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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Periodic Reporting for period 1 - PLEIADES (Project to Lead Ecodesign Integration with Aerospace Development and Engineering Systems)
The primary industrial objective of the PLEIADES project is to enable an integrated approach for the eco-design of aerospace products.• Combining engineering, environmental, sustainability, and business considerations, particularly through the linking role of materials and...
Programme: H2020-EU.3.4.5.5.
Record Number: 242620
Last updated on: 2018-11-30
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
ADVANCE: Sophisticated experiments and optimisation to advance an existing CALPHAD database for next generation TiAl alloys
ID: 820647
Start date: 2018-10-01, End date: 2021-09-30
To meet the Clean Sky 2 goals to reduce aircraft noise and CO2 and NOx emissions, an optimised titanium aluminide (TiAl) CALPHAD database is needed. Such a database is an integral step to meet these goals as it can be used in the aviation industry to improve existing alloys...
Programme: H2020-EU.3.4.5.5.
Record Number: 218769
Last updated on: 2018-11-20
Smart Acoustic Lining for UHBR Technologies Engines
ID: 821093
Start date: 2018-11-01, End date: 2022-04-30
Reducing noise emissions is one of the main design targets driving the development of new aircraft engines, and is therefore a key priority for the competitiveness of the aerospace sector. Ultra-high bypass ratios (UHBR) turbofan engines are expected to equip the next...
Programme: H2020-EU.3.4.5.5.
Record Number: 218789
Last updated on: 2018-11-20
Aicraft Design and nOise RatiNg for regiOnal aicraft
ID: 821043
Start date: 2018-11-01, End date: 2022-10-31
Aicraft Design and nOise RatiNg for regiOnal aicraft. The activities related to the ADORNO project are focused on the development of aircraft models for a regional aircraft engine platform. The main objective is to provide aircraft requirements (e.g. thrusts, offtakes...
Programme: H2020-EU.3.4.5.5.
Record Number: 218606
Last updated on: 2018-11-15
Development and validation of a powder HIP route for high temperature Astroloy to manufacture Ultrafan® IP Turbine Casings
ID: 821044
Start date: 2018-10-01, End date: 2021-09-30
This is a response to the Call for Proposal under Clean Sky 2 and JU to manufacture IP Turbine casings for the new generation Ultrafan® engine from Astroloy using Net Shape Hot Isostatic Pressing of powder (NSHIP). Astroloy with high γ’ volume fraction have the required...
Programme: H2020-EU.3.4.5.5.
Record Number: 218608
Last updated on: 2018-11-15
FLOw control in RAdial compressor
ID: 820099
Start date: 2018-09-01, End date: 2022-08-31
The enhancement of an engine operability involves increasing the compressor surge margin which is still an open challenge. The project FLORA (FLOw control in RAdial compressor) is twofold.First, it proposes to achieve a comprehensive understanding of the transient behavior of...
Programme: H2020-EU.3.4.5.5.
Record Number: 218091
Last updated on: 2018-11-12
Cooled Fast-Response Wall Pressure Taps for Combustion Chamber Measurements
ID: 820946
Start date: 2018-11-05, End date: 2021-05-04
FAST TAPS aims at designing, validating and put in operation 8 cooled fast-response wall pressure taps for combustion chamber measurements.The project is based upon a three steps approach, the three technical work packages of the project, with two distinct iterative design and...
Programme: H2020-EU.3.4.5.5.
Record Number: 218314
Last updated on: 2018-11-13
Experimental Aero- and Thermal investigation for a next generation Engine Exit Module
ID: 821398
Start date: 2018-10-01, End date: 2021-03-31
A unique facility for experimental testing of engine exit modules (EEM) at engine-realistic flow conditions is currently available at Chalmers University of Technology and will be used to address this JTP action. The unique design of the facility includes an open test section...
Programme: H2020-EU.3.4.5.5.
Record Number: 218202
Last updated on: 2018-11-13
FLOw COntrol TEChniques Enabling Increased Pressure Ratios in Aero Engine Core Compressors for Ultra-High Propulsive Efficiency Engine Architectures
ID: 821435
Start date: 2018-10-01, End date: 2022-03-31
The ultra-high propulsive efficiency demonstrator engine developed by Safran Aircraft Engines and GE Germany (GEDE) within Clean Sky 2 promises a considerable reduction of pollutant and noise emissions as well as aero engine fuel burn. While the geared architecture allows a...
Programme: H2020-EU.3.4.5.5.
Record Number: 218242
Last updated on: 2018-11-13
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List retrieved on: 2018-12-10
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