Servicio de Información Comunitario sobre Investigación y Desarrollo - CORDIS

CORDIS reúne toda la información sobre los proyectos financiados por Horizonte 2020 , y ahora también resúmenes de los informes relacionados. Se puede descargar toda la documentación de estos proyectos en el Portal de datos abiertos de la UE .

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New Additive manufacTuring Heat ExchaNger for Aeronautic
ID: 785520
Fecha de inicio: 2018-03-01, Fecha de finalización: 2022-02-28
New Additive manufacTuring Heat ExchaNger for AeronauticToday’s technologies and processes dedicated to the exchangers manufacturing hamper progress on higher performances (mechanical assies of repetitive and regular unitary components like folded sheet metal and/or tubing...
Programme: H2020-EU.3.4.5.1.
Record Number: 213938
Last updated on: 2018-03-14
Keel beam manufacturing oriented solution
ID: 785435
Fecha de inicio: 2018-03-01, Fecha de finalización: 2019-08-31
The Project address the manufacturing of a keelbeam using thermoplastic resin reinforced with carbon fiber. The use of manufacturing technologies with a lot of potential for automation is also explored.The Main target of reducing assembly cost is addressed with minimizing the...
Programme: H2020-EU.3.4.5.1.
Record Number: 213811
Last updated on: 2018-02-22
Coatings with Hydrophobic and/or Omniphobic Properties against INsect contamination.
ID: 785484
Fecha de inicio: 2018-03-01, Fecha de finalización: 2021-02-28
The aircraft industry has long been concerned with the increase of drag impacting directly the fuel consumption of airplanes. Different researches have shown that the insect sticking causes a surface roughness disrupting the laminar flow. Several methods have been used to...
Programme: H2020-EU.3.4.5.1.
Record Number: 213937
Last updated on: 2018-03-14
MULTI-PHYSICS METHODOLOGY FOR PHASE CHANGE DUE TO RAPIDLY DEPRESSURISED TWO-PHASE FLOWS
ID: 785549
Fecha de inicio: 2018-03-01, Fecha de finalización: 2020-02-29
A multi-physics methodology is proposed to couple CFD calculations with models for phase change of rapidly depressurised mist of a fire suppression system. The methodology combines existing models with newly developed ideas with considers the coupling between large and small...
Programme: H2020-EU.3.4.5.1.
Record Number: 213823
Last updated on: 2018-02-22
Wind tunnel test for flow control at the engine/pylon with a representative aircraft configuration under fully realistic flow conditions
ID: 738196
Fecha de inicio: 2017-01-01, Fecha de finalización: 2018-12-31
The Active Flow Wind tunnel Test (AFloWTest) project considers the testing of a realistic high lift configuration half-model with a large and with a Ultra High Bypass Ratio (UHBR) flow-through nacelle. An existing half model will be adapted with an UHBR nacelle and for the...
Programme: H2020-EU.3.4.5.1.
Record Number: 207701
Last updated on: 2016-12-23
Periodic Reporting for period 1 - TAVAC (Technologies for Active Vibration and Acoustic Comfort)
In aircraft cabin environments, vibrations and noise co-exist which affect the passenger comfort and quality of flight. Vibrations are typically generated by two main sources: (1) the aircraft engines (turbojet or turboprop) rotating at high speeds and transferred via the...
Programme: H2020-EU.3.4.5.1.
Record Number: 232142
Last updated on: 2018-06-22
Structural pOweR CompositEs foR futurE civil aiRcraft
ID: 738085
Fecha de inicio: 2017-02-01, Fecha de finalización: 2020-01-31
In SORCERER revolutionary lightweight electrical energy storing composite materials for future electric and hybrid-electric aircraft are to be developed. Building on previous research novel lightweight supercapacitor composites, structural battery and structural energy...
Programme: H2020-EU.3.4.5.1.
Record Number: 207252
Last updated on: 2017-03-20
ITEMB: Integrated Full Composite Main Landing Gear Bay Concept
ID: 717190
Fecha de inicio: 2016-09-01, Fecha de finalización: 2018-08-31
The standard solution of a landing gear integrated into the wings, that is widely used in the actual single aisle aircraft configuration, even if extensively safe in terms of structural load distribution, leads to many drawbacks both referred to the structural configuration...
Programme: H2020-EU.3.4.5.1.
Record Number: 205612
Last updated on: 2016-07-12
Design, test, and manufacturing of robust fluidic actuators
ID: 715796
Fecha de inicio: 2016-06-01, Fecha de finalización: 2019-05-31
This project adresses the development of two-stage no-moving-parts fluidic actuator systems for use in active flow control applications. The work is based on the actuator technology created in the EC-funded Clean Sky projects DT-FA-AFC, FloCoSys, and robustAFC, but goes vastly...
Programme: H2020-EU.3.4.5.1.
Record Number: 204211
Last updated on: 2016-06-02
TItanium COmposite Adhesive JOints
[PROYECTO] TICOAJO - TItanium COmposite Adhesive JOints
ID: 737785
Fecha de inicio: 2017-02-01, Fecha de finalización: 2019-01-31
Future aircraft will have to be more fuel efficient in order to accomplish sustainable air transport growth. One of the key enablers to achieve this fuel efficiency is drag reduction by improved aerodynamic efficiency. On its turn, a key enabler within this aerodynamic...
Programme: H2020-EU.3.4.5.1.
Record Number: 208060
Last updated on: 2017-01-18
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