Innovation Takes Off - Clean Sky · owned by Alenia Aermacchi and EADS). • Traditional European aircraft manufacturers like Fokker, Fairchild-Dornier, Shorts, Saab and Bae have

Innovation Takes Off

Clean Sky 2 Information Day28 November 2013, Lisbon

Regional Aircraft (RA) IADPVito PERRUPATO, Alenia AermacchiMiguel Angel LLORCA, EADS-CASA

Innovation Takes Off

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

PRESENTATION OUTLINE

Regional AircraftFrom Clean Sky towards Clean Sky 2

• Clean Sky GRA demonstrators on-track for 2015 demo’s:

• Strong need of a much higher level of technologies integration through Clean Sky 2 Demonstrators: regiona:

Electric

ECS

Electrical

Energy

Management

270 HVDC

network

demo channel

Advanced

Fuselage Panel

Static and Fatigue tests on:

Fwd Fuselage SectionWing Box Section Cockpit Section

Full Scale Flying and

GroundDemonstrations

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)

Fuselage

Wing

High Integration of Technologies at Aircraft Level

GRA

CS2

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 AircraftFrom Clean Sky towards Clean Sky 2

EnvironmentSocietal Benefit

Competitiveness

Horizon 2020 - Transport

• Regional traffic is expected to triplicate in the next 20 years.

Potential Market of New RegionalA/C for the next 20 years

Regional Jet6250 units

Turboprop3100 units

European Regional Aviation Turnover (2031 forecast)

€ 400 Bln

Turnover accounted as sum of passengers revenues, cargo revenues, European aircraftmanufacturers sales, services to passengers (parking, intermodal mobility to reachairports, …), MRO, …

Impact on European GDP ≈ 2.5%

®Alenia Aermacchi Marketing Elaborations

It is forecasted about 9350 new regionalaircraft (both tp and jet) will be deliveredworldwide in the next 20 years for a valueof about $ 370 Billions (€ 280 Billions – avg.€ 14Billions per year) in EC 2012.

Regional AircraftHigh-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

Regional AircraftHigh-Level Objectives




4. LEADERS POCs


The need to further address the environment (integrating maturedtechnologies, mainly from current CS GRA) as well as to matureother technologies necessary for a future regional a/c to besuccessful and make a real change towards the strategic objectivesset, has driven the need for a Regional Aircraft IADP and RegionalA/C activities in the ITDs of the Clean Sky 2 Proposal.

Setup and Implementation The Regional Aircraft IADP (R-IADP)

Major involvement of Core Partners

Setup and Implementation The R-IADP WBS

Total R-IADP Funding108 M€

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 3.1Air Vehicle FTB#1

(ALA + Others)

SYSTEMS ITD SYNERGIES

(ALA + Systems)

WP 2.4INNOVATIVE FCS

(ALA + Others) WV4

WP 3.5HL Advanced TP FTB#2 (EADS-CASA + Others)


(ALA + Others)


(ALA + Syst.)

WP 2.3 ENERGY OPTIM. A/C

(ALA + Others) WV5

WP 3.2FUSELAGE/CABIN DEMO

(ALA + Others) WP B-4.3 Airfr. ITDCOMPOSITE FUSELAGE

(ALA + Others)

WP B-4.4 Airfr. ITDHCD-LW-LC CABIN

(ALA + Others)

WP 3.2FUSELAGE/CABIN DEMO

(ALA + Others)

WP B-2.3Airfr. ITD NACELLES

(ALA + Others)

WP B-2.3, B-3.2 Airfr. ITD TP NACELLES(ALA + CASA + Others)


(ALA + Syst.)

WV6

WV7

WV8


WP B-3.3 Airfr. ITDGROUND WING DEMO (EADS-CASA + Others)


(ALA + Others)

SYSTEMS ITDSYNERGIES

(EADS-CASA + Syst.)

WP B-2.3 Airfr.ITDHigh Lift Wing

(EADS-CASA + Others)

WP 2.1 Adaptive Electric Wing

(ALA + Others) WV1

WP 3.3FLIGHT SIMULATOR

(ALA + Others)


(ALA + Systems)

WP 2.2 REGIONAL AVIONICS

(ALA + Others)

WV3 WP B-3.1 Airfr. ITDCOCKPIT GND DEMO (EADS-CASA + Others)

WP B-3.1 Airfr. ITD COCKPIT

(EADS-CASA + Others)

WP 3.4 IRON BIRD

(ALA + Others)

WV2


WP 2Technologies Development

WP 3Demonstrations


(EADS-CASA + Systems)


(ALA + Syst.)

Setup and Implementation The R-IADP Demonstrators (“Waves of Waves”)

CLEAN SKY 2

“REGIONAL”

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

Flight Demonstration Ground Demonstration

NG HE Regional A/C

FTB1

Horizon 2020Flightpath2050

mid-term

ALENIA EADS-CASA

ALENIA

ALENIA

ALENIA

FP-7

FTB2

CMC Chairman

Programme Manager

FTB1Demo Leader

Waves

(ITD’s interfaces)

Roadmap

FTB2 WING COCKPIT Fuselage Flight Sim Iron Bird A/C CONFIG. DEMO RES.

Deliver’s

RA-IADP Steering Committe

(CSJU+ITD’s as permitted non-voting observers)

Programme Policy & Steering

14

Setup and Implementation R-IADP Organization

WV1 -WV2 -WV3 -WV4 -WV5 -WV6 -WV7 -WV8 -

CS2 “Regional” RBS

RISK MANAGER

Tech. Waves Deliverables RISKS OWNERS

Flying Demonstrators

RISK OWNERS

Ground Demonstrators

RISK OWNERS

FTB2

Tech. Waves Deliverables RISKS OWNERS

CS2 “Regional” SC

RISKS STEERINGCS2 “Regional” Coordinator

OVERALL RISKS MGMT

FTB1

- WV1

- WV4- WV5

- WV8

A/C Config. Demonstrators

RISK OWNERS

15

Setup and Implementation R-IADP Risk Management Organization

• 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

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

CP

Setup and Implementation R-IADP A Widely Open Programme




4. LEADERS POCs


Hi-Level Technical ContentsWP1 – 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 associatedsystems

•Thermal management and energyharvesting

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

Fuselage•Composite fuselage with SHM•All / More Electric Aircraft

•Thermal Management •Cabin Systems

•Scraps and EoL recyclingAdvanced 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

Maintenance• Simplification of maintenance operations• Availability improvements

• Wireless centralized maintenance• Systems heath monitoring

WTT DEMONSTRATION OF A BREAKTHROUGH REGIONAL

AIRCRAFT CONFIGURATION

CP

WP1 – High Efficiency Regional AircraftSynthesis of added-value w.r.t. H2020 Targets

Demostrator Technology Greening IndustrialLeadership

Enhanced Mobility LeadActors

WTT for Configuration of Next Generation Hi-Efficient Regional A/C

Innovative configuration, advanced powerplantintegration, efficient technologies insertion at A/C level

-10 / -15% CO2

-10 / - 15% NOx

-3 / - 6 EPNdB

(These include individual tech's contribution as well as engine contribution)

All above targets are to be considered w.r.t. Clean Sky GRA (90 Pax TP) achievements in 2015

To maintain the European leadership in regional aircraft design, integration, maintenance and recyclability of new advanced and disruptive systems

- Fuel efficiency

- Noise abatement

- STOL

- Reduction of costs of transport (DOC)

ALENIA,EADS-CASA,Leaders andothers (CorePartners, CfPPartners)

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

The starting point for this WP will be the development of relevanttechnologies achieved in the current Clean Sky GRA ITD. Thesetechnologies will be further developed with the aim to achieve muchhigher integration and validation levels. Other technologies,including the ones from FP7, H2020 L2 projects and National Projectswill be considered as well.

Hi-Level Technical ContentsWP2 – Technologies Development

Wing technologies for regional a/c willbe developed in the R-IADP as well asin the Airframe ITD. The related wavemanagement will contribute to assure astrong synergy between the R-IADP andthe Airframe ITD.Main objective of this WP is to furtherdevelop and mature the integration ofGRA wing technologies, featuringadvanced performances (highaerodynamic efficiency, load control &alleviation functions, low noise impact,low-weight).

WP 2.1ADAPTIVE ELECTRIC

WING

WP 2.1.1Innovative Wing Structure

D&M

WP 2.1.2Morphing Structures

WP 2.1.3Advanced HLD

WP 2.1.4Load Control & Alleviation

WP 2.1.5Wing NLF

WP 2.1.6Drag Reduction

CP

CP

CP

CP

CP

CP

Hi-Level Technical ContentsWP2.1 – Adaptive Electric Wing

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.

WP 2.2REGIONAL AVIONICS

WP 2.2.1Avionic Functions

WP 2.2.2Innovative Flight Deck

WP 2.2.3Performance / Health

Monitoring

WP 2TECHNOLOGIES DEVELOPMENT

CP

CP

Hi-Level Technical ContentsWP2.2 – Regional Avionics

• Avionics Functions: FMS NG including

Green Functions and taking into account newATM constraints

• Innovative Flight Deck: Pilot interaction,

Data Fusion, Data format presentation

• Performance/Health Monitoring: architectures, integration in avionics, data collection, advanced model

The aim of this work package is to addresstechnologies related to innovative on-boards systems for regional a/c, mainlythrough synergies between the R-IADP andthe Systems ITD.

W.r.t. current Clean Sky, furtherdevelopment of the innovativetechnologies for aircraft systems will bepursued, so as to:

• effectively improve the overall aircraft energyefficiency, reducing the environmental impact

• simplify the maintenance, reducing theownership costs

WP 2.3.8Other Novel Technologies

WP 2.3ENERGY OPTIMIZED REGIONAL AIRCRAFT

WP 2.3.1Low Power WIPS

WP 2.3.2Electrical Landing Gear

WP 2.3.3Thermal Management


WP 2.3.4Advanced EPGDS

WP 2.3.5Electrical ECS

WP 2.3.6Advanced Low Noise

Propeller

WP 2.3.7Ehnanced Fuel System &

Inerting

CP

CP

CP

High-Level Technical ContentsWP2.3 – Energy Optimized Regional Aircraft

Hi-Level Technical ContentsWP2.4 – 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 2.4INNOVATIVE FCS

WP 2.4.1Advanced Fly-by-Wire

WP 2.4.2EMA


CP

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 ContentsWP3 – 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 3.5INTEGRATED TECHNOLOGIES

DEMONSTRATORFTB2

•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

ALENIA EADS-CASAALENIA ALENIA ALENIA

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.

WP 3.1Air Vehicle Technologies

Demonstrator (FTB1)

WP 3.1.1Demo A/C Mod’s Requirements

and Flight Test Requirements

WP 3.1.2Demo A/C Mod’s design and

manufacturing

WP 3.1.3Components / Equipment Design,

Manufacturing, Procurement

WP 3.1.4Demo A/C Integration, Ground

Testing and Permit to Fly

WP 3.1.5In-flight Demonstrations

Hi-Level Technical ContentsWP3.1 – Air Vehicle Technologies Demonstrator (FTB1)

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

WP 3.1Air Vehicle Technologies

Demonstrator (FTB1)

WP 3.1.1Demo A/C Mod’s Requirements

and Flight Test Requirements

WP 3.1.2Demo A/C Mod’s design and

manufacturing

WP 3.1.3Components / Equipment Design,

Manufacturing, Procurement

WP 3.1.4Demo A/C Integration, Ground

Testing and Permit to Fly

WP 3.1.5In-flight Demonstrations


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

CP

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


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

CP

Main objective is the integration andtesting of a full scale innovativefuselage and passenger cabin includingon board systems and advancedsolutions for increasing passengercomfort and safety.

The structural demonstration willintegrate in a Long One Piece FuselageBarrel, in composite, all feasibletechnologies and methodologiesdeveloped within the Airframe ITD forregional a/c.

WP 3.2.1Demonstration Definition

WP 3.2.2Full Fuselage Design

WP 3.2.3Full Fuselage Manufacturing

and Assembly

WP 3DEMONSTRATIONS

WP 3.2.4Demonstration Preparation

WP 3.2.5Full Fuselage Demonstration

(Structural Tests )

WP 3.2.6Systems and Pax CabinIntegration (one barrel)

WP 3.2.7Pax Cabin Demonstration

(Systems, Thermal, ComfortTests )

WP 3.2FUSELAGE / CABIN

INTEGRATED DEMONSTRATION

Hi-Level Technical ContentsWP3.2 – Fuselage/Cabin Integrated Demonstration

A full scale equipped fuselage barrel(length to be defined) will be producedfor demonstration and validation ofidentified cabin comfort objectives.

Dedicated ground tests will be carriedout to validate the innovativecabin/systems integrated solutions, toverify cabin thermal behavior, validatelocal and global cabin thermal modelsand E-ECS pack performances at Cabinenvironment level, cabin airdistribution, humidity and temperaturecontrol




and Assembly

WP 3DEMONSTRATIONS



(Structural Tests )






High-Level Technical ContentsWP3.2 – Fuselage/Cabin Integrated Demonstration (cont’d)




and Assembly

WP 3DEMONSTRATIONS



(Structural Tests )






WP3.2 – Fuselage/Cabin Integrated Demonstration (cont’d)

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.

CP


WP 3.3.1Regional Flight Simulator

Set-up

WP 3.3.2Technologies Customization

WP 3.3.3Technologies Integration

WP 3.3.4Demo Test Preparation and

execution

WP 3.3.5Reporting

Starting from the Clean Sky GRA FlightSimulator, an advanced Flight Simulatorwill be set up and used to demonstratenew cockpit interaction concepts aswell as advanced avionicsfunctionalities.The purpose of the Clean Sky 2 RegionalFlight Simulator is to validate atsimulation level Clean Sky 2technologies, belonging to WP 2.2Regional Avionics.

Hi-Level Technical ContentsWP3.3 – Flight Simulator

WP3.3 – Flight Simulator


WP 3.3.1Regional Flight Simulator

Set-up

WP 3.3.2Technologies Customization

WP 3.3.3Technologies Integration


execution

WP 3.3.5Reporting

Opportunity Areas for Participants• Flight simulator models• Equipment Prototypes (hardware /software).

CP

WP 3.4.1Iron Bird Definition

WP 3.4.2Iron Bird Design

WP 3.4.3Iron Bird Manufacturing and

Assembly

WP 3.4.4Integration of Equipment

and Software


execution

WP 3.4IRON BIRD

WP 3.4.6Reporting

Main objectives of this WP are:• On ground full-scale demonstration, as essential step

towards the optimization and validation of Regional A/Cadvanced flight control system configuration andinteracting aircraft systems incorporating innovativetechnologies enabling the application of the All/MoreElectrical Regional Aircraft Concept such as the Electro-mechanical Actuation (for Flight Control and LandingGear), the Enhanced Electrical Power Distribution andPower/Load Management .

• Support the permit-to-fly process for FTB1

Hi-Level Technical ContentsWP3.4 – Iron Bird

Opportunity Areas for Participants

• FCS Equipment (hw/sw) and Models• Electrical Distribution Equipment (hw/sw) and

Models • Test Benches Items: hardware/software.

CP

Hi-Level Technical ContentsWP4 – 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




4. LEADERS POCs


Leaders PoCs

• Leader PoC:Maurizio Fornaiolo Vito Perrupato

Business Development & Research Business Development&Research

Clean Sky Project Head Clean Sky Project

Alenia Aermacchi Alenia Aermacchi

Corso Francia, 426 Viale dell’Aeronautica, s/n

10146 Turin (Italy) 80038 – Pomigliano d’Arco (Naples), Italy

Phone: +39.011.756.5002 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]

Documents

Innovation Takes Off - Clean Sky · owned by Alenia Aermacchi and EADS). • Traditional European aircraft manufacturers like Fokker, Fairchild-Dornier, Shorts, Saab and Bae have