1 1 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Clean Sky Programme Helmut Schwarze, Project Officer CSJU Aerospace Technology 2010 18 th & 19

Aerospace Technology 2010, Stockholm, 18-19/10/2010

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Clean Sky ProgrammeHelmut Schwarze, Project Officer CSJU

Aerospace Technology 2010

18th & 19th of October 2010, Stockholm


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Outlines

Clean Sky Programme OverviewACARE goalsExpected benefitsTechnical areas & projects Implementation & membershipResults-oriented project: environmental objectives & more mature

demonstrationCall for proposals

Main Technical achievements SFWASAGESGOGRATE


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Clean Sky ProgrammeClean Sky ProgrammeOverviewOverview


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ACARE Goals: Vision 2020 Challenges

2002 Strategic Research AgendaStrategic Research AgendaFive Challenges for Aeronautics

20042nd Issue of the Strategic Research Agenda

Five High Level Target Concepts

2000European Aeronautics:

A Vision for 2020

2008 AddendumAddendum

Focus on recent developments

ACARE

GoalsGoals

Vision 2050 – Aviation platformToday


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ACARE Goals: Vision 2020 Challenges

ACAREOctober 2002 : The Strategic Research Agenda (SRA) 5 Challenges

Quality and Affordability

Environment SafetyAir Transport

System Efficiency Security

Vision 2020 (January 2001)• To meet Society’s needs

• To achieve global leadership for Europe

October 2004 : The SRA 2 High level Target Concepts

Very Low Cost ATS

Ultra Green ATS

Highly Customer

oriented ATS

Highly time-efficient ATS

Ultra Secure ATS

22nd Century

JTI

50% cut in CO2 emissions per pass-Km by drastic fuel consumption reduction

80% cut in NOx emissions Halving perceived aircraft noise A green design, manufacturing, maintenance and disposal product life cycle


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Benefits of investing in aeronautics technologies

EnvironmentGreener products into service sooner

Less noise, lower emissions Reduced fuel consumption Greener design, production and maintenance Faster introduction of innovative technologies

Application across all commercial aircraft

Socio-economic impact Integrating European industryOpen access to SMEs and New Member StatesExpected multiplier effect via complementary National ProgrammesA competitive European industry leading the introduction of more

environmentally friendly products and sustaining the creation of highly qualified jobs

Major contribution to sustainable growth in Europe


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Expected results from Clean Sky

Multiple of yr 2005 CO2 Emissions

Business as usual

Clean Sky

Emissions reduction expected from existing technology programmes

Expected CO2 reduction from Clean Sky Gap to ACARE target of 50% emissions reduction from a year 2000 base traffic

Assuming an expected traffic growth of 4.25% per annum


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Clean Sky Technologies meeting ACARE goals

Power plant Loads & Flow Control New Aircraft Configurations Low weight Aircraft Energy Management Mission & Trajectory Management

Power Plant Mission & Trajectory Management Configurations Rotorcraft Noise Reduction

Aircraft Life Cycle

50%CO280% NOx

50% noise

Green design..

"Ecolonomic"

life cycle

Reduced fuel consumption (CO2 & NOx reduction)

External noise reduction

ACARE GOALS Technology Domains


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Smart Fixed Wing Aircraft

Systems for Green Operations

2 years 3 years 3 years

First Definitionof ecology efficiency

Refined Definitionof ecology efficiency

2 years 3 years 3 years

First Definitionof ecology efficiency

Refined Definitionof ecology efficiency

Green Rotorcraft

Technology EvaluatorSustainable and Green Engines

Eco-Design

Green Regional Aircraft

Clean Sky Integrated Technology Demonstrators

Rolls-Royce & Safran

Airbus & SAAB

Eurocopter & AgustaWestlandAlenia & EADS-CASA

Dassault & Fraunhofer

Thales & Liebherr

DLR & Thales


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Clean Sky is a Joint Technical Initiative (JTI) Public-Private Partnership between Commission and Industry Total budget 1.6 billion €

800 million € from Commission in-cash800 million € from industry in-kind

7-year research project on Greening of Aeronautics: 2008-2015

Clean Sky: implementation

20152015201420142013201320122012201120112010201020092009

FP7 related projects


20152015201420142013201320122012201120112010201020092009




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Clean Sky targetsPreliminary targets were set for each « Integrated Technology Demonstrator »: CO2, NOx, noise

Integrated at aircraft level (2020 as compared to 2000)

Targets to be refined by end of October 2010

Wide body

Narrow body

Regional Bizjets Rotorcraft

CO2 - 30% - 20% - 40% - 30% - 30%

NOX - 30% - 20% - 40% - 30% - 60%

Noise - 20 dB - 15 dB - 20 dB - 10 dB - 10 dB

ACARE targets:

-50% C02

-50% noise

-80% Nox

in 2020 vs 2000


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Clean Sky: split of the public funding

ITD leaders & AssociatesOrganisation necessary to the

delivery of the platform objectives

7 years commitment Sign the JTI StatutesParticipate in JTI operational

costsCannot respond to the Calls for

Proposals of the platform Partners

will respond to the calls for proposal (CFP) organised by Clean Sky JU

CFP follows the ITDs Specifications

Contract for a limited duration up to 7 years

SMEs12% will represent ~200M€Representing 1000 to 2000 SME

contracts

Maximum Overall EC Contribution: 800 M€

Partners(min 200 M€

i.e.25%)

Callfor

Proposals

Members(max. 600 M€ i.e. 75%)

ITD Leaders(max 400 M € i.e. 50%)

Associates(max 200 M €

i.e. 25%)

match EC contribution 50% (in-kind)

match EC contribution 50%

(in-kind)



i.e.25%)

Callfor

Proposals




i.e. 25%)



(in-kind)



i.e.25%)

Callfor

Proposals




i.e. 25%)



(in-kind)



i.e.25%)

Callfor

Proposals




i.e. 25%)



(in-kind)

12 67


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Split of the 800 M€ public funding

6x2 ITD leaders

Up to 50%

74 associates

Up to 25%

MEMBERSare committed for the full duration of CSJUPARTNERS are committed for the duration of their topic(s)

~500 partners (*) through calls

At least 25%

(*) ~100 today


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Towards a High maturity

Demonstrators definition close to the market needs: the demonstrator is the last R&T phase, before starting a development

Schedule is key to keep this link (be neither too early, nor too late)

A large part of this downstream research activity lays within big players, « integrators » - a typical feature of aeronautics

These activities must be thoroughly coordinated

A large programme focused on environment…… and competitiveness

A high level of « technology readiness »: the technologies are integrated into large demonstrators, in-flight or on-ground

These features create the conditions for a Public-Private Partnership


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Clean Sky deliverables

Innovative technology demonstrators at a system level

Integrate and validate at a system level to facilitate industry investment in new aircraft programmes

Multiple ground and flight test vehicles

Integrate the emerging technologies in a realistic environment to accelerate their use in new products

Meet the needs of each aircraft segment


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Calls for proposals

Clearly defined topics Focused to fit into the demonstrators or

demonstrations Easy to apply and compete: one company can apply

alone, and “the winner takes all” Info days in different countries

Fair and straight selection process, closely inspired by the FP’s process and spirit

A promising start for SME and research organisations (academic or not)


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Governance

Governing Board:12 industrial leaders + 6 associates +

EU Commission

Joint Undertaking Executive Team

ITD ITD

European Parliament

Annual dischargeScientific and

Tech. Advisory board

General Forum

ITD: integrated Technology Demonstrator

Technology

evaluator

National States representatives

Group

Partners ITD ITDITDITDPartners


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Calls for proposals: some average figures

400 M€ dedicated to calls for proposals 3-4 Calls per year in 2010, 2011,…2012 40 Topics per call 400 K€ as total budget by proposals

1,7 Partners by proposal 30% Success rate 6 Months targeted as time to contract 20 Months as topic duration

37% to SMEs


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Swedish Participation

• Members share– SFWA ~21 Mio€ (5,3%)– SGO ~ 5 Mio€ (1,6%)– SAGE ~ 23 Mio€ (5,0%)– TE ~0,3 Mio€ (1,0%)

• CfP (Call 1 - 5)– Total ~217 Mio€; Sweden ~ 3,4 Mio€( ~1,5%)– Total no participants: 876; Sweden: 18 (2,1%)


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For further information: www.cleansky.eu

Helmut Schwarze

SFWA Project Officer [email protected]

Contact us


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Clean Sky ProgrammeClean Sky ProgrammeMain Technical AchievementsMain Technical Achievements


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Reduced fuel consumptionReduction of CO2 and NOX

Engines Loads & Flow Control New Aircraft Configurations Low weight Aircraft Energy Management Mission & Trajectory Management


„Ecolonomic“ life cycle

Engines Mission & Trajectory Management Configurations Rotorcraft Noise Reduction

Aircraft Life Cycle

Smart Fixed Wing Aircraft – Contribution to environmental targetsSmart Fixed Wing Aircraft – Contribution to environmental targets


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Port wing

Laminar wing structure concept option 2

Starboard wing

Laminar wing structure concept option 1

Smart Passive Laminar Flow Wing Design of an all new natural laminar wing

Proof of natural laminar wing concept in wind tunnel tests

Use of novel materials and structural concepts

Exploitation of structural and system integration together with tight tolerance / high quality manufacturing methods in a large scale ground test demonstrator

Large scale flight test demonstration of the laminar wing in operational conditions

High Speed Demonstrator Passive (HSDP)High Speed Demonstrator Passive (HSDP)


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Smart Wing Flight Test InstrumentationSmart Wing Flight Test Instrumentation


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Integration of the Counter Rotating Open Integration of the Counter Rotating Open Rotor ConceptRotor Concept


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Reduced fuel consumption (CO2 & NOx reduction


« Ecolonomic » life cycle

Engines Loads & flow control New Aircraft Configurations Low weight Aircraft Energy Management Mission & Trajectory Management

Engines Mission & Trajectory Management Configuration Rotorcraft noise reduction

Aircraft Life Cycle

CO up to 20%

NOx up to 60%

Noise up to 20 dB

Sustainable and Green Engine – Contribution to environmental targetsSustainable and Green Engine – Contribution to environmental targets

goulami

Is it the right spelling? not ecolonomic?


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Contra-rotating open rotor (CROR) propulsion systems, demonstrating

– Feasibility of both geared & direct drive power transmission

– Ability to control contra-rotating propeller blade pitch

– Ability to control system noise levels equal to or better than current engines

Lightweight Low Pressure (LP) systems for turbofans, including

– Composite fan blades & fancase – Lightweight structures– High efficiency low pressure turbine

Advanced engine externals & installations including novel noise attenuation

For advanced geared fan engine concepts– High efficiency LP spool technology – High speed LP turbine design– Aggressive mid turbine interduct

For next generation rotorcraft engine– High efficiency & lightweight compressor – High efficiency & lightweight turbine– Low emission combustion chamber

To develop and validate technologies Contributing to the environmental targets On 5 complementary demonstrator engines for regional, narrow body, wide body & rotorcraft

applications Raising the Technology Readiness Levels to TRL 6

Sustainable and Green Engine – Objectives and contentSustainable and Green Engine – Objectives and content


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Rotating structure

Shafts

Modules, sub-systems, nacelle items

Design integration, assemblyTest Programme

Power Turbine items

PGB for alternate architecture

Airframer requirements and installations

Project launch1 June 2008

Project completion2013

Prelim. DRJune 2011

Interim ReviewNov. 2009

Concept studiesDemo spec.

Prelim. designPartner selection

Detail designManufacture

Build and test

Critical DRDec. 2011

Open rotor technology development → full-scale engine demonstration

Concept DRSept. 2010

Nacelle items

Pitch Change Mechanism

PGB

Bearings

Sustainable and Green EngineSustainable and Green Engine


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CROR engine integration conceptsCROR engine integration concepts


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"Ecolonomic" life cycle



Aircraft Life Cycle

Green Regional Aircraft – Contribution to Green Regional Aircraft – Contribution to environmental targetsenvironmental targetsGreen Regional Aircraft – Contribution to Green Regional Aircraft – Contribution to environmental targetsenvironmental targets


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Green Regional – Objectives and contentGreen Regional – Objectives and content

• Demonstrate technologies for future regional aircraft aiming at the reduction

of fuel consumption, pollution and external noise

By means of :

mature, validate and demonstrate advanced aerodynamics (LNC domain), advanced structures and materials (LWC domain) all electric aircraft architectures (AEA domain) advanced avionics architectures (MTM domain) integration of these technologies in advanced aircraft configurations interfacing new powerplants types (NC domain)

integrate technical solutions from other technical platforms of the Clean Sky (energy management and Mission & Trajectory managements for SGO, engines for SAGE, Eco Design) in the Demonstrators of the Green Regional Aircraft, using a multidisciplinary approach.

Electrical Generators & Controls

ECS Electrical Compressor

With reference to the generic regional aircraft type, the following Demonstrators will be produced:

Aerodynamic & Aeroacoustic WT test

Cockpit Fuselage Wing BoxGround Demonstration

Flight Demonstration


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Aircraft Life Cycle

Green Rotorcraft – Contribution to environmental targetsGreen Rotorcraft – Contribution to environmental targets


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1. Innovative Rotor Blades Active blade devices Blade stall alleviation, profile drag reduction (tayloring of blade design)

Achievements: Baseline reference definition, techno reviews & preliminary selections2. Drag reduction, required power reduction

Passive and active flow controls for helicopter and tiltorotor components Integration of MR pylon, hub, aft body, tail, turboshaft engine installation

Achievements: Tech Reviews for hub, engine installation, wing & tail design of tilt-rotor3. More electrical Helicopter

Elimination of noxious hydraulic fluid; optimised on-board energy ; weight reduction4. Lean powerplant

installation of a Diesel engine on a light single HC for low CO2 emission

Achievements: Preliminary requirements (installation, certification, environmental targets)5. Environment-Friendly Flight Path

Noise abatement with optimized flight procedures in VFR & IFR including ATM constraints Fuel consumption and pollutant emissions reduction through a mission profile optimization

6. EcoDesign Participation to generic studies +demo on specific rotorcraft technologies & components

7. Technical Evaluator1. Interfacing to the assessment of actual impact of selected technologies for rotorcraft

Achievements: 1st release of the simulated platform (Phoenix) to the TE for integration

Green Rotorcraft – Objectives and contentGreen Rotorcraft – Objectives and content


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Rotor Blades - TechnologiesRotor Blades - Technologies

• Active control

active blade deformation e.g. active twist (further to Friendcopter) :

• Optimized design

3D blade profile tayloring

Active control surface e.g. Gurney flap :


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Aircraft Life Cycle

Systems for Green Operations - Contribution to environmental targetsContribution to environmental targets


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Ground Tests

Technology Development

COPPER Test Rig at Hispano -Suiza PROVEN Test Rig at Airbus Flight Test Aircraft

Electrical ECSElectrical Engine Start and Power Generation

Electrical WIPSElectrical Power Distribution

and Management

Electrical Power Drive Systems

Thermal Management Equipment

►Management of Aircraft Energy (MAE) branch of SGO ITD encompasses all aspects of on-board energy provision, storage, distribution and consumption

►MAE aims at developing electrical system technologies and energy management functions to reduce fuel consumption and overall aircraft emissions through:

• Development of all-electrical system architectures and equipment

• Validation and maturation of electrical technologies to TRL 6 by large scale ground and flight demonstrations.

Flight Demonstration

Systems for Green operations - Objectives and content (1/2)Objectives and content (1/2)


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Multi-criteria optimisation

Fuel

NoiseNOxContrailsCO2

CruiseT/O Climb Descent Approach

►Management of Trajectory and Mission (MTM) branch of SGO ITD aims at reducing the environmental impact in the way the aircraft manages its trajectory either on ground or in flight

►Two main fields of research : • Improve in-flight trajectories, including overall missions profiles

• Reduce the need to use main engines during taxiing operations Electrical taxiingGreen FMS Robustness to Weather

Technology Development

Systems - Objectives and content (2/2)Objectives and content (2/2)

SESAR


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Eco-Design – Contribution to Environmental Targets




Power Plant Loads & Flow Control New Aircraft Configurations Low Weight Aircraft Energy Management Mission & Trajectory Management


Aircraft Life Cycle


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Eco-Design ITD - Objectives and ContentsEco-Design ITD - Objectives and Contents

To design airframes for decreasing inputs, outputs andnuisances during A/C design & production and withdrawalphases

To design architectures of a/c systems, towards themore/all electrical a/c, with the objective of reducing use of non-renewable and noxious fluids/materials

Eco-Design for Airframe (EDA) main objective Eco-Design for Systems (EDS) main objective

Modelling

EcoEco--Design for AirframeDesign for Airframe

EcoEco--DesignDesignFor systemsFor systems

Inputs :

Raw materialsWaterEnergy …

Outputs,Nuisances :

Energy (warming)Liquid effluents

Gaseous effluentsSolid waste …

a/c Design &

Production

Inputs :

FuelLubricantsEnergy …

Nuisances :Energy (warming)

CO2, NOxNoise

ContrailsCrash waste …

a/c Use & Maintenance

Inputs :

FuelWaterEnergy …


Liquid effluentsGaseous effluents

Solid waste …

a/c

Withdrawal(Recycling)

EcoEco--Design for AirframeDesign for Airframe

EcoEco--DesignDesignFor systemsFor systems

Inputs :


Outputs,Nuisances :



a/c Design &

Production

Inputs :


Outputs,Nuisances :



a/c Design &

Production

Inputs :

FuelLubricantsEnergy …


CO2, NOxNoise

ContrailsCrash waste …

a/c Use & Maintenance

Inputs :

FuelWaterEnergy …


Liquid effluentsGaseous effluents

Solid waste …

a/c

Withdrawal(Recycling)


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Eco-Design ITD


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Technology EvaluatorTechnology Evaluator

•Technology Evaluator : integrator of the outcomes of the different ITDs in order to provide an assessment of the actual environmental benefits

•TE is tasked to coordinate the revision of the targets set at the beginning of the program

•TE is also the focal point for the links with other programs or bodies like SESAR, EASA and Eurocontrol


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Reference vs Clean Sky aircraft Reference vs Clean Sky aircraft and fleet at global leveland fleet at global level

flow

s&

im

pact

s flow

s&

im

pact

s

Current technologyAircraft (Reference)

Without Clean Sky

2020 / 2020+ forecast (incl. SESAR)2000

List of Clean Sky Conceptual Aircraft

Promisingtechnologies

from ITDsGeneric fleet

inserted into traffic

Performances of technologies

Performances of aircraft

flows&

impacts

Environment impacts

Deltas

With Clean Sky


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Thank you for your attention


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© 2010 by the CleanSky Leading Partners: Airbus, AgustaWestland, Alenia Aeronautica, Dassault Aviation, EADS-CASA, Eurocopter, Fraunhofer Institute, Liebherr Aerospace, Rolls-Royce, Saab AB, Safran Thales and the European Commission.

Permission to copy, store electronically, or disseminate this presentation is hereby granted freely provided the source is recognized. No rights to modify the presentation are granted.

Documents

1 1 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Clean Sky Programme Helmut Schwarze, Project Officer CSJU Aerospace Technology 2010 18 th & 19