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  • H2020-EU.3.4.5.3. IADP Fast Rotorcraft

H2020-EU.3.4.5.3. IADP Fast Rotorcraft

  • H2020-CS2-CFP01-2014-01
    • JTI-CS2-2014-CFP01-FRC-02-01 Support to the aerodynamic and aeroelastic analysis of a trimmed, complete compound R/C and related issues
    • JTI-CS2-2014-CFP01-FRC-02-02 Aerodynamic and functional design study of a full-fairing semi-watertight concept for an articulated rotor head
    • JTI-CS2-2014-CFP01-FRC-02-03 Support to the aerodynamic analysis and design of propellers of a compound helicopter
    • JTI-CS2-2014-CFP01-FRC-02-04 Tools development for aerodynamic optimization on engine air intake
    • JTI-CS2-2014-CFP01-FRC-02-05 HVDC Starter/Generator
    • JTI-CS2-2014-CFP01-FRC-02-06 High Voltage Network Battery
    • JTI-CS2-2014-CFP01-FRC-02-07 Power Conversion
    • JTI-CS2-2014-CFP01-FRC-02-08 HVDC Network management
  • H2020-CS2-CFP02-2015-01
    • JTI-CS2-2015-CFP02-FRC-01-01 Development and demonstration of materials and manufacturing process for ultra high reliability electric Anti-ice/De-ice thermal layers for high strain civil rotor blades and airframe sections of tiltrotor
    • JTI-CS2-2015-CFP02-FRC-01-03 Development and validation of an optimised gearbox housing structural design and manufacturing process, based on additive layer manufacturing concept leading to a flight cleared demonstrator.
    • JTI-CS2-2015-CFP02-FRC-01-05 Design, development and flight qualification of a novel, integrated high efficiency heat exchanger for tiltrotor transmission oil cooling
    • JTI-CS2-2015-CFP02-FRC-01-06 Design, development, testing and qualification of a high-reliability integrated fuel gauging and distribution system providing active CG management in a civil tiltrotor
    • JTI-CS2-2015-CFP02-FRC-02-10 Multipurpose test rig for transmission gear boxes
    • JTI-CS2-2015-CFP02-FRC-02-12 Fuel bladder tanks for a fast compound rotorcraft
    • JTI-CS2-2015-CFP02-FRC-02-13 HVDC Generator
  • H2020-CS2-CFP03-2016-01
    • JTI-CS2-2016-CFP03-FRC-01-08 High Speed HVDC Generator/Motor
    • JTI-CS2-2016-CFP03-FRC-01-09 Power Distribution
    • JTI-CS2-2016-CFP03-FRC-01-10 Next Generation Fuel Storage System
    • JTI-CS2-2016-CFP03-FRC-02-09 Light weight, impact resistant, canopy for fast compound rotorcraft
    • JTI-CS2-2016-CFP03-FRC-02-11 Design and realization of equipped engine compartments for a fast compound rotorcraft
    • JTI-CS2-2016-CFP03-FRC-02-15 Advanced Health Monitoring System for next generation materials
  • H2020-CS2-CFP04-2016-02
    • JTI-CS2-2016-CFP04-FRC-01-11 Hydrophobic Windscreen Protection for Next Generation Civil Tilt Rotor
    • JTI-CS2-2016-CFP04-FRC-01-12 Flight critical wireless slip ring for a civil tiltrotor
    • JTI-CS2-2016-CFP04-FRC-02-16 Bird strike - Erosion resistant and fast maintainable windshields
    • JTI-CS2-2016-CFP04-FRC-02-17 Flight management system providing noise abatement flight procedures for compound rotorcraft
    • JTI-CS2-2016-CFP04-FRC-02-18 Full Fairing for Main Rotor Head or the LifeRCraft demonstrator
  • H2020-CS2-CFP06-2017-01
    • JTI-CS2-2017-CFP06-FRC-01-14 Contactless measurement system for real time monitoring of proprotor flapping angle
    • JTI-CS2-2017-CFP06-FRC-01-15 Interactional aerodynamic assessment of advanced Tilt Rotor configuration
    • JTI-CS2-2017-CFP06-FRC-02-20 Lateral rotor noise prediction dedicated to low noise footprint optimisation of a compound helicopter
    • JTI-CS2-2017-CFP06-FRC-02-21 Emergency Exits and Cabin Footstep for the Fast Rotorcraft
    • JTI-CS2-2017-CFP06-FRC-02-24 Hybrid bearings technologies
    • JTI-CS2-2017-CFP06-FRC-02-25 Fuel System Detail Development, Testing and Manufacturing
    • JTI-CS2-2017-CFP06-FRC-02-26 Compound Rotorcraft Assembly Tooling
    • JTI-CS2-2017-CFP06-FRC-02-27 Rotor’s Flight Test Instrumentation on demonstrator Fast Rotorcraft Project
  • H2020-CS2-CFP07-2017-02
    • JTI-CS2-2017-CfP07-FRC-01-16 Full scale High speed aerodynamics characteristics of the Civil Tilt Rotor
  • H2020-CS2-CFP08-2018-01
    • JTI-CS2-2018-CfP08-FRC-01-18 Adoption of a “Digital Transformation” approach to improve NGCTR design and simulation
    • JTI-CS2-2018-CfP08-FRC-01-19 Certification by Simulation for Rotorcraft Flight Aspects (CSRFA)
    • JTI-CS2-2018-CfP08-FRC-01-20 Design, development and flight qualification of a supercritical composite shaft drive line for tiltrotor main drive system
    • JTI-CS2-2018-CfP08-FRC-01-21 Development of integrated engine air intake and protection systems for Tilt Rotor
    • JTI-CS2-2018-CfP08-FRC-01-23 Experimental characterization and optimization of the RH and LH Engine intakes configuration of the next generation Tilt Rotor
    • JTI-CS2-2018-CfP08-FRC-01-24 High efficiency full electrical low pressure Compartment Pressure Control System for tilt-rotor applications
  • H2020-CS2-CFP09-2018-02
    • JTI-CS2-2018-CFP09-FRC-01-25 Smart Active Inceptors System definition for Tilt Rotor application
    • JTI-CS2-2018-CFP09-FRC-01-26 Design, manufacture and deliver a high performance, low cost, low weight Nacelle Structure for Next Generation TiltRotor (NGCTR) - Technology Demonstrator (TD)
    • JTI-CS2-2018-CFP09-FRC-01-27 Tilt Rotor Whirl Flutter experimental investigation and assessment
  • H2020-CS2-CFP10-2019-01
    • JTI-CS2-2019-CFP10-FRC-01-28 Innovative kinematic analysis to incorporate multiple functions within a movable surface
    • JTI-CS2-2019-CFP10-FRC-01-29 Smart Active Inceptors System development for Tilt Rotor application
    • JTI-CS2-2019-CFP10-FRC-01-30 Multipurpose bench for Tiltrotor equipment functional test
  • H2020-IBA-CS2-GAMS-2017
    • CS2-GAM-2018-FRC Fast Rotorcraft
  • H2020-IBA-CS2-GAMS-2019
    • CS2-GAM-2020-FRC Fast Rotorcraft ITD GAM 2020
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