Forschungs- & Entwicklungsinformationsdienst der Gemeinschaft - CORDIS

Informationen von Horizont-2020-Projekten und nun auch Berichtzusammenfassungen stehen jetzt auf CORDIS bereit. Alle H2020-Projekte können jetzt vom Offenen Datenportal der EU heruntergeladen werden.

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Indra HVDC Distribution system
[PROJEKT] INDIS - Indra HVDC Distribution system
ID: 755654
Anfangsdatum: 2017-10-01, Enddatum: 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
HyBRid photocatalyitic air filtEr for rEmoving pollutants and odours from aircraft cabin ZonE
ID: 755563
Anfangsdatum: 2017-06-01, Enddatum: 2020-05-31
An aircraft cabin is a unique environment due to the extremely high density of occupation and limited available air volume. This favours the dispersion of germs and the accumulation of pollutants such as Volatile Organic Compounds (VOCs), polybrominated diphenyl ethers (PBDEs)...
Programme: H2020-EU.3.4.5.6.
Record Number: 210842
Last updated on: 2017-05-23
Development of Electromechanical Actuators and Electronic control Units for Flight Control Systems
ID: 738042
Anfangsdatum: 2017-02-01, Enddatum: 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.3.4.5.6.
Record Number: 208051
Last updated on: 2017-03-09
Optimization two phases cooling solution using micro pump brick
ID: 738094
Anfangsdatum: 2017-02-01, Enddatum: 2018-07-31
Traditionally, aeronautical power electronics use liquid and/or air forced cooling systems. These techniques are proven, reliable and robust technology but drawbacks are overweight and limited efficiency to extract heat flow generated in high power and dense converters.This...
Programme: H2020-EU.3.4.5.6.
Record Number: 208047
Last updated on: 2017-01-18
Eco Design: Composite functionalization: thermal and electricalconductivity
ID: 738047
Anfangsdatum: 2017-02-01, Enddatum: 2020-01-31
The aim is to reduce weight of metallic parts but keeping conductivity properties. Potential application is a valveactuator body for which EMI protection and bonding is required. Additionally it will be explored various manufacturing process with thermoplastic composites...
Programme: H2020-EU.3.4.5.6.
Record Number: 208050
Last updated on: 2017-01-26
Efficient Energy Management for Greener Aviation
ID: 737792
Anfangsdatum: 2017-02-01, Enddatum: 2021-01-31
The trend towards More Electric Aircraft with higher integration of different sub-systems into a common energy network requires innovative approaches for the energy management. First, a well-designed energy management saves energy by optimizing power split. Second and more...
Programme: H2020-EU.3.4.5.6.
Record Number: 208044
Last updated on: 2017-01-26
Sensors for Oil COoling SYStem
[PROJEKT] SOCOSYS - Sensors for Oil COoling SYStem
ID: 738087
Anfangsdatum: 2017-02-01, Enddatum: 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.3.4.5.6.
Record Number: 208068
Last updated on: 2017-02-01
Injection Moulding with Continuous Local Reinforcements
ID: 738131
Anfangsdatum: 2017-02-01, Enddatum: 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.3.4.5.6.
Record Number: 208052
Last updated on: 2017-01-26
non-structural landing gear parts made of composite
ID: 737721
Anfangsdatum: 2017-02-01, Enddatum: 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.3.4.5.6.
Record Number: 208053
Last updated on: 2017-03-07
SEaSiDE (Smart Electro-expulsive System for SAT Aircrafts De-Icing)
ID: 738043
Anfangsdatum: 2017-02-01, Enddatum: 2020-01-31
Aviation has become an indispensable part of European transportation system, however, the system as it existstoday is reaching full capacity and beginning to limit mobility. In addition, there is a demand formore people and goods to travel faster and farther, with fewer...
Programme: H2020-EU.3.4.5.6.
Record Number: 207699
Last updated on: 2016-12-26
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List retrieved on: 2017-06-23