Innovation Takes Off. Not legally binding

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1 Innovation Takes Off

2 Clean Sky 2 Information Day 2nd Call for Proposals (CfP02) Small Air Transport (SAT) TA September 2015 Innovation Takes Off 2

3 Setup and Implementation ITD SYSTEMS /LLI WP0: Management Lead : TAV/LLI WP0.1: Interface ITDs / IADPs Lead : TAV/LLI WP0.2: Interface TE Lead : TAV/LLI WP0.3: Interface SESAR Lead : TAV/LLI WP1: Avionics Extended Cockpit WP2: Cabin & Cargo Systems WP3: Innovative Electrical Wing WP4: Landing Gear System WP5: Electrical Chain WP6: Major loads Lead: LTS WP7: Small Air Transport Activities WP1.1: Requirements, architecture WP2.1: Cabin systems power WP3.1: System architecture WP4.1: Main Landing Gear WP5.0: AC electrical architecture Lead: Airbus WP6.0: Aircraft loads architecture Lead: Airbus WP7.1: Affordable Health monitoring WP1.2: Displays & HSI WP2.2: Cabin Systems WP3.2: FCS Component Techno. WP4.2: Nose Landing Gear WP5.1: Power Generation Lead: TAES WP6.1: Elec. Air sys. & Thermal Mgt Lead: LTS WP7.2: More electrical SAT WP1.3: FMS & Functions WP2.3: Cargo Systems WP3.3: Other Wing systems Techno. WP4.3: Rotorcraft LG System WP5.2: Energy Management WP6.2: Ice Protection System Lead: LTS WP7.3: Fly-by-wire architecture for SAT WP1.4: Avionics & Platforms WP2.4: Sensors & Networks WP3.4: Demonstration WP6.3: Other loads Lead: TAES WP7.4: Affordable SESAR Operation WP1.5: Demonstrations WP6.4: Integrated Demonstration and validation Lead: Airbus WP7.5: Comfortable and safe cabin WP100.1: Power Electronics (Lead: Core Partner) WP100.2: Product Life Cycle Optimization: ECO Design (Materials & Processes, Green Maintenance, End of Life, LCA) () WP100.3: Model Tools & Simulations (Lead: Core Partner)

4 WP 7: Small Air Transport ITD SYSTEMS /LLI WP0: Management Lead : TAV/LLI WP0.1: Interface ITDs / IADPs Lead : TAV/LLI WP0.2: Interface TE Lead : TAV/LLI WP0.3: Interface SESAR Lead : TAV/LLI WP1: Avionics Extended Cockpit WP2: Cabin & Cargo Systems WP3: Innovative Electrical Wing WP4: Landing Gear System WP5: Electrical Chain WP6: Major loads Lead: LTS WP7: Small Air Transport Activities WP1.1: Requirements, architecture WP2.1: Cabin systems power WP3.1: System architecture WP4.1: Main Landing Gear WP5.0: AC electrical architecture Lead: Airbus WP6.0: Aircraft loads architecture Lead: Airbus WP7.1: Affordable Health monitoring WP1.2: Displays & HSI WP2.2: Cabin Systems WP3.2: FCS Component Techno. WP4.2: Nose Landing Gear WP5.1: Power Generation Lead: TAES WP6.1: Elec. Air sys. & Thermal Mgt Lead: LTS WP7.2: More electrical SAT WP1.3: FMS & Functions WP2.3: Cargo Systems WP3.3: Other Wing systems Techno. WP4.3: Rotorcraft LG System WP5.2: Energy Management WP6.2: Ice Protection System Lead: LTS WP7.3: Fly-by-wire architecture for SAT WP1.4: Avionics & Platforms WP2.4: Sensors & Networks WP3.4: Demonstration WP6.3: Other loads Lead: TAES WP7.4: Affordable SESAR Operation WP1.5: Demonstrations WP6.4: Integrated Demonstration and validation Lead: Airbus WP7.5: Comfortable and safe cabin WP100.1: Power Electronics (Lead: Core Partner) WP100.2: Product Life Cycle Optimization: ECO Design (Materials & Processes, Green Maintenance, End of Life, LCA) () WP100.3: Model Tools & Simulations (Lead: Core Partner)

5 SAT Scope & Objectives SAT objective within System ITD is to research and develop application of cost effective technologies new generation small transport aircraft. The main target is to achieve the high level objectives: Reduction of the Operational Costs Reduction of Total Maintenance Cost Improved Cabin (Noise, Thermal, Entertainment) & Flight comfort; Safety and Security. WP7.1 EMA Health Monitoring WP7.4 Affordable SESAR operation WP7.2 More Electrical WP7.3 FbW WP7.5 Comfortable and safe cabin

6 List of SAT topics Identification Topic # Title WP Code Ref. (JTP V5) JTI-CS CFP02-ENG JTI-CS CFP02-SYS Indi Durati cati on ve Star t Dat e of acti vitie s 7 Powerplant Shaft Dynamic WP7.1 Q2 and associated damping system Electromechanical actuatorwp7.1 Q2 for primary moveable 201 surfaces of small aircraft 6 with health monitoring JTI-CS Passive thermo-acousticwp7.5 Q2 CFP02-SYS- insulation for small aircraft WP JTI-CS Database of dynamicwp7.5 Q2 CFP02-SYS- material properties for selected materials 6 commonly used in aircraft industry. (numb er Years) Value (Fundi ng in M ) Topic Leader SAFRAN SMA ToA IA 3-line short Summary Powerplant shaft dynamic behaviour analysis and demonstration with propeller and engine optimisations including damping devices Piaggio IA To test an available EMA up to failure. Based on the evaluation of failure conditions to identify technologies that improve EMA reliability in respect of any failure leading to an uncontrolled EMA position. Health monitoring and any other technology which do not require additional sensors and/or electromechanical devices are preferred. The initial tests have to repeated on the improved EMA to demonstrate compliance with reliability requirements EVEKTOR IA Preparation of small testing specimens of basic insulation materials (passive system of insulation) and their testing in lab, development of the composites for optimal insulation, preparation of small testing specimens of this composite, testing this composites in lab, development and production of reference demonstrator (without optimization), development and production of demonstrator (optimized according to new results) EVEKTOR IA The aim of this CfP is to develop a test methodology (Including design&manufacturing of specimens), and to perform testing of the material specimens in order to create a database of selected materials with sufficient amount of material properties which are to be used in computer simulation of crash behavior.

7 ITD Engines JTI-CS CFP01-ENG Innovation Takes Off

8 List of Topics ITD ENG Identification Code Title Type of Action JTI-CS CFP02-ENG Conventional and Smart Bearings for Ground Test Demo IA 2 JTI-CS CFP02-ENG More electric, advanced hydromechanics propeller IA 0,25 control components JTI-CS CFP02-ENG Engine Mounting System (EMS) for Ground Test IA 0,4 Turboprop Engine Demonstrator JTI-CS CFP02-ENG Integration of Laser Beam Melting Simulation in the tool RIA 0,7 landscape for process preparation of Additive Manufacturing (AM) for Aero Engine applications JTI-CS CFP02-ENG Integration of a property simulation tool for integrated RIA 0,45 virtual design & manufacturing of forged discs/rotors for aero engine applications JTI-CS CFP02-ENG Industry focused eco-design RIA 2,5 JTI-CS CFP02-ENG Jet Noise Reduction Using Predictive Methods RIA 0,4 JTI-CS CFP02-ENG Catalytic control of fuel properties for large VHBR engines RIA 0,35 JTI-CS CFP02-ENG Development of coupled short intake / low speed fan IA 2,8 methods and experimental validation JTI-CS CFP01-ENG Powerplant Shaft Dynamic and associated damping IA 0,35 system JTI-CS CFP02-ENG 10,2 7 Est. Funding Value (M )

9 WP7.3 DIESEL ENGINES PROPELLER WP7 Light weight & Efficient Jet-fuel reciprocating engine Call For Proposal #2 Propeller and powerplant dynamic Main Technology Objectives Design and test a propeller dedicated for direct drive diesel engines. Key Technologies Propellers systems Dampers Timeframe: 18 months between

10 ITD Systems JTI-CS CFP02-SYS JTI-CS CFP02-SYS JTI-CS CFP02-SYS Innovation Takes Off

11 JTI-CS CFP02-SYS-03-01: Efficient operation of small aircraft with affordable health monitoring systems Context and applications : In the context of the SAT one of the main technical issues for implementing a fault-tolerant electromechanical actuator is the low reliability. To overcome this problem one of the most promising is to implement new technologies, including advanced monitoring system, both in term of safety and in economical affordable point of view. The aim to introduce such technologies in the future EMA is to reduce complexity and costs of a FBW (flight by wire) for SAT A/C control system through the use of a single EMA for each primary control surface. Technical Target in the project: - To test an available EMA up to failure. - Based on the evaluation of failure conditions to identify technologies that improve EMA reliability in respect of any failure leading to an uncontrolled EMA position. - Health monitoring and any other technology which do not require additional sensors and/or electromechanical devices are preferred. The initial tests have to be repeated on the improved EMA to demonstrate compliance with reliability requirements. Timeframe and funding: Foreseen start : Mar-2016 Indicative Funding Topic Value Foreseen end : Sep K

12 JTI-CS CFP02-SYS-03-01: Efficient operation of small aircraft with affordable health monitoring systems Proposed WBS To be refined by applicant T1 T2 T3 T4 T5 Test Bench definition Running Test on existing EMA Technologies identification EMA design and manufacturing Running Test on innovative EMA

13 JTI-CS CFP02-SYS : Passive thermo-acoustic insulation for small aircraft Context and applications : Content is focused on the development of passive noise reduction insulation and heat insulation as complex material required by small aircraft producers. The development activity is focused on decreasing of noise level during cruising speed regime and stable heat comfort. The aim is demonstrator of complex acoustic and heat insulation installed inside aircraft fuselage. Technical Target in the project: Selection of optimal materials with requested structure Design of samples (separately for noise and heat insulation) for testing in laboratory and real conditions Design of demonstrator final parts and their application on the fuselage panels (complex material structure or sandwiches structure for noise and heat insulation with standards FAR) - Main characteristics : - Testing should cover this materials: porosity polymers, fibres structure, adhesive systems, AL foils, plastics, etc.) and typically materials used on the walls of fuselage aircrafts - Tests are focused on SPL with dynamic range dB / f = Hz, SPL eq = 50-65dB. - Vibration on walls: D walls = 1-5dB, f = Hz/vibration tests. - Material structure: optimal porosity, density, mechanical properties, adhesive ability, self-extinguishing, weight, etc) Timeframe and funding: Foreseen start : Q1/2016 Indicative Funding Topic Value Foreseen end : Q1/ K

14 JTI-CS CFP02-SYS : Passive thermo-acoustic insulation for small aircraft Proposed WBS To be refined by applicant Deliverables Ref. No. Title - Description Type Due Date D1 D2 Typical materials research study and selection of materials for testing Research study of optimal testing methods and type of samples R and RM R T0 + 4 month T0 + 4 month D3 Test and test evaluation progress report R and RM T month D4 Test report and calculating review R and RM T month D5 Production and technological documentation, detailed material specification (certification according to FAR/CS 23 included) TD T month D6 Production and technological documentation, detailed material specification (certification according to FAR/CS 23 included) TD T month D7 Demonstrator of normal passive insulation D T month D8 Production and technological documentation, detailed material specification (certification according to FAR/CS 23 included) TD T month D9 Demonstrator of optional passive insulation (TRL 3-4) D T month D10 Delivery of sample series used for design of demonstrator TD T month

15 JTI-CS CFP02-SYS : Database of dynamic material properties for selected materials commonly used in aircraft industry Context and applications : In order to perform the simulation of complex crash behaviour of aircraft seat, with results close to the real behaviour during crash test, among other parameters, high speed dynamic material properties have to be used. Technical Target in the project: - Selection of reasonable range of materials intended for testing - Creation of test methodology (Including design & manufacturing of specimens) for material high speed testing - Performance of high speed material tests - Creation of material properties database which will be used as an input for crash simulations - Main characteristics : - Testing should cover about 12 materials (Al, steel, composite, plastics, etc.) which are typically used in aircraft industry - Coupon testing for expected strain rates from 5s -1 to 500s -1 Timeframe and funding: Foreseen start : Q1/2016 Indicative Funding Topic Value Foreseen end : Q1/ K

16 JTI-CS CFP02-SYS : Database of dynamic material properties for selected materials commonly used in aircraft industry Proposed WBS To be refined by applicant Deliverables Ref. No. Title - Description Type Due Date D1 Research study of typical material and selection of materials for testing R and RM T0+2 month D2 Research study of regulations for dynamic testing R T0+2 month D3 Test specification and specimen design progress report R T0+3 month D4 Test specification, test specimen drawings R and RM T0+4 month D5 Specimen manufacturing progress report R T0+8 month D6 Test and test evaluation progress report R T0+11 month D7 Test evaluation report and material dynamic property database R T0+13 month

17 Questions? Any questions on the 2 nd Call for Proposals can be addressed to the following mailbox: Info-Call-CFP @cleansky.eu Last deadline to submit questions: 15 th October 2015, COB. Thank you! 26

18 Thank You Disclaimer The selection of Partners is based on Horizon 2020 Rules for Participation, the rules for submission of proposals, evaluation and selection of Partners as adopted by the Governing Board of Clean Sky 2 JU and as published on the JU s website. The content of this presentation is not legally binding. This presentation wishes to provide an overview of the call and rules. The proposed content/approach is based on the consultation with the National States Representative Group and the Task Force of the Clean Sky 2 Programme. 7