Call for Proposals 2019 - 09 - Clean Sky 2 H2020-CS2-CFP09-2018-02 Open!

Objectives

The overall objectives for the Clean Sky 2 programme for the period 2018-2019 are:

  • To execute the technical content as defined for the two-year period and as stabilized at the end of 2017 and upon completion of the private member accession through the four core partner calls executed from 2014 through 2017, and ensure this is adequately incorporated in the Clean Sky 2 Development Plan and the grant agreements;
  • To determine in the course of 2018 – 2019 the definitive configuration of the Programme’s major demonstrators and technology development themes, based on robust risk and progress reviews based on the 2017 baseline set in the CS2DP; where necessary diverting resources to safeguard the achievement of the programme’s High-Level Goals [HLGs];
  • To implement solutions for leveraging Clean Sky 2 funding with structural funds;
  • To implement an effective and efficient management and governance of the programme ;
  • To implement an appropriate and agreed approach for each transverse area that allows for the transversal coordination to be executed and technical synergies to be extracted;
  • To implement four further calls for proposals [including the seventh call to be launched end 2017 and closing in the first quarter of 2018], and implement within these calls the additional and complementary format of “thematic topics” enabling a wide range of competing technology solutions to address broad problem-oriented topics that are geared towards the Clean Sky 2 programme-level HLGs;
  • To widely disseminate the information about the calls for proposals (for partners), in order to reach a healthy level of applications and ensure the success of the topics; including participation from SMEs higher than 35%. To proceed with the selection of participants through these calls;
  • To ensure a time-to-grant no greater than eight months for the calls for proposal in no less than 80% of topics and selected proposals;
  • To execute at least 90% of the budget and of the relevant milestones and deliverables;
  • To ensure a high level of technical and process integrity in the execution of the programme, including the calls and their resulting selection of CS2 participants; and a maximum relevance of research actions performed towards the programme’s goals.
  • To finalise and implement the impact assessment strategy and reference framework for the TE (including the selection of and the performance levels of reference aircraft against which the progress in CS2 will be monitored); to finalize the assessment criteria and evaluation schedule for the TE for each technical area. To complete the selection of its key participants; to conduct within the timeframe of the work plan the first TE assessment of CS2 in order for its completion in early 2020.

 

Actions

This call covers the following topics:

  • JTI-CS2-2018-CFP09-AIR-01-40: Anticontamination Coatings and Cleaning Solutions for Laminar Wings
  • JTI-CS2-2018-CFP09-AIR-02-68: Spring-in prediction capability for large integral wing structure [SAT]
  • JTI-CS2-2018-CFP09-AIR-02-69: Biphasic Heat Transport Integration for Efficient Heat Exchange within Composite materials Nacelle
  • JTI-CS2-2018-CFP09-AIR-02-70: Development and application of an innovative methodology devoted for high temperature characterization of high efficient composite structures
  • JTI-CS2-2018-CFP09-AIR-02-71: Model Manufacturing and Wind Tunnel Testing of High Lift System for SAT Aircraft
  • JTI-CS2-2018-CFP09-AIR-02-72: MEMS sensors, wireless and innovative measurement systems for validation of HVDC system Structure integration and for new SHMS architectures
  • JTI-CS2-2018-CFP09-AIR-02-73: Material modelling platform for generation of thermoplastic material allowable
  • JTI-CS2-2018-CFP09-AIR-02-74: Development of a multipurpose test rig and validation of an innovative rotorcraft vertical tail
  • JTI-CS2-2018-CFP09-AIR-02-75: Design Against Distortion: Part distortion prediction, design for minimized distortion, additive manufactured polymer aerospace parts
  • JTI-CS2-2018-CFP09-AIR-02-76: Cost analysis software platform for evaluating innovative manufacturing technology for SMART fuselage
  • JTI-CS2-2018-CFP09-AIR-03-06: Calibrating Ultrasonic Sensors for atmospheric corrosion.
  • JTI-CS2-2018-CfP09-ENG-01-39: Measurement of rotor vibration using tip-timing for high speed booster and evaluation of associated uncertainties
  • JTI-CS2-2018-CfP09-ENG-01-40: Turbulence modeling of heat exchangers and roughness impact
  • JTI-CS2-2018-CfP09-ENG-01-41: Ground vortex characterization method applicable for engine testing
  • JTI-CS2-2018-CfP09-ENG-01-42: Additive manufacturing boundary limits assessment for Eco Design process optimization [ECO]
  • 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
  • JTI-CS2-2018-CfP09-LPA-01-58: BLI configurations of classical tube and wing aircraft architecture - Wind tunnel tests insight into propulsor inlet distortion and power saving
  • JTI-CS2-2018-CfP09-LPA-01-59: Fan inlet advanced distortion simulator
  • JTI-CS2-2018-CfP09-LPA-01-60: Innovative low noise fan stator technologies for 2030+ powerplants
  • JTI-CS2-2018-CfP09-LPA-01-61: Fatigue life prediction on Inco 718 part subject to service induced damages
  • JTI-CS2-2018-CfP09-LPA-01-62: Rear End Structural Test Program – Component & Subcomponent tests
  • JTI-CS2-2018-CfP09-LPA-01-63: Rear End Aerodynamic and Aeroelastic Studies
  • JTI-CS2-2018-CfP09-LPA-01-64: Rear End Structural Test Program - Low level tests
  • JTI-CS2-2018-CfP09-LPA-01-65: Development of System pipework and Tooling for Sub-Assembly, Final-Assembly of the HLFC-wing Prototype
  • JTI-CS2-2018-CfP09-LPA-01-66: Shielding/High-lift composite thermoplastic flap manufacturing, tool design and manufacturing & process definition
  • JTI-CS2-2018-CfP09-LPA-01-67: UHBR Installed Advanced Nacelle Optimisation and Evaluation Close Coupled to Wing
  • JTI-CS2-2018-CfP09-LPA-01-68: Non-Intrusive Flow Field Measurement within a UHBR Intake
  • JTI-CS2-2018-CfP09-LPA-01-69: Insulation Monitoring for IT Grounded (Isolation Terra) Aerospace Electrical Systems
  • JTI-CS2-2018-CfP09-LPA-01-70: Assessment of arc tracking hazards in high voltage aerospace systems
  • JTI-CS2-2018-CfP09-LPA-01-71: Innovative Nacelle cowl opening system
  • JTI-CS2-2018-CFP09-LPA-02-27: Innovative mould for thermoplastic skin of the lower fuselage demonstrator
  • JTI-CS2-2018-CFP09-LPA-02-28: Innovative tooling, end-effector development and industrialisation for welding of thermoplastic components
  • JTI-CS2-2018-CFP09-LPA-02-29: High performance gas expansion system for halon-free cargo hold fire suppression system.
  • JTI-CS2-2018-CFP09-LPA-03-16: Automated data collection and semi-supervised processing framework for deep learning
  • JTI-CS2-2018-CFP09-LPA-03-17: Audio Communication Manager for Disruptive Cockpit demonstrator
  • JTI-CS2-2018-CFP09-LPA-03-18: Safe emergency trajectory generator
  • JTI-CS2-2018-CfP09-SYS-01-11: Machine learning to detect Cyber intrusion and anomalies
  • JTI-CS2-2018-CfP09-SYS-01-12: Software engine for multi-criteria decision support in civil aircraft flight management
  • JTI-CS2-2018-CfP09-SYS-01-13: Camera-based smart sensing system for cabin readiness
  • JTI-CS2-2018-CfP09-SYS-01-14: Multi-Material Thermoplastic high pressure Nitrogen Tanks for Aircrafts
  • JTI-CS2-2018-CfP09-SYS-02-56: Additive Manufacturing Magnetic Motor
  • JTI-CS2-2018-CfP09-SYS-02-57: Complex cores for CFRP primary structural products manufactured with high pressure RTM
  • JTI-CS2-2018-CfP09-SYS-03-19: Flexible and Automated Manufacturing of wound components for high reliability
  • JTI-CS2-2018-CfP09-SYS-03-20: Demonstration and test of low-loss, high reliability, high speed, bearing-relief generators
  • JTI-CS2-2018-CfP09-SYS-03-21: Aircraft wing architecture optimal assembly
  • JTI-CS2-2018-CfP09-SYS-03-22: Virtual Testing Based Certification
  • JTI-CS2-2018-CfP09-TE2-01-07: Alternative energy sources and novel propulsion technologies
  • JTI-CS2-2018-CfP09-TE2-01-08: Overall Air Transport System Vehicle Scenarios
  • JTI-CS2-2018-CfP09-TE2-01-09: Environmental regulations and policies
  • JTI-CS2-2018-CFP09-THT-03: Conceptual Design of a 19-passenger Commuter Aircraft with near zero emissions
  • JTI-CS2-2018-CFP09-THT-04: Aircraft Design Optimisation providing optimum performance towards limiting aviation’s contribution towards Global Warming
  • JTI-CS2-2018-CFP09-THT-05: Advanced High Bypass Ratio Low-Speed Composite Fan Design and Validation
  • JTI-CS2-2018-CFP09-THT-06: Research for the development of Particulate Matter (PM) regulations and guidelines

European community funding

The Community provisional funding available for the call for proposals is:

  • 69,10 Million EUR (Global Budget)

All the important deadlines

  • 06 February 2019 - in one month (Deadline for the presentation of proposals)

Further information about the call

Official webpage of the call

Useful documents

  • Work Programme 2018-2019 (Work programme)

Organisations eligible to participate

Opened to the following bodies or institutes with legal status established in the covered areas:

  • Any legal organisation

Covered areas

Bodies or institutes must have their registered legal seat in one of the countries taking part in the Programme which are:

  • European Union (EU)

Directorate-Generale responsible

Directorate-General for Research

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