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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Periodic Reporting for period 1 - ACOTAAL (Automation COncepts and Technologies for Aircraft Assembly Lines in the Aircraft Factory of the Future)
Final assembly of aircrafts including structural assembly, system and cabin installation is today largely a craft based activity, which is also true for the supporting activities like logistics. The assembly process is essentially manual and use of automated or robotic means...
Programme: H2020-EU.3.4.5.1.
Record Number: 198413
Last updated on: 2017-05-19
Simulations of CrOr and fan broadband NoisE with reduced order modelling
ID: 755543
Fecha de inicio: 2017-09-01, Fecha de finalización: 2020-12-31
The prediction of Open Rotor and UHBR Fan broadband noise on realistic configurations is still an open challenge. The two major sources of broadband noise are the trailing edge noise and the wake interaction noise. The first source is related to a strong vortex shedding at the...
Programme: H2020-EU.3.4.5.1.
Record Number: 211043
Last updated on: 2017-05-30
High performance laser micro drilling machine for large Hybrid Laminar Flow Control suction panels
ID: 755620
Fecha de inicio: 2017-06-01, Fecha de finalización: 2020-05-31
The main goal of the Hyper-Drill project is the development of a laser micro-drilling machine prototype for the manufacture of Hybrid Laminar Flow Control (HLFC) titanium suction panels with dimensions up to 5 m x 2 m and able to fulfil the requirement of a production rate ≥...
Programme: H2020-EU.3.4.5.1.
Record Number: 210622
Last updated on: 2017-05-17
Active Simulator Cockpit Enhancement
ID: 755652
Fecha de inicio: 2017-06-01, Fecha de finalización: 2019-05-31
The main objective of ASCENT project is to implement the concepts and define other novel functions up to a functional demonstration (pilot in the loop simulation when relevant), in order to validate the functional requirements. The enhance Active Cockpit simulator enviroment...
Programme: H2020-EU.3.4.5.1.
Record Number: 210624
Last updated on: 2017-05-17
ADvanced Aeroacoustic Processing Techniques
ID: 754881
Fecha de inicio: 2017-09-01, Fecha de finalización: 2020-08-31
Airbus is currently conducting various experimental studies, dealing with installing microphones on the fuselage, on the wall of a wind tunnel test section or on specific microphone supports on the flow, in order to record the sounds emitted by each aircraft component (i.e...
Programme: H2020-EU.3.4.5.1.
Record Number: 210828
Last updated on: 2017-05-23
INnovative Actuation Concepts for Engine/Pylon/Wing Separation FLOw Control (Design, Build and Wind Tunnel Test)
ID: 754307
Fecha de inicio: 2017-06-01, Fecha de finalización: 2020-09-30
The objective of the INAFLOWT project is to use combinations of existing active flow control (AFC) concepts to generate a major advance in AFC aerodynamic efficiency and reliability. Steady suction in combination with oscillatory blowing will be combined using arrays of the...
Programme: H2020-EU.3.4.5.1.
Record Number: 210820
Last updated on: 2017-05-23
Development and Manufacturing of a Smart AFC Drive and Control System
ID: 754989
Fecha de inicio: 2017-06-01, Fecha de finalización: 2019-09-30
The project FloCoS will focus on an integrated flow control actuator driving system taking into account the specific requirements of piezoelectrically driven Synthetic Jet Actuators. The system will be divided into two different main parts: The amplifier unit on the one hand...
Programme: H2020-EU.3.4.5.1.
Record Number: 210612
Last updated on: 2017-05-18
Synthetic Jet flow Control CFD and Characterization
ID: 754811
Fecha de inicio: 2017-10-01, Fecha de finalización: 2020-09-30
The objective of the project is is to develop scale models for the Synthetic Jet Actuator (SJA), that shall be used to enable the design of next generation SJA’s, compared to state of the art. The development of this scale model is intented for improvement of performance...
Programme: H2020-EU.3.4.5.1.
Record Number: 210610
Last updated on: 2017-05-17
Multiscale Analysis of AiRframe Structures and Quantification of UncErtaintieS System
ID: 754581
Fecha de inicio: 2017-06-01, Fecha de finalización: 2020-05-31
MARQUESS has been specifically designed to address the challenges outlined in the Topic Description reference JTI-CS2-2016-CFP04-LPA-02-15 to fit into the activities of WP2.4.3 in the LPA IADP in Clean Sky 2. MARQUESS will serve as a valuable precursor to the above as it will...
Programme: H2020-EU.3.4.5.1.
Record Number: 210608
Last updated on: 2017-05-18
Turbo electRic Aircraft Design Environment (TRADE)
ID: 755458
Fecha de inicio: 2017-09-01, Fecha de finalización: 2020-02-29
The improvement potential in conventional aero engines will be realized over the next decades. While a number of evolutionary improvements remain, the limits to thermal efficiency are becoming visible in terms of material constraints, NOx emissions and engine operability. The...
Programme: H2020-EU.3.4.5.1.
Record Number: 210614
Last updated on: 2017-05-23
12 3 4 5 > 
List retrieved on: 2017-09-22
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