Wspólnotowy Serwis Informacyjny Badan i Rozwoju - CORDIS

Informacje o projektach programu „Horyzont 2020” , a teraz także streszczenia sprawozdań , są dostępne w serwisie CORDIS. Wszystkie projekty H2020 można pobrać z Portalu Otwartych Danych UE .

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Projekt (18)

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Distribution and Gauging Interconnected Fuel System for the Next Generation Civil Tilt Rotor
ID: 717069
Data rozpoczęcia: 2016-12-01, Data zakończenia: 2021-11-30
Secondo Mona, an established Italian aerospace SME with over 100 years of contributions to the aerospace industry, proposes to design, develop, test and qualify a high reliability integrated Fuel Gauging and Distribution System (DIGIFuel), providing active CG management, for...
Programme: H2020-EU.3.4.5.3.
Record Number: 206562
Last updated on: 2017-02-14
A.dditive MA.nufacturing for T.iltrotor HO.using
ID: 717194
Data rozpoczęcia: 2016-12-01, Data zakończenia: 2021-11-30
AMATHO (A.dditive MA.nufacturing T.iltrotor HO.using) is aimed to design, assess and manufacture a novel tiltrotor drive system housing exploiting the features of additive manufacturing techniques. Preliminarily, functional, structural and technological peculiarities of...
Programme: H2020-EU.3.4.5.3.
Record Number: 206580
Last updated on: 2017-02-14
High Speed HVDC Generator / Motor
[PROJEKT] HVDCGEN - High Speed HVDC Generator / Motor
ID: 738072
Data rozpoczęcia: 2017-03-01, Data zakończenia: 2022-08-31
The scope of the topic is to design, develop; test and flight qualify a high speed / high voltage direct current (HVDC) generator system with an integral motor function to be installed onto the Next Generation Civil Tilt Rotor.The Denis Ferranti Group addresses this scope...
Programme: H2020-EU.3.4.5.3.
Record Number: 208210
Last updated on: 2017-02-09
INnovative SmarT Electric Power Distribution
ID: 738064
Data rozpoczęcia: 2017-02-01, Data zakończenia: 2022-07-31
The INSTEP Consortium will bring together their world-leading expertise in aircraft Electrical Power Systems (EPS) and Power Electronics (PE) in order to design, develop, manufacture, test and provide qualification for flight of an innovative Power Distribution Units (PDUs)...
Programme: H2020-EU.3.4.5.3.
Record Number: 208064
Last updated on: 2017-01-26
Design and Realization of equipped engine compartments including cowling for a fast compound rotorcraft
ID: 737955
Data rozpoczęcia: 2017-01-01, Data zakończenia: 2021-12-31
Continuously increasing number of flights and predicted further growth of air travel, results in increased impact on environment and is a challenge facing aviation industry in terms of finding new and more environmentally-friendly solutions that can enter into service in a...
Programme: H2020-EU.3.4.5.3.
Record Number: 208054
Last updated on: 2017-01-26
DEsign, development, manufacture, testing and Flight qualification of nExt geNeration fuel storage system with aDvanced intEgRated gauging and self-sealing capabilities
ID: 738078
Data rozpoczęcia: 2017-04-01, Data zakończenia: 2021-03-31
The DEFENDER project is aimed at developing, manufacturing, testing, and qualifying innovative next generation fuel storage system with advanced integrated gauging, self-sealing capabilities and high performing closed cells foams to be integrated into the Next Generation Civil...
Programme: H2020-EU.3.4.5.3.
Record Number: 208055
Last updated on: 2017-02-01
9eGEN - Development of innovative lightweight HVDC 9-phase Brushless/Generator for Clean Sky Rotorcraft
ID: 717218
Data rozpoczęcia: 2016-07-01, Data zakończenia: 2019-12-31
Scope of this project (referred to as 9eGEN in the Technical and Administrative Section) is to develop a High Voltage Direct Current (HVDC) Brushless/Generator up to TRL6 intended to be installed on Clean Sky Life Craft helicopter for demonstration in flight.ASE S.p.A., an...
Programme: H2020-EU.3.4.5.3.
Record Number: 205672
Last updated on: 2016-06-20
Anti-Crash lightweight fuel bladder Tank Integrated on a new RotorCraft
ID: 714249
Data rozpoczęcia: 2016-06-20, Data zakończenia: 2020-12-19
ACTIonRCraft will design, develop, manufacture, verify and validate [qualification tests (leakproofness, temperature, pressure, fluid susceptibility, mechanical and drop tests) up to flight tests] five qualified anti-crash lightweight fuel bladder tanks which will integrate...
Programme: H2020-EU.3.4.5.3.
Record Number: 205691
Last updated on: 2016-06-20
Development and demonstration of materials and manufacturing process for ultra high reliability electric Anti-ice/De-ice thermal layers for high strain rotor blades and helicopter airframe sections
ID: 714039
Data rozpoczęcia: 2017-01-01, Data zakończenia: 2020-12-31
The expected outcome of the NO-ICE-ROTOR project is structural and environmental test substantiation of ultra high reliability heater layers which are capable to be integrated into an advanced tilt civil rotorcraft configuration with high cruise speed, low fuel consumption and...
Programme: H2020-EU.3.4.5.3.
Record Number: 207494
Last updated on: 2016-12-15
Multipurpose test rig for transmissions gearboxes.
ID: 717199
Data rozpoczęcia: 2016-09-01, Data zakończenia: 2020-04-30
Objective of this proposal is to design, manufacture, test and support the adaptation of the test rig used to develop the Drive System for Compound Rotorcraft Demonstrator in the frame of IADP FRC.Based on the topic description published in this call our proposal suppose...
Programme: H2020-EU.3.4.5.3.
Record Number: 206097
Last updated on: 2016-10-17
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List retrieved on: 2017-02-25