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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Developing advanced Engine Multi-disciplinary Optimization Simulations (DEMOS)
ID: 686340
Start date: 2016-01-01, End date: 2019-12-31
The “Innovative Aircraft Architecture” technology stream of the Clean Sky 2 Airframe ITD focuses on advanced power-plant solutions (such as CROR and UHBR) that are able to deliver a significant gain in aircraft performance. Project DEMOS will develop advanced predictive...
Programme: H2020-EU.3.4.5.4.
Record Number: 199447
Last updated on: 2015-12-15
Simulation tool development for a composite manufacturing process default prediction integrated into a quality control system
ID: 686493
Start date: 2016-01-01, End date: 2018-12-31
Resin Transfer Moulding (RTM) involves moderate pressure resin injection of a dry preform placed in sealed rigid tooling. Fast and effective processing requires correct placement of the reinforcement to avoid defects and potential race tracking, appropriate selection of inlet...
Programme: H2020-EU.3.4.5.4.
Record Number: 199349
Last updated on: 2017-02-14
Integration of Innovative Ice Protection Systems
ID: 785550
Start date: 2018-03-01, End date: 2020-02-29
This proposal fits within the framework of aircraft effectiveness constant improvement by reducing fuel and power consumptions. Its ultimate goal is to economically remove ice accreting on aircraft structure critical parts and thus increase reliability and mass saving on the...
Programme: H2020-EU.3.4.5.4.
Record Number: 213822
Last updated on: 2018-02-22
Composite joints for improved mechanical and electrical performance
ID: 755609
Start date: 2017-04-01, End date: 2019-09-30
CC-JOINTS will explore new innovative joint designs that can be broadly described in two ways:• Modification of the metal in order to facilitate improved joint strength• Introduction of through-thickness reinforcements that can improve the composite performance and provide...
Programme: H2020-EU.3.4.5.4.
Record Number: 210008
Last updated on: 2017-04-11
Collaborative OWA robots for drilling and fasteners insertion in assembly lines
ID: 738200
Start date: 2017-02-01, End date: 2020-01-31
The overall objective of the CORDIAL project is to develop a new compact drilling and fastening unit for One Way Assembly. The effector has to be used by operator or lightweight industrial robots. Six sub-objectives contribute to achieve such a goal:- To define how robots and...
Programme: H2020-EU.3.4.5.4.
Record Number: 208045
Last updated on: 2017-02-14
In situ manufactured carbon-thermoplast curved stiffened panel
ID: 686894
Start date: 2016-01-01, End date: 2018-01-31
INSCAPE (In situ manufactured carbon-thermoplast curved stiffened panel) main objective is to enhance the automated thermoplastic fiber placement process and machine to manufacture an in situ consolidated double-curved structure including in situ joining of stiffener and skin...
Programme: H2020-EU.3.4.5.4.
Record Number: 199354
Last updated on: 2017-08-17
TRANSITION -  Tool-Part-Interaction simulation process linked to laminate quality
ID: 717145
Start date: 2016-07-01, End date: 2019-06-30
Highly integrated, complex composite structures require a thorough evaluation of processing tools and parameters in order to achieve a competitive time-to-market as well as a cost efficient solution. The link between processing conditions and final laminate quality as to...
Programme: H2020-EU.3.4.5.4.
Record Number: 205633
Last updated on: 2017-02-14
Aerodynamic and acouStic for high-by-Pass ratIo tuRbofan intEgration
ID: 681856
Start date: 2016-01-01, End date: 2018-09-30
The ASPIRE proposal, gathering DLR, NLR, ONERA and TsAGI, responds to the topic JTI-CS2-2014-CFP01-AIR-01-01 “Aerodynamic and acoustic capabilities developments for close coupling, high by-pass ration turbofan Aircraft integration”. The comprehensive experience of the...
Programme: H2020-EU.3.4.5.4.
Record Number: 199347
Last updated on: 2017-08-22
Optimisation of Friction Stir Welding (FSW) and Laser Beam Welding (LBW) for assembly of structural aircraft parts
ID: 785557
Start date: 2018-02-01, End date: 2020-07-31
Riveting is the defacto method for the assembly of aluminium aerostructures, with large commercial aircraft fuselages typically containing 100’000s of rivets. However, riveting is known as a time-consuming, expensive and weight-adding operation. From a design perspective, it...
Programme: H2020-EU.3.4.5.4.
Record Number: 213824
Last updated on: 2018-02-22
Metitalia prototype tooling for fuselage panel
ID: 785534
Start date: 2018-02-01, End date: 2018-11-30
This proposal responds to the call of Clean Sky 2 JTI-CS2-2017-CFP06-AIR-02-50, Prototype Tooling for subcomponents manufacturing for fuselage. The aim of this Call for Proposal is to develop, design, manufacture and deliver to the Topic Manager facilities, all the prototype...
Programme: H2020-EU.3.4.5.4.
Record Number: 213821
Last updated on: 2018-02-22
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List retrieved on: 2018-02-24
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