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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Results 1 - 10 of 113
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Periodic Reporting for period 1 - TR4EMACS (Flexible Test Rig of Aircraft Control Surfaces powered by EMAs)
This proposal applies to a topic is intended to support the development of all electrical wing actuated and sourced Regional Turboprop Aircraft concept (FTB2 demonstrator). The topic targets four control surfaces, which are actuated by electro-mechanical actuators (EMAs).The...
Programme: H2020-EU.
Record Number: 242602
Last updated on: 2018-11-29
Flexible Test Rig of Aircraft Control Surfaces powered by EMAs
ID: 738110
Start date: 2017-06-01, End date: 2020-11-30
The objective of this project is the design, manufacture and power on of a flexible and complete test rig for the on ground complete evaluation and validation of electromechanical actuators (EMA) and corresponding control units that will equip the control surfaces of the wings...
Programme: H2020-EU.
Record Number: 207704
Last updated on: 2016-12-23
Evaluation of the Benefits of innovative Concepts of laminar nacelle and HTP installed on a business jet configuration
ID: 821048
Start date: 2018-11-01, End date: 2019-10-31
The global target of the project “BinCola” is the experimental verification of benefits coming along with the replacement of classically designed nacelles and HTP by enhanced components specifically developed for natural laminar flow (NLF) development. To ensure a...
Programme: H2020-EU.
Record Number: 218818
Last updated on: 2018-11-20
EUropean LOw Speed Aircraft Model at high Reynolds II
ID: 821020
Start date: 2018-10-01, End date: 2020-03-31
In laminar flow investigations, several parameters related to manufacturing quality of the aircraft wind tunnel model have to be taken into account since they can strongly affect the laminar-turbulent transition location. Model shape, steps and gaps, waviness and surface...
Programme: H2020-EU.
Record Number: 218768
Last updated on: 2018-11-20
ReliabilitY of opto-Transceivers for Health Monitoring Systems
ID: 821336
Start date: 2018-11-01, End date: 2021-10-31
For aeronautic applications, in-service Structural Health Monitoring (SHM) is now established as a key technique to assess the performance and the integrity of composite aircraft structures for real-time in situ monitoring. In space industry, the Assembly Integration and Test...
Programme: H2020-EU.
Record Number: 218778
Last updated on: 2018-11-20
Development of Integrated MEasurement Systems
ID: 820951
Start date: 2019-01-01, End date: 2020-12-31
The aim of the project is to develop advanced integrated testing methods that have the capability to detect a crack or delamination in a metallic or composite structure and have the potential to be deployed as part of an on-board structural health monitoring system for...
Programme: H2020-EU.
Record Number: 218805
Last updated on: 2018-11-20
Light weight airframe structures through combination with high performance materials
ID: 821276
Start date: 2018-11-01, End date: 2020-08-31
A further step towards more light weight airframe parts is the combination of existing materials with new high performance materials. This project aims at qualifying new high performance materials for airframe structures following a bulding block approach. To do so, the three...
Programme: H2020-EU.
Record Number: 218798
Last updated on: 2018-11-20
ID: 821339
Start date: 2018-11-01, End date: 2021-10-31
The RADIANT Project has for ambition to create the smartest self-limiting heating system integrated on cabin panel to revolutionize the thermal comfort of Aircraft while contributing to the competitiveness of our industry. The consortium members are HUTCHINSON, a world leader...
Programme: H2020-EU.
Record Number: 218628
Last updated on: 2018-11-15
ADDitive mAnufacturing oPTimized TAilored SEALS
ID: 821040
Start date: 2018-10-01, End date: 2020-03-31
Primary mission of the wing and the different aerodynamic surfaces is creating lift as optimum as possible. Elastic seals are needed to avoid the air to flow by the gaps between the different surfaces that could cause a malfunction of the aerodynamic component or even the...
Programme: H2020-EU.
Record Number: 218607
Last updated on: 2018-11-15
Flexible RTM tool with automated distortion correction
ID: 821488
Start date: 2018-09-01, End date: 2020-08-31
The FLEX proposal answers to the scope of JTI-CS2-2017-CfP07-AIR-01-33 call on the topic “Flexible RTM tool concept for composites with spring back adjustments capabilities”. The high-level challenge FLEX project will be addressing is to develop the next generation RTM...
Programme: H2020-EU.
Record Number: 218288
Last updated on: 2018-11-13
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List retrieved on: 2018-12-13
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