• Guidance
  • Interesting shortcuts
  • EFFRA Members' Perspectives
  • News Dashboard
  • Structured Wiki
    • Search
    • FoF and Made in Europe Partnership
    • Demonstrators, pilots, prototypes
    • Exploitable result(s)
    • Significant innovations and lessons learned, training aspects
    • Report - Video - Presentation - Publication....?
    • Project clusters
    • EFFRA member perspectives
    • Manufacturing future products
    • Manufacturing performance characteristics
    • Technologies and enablers
    • ICT performance characteristics
    • Standards, technical committees and working groups
    • Contribution of R&I projects to standardisation
    • Regulatory and policy aspects
    • Standards - other classifications
    • Business model aspects
    • Pathways
    • MiE SRIA R&I Priorities
    • MiE WP26-27 Consultation - Potential Research Topics only
    • MiE WP26-27 Consultation and context pointers
    • MiE WP26-27 Consultation with pointers to WP25-27 consultation
    • MiE KPIs
    • Relevant (future) calls
    • EU-Programme-Call
    • NACE code
    • EFFRA Organisations - members
    • EFFRA WG pointers
  • Pathways
    • Pathways
  • Projects
    • Projects
  • Resources
    • Resources
  • Project ideas
    • Project ideas
  • People & organisations
    • People
    • Organisations
  • portal@effra.eu
  • Visit the EFFRA website
    • Login
  • Structured Wiki
  • EU-Programme-Call
  • Horizon 2020
  • H2020-EU.3. SOCIETAL CHALLENGES
  • H2020-EU.3.4. SOCIETAL CHALLENGES - Smart, Green And Integrated Transport
  • H2020-EU.3.4.5. CLEANSKY2
  • H2020-EU.3.4.5.4. ITD Airframe
  • H2020-CS2-CFP06-2017-01

H2020-CS2-CFP06-2017-01

  • JTI-CS2-2017-CFP06-AIR-01-25 Prediction of aerodynamic loads at high Reynolds Number
  • JTI-CS2-2017-CFP06-AIR-01-26 Development of innovative and optimized stiffeners run-out for overall panel weight saving of composite wing
  • JTI-CS2-2017-CFP06-AIR-01-27 Innovative solutions for metallic ribs or fittings introduced in a composite box to optimally deal with thermo-mechanical effects
  • JTI-CS2-2017-CFP06-AIR-01-28 Optimized cockpit windshields for large diameter business aircrafts
  • JTI-CS2-2017-CFP06-AIR-01-29 Optimisation of Friction Stir Welding (FSW) and Laser Beam Welding (LBW) for assembly of structural aircraft parts
  • JTI-CS2-2017-CFP06-AIR-02-39 Integration of innovative ice protection systems into structure and their validation
  • JTI-CS2-2017-CFP06-AIR-02-41 Integrated electronics for actuator data and power management for Morphing Leading Edge activities
  • JTI-CS2-2017-CFP06-AIR-02-42 Lay-up tools for net-shape AFP-manufacturing of geometrically complex helicopter sideshell sandwich-panels
  • JTI-CS2-2017-CFP06-AIR-02-43 Low cost optical wave guides for damage detection including analysis and aircraft data transfer related to aircraft functional needs with self-testing connection
  • JTI-CS2-2017-CFP06-AIR-02-44 Adjustable high loaded rod
  • JTI-CS2-2017-CFP06-AIR-02-45 Development and deployment of PLM Tools for A/C Ground Functional testing with Eco-design criteria.
  • JTI-CS2-2017-CFP06-AIR-02-46 Auto testing technologies and more automated factories for Aircraft validation test process
  • JTI-CS2-2017-CFP06-AIR-02-47 Part specific process optimization in SLM
  • JTI-CS2-2017-CFP06-AIR-02-49 Development and validation of a self-adaptive system for automated assembly of major composite aerostructures
  • JTI-CS2-2017-CFP06-AIR-02-50 Prototype Tooling for subcomponents manufacturing for fuselage.
Powered by Chris Decubber BV