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 2 - BALANCE (Business Aviation Laminar Nacelle)
BALANCE (Business Aircraft LAminar NaCellE) is a 20 month research and innovation project in the field of aeronautical engineering, launched in January 2016. The global strategic objective behind the BALANCE project is to provide technologies that enable reduction of the drag...
Programme: H2020-EU.3.4.5.4.
Record Number: 198699
Last updated on: 2017-05-23
Periodic Reporting for period 1 - RESET (Re-use of Thermoplastic Composite)
Current European policies plead for new technologies capable to implement feasible processes for recycling of products in their end of life cycle. Within this framework the re-use of thermoplastic composites, is a recurrent topic within the aircraft manufacturing industry...
Programme: H2020-EU.3.4.5.4.
Record Number: 198194
Last updated on: 2017-05-17
Periodic Reporting for period 1 - ASPIRE (Aerodynamic and acouStic for high-by-Pass ratIo tuRbofan intEgration)
The latest engine technologies, which are about to enter into service around 2025 via the new generation of engines of for new Aircraft (Short range or Long range), will offer a substantial specific fuel consumption (SFC) improvement of 15-17% compared with reference EIS 2000...
Programme: H2020-EU.3.4.5.4.
Record Number: 198557
Last updated on: 2017-05-22
Composite tool for winglet manufacturing
ID: 738220
Start date: 2017-02-01, End date: 2019-03-31
An all composite tool for the manufacturing of winglet pairs will be designed and manufactured. The tool will be self heated. Separate cavities will be fed by a single injection system, ensuring identical quality and dimensional tolerances for both winglets.
Programme: H2020-EU.3.4.5.4.
Record Number: 208823
Last updated on: 2017-03-09
DESIGN AGAINST DISTORTION WITH LAYUP AND SHAPE OPTIMIZATION OF CARBON-EPOXY AEROSPACE COMPOSITES
ID: 716864
Start date: 2016-09-01, End date: 2019-02-28
In the “DADIYSO COMP” project Swerea SICOMP covers the entire topic and will be the only partner. Swerea SICOMP will develop an FE-based simulation tool for rapid predictions of cure induced part distortions including sub models for cure kinetics, glass transition, and...
Programme: H2020-EU.3.4.5.4.
Record Number: 204217
Last updated on: 2016-05-31
CROR Engine debris Middle level Impact and Mechanical test
ID: 715873
Start date: 2016-09-01, End date: 2019-08-31
This project focus on the analysis of different shielding configurations to protect a rear-end structure of an open rotor aircraft from an engine failure. The analysis will be performed against simple panels in the first place. The best configurations will then be studied as...
Programme: H2020-EU.3.4.5.4.
Record Number: 204212
Last updated on: 2017-05-17
Robotized Orbital Drilling Equipment and Optimized residual stresses
ID: 738219
Start date: 2017-02-01, End date: 2020-01-31
The main objective of the RODEO project is to propose a lightweight robotized orbital drilling equipment, and associated operating conditions and tools, to enable the drilling of tightly spaced small diameter holes in aluminium with the control of induced residual stresses...
Programme: H2020-EU.3.4.5.4.
Record Number: 208062
Last updated on: 2017-01-12
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.3.4.5.4.
Record Number: 207704
Last updated on: 2016-12-23
Forming and Modular Integration of Thermoplastics
ID: 738044
Start date: 2016-12-01, End date: 2019-05-31
The main objective of FORMIT is to develop a modular tooling to integrate a wing upper skin and an external wing leading edge with several T-Shape and omega stringers. Skins will be laminated on the integration tool by Topic Manager with Automated Fiber Placement technology...
Programme: H2020-EU.3.4.5.4.
Record Number: 207496
Last updated on: 2016-12-15
Adaptive Multifunctional Test Rigs for Aeronautical Structures
ID: 738228
Start date: 2017-01-01, End date: 2018-12-31
CleanSky2 has addressed the development of new aircraft concepts and architectures including new materials and manufacturing. In this respect, Adaptive Multifunctional Test Rigs for Aeronautical Structures (AMTRAS project) will contribute to the CleanSky2 objectives with the...
Programme: H2020-EU.3.4.5.4.
Record Number: 207253
Last updated on: 2016-12-08
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List retrieved on: 2018-04-22
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