Innovation Takes Off

Clean Sky 2 Information Day 30 April 2014, Tel Aviv Regional Aircraft (RA) IADP Vito PERRUPATO, Alenia Aermacchi Innovation Takes Off

PRESENTATION OUTLINE 1. THE REGIONAL AIRCRAFT From Clean Sky towards Clean Sky 2 High Level Objectives 2. SET-UP AND IMPLEMENTATION The Regional Aircraft IADP (R-IADP) Work Breakdown Structure Technologies Waves Demonstrators Organization, Risk Management Widely opened programme 3. R-IADP HI-LEVEL TECHNICAL CONTENTS, PLANNING, OPPORTUNITIES WP1 High Efficiency Regional Aircraft WP2 Technologies Development WP3 Demonstrations WP4 Technologies Development & Demonstrations Results 4. LEADERS POCs

Regional Aircraft From Clean Sky towards Clean Sky 2 Clean Sky GRA demonstrators on-track for 2015 demo s: Advanced Fuselage Panel 270 HVDC network demo channel Electric ECS Electrical Energy Management Static and Fatigue tests on: Fwd Fuselage Section Wing Box Section Cockpit Section Strong need of a much higher level of technologies integration through Clean Sky 2 Demonstrators: regiona:

Regional Aircraft From Clean Sky towards Clean Sky 2 C S 2 High Integration of Technologies at Aircraft Level Full Scale Flying and Ground Demonstrations Fuselage Wing G R A Component Flying Demonstrator (Structural Panel, Electrical Energy Management, E-ECS) Ground Validation tests Scope : Component, Single Discipline (E.g. Struct. Component Tests, W/TT, Test Rigs) In Clean Sky GRA, several advanced technologies will be demonstrated but not fully integrated. Coherently with budget and time schedule constraints, GRA covers: Green Impact (yes) Integration and Flight Testing (limited) Industrial Impact (very limited) Industrial Competitiveness (very limited )

Regional Aircraft High-Level Objectives Regional traffic is expected to triplicate in the next 20 years. It is forecasted about 9350 new regional aircraft (both tp and jet) will be delivered worldwide in the next 20 years for a value of about $ 370 Billions ( 280 Billions avg. 14Billions per year) in EC 2012. Potential Market of New Regional A/C for the next 20 years Regional Jet 6250 units Turboprop 3100 units Horizon 2020 - Transport Societal Benefit Competitiveness Environment European Regional Aviation Turnover (2031 forecast) Turnover accounted as sum of passengers revenues, cargo revenues, European aircraft manufacturers sales, services to passengers (parking, intermodal mobility to reach airports, ), MRO, 400 Bln Impact on European GDP 2.5% Alenia Aermacchi Marketing Elaborations

Regional Aircraft High-Level Objectives The growing regional market is currently led by non European actors with the exception of turboprop manufacturer ATR (50/50 owned by Alenia Aermacchi and EADS). Traditional European aircraft manufacturers like Fokker, Fairchild- Dornier, Shorts, Saab and Bae have stopped their regional aircraft production. New regional programs from both emerging and mature countries are entering into service and the role of European regional aviation industry is likely to become more and more marginal..there is the need to invest in developing / integrating new technologies in order to recover the global leadership

Setup and Implementation The Regional Aircraft IADP (R-IADP) The need to further address the environment (integrating matured technologies, mainly from current CS GRA) as well as to mature other technologies necessary for a future regional a/c to be successful and make a real change towards the strategic objectives set, has driven the need for a Regional Aircraft IADP and Regional A/C activities in the ITDs of the Clean Sky 2 Proposal.

Setup and Implementation The R-IADP WBS Total R-IADP net funding ~104 M Major involvement of Core Partners

Setup and Implementation Management Approach The Technological Waves WV1 ADAPTIVE WING (Liquid Infusion, Morphing, HLD, Winglets, NLF, Drag, High Lift ) WV2 - REGIONAL AVIONICS (FMS, HMI, Health Monitoring ) WV3 - COCKPIT (Advanced composite materials, systems,.) WV4 - INNOVATIVE FLIGHT CONTROL SYSTEM (Fly-by-Wire, EMA, ) WV5 - ENERGY OPTIMIZED REGIONAL A/C (Low Power WIPS, Electrical Landing gears, EPGDS, E-ECS,..) WV6 - FUSELAGE STRUCTURE (Advanced composite materials, advanced manufacturing,.) WV7 - PAX CABIN (Human centered design, Materials, ) WV8 - NACELLE FOR REGIONAL A/C (JET + TP) (Nacelle Materials, Ice protection, Drag Reduction )

Setup and Implementation Management Approach The Technological Waves WP 2 Technologies Development WP 3 Demonstrations WV1 WP 2.1 Adaptive Electric Wing (ALA + Others) WP B-2.3 Airfr.ITD High Lift Wing (EADS-CASA + Others) SYSTEMS ITD SYNERGIES (EADS-CASA + Syst.) WP B-3.3 Airfr. ITD GROUND WING DEMO (EADS-CASA + Others) WP 3.1 Air Vehicle FTB#1 (ALA + Others) WP 3.5 HL Advanced TP FTB#2 (EADS-CASA + Others) WV2 WP 2.2 REGIONAL AVIONICS (ALA + Others) SYSTEMS ITD SYNERGIES (ALA + Systems) WP 3.3 FLIGHT SIMULATOR (ALA + Others) WV3 WP B-3.1 Airfr. ITD COCKPIT (EADS-CASA + Others) SYSTEMS ITD SYNERGIES (EADS-CASA + Systems) WP B-3.1 Airfr. ITD COCKPIT GND DEMO (EADS-CASA + Others) WV4 WV5 WV6 WV7 WP 2.4 INNOVATIVE FCS (ALA + Others) WP 2.3 ENERGY OPTIM. A/C (ALA + Others) WP B-4.3 Airfr. ITD COMPOSITE FUSELAGE (ALA + Others) WP B-4.4 Airfr. ITD HCD-LW-LC CABIN (ALA + Others) SYSTEMS ITD SYNERGIES (ALA + Systems) SYSTEMS ITD SYNERGIES (ALA + Syst.) SYSTEMS ITD SYNERGIES (ALA + Syst.) WP 3.4 IRON BIRD (ALA + Others) WP 3.2 FUSELAGE/CABIN DEMO (ALA + Others) WP 3.2 FUSELAGE/CABIN DEMO (ALA + Others) WP 3.1 Air Vehicle FTB#1 (ALA + Others) WP 3.1 Air Vehicle FTB#1 (ALA + Others) WP 3.5 HL Advanced TP FTB#2 (EADS-CASA + Others) WV8 WP B-2.3, B-3.2 Airfr. ITD TP NACELLES (ALA + CASA + Others) SYSTEMS ITD SYNERGIES (ALA + Syst.) WP B-2.3 Airfr. ITD NACELLES (ALA + Others) WP 3.5 HL Advanced TP FTB#2 (EADS-CASA + Others)

Setup and Implementation The R-IADP Demonstrators ( Waves of Waves ) FP-7 CLEAN SKY 2 REGIONAL NG HE Regional A/C Horizon 2020 Flightpath2050 mid-term Regional a/c IADP Airframe ITD A/C Syst&Eq. ITD Engines ITD Flight Demonstration Ground Demonstration ALENIA ALENIA FTB1 EADS-CASA FTB2 ALENIA ALENIA

Setup and Implementation R-IADP Organization RA-IADP Steering Committe (CSJU+ITD s as permitted non-voting observers) Programme Policy & Steering CMC Chairman Programme Manager FTB1 Demo Leader FTB2 WING COCKPIT Fuselage Flight Sim Iron Bird A/C CONFIG. DEMO RES. Waves (ITD s interfaces) Roadmap Deliver s 14

Setup and Implementation R-IADP Risk Management Organization CS2 Regional SC RISKS STEERING CS2 Regional Coordinator OVERALL RISKS MGMT CS2 Regional RBS RISK MANAGER A/C Config. Demonstrators RISK OWNERS Flying Demonstrators RISK OWNERS Ground Demonstrators RISK OWNERS FTB1 FTB2 Tech. Waves Deliverables RISKS OWNERS Tech. Waves Deliverables RISKS OWNERS - WV1 - WV4 - WV5 WV1 - WV2 - WV3 - WV4 - WV5 - WV6 - WV7 - WV8 - - WV8 15

The R-IADP is widely open to participation of Core Partners (long term participation, from technologies development up to development of complex end items for the demonstrators) and Partners (for specific projects with limited duration) Main expected Core Partners / Partners: EU supply chain of regional a/c manufactures Systems Suppliers Propeller Manufacturer(s) Academia Research Centers with complex test facilities and other SMEs Setup and Implementation R-IADP A Widely Open Programme In the following charts, this symbol is used to highlight the WPs where contributions from Core Partners is expected

Hi-Level Technical Contents WP1 High Efficiency Regional Aircraft WP 1 HIGH EFFICIENCY REGIONAL AIRCRAFT WP 1.1 INNOVATIVE A/C CONFIGURATIONS WP 1.2 TOP LEVEL A/C REQUIREMENTS WP 1.3 TECHNOLOGIES REQUIREMENTS More efficient powerplant Bleedless engine/aircraft integration High temperature nacelle composite structure Innovative low power ice protection Highly integrated nacelle and associated systems Thermal management and energy harvesting Air Vehicle Low drag and noise with morphing wing /winglet, hingeless devices Relaxed Stability to reduce trim drag Gust effects Active Control Advanced Flight Controls Low speed / short field performance optimized wing WTT DEMONSTRATION OF A BREAKTHROUGH REGIONAL AIRCRAFT CONFIGURATION Preliminary Timescale: WT Model Available: Q2 2019 WT Tests...: Q2 2020 Advanced Cockpit and Avionics Optimized Hybrid Multifunctional CFRP cockpit structure with integrated systems New Cockpit Interaction Concepts and functionalities for pilot reduction workload Mission management in a global environment Fuselage Composite fuselage with SHM All / More Electric Aircraft Thermal Management Cabin Systems Scraps and EoL recycling Maintenance Simplification of maintenance operations Availability improvements Wireless centralized maintenance Systems heath monitoring

Hi-Level Technical Contents WP2 Technologies Development The starting point for this WP will be the development of relevant technologies achieved in the current Clean Sky GRA ITD. These technologies will be further developed with the aim to achieve much higher integration and validation levels. Other technologies, including the ones from other EU projects and National Projects will be considered as well. WP 2 TECHNOLOGIES DEVELOPMENT WP 2.1 ADAPTIVE ELECTRIC WING WP 2.2 REGIONAL AVIONICS WP 2.3 ENERGY OPTIMIZED REGIONAL AIRCRAFT WP 2.4 INNOVATIVE FCS

WP2 Technologies Development (Preliminary Schedule) Activity 2014 2015 2016 2017 2018 2019 2020 2021 2022 2023 2024 I II III IV I II III IV I II III IV I II III IV I II III IV I II III IV I II III IV I II III IV I II III IV I II III IV I II III IV GRA Domains Outcomes: Low Weight Configuration (LWC) Low Noise Configuration (LNC) All Electric Aircraft (AEA) Mission and Trajectory Management (MTM) WP 2 - Technologies Development WP 2.1 - Adaptative Electric Wing WP 2.2 - Regional Avionics LWC LNC MTM Down-selection of technologies for flight test Initial set of technologies for the Flight Simulator Final selection of technologies for flight test TRL 5 GATE ECD TRL 4 GATE ECD Technologies passing this gate will go to R-IADP WP 3.1 FTB1 Technologies passing this gate will be further developed and demonstrated in R-IADP WP 3.3 Flight Simulator WP 2.3 - Energy Optimized Regional Aircraft AEA TRL 4 GATES ECD TRL 5 GATE ECD Selected technologies passing this gate will go to R-IADP WP 3.1 FTB1 and to WP 3.2 Fuselage / Cabin Demo WP 2.4 - Innovative Flight Control Systems Down-selection of technologies for ground / flight demos LNC AEA Final selection of technologies for ground / flight demos 1st TRL 4 GATE ECD 2nd TRL 4 GATE ECD Selected technologies passing this gate will go to R-IADP WP 3.2 Fuselage / Cabin Demo and to WP 3.4 Iron Bird Technologies passing this gate will be further developed and demonstrated in R-IADP WP 3.4 Iron Bird ECD = Estimated Completion Date Technologies passing this gate will be further developed in R-IADP WP 3.4 Iron Bird and are candidate for Flight Test in WP

Hi-Level Technical Contents WP2.1 Adaptive Electric Wing Main objective of this WP is to further develop and mature the integration of GRA wing technologies, featuring advanced performances (high aerodynamic efficiency, load control & alleviation functions, low noise impact, low-weight). WP 2.1 ADAPTIVE ELECTRIC WING WP 2.1.1 Innovative Wing Structure D&M WP 2.1.2 Morphing Structures WP 2.1.3 Advanced HLD WP 2.1.4 Load Control & Alleviation Wing technologies for regional a/c will be developed in the R-IADP as well as in the Airframe ITD. WP 2.1.5 Wing NLF WP 2.1.6 Drag Reduction

Hi-Level Technical Contents WP2.2 Regional Avionics WP 2 TECHNOLOGIES DEVELOPMENT Avionics Functions: FMS NG including Green Functions and taking into account new ATM constraints Innovative Flight Deck: Pilot interaction, Data Fusion, Data format presentation Performance/Health Monitoring: architectures, integration in avionics, data collection, advanced model WP 2.2 REGIONAL AVIONICS WP 2.2.1 Avionic Functions WP 2.2.2 Innovative Flight Deck WP 2.2.3 Performance / Health Monitoring In this WP, starting from common solutions developed in Systems ITD, regional specificities (e.g. HMI, regional a/c constraints and capabilities) will be identified in order to customize them for New Generation Regional a/c.

High-Level Technical Contents WP2.3 Energy Optimized Regional Aircraft WP 2 TECHNOLOGIES DEVELOPMENT The aim of this work package is to address technologies related to innovative onboards systems for regional a/c, mainly through synergies between the R-IADP and the Systems ITD. W.r.t. current Clean Sky, further development of the innovative technologies for aircraft systems will be pursued, so as to: effectively improve the overall aircraft energy efficiency, reducing the environmental impact simplify the maintenance, reducing the ownership costs WP 2.3 ENERGY OPTIMIZED REGIONAL AIRCRAFT WP 2.3.1 Low Power WIPS WP 2.3.2 Electrical Landing Gear WP 2.3.3 Thermal Management WP 2.3.4 Advanced EPGDS WP 2.3.5 Electrical ECS WP 2.3.6 Advanced Low Noise Propeller WP 2.3.7 Ehnanced Fuel System & Inerting WP 2.3.8 Other Novel Technologies

Hi-Level Technical Contents WP2.4 Innovative Flight Control Systems The high-level objective is to replace on Regional A/C all or part of the hydraulic systems that feed the FCS with lighter and simpler electrical systems offering unchanged reliability and performances, by means of: WP 2 TECHNOLOGIES DEVELOPMENT WP 2.4 INNOVATIVE FCS WP 2.4.1 Advanced Fly-by-Wire WP 2.4.2 EMA Advanced Fly-by-Wire: - Advanced and affordable flight control system architecture for regional A/C - Load control and Load Alleviation System (sensor, control laws and actuation for new aerodynamic devices/conventional control surfaces actuated I also in unconventional ways) Electro-Mechanical Actuation: EMAs of different types will be investigated / integrated

Hi-Level Technical Contents WP3 Demonstrations WP 3 DEMONSTRATIONS WP 3.1 AIR VEHICLE TECHNOLOGIES FTB1 WP 3.2 FUSELAGE / CABIN INTEGRATED GROUND DEMO WP 3.3 FLIGHT SIMULATOR WP 3.4 IRON BIRD WP 3.5 INTEGRATED TECHNOLOGIES DEMONSTRATOR FTB2 ALENIA ALENIA ALENIA ALENIA EADS-CASA To minimize technical and program risks, two Flying Test Beds are foreseen for demonstration campaigns of: Wing structure, aerodynamic and loads alleviation flight testing, Advanced Flight Controls and General Systems. Flight Simulator and Iron Bird Demonstrator are linked to FTB#1 A full scale fuselage/pax cabin demonstrator will integrate technologies to be matured in the Airframe ITD WPs B-4.3 and B-4.4

Hi-Level Technical Contents WP3.1 Air Vehicle Technologies Demonstrator (FTB1) Objective of this demonstrator is the integration and flight-testing, focusing on high speed cruise and climb performance, of innovative technologies, mainly from GRA, for a new generation wing with advanced flight control systems as well as for innovative systems. An existing aircraft will be modified to integrate advanced technologies in the following main areas: Aerodynamics Load Control and Load Alleviation Aerolasticity (models validation) Wing structure Fligh Controls Onboard Systems

Hi-Level Technical Contents WP3.1 Air Vehicle Technologies Demonstrator (FTB1) WP 3.1 Air Vehicle Technologies Demonstrator (FTB1) WP 3.1.1 Demo A/C Mod s Requirements and Flight Test Requirements WP 3.1.2 Demo A/C Mod s design and manufacturing WP 3.1.3 Components / Equipment Design, Manufacturing, Procurement WP 3.1.4 Demo A/C Integration, Ground Testing and Permit to Fly Main Opportunity Areas for Participants: Demo aircraft, a/c modification and flight tests execution Design and manufacturing of innovative wing structural parts Design and manufacturing of equipment WT Models design and manufacturing 3D WT testing/validation 3D IWT testing/validation Engineering WPs for demo a/c modification design WP 3.1.5 In-flight Demonstrations Preliminary Timescale: Demonstration Flight Tests: Q2 2021

Hi-Level Technical Contents WP3.5 Air Vehicle Technologies Demonstrator (FTB2) Objective of this demonstrator is the integration and flight-testing, focusing on Low Speed and High Lift Performance, of innovative technologies, for a new generation wing with advanced high lift devices. Most of the technologies to be tested on FTB2 will come from other ITDs. FTB2 will integrate and Flight Test Advanced technologies in the following main areas: Composite wingbox structure, including System integration Adaptive winglet More Electrical wing High Lift devices Integrated Flight Controls including MLA/GLA

Hi-Level Technical Contents WP3.5 Air Vehicle Technologies Demonstrator (FTB2) Main Opportunity Areas for Participants: Design and manufacturing of Wing CFRP structure Wing systems integration A/C integration Engineering WPs for demo a/c modification design Preliminary Timescale: Demonstration Flight Test (1 st campaign): Q1-Q2 2018 Demonstration Flight Test (2 nd campaign): Q1-Q2 2020

Hi-Level Technical Contents WP3.2 Fuselage/Cabin Integrated Demonstration Main objective is the integration and testing of a full scale innovative fuselage and passenger cabin including on board systems and advanced solutions for increasing passenger comfort and safety. Structural demonstration: Long One Piece Fuselage Barrel, in composite, integrating all feasible technologies and methodologies developed within the Airframe ITD for regional a/c. Pax Cabin demonstration: full scale equipped fuselage barrel (length tbd) for demonstration and validation of identified cabin comfort objectives as well as of innovative cabin/systems integrated solutions.

WP3.2 Fuselage/Cabin Integrated Demonstration (cont d) WP 3 DEMONSTRATIONS WP 3.2 FUSELAGE / CABIN INTEGRATED DEMONSTRATION WP 3.2.1 Demonstration Definition WP 3.2.2 Full Fuselage Design WP 3.2.3 Full Fuselage Manufacturing and Assembly WP 3.2.4 Demonstration Preparation WP 3.2.5 Full Fuselage Demonstration (Structural Tests ) WP 3.2.6 Systems and Pax Cabin Integration (one barrel) WP 3.2.7 Pax Cabin Demonstration (Systems, Thermal, Comfort Tests ) Opportunity Areas for Participants Aeronautical Materials Manufacturing and assembling tools High-Automated Devices for manufacturing and assembly Advanced Window Frames and Doors Floor Design and Manufacturing OOA Infused pressure bulkhead Thermoplastic ATL Tailcone Cabin Systems Items and support to testing Ground Test Facility and Test Execution. Preliminary Timescale: Final Demonstration Tests: Q1-Q2 2021

WP3.3 Flight Simulator Starting from the Clean Sky GRA Flight Simulator, an advanced Flight Simulator will be set up and used to demonstrate new cockpit interaction concepts as well as advanced avionics functionalities. WP 3.3 FLIGHT SIMULATOR WP 3.3.1 Regional Flight Simulator Set-up WP 3.3.2 Technologies Customization WP 3.3.3 Technologies Integration Opportunity Areas for Participants Flight simulator models Equipment Prototypes (hardware /software). WP 3.3.4 Demo Test Preparation and execution WP 3.3.5 Reporting Preliminary Timescale: Demonstration Tests: Q1-Q2 2020

Hi-Level Technical Contents WP3.4 Iron Bird Main objectives of this WP are: On ground full-scale demonstration, as essential step towards the optimization and validation of Regional A/C advanced flight control system configuration and interacting aircraft systems incorporating innovative technologies enabling the application of the All/More Electrical Regional Aircraft Concept such as the Electromechanical Actuation (for Flight Control and Landing Gear), the Enhanced Electrical Power Distribution and Power/Load Management. Support the permit-to-fly process for FTB1 WP 3.4 IRON BIRD WP 3.4.1 Iron Bird Definition WP 3.4.2 Iron Bird Design WP 3.4.3 Iron Bird Manufacturing and Assembly WP 3.4.4 Integration of Equipment and Software WP 3.4.5 Demo Test Preparation and execution Opportunity Areas for Participants FCS Equipment (hw/sw) and Models Electrical Distribution Equipment (hw/sw) and Models Test Benches Items: hardware/software. Preliminary Timescale: Demo Tests: Q1-Q2 2020 WP 3.4.6 Reporting

Hi-Level Technical Contents WP4 Technologies Development & Demostration Results WP 4 TECHNOLOGIES DEVELOPMENT & DEMONSTRATION RESULTS WP 4.1 TECHNOLGY ASSESSMENT WP 4.2 ECODESIGN Information flows for R-IADP Interfaces with TE and ECO Transverse activity

Leader PoC: Marco Protti Business Development & Research Head of Advanced Research Alenia Aermacchi Corso Francia, 426 Leaders PoCs Vito Perrupato Business Development&Research Advanced Research Clean Sky 2 Program Manager Alenia Aermacchi Viale dell Aeronautica, s/n 10146 Turin (Italy) 80038 Pomigliano d Arco (Naples), Italy Phone: +39.011.756.2871 Phone: +39.081.887.3116 E-mail: marco.protti@alenia.it E-mail: vito.perrupato@alenia.it Co-Leader PoC: Miguel Angel Llorca Sanz Head of Clean Sky II Airbus Military Paseo de John Lennon, s/n 28906 Getafe-Madrid Phone: +34.91.443.1418 E-mail: miguel.llorca@military.airbus.com