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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Turbo electRic Aircraft Design Environment (TRADE)
ID: 755458
Start date: 2017-09-01, End date: 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
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
Active Simulator Cockpit Enhancement
ID: 755652
Start date: 2017-06-01, End date: 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
High performance laser micro drilling machine for large Hybrid Laminar Flow Control suction panels
ID: 755620
Start date: 2017-06-01, End date: 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
INnovative Actuation Concepts for Engine/Pylon/Wing Separation FLOw Control (Design, Build and Wind Tunnel Test)
ID: 754307
Start date: 2017-06-01, End date: 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
ADvanced Aeroacoustic Processing Techniques
ID: 754881
Start date: 2017-09-01, End date: 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
Synthetic Jet flow Control CFD and Characterization
ID: 754811
Start date: 2017-10-01, End date: 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
Start date: 2017-06-01, End date: 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
Fully automated, controlled and versatile system for low cost, high rate and energy efficient production of highly loaded aeronautical structural parts
ID: 754274
Start date: 2017-06-01, End date: 2018-11-30
The main objective of the FALCON project is the design and manufacturing a versatile tooling system (reduction of tooling by up 40%) for the effective (30% reduction in time, 20% in cost and 20% in energy) and high quality (Aeronautic Quality Standards) production of CFRP...
Programme: H2020-EU.3.4.5.1.
Record Number: 210595
Last updated on: 2017-05-17
Development and Manufacturing of a Smart AFC Drive and Control System
ID: 754989
Start date: 2017-06-01, End date: 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
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List retrieved on: 2017-06-29