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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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
Project to Lead Ecodesign Integration with Aerospace Development and Engineering Systems
ID: 715775
Start date: 2016-08-01, End date: 2020-07-31
The primary industrial objective of the PLEIADES project is to enable an integrated approach to the industry focused eco-design of aerospace products as part of existing engineering development workflows. The project will focus on the further development of the existing...
Programme: H2020-EU.3.4.5.5.
Record Number: 205411
Last updated on: 2017-04-05
Orbiting Journal Bearing Experiment
ID: 738176
Start date: 2017-03-01, End date: 2019-02-28
This proposal addresses call JTI-CS2_2016-CFP03-ENG-03-09 entitled “Orbiting Journal Bearing Rig Test”. We show that all requirements identified in the call can be met within the timescale and budget allocated for this call. Indeed, the approach taken to the research goes...
Programme: H2020-EU.3.4.5.5.
Record Number: 208043
Last updated on: 2017-01-26
inveSTigation of an ultrA compact Reverse flow combusTor
ID: 785217
Start date: 2018-02-01, End date: 2020-01-31
The main objective of START project is to carry out a series of advanced investigations on a prototypical reverse flow, ultra compact, combustor designed and manufactured by GE-Avio for turboprop engine as a part of the SAT ITD MAESTRO. The aim is to support the validation of...
Programme: H2020-EU.3.4.5.5.
Record Number: 213585
Last updated on: 2018-02-22
Adding Simulation to the Corporate ENvironmenT for Additive Manufacturing
ID: 714246
Start date: 2016-08-01, End date: 2019-07-31
The achievement of the Clean Sky 2 (CS 2) objectives, concerning the reduction of CO2 and fuel burn by up to 30 % as well as the reduction of NOX by up to 40 %, is strongly associated with the availability of innovative technologies and adapted structural design. Additive...
Programme: H2020-EU.3.4.5.5.
Record Number: 205690
Last updated on: 2017-02-14
Combustion species Imaging Diagnostics for Aero-engine Research
ID: 785539
Start date: 2018-03-01, End date: 2020-08-31
The CIDAR project is the result of a Consortium formed by Academic Parties (Manchester, Strathclyde and Edinburgh Universities), a Research and Development Organization (INTA) and private companies (DAS and OptoSci). Therefore, CIDAR builds upon the expertise of the UK's and...
Programme: H2020-EU.3.4.5.5.
Record Number: 213940
Last updated on: 2018-03-14
Crack growth threshold analysis in TiAl alloys
ID: 686711
Start date: 2016-03-01, End date: 2019-10-31
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
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
Advanced mechatronics devices for a novel turboprop Electric starter-generator and health monitoring system
ID: 737814
Start date: 2017-01-16, End date: 2020-01-15
The ACHIEVE Consortium will bring together their world-leading expertise in the design and manufacturing of electrical machines for aircraft Advanced Generation Systems (AGS), integrated Power Electronics (PE), advanced control systems and intelligent thermal management, to...
Programme: H2020-EU.3.4.5.5.
Record Number: 207250
Last updated on: 2016-12-08
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List retrieved on: 2018-04-23
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