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

Static and Fatigue tests on: Electrical Energy  Electric Management Fwd Fuselage Section ECS  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

High Integration of Technologies at Aircraft Level C Fuselage S Full Scale Wing 2 Flying and Ground Demonstrations

G Component Flying R Demonstrator (Structural Panel, In Clean Sky GRA, several advanced technologies A Electrical Energy Management, E-ECS) will be demonstrated but not fully integrated. Coherently with budget and time schedule Ground Validation tests constraints, GRA covers: Scope : Component, Single Discipline • Green Impact (yes) (E.g. Struct. Component Tests, W/TT, Test Rigs) • 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. Potential Market of New Regional It is forecasted about 9350 new regional A/C for the next 20 years aircraft (both tp and jet) will be delivered Regional Jet Turboprop worldwide in the next 20 years for a value 6250 units 3100 units of about $ 370 Billions (€ 280 Billions – avg. € 14Billions per year) in EC 2012.

Horizon 2020 - Transport European Regional Aviation Turnover (2031 forecast) Societal Environment Turnover accounted as sum of passengers revenues, cargo revenues, European aircraft Benefit manufacturers sales, services to passengers (parking, intermodal mobility to reach airports, …), MRO, … Competitiveness € 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 PRESENTATION OUTLINE

1. THE REGIONAL AIRCRAFT • From Clean Sky towards Clean Sky 2 • High Level Objectives

4. LEADERS POCs

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 WP 3 Technologies Development Demonstrations

WP 2.1 WP B-2.3 Airfr.ITD SYSTEMS ITD WP B-3.3 Airfr. ITD WP 3.1 WP 3.5 Adaptive Electric Wing High Lift Wing SYNERGIES GROUND WING DEMO Air Vehicle FTB#1 HL Advanced TP FTB#2 WV1 (ALA + Others) (EADS-CASA + Others) (EADS-CASA + Syst.) (EADS-CASA + Others) (ALA + Others) (EADS-CASA + Others)

WP 2.2 SYSTEMS ITD WP 3.3 REGIONAL AVIONICS SYNERGIES FLIGHT SIMULATOR WV2 (ALA + Others) (ALA + Systems) (ALA + Others)

WP B-3.1 Airfr. ITD SYSTEMS ITD WP B-3.1 Airfr. ITD WV3 COCKPIT SYNERGIES COCKPIT GND DEMO (EADS-CASA + Others) (EADS-CASA + Systems) (EADS-CASA + Others)

WP 2.4 SYSTEMS ITD WP 3.1 WV4 INNOVATIVE FCS SYNERGIES Air Vehicle FTB#1 (ALA + Others) (ALA + Systems) WP 3.4 (ALA + Others) IRON BIRD (ALA + Others) WP 2.3 SYSTEMS ITD WP 3.1 WP 3.5 ENERGY OPTIM. A/C SYNERGIES Air Vehicle FTB#1 HL Advanced TP FTB#2 WV5 (ALA + Others) (ALA + Syst.) (ALA + Others) (EADS-CASA + Others) WP 3.2 FUSELAGE/CABIN DEMO WP B-4.3 Airfr. ITD (ALA + Others) WV6 COMPOSITE FUSELAGE (ALA + Others) SYSTEMS ITD SYNERGIES WP 3.2 (ALA + Syst.) FUSELAGE/CABIN DEMO WP B-4.4 Airfr. ITD (ALA + Others) HCD-LW-LC CABIN WV7 (ALA + Others)

WP B-2.3, B-3.2 SYSTEMS ITD WP B-2.3 WP 3.5 Airfr. ITD TP NACELLES SYNERGIES Airfr. ITD NACELLES HL Advanced TP FTB#2 WV8 (ALA + CASA + Others) (ALA + Syst.) (ALA + Others) (EADS-CASA + Others) Setup and Implementation The R-IADP Demonstrators (“Waves of Waves”)

FP-7 NG HE Regional A/C

CLEAN SKY 2

Flightpath2050

“REGIONAL” Horizon 2020

mid-term

Regional a/c IADP Airframe ITD A/C Syst&Eq. ITD Engines ITD

Flight Demonstration Ground Demonstration

ALENIA

FTB1 FTB2 ALENIA ALENIA EADS-CASA 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 FTB2 WING COCKPIT Fuselage Flight Sim Iron Bird A/C CONFIG. DEMO RES. Demo Leader

Waves Roadmap Deliver’s (ITD’s interfaces)

14 Setup and Implementation R-IADP Risk Management Organization

CS2 “Regional” SC CS2 “Regional” Coordinator RISKS STEERING OVERALL RISKS MGMT

CS2 “Regional” RBS

RISK MANAGER

A/C Config. Demonstrators Flying Demonstrators Ground Demonstrators

RISK OWNERS RISK OWNERS RISK OWNERS

FTB1

FTB2

Tech. Waves Deliverables RISKS OWNERS Tech. Waves Deliverables RISKS OWNERS

WV1 -

WV2 -

WV3 - - WV1 WV4 -

WV5 -

- WV4 WV6 - - WV5 WV7 - WV8 -

- WV8

15 Setup and Implementation R-IADP A Widely Open Programme

• 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

CP In the following charts, this symbol is used to highlight the WPs where contributions from Core Partners is expected

PRESENTATION OUTLINE

1. THE REGIONAL AIRCRAFT • From Clean Sky towards Clean Sky 2 • High Level Objectives

4. LEADERS POCs

Hi-Level Technical Contents WP1 – High Efficiency Regional Aircraft

WP 1 HIGH EFFICIENCY REGIONAL AIRCRAFT

WP 1.1 WP 1.2 WP 1.3 CP INNOVATIVE A/C TOP LEVEL A/C TECHNOLOGIES CONFIGURATIONS REQUIREMENTS REQUIREMENTS

Air Vehicle More efficient powerplant •Low drag and noise with morphing •Bleedless engine/aircraft integration wing /winglet, hingeless devices •High temperature nacelle composite structure •Relaxed Stability to reduce trim drag •Innovative low power ice protection •Gust effects Active Control •Advanced Flight Controls •Highly integrated nacelle and associated systems •Low speed / short field performance •Thermal management and energy harvesting optimized wing

Fuselage •Composite fuselage with SHM •All / More Electric Aircraft WTT DEMONSTRATION •Thermal Management OF A BREAKTHROUGH REGIONAL •Cabin Systems •Scraps and EoL recycling AIRCRAFT CONFIGURATION Advanced Cockpit and Avionics •Optimized Hybrid Multifunctional CFRP cockpit Maintenance structure with integrated systems • Simplification of maintenance operations • New Cockpit Interaction Concepts and functionalities • Availability improvements for pilot reduction workload • Wireless centralized maintenance Preliminary Timescale: • Mission management in a global environment • Systems heath monitoring

. WT Model Available: Q2 2019 . WT Tests…...... : Q2 2020 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 WP 2.3 WP 2.2 WP 2.4 ADAPTIVE ELECTRIC ENERGY OPTIMIZED REGIONAL AVIONICS INNOVATIVE FCS WING REGIONAL AIRCRAFT WP2 – Technologies Development (Preliminary Schedule)

2014 2015 2016 2017 2018 2019 2020 2021 2022 2023 2024 Activity 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) Final selection All Electric Aircraft (AEA) of technologies Technologies passing Mission and Trajectory Management (MTM) for flight test this gate will go to Down-selection R-IADP WP 3.1 FTB1 of technologies for flight test WP 2 - Technologies Development TRL 5 LWC GATE ECD WP 2.1 - Adaptative Electric Wing Technologies passing this gate will be LNC further developed and demonstrated Initial set of in R-IADP WP 3.3 Flight Simulator technologies for TRL 4 MTM the Flight Simulator GATE ECD WP 2.2 - Regional Avionics

Selected technologies passing TRL 4 TRL 5 this gate will go to R-IADP WP GATES GATE 3.1 FTB1 and to WP 3.2 AEA ECD ECD Fuselage / Cabin Demo WP 2.3 - Energy Optimized Regional Aircraft

Selected technologies passing Down-selection this gate will go to R-IADP WP 3.2 Final selection of technologies Fuselage / Cabin Demo and to of technologies for ground / WP 3.4 Iron Bird flight demos for ground / flight demos 2nd TRL 4 LNC GATE ECD Technologies passing this gate will be WP 2.4 - Innovative Flight Control Systems further developed and demonstrated in R-IADP WP 3.4 Iron Bird AEA 1st TRL 4 GATE ECD

Technologies passing this gate will be further developed in R-IADP WP 3.4 Iron Bird and are candidate for Flight Test in WP ECD = Estimated Completion Date Hi-Level Technical Contents WP2.1 – Adaptive Electric Wing

WP 2.1 ADAPTIVE ELECTRIC WING Main objective of this WP is to further WP 2.1.1 develop and mature the integration of Innovative WingStructure CP D&M GRA wing technologies, featuring WP 2.1.2 advanced performances (high MorphingStructures CP aerodynamic efficiency, load control & WP 2.1.3 alleviation functions, low noise impact, AdvancedHLD CP low-weight). WP 2.1.4 CP Load Control & Alleviation Wing technologies for regional a/c will WP 2.1.5 CP be developed in the R-IADP as well as in WingNLF the Airframe ITD. WP 2.1.6 CP Drag Reduction

Hi-Level Technical Contents WP2.2 – Regional Avionics

WP 2 TECHNOLOGIES DEVELOPMENT

WP 2.2 • Avionics Functions: FMS NG including REGIONAL AVIONICS Green Functions and taking into account new

ATM constraints WP 2.2.1 • Innovative Flight Deck: Pilot interaction, AvionicFunctions Data Fusion, Data format presentation WP 2.2.2 CP • Performance/Health Monitoring: Innovative Flight Deck architectures, integration in avionics, data WP 2.2.3 Performance / Health CP collection, advanced model 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

WP 2.3 ENERGY OPTIMIZED The aim of this work package is to address REGIONAL AIRCRAFT WP 2.3.1 technologies related to innovative on- Low Power WIPS boards systems for regional a/c, mainly WP 2.3.2 through synergies between the R-IADP and Electrical Landing Gear WP 2.3.3 CP the Systems ITD. Thermal Management

W.r.t. current Clean Sky, further WP 2.3.4 Advanced EPGDS CP development of the innovative WP 2.3.5 technologies for aircraft systems will be Electrical ECS WP 2.3.6 pursued, so as to: Advanced Low Noise CP • effectively improve the overall aircraft energy Propeller WP 2.3.7 efficiency, reducing the environmental impact Ehnanced Fuel System & Inerting • simplify the maintenance, reducing the WP 2.3.8 ownership costs OtherNovel Technologies Hi-Level Technical Contents WP2.4 – Innovative Flight Control Systems

The high-level objective is to WP 2 replace on Regional A/C all or TECHNOLOGIES part of the hydraulic systems DEVELOPMENT WP 2.4 that feed the FCS with lighter INNOVATIVE FCS and simpler electrical systems WP 2.4.1 CP offering unchanged reliability Advanced Fly-by-Wire WP 2.4.2 and performances, by means of: EMA CP • 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 WP 3.2 WP 3.5 WP 3.3 WP 3.4 AIR VEHICLE TECHNOLOGIES FUSELAGE / CABIN INTEGRATED TECHNOLOGIES INTEGRATED GROUND FLIGHT SIMULATOR IRON BIRD DEMONSTRATOR FTB1 DEMO 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 Main Opportunity Areas for Participants: CP and Flight Test Requirements •Demo aircraft, a/c modification and flight tests WP 3.1.2 execution Demo A/C Mod’s design and manufacturing •Design and manufacturing of innovative wing structural parts WP 3.1.3 Components / Equipment Design, •Design and manufacturing of equipment Manufacturing, Procurement •WT Models design and manufacturing •3D WT testing/validation WP 3.1.4 Demo A/C Integration, Ground •3D IWT testing/validation Testing and Permit to Fly •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)

CP 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 (1st campaign): Q1-Q2 2018 .Demonstration Flight Test (2nd 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 CP Demonstration Definition Opportunity Areas for Participants

WP 3.2.2 •Aeronautical Materials Full Fuselage Design •Manufacturing and assembling tools

WP 3.2.3 •High-Automated Devices for manufacturing and Full Fuselage Manufacturing and Assembly assembly •Advanced Window Frames and Doors WP 3.2.4 Demonstration Preparation •Floor Design and Manufacturing •OOA Infused pressure bulkhead WP 3.2.5 Full Fuselage Demonstration •Thermoplastic ATL Tailcone (Structural Tests ) •Cabin Systems Items and support to testing WP 3.2.6 Systems and Pax Cabin •Ground Test Facility and Test Execution. Integration (one barrel)

WP 3.2.7 Preliminary Timescale: Pax Cabin Demonstration

(Systems, Thermal, Comfort Tests ) . 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 CP WP 3.3.2 Technologies Customization Opportunity Areas for Participants • Flight simulator models WP 3.3.3 • Equipment Prototypes (hardware /software). Technologies Integration

WP 3.3.4 Demo Test Preparation and execution Preliminary Timescale:

. Demonstration Tests: Q1-Q2 2020 WP 3.3.5 Reporting Hi-Level Technical Contents WP3.4 – Iron Bird

WP 3.4 Main objectives of this WP are: IRON BIRD • On ground full-scale demonstration, as essential step WP 3.4.1 towards the optimization and validation of Regional A/C Iron Bird Definition advanced flight control system configuration and WP 3.4.2 interacting aircraft systems incorporating innovative Iron Bird Design technologies enabling the application of the All/More WP 3.4.3 Electrical Regional Aircraft Concept such as the Electro- Iron Bird Manufacturing and Assembly mechanical Actuation (for Flight Control and Landing WP 3.4.4 Gear), the Enhanced Electrical Power Distribution and Integration of Equipment Power/Load Management . and Software WP 3.4.5 • Support the permit-to-fly process for FTB1 Demo Test Preparation and execution

Opportunity Areas for Participants CP WP 3.4.6 Reporting • FCS Equipment (hw/sw) and Models • Electrical Distribution Equipment (hw/sw) and Preliminary Timescale: Models • Test Benches Items: hardware/software. . Demo Tests: Q1-Q2 2020

Hi-Level Technical Contents WP4 – Technologies Development & Demostration Results

WP 4 TECHNOLOGIES DEVELOPMENT & DEMONSTRATION RESULTS

WP 4.1 WP 4.2 TECHNOLGY ASSESSMENT ECODESIGN

Information flows for R-IADP Interfaces with TE and ECO Transverse activity PRESENTATION OUTLINE

1. THE REGIONAL AIRCRAFT • From Clean Sky towards Clean Sky 2 • High Level Objectives

4. LEADERS POCs

Leaders PoCs • Leader PoC: Marco Protti Vito Perrupato Business Development & Research Business Development&Research – Advanced Research Head of Advanced Research Clean Sky 2 Program Manager Alenia Aermacchi Alenia Aermacchi Corso Francia, 426 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: [email protected] E-mail: [email protected] • 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: [email protected]