Call for Proposals 2019 - 10 - Clean Sky 2 H2020-CS2-CFP10-2019-01 Closed!

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-CS2-2019-CFP10-AIR-01-41: Low speed handling quality and innovative engine integration of a new configuration aircraft
  • JTI-CS2-2019-CFP10-AIR-01-42: Development of a methodology (test, measurement, analysis) to characterize the behaviour of composite structures under dynamic loading
  • JTI-CS2-2019-CFP10-AIR-01-43: Verification of advanced simplified HLFC concept with variable porosity
  • JTI-CS2-2019-CFP10-AIR-01-44: Development of a methodology to optimize a wing composite panel with respect to tyre damage certification requirement
  • JTI-CS2-2019-CFP10-AIR-01-45: Coupon and element testing and manufacturing of test article for morphing technologies
  • JTI-CS2-2019-CFP10-AIR-02-77: Increasing the efficiency of pulsed jet actuators for flow separation control
  • JTI-CS2-2019-CFP10-AIR-02-78: Application of graphene based materials in aeronautical structures for de-icing, lightning strike protection, fire barrier and water absorption prevention purposes
  • JTI-CS2-2019-CFP10-AIR-02-79: Development of FEM fastener parametric/adaptable sizing tool including EMC impact, and manufacturing and EMC/LSP testing of demonstrators
  • JTI-CS2-2019-CFP10-AIR-02-80: Innovative flight data measurements to support the aerodynamic analysis of a compound helicopter demonstrator
  • JTI-CS2-2019-CFP10-AIR-02-81: Active Flow control on Tilt Rotor lifting surfaces
  • JTI-CS2-2019-CFP10-AIR-02-82: Innovative approaches for interior Noise Control for Next Generation Civil Tilt Rotor
  • JTI-CS2-2019-CFP10-AIR-02-83: Innovative weight measurement system for Tilt Rotor application
  • JTI-CS2-2019-CFP10-AIR-02-84: Modular platform development for Tilt Rotor final assembly
  • JTI-CS2-2019-CFP10-AIR-02-85: Development of a multifunctional system for complex aerostructures assembly, assisted by neural network softwares
  • JTI-CS2-2019-CFP10-AIR-02-86: Development of equipment for composite recycling process of uncured material
  • JTI-CS2-2019-CFP10-AIR-03-07: End of Life (EoL) for biomaterials
  • JTI-CS2-2019-CFP10-AIR-03-08: Disassembly and recycling of innovative structures made of different Al-Li alloys
  • JTI-CS2-2019-CFP10-AIR-03-09: Scrapping of carbon reinforced thermoplastic materials
  • 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
  • JTI-CS2-2019-CFP10-REG-01-18: Theoretical and experimental evaluations of strain field modification induced by flaws in loaded composite structures
  • JTI-CS2-2019-CFP10-REG-01-19: Innovative Noise Generation System for testing of Regional Cabin Interior Noise reduction
  • JTI-CS2-2019-CFP10-REG-02-06: SHMS and Dynamic fields sensors development
  • JTI-CS2-2019-CFP10-THT-07: Ultra-High Aspect ratio wings
  • JTI-CS2-2019-CFP10-THT-08: Experimental and numerical noise assessment of distributed propulsion configurations
  • JTI-CS2-2019-CFP10-THT-09: Disruptive Active Flow Control for aircraft engine applications
  • JTI-CS2-2019-CFP10-THT-10: Non-intrusive, seedless measurement system: design, development, and testing
  • JTI-CS2-2019-CfP10-ENG-01-43: Low NOx / Low soot injection system design for spinning combustion technology
  • JTI-CS2-2019-CfP10-ENG-04-08: Revalorisation of Recycled Carbon Fibers and CFRP preparation through Eco design [ECO]
  • JTI-CS2-2019-CfP10-LPA-01-72: Development of a distributed CFD platform for collaborative design
  • JTI-CS2-2019-CfP10-LPA-01-73: Innovative Thrust Reverser Actuator System (ITRAS)
  • JTI-CS2-2019-CfP10-LPA-01-74: UHBR Engine Studies for Aircraft Operations and Economics
  • JTI-CS2-2019-CfP10-LPA-01-75: Advanced solutions for 2030+ UHBR Core Noise reduction
  • JTI-CS2-2019-CfP10-LPA-01-76: Supporting implementation of 2030+ UHBR low noise fan technology solutions through enhanced modeling capabilities
  • JTI-CS2-2019-CfP10-LPA-01-77: Advanced Pitch Control Mechanism TRL4 Demonstration
  • JTI-CS2-2019-CfP10-LPA-01-78: Innovative turbine cavity swirl control systems through Additive Manufacturing
  • JTI-CS2-2019-CfP10-LPA-01-79: Development of multidisciplinary design tools for rapid concept design for aero engine components
  • JTI-CS2-2019-CfP10-LPA-01-80: Rear fuselage and empennage shape optimization including anti-icing technologies
  • JTI-CS2-2019-CfP10-LPA-01-81: Fiber reinforced thermoplastics manufacturing for stiffened, complex, double curved structures
  • JTI-CS2-2019-CfP10-LPA-01-82: Development of Thermoplastic press forming Tool for Advanced Rear End Closing Frame Prototype and Tooling 4.0 for Assembly and transportation of the Advanced Rear End Prototype
  • JTI-CS2-2019-CfP10-LPA-01-83: Development and simulation of a forming process for LE HLFC wing outer skins
  • JTI-CS2-2019-CfP10-LPA-01-84: Development of a manufacturing process and a manufacturing unit for production of a laser treated titanium panel with a 3D printed substructure
  • JTI-CS2-2019-CfP10-LPA-01-85: Design and manufacturing of multi-functional Ice Protection System power feed/monitoring lines and Shielding/High-lift electrical actuation system for a HLFC Wing demonstrator  
  • JTI-CS2-2019-CfP10-LPA-01-86: Develop and test Power Efficient Actuation Concepts for Separation Flow Control at large aerodynamic areas requiring very low actuation energy
  • JTI-CS2-2019-CfP10-LPA-01-87: Loop Heat Pipe development for severe environment
  • JTI-CS2-2019-CfP10-LPA-02-30: Development of innovative welding systems for structural joints of Thermoplastic matrix based Composites
  • JTI-CS2-2019-CfP10-LPA-02-31: Development of short fibre reinforced thermoplastic airframe clips and brackets using factory waste
  • JTI-CS2-2019-CfP10-LPA-02-32: Innovative miniaturized sensing device for large wave length spectrum reception capability as a tool for quality control and aircraft maintenance
  • JTI-CS2-2019-CfP10-SYS-01-15: Enhanced digital georeferenced data models for cockpit use
  • JTI-CS2-2019-CfP10-SYS-01-16: Innovative processing for flight practices improvement
  • JTI-CS2-2019-CfP10-SYS-01-17: New Efficient production methods for 94 GHz (W-band) waveguide antennas
  • JTI-CS2-2019-CfP10-SYS-01-18: Low-profile/drag electronically steerable antennas for In-Flight Connectivity  
  • JTI-CS2-2019-CfP10-SYS-01-19: VOC filtration device for Inerting System
  • JTI-CS2-2019-CfP10-SYS-01-20: Innovative high flow rate constant pressure valve for inert gas discharge from pressurized vessels  
  • JTI-CS2-2019-CfP10-SYS-01-21: Grey Water Container with Reduced Biofilm Growth
  • JTI-CS2-2019-CfP10-SYS-02-58: Automatic Haptic System Test Bench for Active Inceptors
  • JTI-CS2-2019-CfP10-SYS-02-59: Innovative DC/DC converter for HVDC power sources hybridization
  • JTI-CS2-2019-CfP10-SYS-02-60: Toward a Digital Twin ECS and thermal management architecture models : Improvement of MODELICA libraries and usage of Deep Learning technics
  • JTI-CS2-2019-CfP10-SYS-02-61: Vapor Cycle System - Heat Exchanger performance 3D modeling with different new low GWP refrigerants   
  • JTI-CS2-2019-CfP10-SYS-03-23: Electro-Mechanical Landing Gear system integration for Small Aircraft [SAT]  
  • JTI-CS2-2019-CfP10-SYS-03-24: Power Semiconductor Device module using Silicon Carbide devices for a relatively high-frequency, circa 100kW aircraft motor drive applications

European community funding

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

  • 59,45 Million EUR (Global Budget)

All the important deadlines

  • 03 September 2019 - more than one month ago (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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