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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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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.
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.
Record Number: 200865
Last updated on: 2017-07-07
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.
Record Number: 211049
Last updated on: 2017-07-12
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.
Record Number: 211047
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.
Record Number: 211045
Last updated on: 2017-07-12
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.
Record Number: 210625
Last updated on: 2017-05-18
Sensors for Oil COoling SYStem
[PROJECT] SOCOSYS - Sensors for Oil COoling SYStem
ID: 738087
Start date: 2017-02-01, End date: 2018-07-31
Oil cooling machines are the preferred solution in the aeronautic field to cool electrical rotating machines as they allow more compact equipment and more efficient and stable heating transfer. However they suffer some limitations: they provide only binary information, lack...
Programme: H2020-EU.
Record Number: 208068
Last updated on: 2017-02-01
non-structural landing gear parts made of composite
ID: 737721
Start date: 2017-02-01, End date: 2019-07-31
The objective of this proposal is to develop, manufacture and test non-structural landing gear parts for helicopter and aircrafts based on advance carbon fiber material system, the proposal introduce the methods, capabilities and resources of IAI and CirComp to fulfill the...
Programme: H2020-EU.
Record Number: 208053
Last updated on: 2017-03-07
Injection Moulding with Continuous Local Reinforcements
ID: 738131
Start date: 2017-02-01, End date: 2020-01-31
In the IMCoLoR project the scroll of an air cycle machine is manufactured with an injection molding process with the local integration of continuous carbon fiber reinforcements. The local reinforcements are placed along the main load paths in order to lead to a higher pressure...
Programme: H2020-EU.
Record Number: 208052
Last updated on: 2017-01-26
Development of Electromechanical Actuators and Electronic control Units for Flight Control Systems
ID: 738042
Start date: 2017-02-01, End date: 2019-01-31
Nowadays, there is a trend towards the More-Electric Aircraft (MEA) concept. MEA would replace the secondary aircraft power systems (electric, hydraulic and pneumatic) with a globally optimized electrical system. However, the architecture of the electric system must be...
Programme: H2020-EU.
Record Number: 208051
Last updated on: 2017-07-12
12 3 4 > 
List retrieved on: 2017-12-18
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