Programme: H2020-EU.3.4.5.5.
Record Number: 199473
Last updated on: 2015-12-17
Development and Manufacturing of an All-Oxide Inter Turbine Duct for Aeroengines
ID: 686707
Start date: 2015-12-01, End date: 2019-11-30
The objective of the proposal is the development of an all-oxide Ceramic Matrix Composites (CMC) inter turbine duct for testing of the component in a demonstrator engine. The development steps include:- Designing the parts including the attachment to the metallic support...
Programme: H2020-EU.3.4.5.5.
Record Number: 199449
Last updated on: 2015-12-15
Advanced Design of Very High Power Density Piston Engine and Thermal Management Challenges for Aircraft Application
ID: 687039
Start date: 2016-02-01, End date: 2018-11-30
Danielson Engineering is an SME based in Magny Cours (France), SRC certified (Société de Recherche sous Contrat), specialising in the design, the optimisation, the manufacturing and experimental development of innovative engines for automotive and aeronautical applications...
Programme: H2020-EU.3.4.5.5.
Record Number: 202617
Last updated on: 2016-04-12
Development of high performance turbocharger for aeronautical application
ID: 686371
Start date: 2016-01-01, End date: 2017-06-30
The goal of the project is to develop high performance turbocharger for aeronautical application. This machine will allow increasing power density, efficiency and maintainability of the aeronautical piston engine. Key objectives for the equipment are:• High compressor...
Programme: H2020-EU.3.4.5.5.
Record Number: 200827
Last updated on: 2016-03-18
Advanced Bearing Technologies to Increase Capabilities
ID: 686366
Start date: 2016-01-01, End date: 2020-12-31
The development of Very High Bypass Ratio (VHBR) engines is a promising engine concept to fulfil the major milestones of the Sustainable and Green Engines (SAGE) programme. The significant environmental benefits of this new engine are synonymous with an increased speed and...
Programme: H2020-EU.3.4.5.5.
Record Number: 199561
Last updated on: 2015-12-22
Crack growth threshold analysis in TiAl alloys
ID: 686711
Start date: 2016-03-01, End date: 2019-02-28
The objective of the project is to investigate the fatigue crack growth (FCG) threshold and rate for long as well as short cracks of second generation TiAl alloys suitable for use in the Intermediate Pressure Turbine (IPT) of the UltraFanTM engine. The work includes in detail...
Programme: H2020-EU.3.4.5.5.
Record Number: 199486
Last updated on: 2015-12-18
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List retrieved on: 2017-05-23
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