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Le informazioni sui progetti di Orizzonte 2020 e ora anche le relative sintesi delle relazioni sono disponibili su CORDIS. Tutti i progetti H2020 possono essere scaricati dal Portale Open Data dell'UE .

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Results 1 - 10 of 45
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Manufacturing of Integral Stiffened Skin Panels
ID: 755641
Data di inizio: 2017-05-01, Termine: 2019-10-31
MISSP (Manufacturing of Integral Stiffened Skin Panels) project aims at proposing new manufacturing concepts for metallic aircraft cargo doors. The main objective of this project will be to develop cheaper and greener structures as an alternative to CFRP doors but also...
Programme: H2020-EU.3.4.5.4.
Record Number: 210009
Last updated on: 2017-04-11
Composite joints for improved mechanical and electrical performance
ID: 755609
Data di inizio: 2017-04-01, Termine: 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
Development of methods for deriving optimized shapes ofmorphing structures considering both aerodynamic performancesand specific mechanical morphing boundary conditions
ID: 755068
Data di inizio: 2017-06-01, Termine: 2019-06-30
The OPTIMOrph project addresses the development of a robust and reliable numerical optimization methodology able to identify target shapes for deflected positions of morphing structures based on optimal aerodynamic characteristics (i.e. basically lift and drag), while taking...
Programme: H2020-EU.3.4.5.4.
Record Number: 210004
Last updated on: 2017-04-11
Composite tool for winglet manufacturing
ID: 738220
Data di inizio: 2017-02-01, Termine: 2018-07-31
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
Robotized Orbital Drilling Equipment and Optimized residual stresses
ID: 738219
Data di inizio: 2017-02-01, Termine: 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
low-coSt Printing of high-pErformanCe Thermoplastics foR structurAl appLications
ID: 737845
Data di inizio: 2017-01-01, Termine: 2018-12-31
The technology known as Fused Filament Fabrication (FFF) is one of the oldest known methods for 3D printing of objects. In fact, it was the first technology to be widely commercialized, and still has, by far, the largest presence on the market. In addition, printers based on...
Programme: H2020-EU.3.4.5.4.
Record Number: 207251
Last updated on: 2016-12-12
Innovative Re-Design and Validation of Complex Airframe Structural Components Formed by Additive Manufacturing for Weight and Cost Reduction
ID: 738002
Data di inizio: 2017-01-01, Termine: 2019-12-31
Additive manufacturing (AM) is a technology by which physical objects can be built directly from 3D Computer Aided Design (CAD) data, and is widely acknowledged as an enabler for revolutionizing the manufacturing landscape. It replaces traditional production methods like...
Programme: H2020-EU.3.4.5.4.
Record Number: 207502
Last updated on: 2016-12-15
Forming and Modular Integration of Thermoplastics
ID: 738044
Data di inizio: 2016-12-01, Termine: 2017-11-30
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
Development of innovative automated fibre placement machine for composite fuselage manufacturing with high performance hybrid materials
ID: 738114
Data di inizio: 2017-02-01, Termine: 2019-07-31
SMART-LAYUP activities described in the present proposal will contribute to develop and validate an advanced process of hybrid materials automated lay-up for manufacturing of regional aircraft composite fuselage which allows a significant reduction of the overall production...
Programme: H2020-EU.3.4.5.4.
Record Number: 208048
Last updated on: 2017-02-01
varnish and sol-gel multifunctional ProtectIve cLear cOat for aeronauTics
ID: 738123
Data di inizio: 2017-02-01, Termine: 2019-01-31
The project PILOT aims to develop two types of formulation technologies classes; a new UV hybrid varnish, which will combine the use of organic and silicone epoxy materials cured by the UV technology and a new hybrid solgel coating, where organic/silicone networks are...
Programme: H2020-EU.3.4.5.4.
Record Number: 208061
Last updated on: 2017-02-01
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List retrieved on: 2017-04-24