Community Research and Development Information Service - CORDIS

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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SkyLight: Innovations in titanium investment casting of lightweight structural components for aero engines
ID: 737649
Start date: 2017-02-01, End date: 2020-01-31
Project SkyLight is proposed by AMRC Castings (which evolved out of Castings Technology International). AMRC Castings, a department of the University of Sheffield (USFD), is part of the UK’s High Value Manufacturing Catapult. AMRC Castings’ mission is to develop and...
Programme: H2020-EU.3.4.5.5.
Record Number: 207655
Last updated on: 2016-12-21
Planet ROlling Bearing with Advanced TEchnologies
ID: 738029
Start date: 2017-01-01, End date: 2020-06-30
The development of Ultra High Propulsive Efficiency (UHPE) engine is a key factor to fulfil the main milestones of the Sustainable And Green Engines (SAGE) program: high environmental benefits of UHPE will be reached through a power gearbox decoupling fan and turbine...
Programme: H2020-EU.3.4.5.5.
Record Number: 207647
Last updated on: 2016-12-21
Development of Experimental Techniques and Predictive Tools to Characterise Thermo-Mechanical Fatigue Behaviour and Damage Mechanisms
ID: 686600
Start date: 2016-02-01, End date: 2020-01-31
DevTMF takes the collective technical expertise and experience of working on thermo-mechanical fatigue (TMF) problems related to large aero-engines from three major centres of TMF research, namely Linköping, Swansea and Nottingham Universities in order to perform the...
Programme: H2020-EU.3.4.5.5.
Record Number: 199474
Last updated on: 2017-08-17
Inlet PArticle Separator Numerical  ExperiMental Assessment
ID: 755645
Start date: 2017-06-01, End date: 2021-05-31
IPANEMA is a joint numerical and experimental undertaking to understand and improve the separation efficiency of inertial particle separators (IPS), which are integrated in the intake to protect turboprop engines from the ingestion of dust particles and water. The project...
Programme: H2020-EU.3.4.5.5.
Record Number: 210845
Last updated on: 2017-05-23
High load gear and bearings materials
ID: 755602
Start date: 2017-05-01, End date: 2019-11-30
The Ultra High Bypass Ratio technology achieved with the geared turbofan concept, that decouples fan and turbine speeds by means of an Integral Drive System (IDS), is an innovative architecture that can enable significant reduction in fuel burn, noise and emissions.The...
Programme: H2020-EU.3.4.5.5.
Record Number: 210844
Last updated on: 2017-05-23
Aerospace propeller useful for diesel engines with extreme excitation of vibrations
ID: 714030
Start date: 2016-06-01, End date: 2019-09-30
The project proposal is aimed at light weight and efficient jet-fuel aerospace propulsion units based on reciprocating engines. Aerospace propellers useful for jet-fuel reciprocating direct drive engines suffer by extreme excitation of vibrations. The objective of the project...
Programme: H2020-EU.3.4.5.5.
Record Number: 204213
Last updated on: 2017-08-17
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: 2017-06-07
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: 2017-08-03
Integrated Air Cooling Oil Cooled System
ID: 738160
Start date: 2017-01-16, End date: 2020-01-15
The project aims is focused on the design and manufacture of a novel air-oil engine cooling system to be integrated into the engine bay. The project will investigate any better configurations to achieve the same heat rejection with lower weight and smaller overall dimensions...
Programme: H2020-EU.3.4.5.5.
Record Number: 208066
Last updated on: 2017-02-01
Engine Mounting System (EMS) for Ground Test Turboprop Engine Demonstrator
ID: 717239
Start date: 2016-07-04, End date: 2021-07-03
In aircraft, one of the primary sources of vibration is the power plant. Engine vibration could lead to unnecessary expenses for replacing damaged components, cabin noise, crew and passenger discomfort, and structural fatigue. Hutchinson is the major supplier of aircraft main...
Programme: H2020-EU.3.4.5.5.
Record Number: 205413
Last updated on: 2017-02-14
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List retrieved on: 2017-12-15
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