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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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VALidation tests of ElectroMechanical Actuators and its dedicated control units at TRL 6 level
ID: 755615
Start date: 2017-06-01, End date: 2019-05-31
The objective of the VALEMA project is twofold:- On the one hand it is required to manufacture and assembly units (EMAs and ECUs) previously designed and developed according to the JTI-CS2-2016-CFP03-SYS-02-14 Call (Development of electromechanical actuators and electronic...
Programme: H2020-EU.3.4.5.6.
Record Number: 211049
Last updated on: 2017-05-31
Advanced ventilation techniques for modern long-range passenger aircraft to promote future energy management systems
ID: 755596
Start date: 2017-09-01, End date: 2021-08-31
Alternative or novel ventilation concepts with enhanced heat removal efficiency and local ventilation efficiency allow reconsidering the fresh air fraction of modern passenger aircraft cabins and thus help to save bleed air and energy in the future. In order to identify and...
Programme: H2020-EU.3.4.5.6.
Record Number: 211047
Last updated on: 2017-05-30
Innovative COoling system for embedded Power Electronics
ID: 755556
Start date: 2017-06-01, End date: 2019-09-30
The main goal of this project is the design of innovative and efficient air cooled heat sinks to cool the power electronics modules that are a key component of the more electrical aircraft power management centre design. The new design is expected to be developed in two...
Programme: H2020-EU.3.4.5.6.
Record Number: 211044
Last updated on: 2017-05-30
FAil-Safe Electro-mechanical actuation for LAnding Gear
ID: 755562
Start date: 2017-07-01, End date: 2020-06-30
The adoption of electrical equipment for flight-critical applications in future aircrafts is motivated by a number of economic and environmental considerations. Also thank to several research programs, EMA systems are now viewed as the best candidate for the aircraft of the...
Programme: H2020-EU.3.4.5.6.
Record Number: 211045
Last updated on: 2017-06-29
High Luminescence In Cockpit
[PROJECT] HiLICo - High Luminescence In Cockpit
ID: 755497
Start date: 2017-06-01, End date: 2020-05-31
Although the market demand of displays bright enough to allow the diffusion of readable information against a very bright landscape is important, in particular in the avionics application, existing technologies still do not allow the desired brightness combined with very low...
Programme: H2020-EU.3.4.5.6.
Record Number: 211039
Last updated on: 2017-06-23
MULTIivariable Environmental Control System
ID: 755517
Start date: 2017-09-01, End date: 2020-08-31
The goal of this project is the development of a Multivariable Control System (MCS) by means of extended linearization techniques, based on a control-oriented thermodynamical modelling for the electric air conditioning pack. The focus will be on developing real-time capable...
Programme: H2020-EU.3.4.5.6.
Record Number: 211041
Last updated on: 2017-05-30
Aircraft Electrical Model Simulation Identification and Fitting Toolbox
ID: 755332
Start date: 2017-07-01, End date: 2020-06-30
The AEMS-IdFit (Aircraft Electrical Model Simulation Identification and Fitting Toolbox) project addresses the requirement for developers of future MEA aircraft to select technologies and to test, verify and validate electrical system architectures. The limitations of weight...
Programme: H2020-EU.3.4.5.6.
Record Number: 211034
Last updated on: 2017-05-30
Diode Die Fatigue Characterisation and Testing
ID: 686454
Start date: 2016-01-01, End date: 2018-05-31
Future aircraft will use more electrical power, which increases the use of power electronics. The increased demand for electrical power also means that aircraft electrical generators must be scaled up accordingly. One type of power-electronic components is the power diode...
Programme: H2020-EU.3.4.5.6.
Record Number: 199472
Last updated on: 2015-12-17
Periodic Reporting for period 1 - DiDi-FaCT (Diode Die Fatigue Characterisation and Testing)
Future aircraft will use a large amount of electrical power. Not only are extra systems needed for e.g. in-flight entertainment, communication and passenger comfort, but more importantly there is a trend to replace aircraft systems powered by oil or hot engine air (bleed air)...
Programme: H2020-EU.3.4.5.6.
Record Number: 200865
Last updated on: 2017-07-07
Indra HVDC Distribution system
[PROJECT] INDIS - Indra HVDC Distribution system
ID: 755654
Start date: 2017-10-01, End date: 2020-09-30
The INIDIS proposal, presented by INDRA SISTEMAS, try to answer in the best way the call JTI-CS2-2016-CFP04-SYS-03-07.The proposal is based in the prototype development for a new electrical power distribution system (or n-EPDS) to be placed in small aircraft and helicopter.The...
Programme: H2020-EU.3.4.5.6.
Record Number: 210625
Last updated on: 2017-05-18
12 3 4 > 
List retrieved on: 2017-07-21
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