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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The Demonstrator Fast Rotorcraft has to be fully instrumented with a Flight Test Instrumentation in order to acquire data on the systems on board.Focusing on dynamics system and due to the “novelty” of configuration of this rotorcraft with a Main Rotor, Lateral Rotors and...
Record Number: 702507
The primary structure to be designed and produced constitutes the fuselage front section from radar-transparent nose and cockpit section to junction with the central fuselage. It does not include the doors but include the transparent panel. This structure will be integrated in...
Record Number: 701749
A complete set of windshields for the Fast Rotorcraft has to be developed, manufactured and tested. This encompasses both sides of the front area as far as the upper pilot- and the lower- windshields. The requirements for a High Speed Helicopter (min. impact on drag & max...
Record Number: 701748
The objective is to design, develop, manufacture, test and flight qualify a novel type of oil heat exhcanger for integration in the drivetrain of a tiltrotor. The main challenges are due to the need of obtaining extreme relibility and safety in a very compact format. Please...
Record Number: 701745
The objective is to design, develop, manufacture, test and flight qualify a novel type of freewheeling clutch system for high speed / high torque application to be integrated in the drivetrain of a tiltrotor. The main challenges are due to the need of obtaining extreme...
Record Number: 701746
The primary structure to be designed and produced constitutes the fuselage front section from radar-transparent nose and cockpit section to junction with the central fuselage. It does not include the doors but include the transparent panel. This structure will be...
Record Number: 702180
[PROGRAMME] Power Distribution
Design, development, testing and flight qualification of high power Power Distribution Units (PDUs) for the safe control and protection of the High Voltage Direct Current (HVDC), Low Voltage Direct Current (LVDC) electrical generation system supplies on the Next...
Record Number: 700908
The present activity involves the design, development, manufacture, testing and flight qualification of hydrophobic coating protection system to be applied on Next Generation Civil Tilt Rotor wiperless windscreens.
Record Number: 702248
The aim of this call of proposal is to design, develop, manufacture, test and qualify a flight management system which will fulfill requirements that consist on providing complex flight trajectories for compound aircraft in order to minimize noise footprint, and thus...
Record Number: 702252
The aim of this Call for Partner is to define an advanced Health Monitoring System (HMS) for the Lateral Rotor GearBoxes and Engine to Main Gearbox reduction stages, developed for the Compound Rotorcraft Demonstrator in the frame of IADP FRC.The activities to be...
Record Number: 702187
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List retrieved on: 2017-09-22
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