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

2 2 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Outlines  Clean Sky Programme Overview ACARE goals Expected benefits Technical areas & projects Implementation & membership Results-oriented project: environmental objectives & more mature demonstration Call for proposals  Main Technical achievements  SFWA  SAGE  SGO  GRA  TE

3 3 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Clean Sky Programme Overview

4 4 Aerospace Technology 2010, Stockholm, 18-19/10/2010 ACARE Goals: Vision 2020 Challenges

5 5 Aerospace Technology 2010, Stockholm, 18-19/10/2010 ACARE Goals: Vision 2020 Challenges ACARE October 2002 : The Strategic Research Agenda (SRA) 5 Challenges Quality and Affordability EnvironmentSafety Air 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

6 6 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Benefits of investing in aeronautics technologies  Environment Greener 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 industry Open access to SMEs and New Member States Expected multiplier effect via complementary National Programmes A 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

7 7 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Expected results from Clean Sky

8 8 Aerospace Technology 2010, Stockholm, 18-19/10/2010 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%CO2 80% NOx 50% noise Green design.. "Ecolonomic" life cycle Reduced fuel consumption (CO 2 & NOx reduction) External noise reduction ACARE GOALS Technology Domains

9 9 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Smart Fixed Wing Aircraft Systems for Green Operations Green Rotorcraft Technology Evaluator Sustainable and Green Engines Eco-Design Green Regional Aircraft Clean Sky Integrated Technology Demonstrators Rolls-Royce & Safran Airbus & SAAB Eurocopter & AgustaWestland Alenia & EADS-CASA Dassault & Fraunhofer Thales & Liebherr DLR & Thales

10 Aerospace Technology 2010, Stockholm, 18-19/10/2010  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-cash 800 million € from industry in-kind  7-year research project on Greening of Aeronautics: Clean Sky: implementation

11 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Clean Sky targets Preliminary 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 RegionalBizjets Rotor craft CO2- 30%- 20%- 40%- 30% NOX - 30%- 20%- 40%- 30%- 60% Noise - 20 dB- 15 dB- 20 dB- 10 dB ACARE targets: -50% C02 -50% noise -80% Nox in 2020 vs 2000

12 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Clean Sky: split of the public funding  ITD leaders & Associates Organisation necessary to the delivery of the platform objectives 7 years commitment Sign the JTI Statutes Participate in JTI operational costs Cannot 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  SMEs  12% will represent ~200M€  Representing 1000 to 2000 SME contracts

13 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Split of the 800 M€ public funding 6x2 ITD leaders Up to 50% 74 associates Up to 25% MEMBERS are committed for the full duration of CSJU PARTNERS are committed for the duration of their topic(s) ~500 partners (*) through calls At least 25% (*) ~100 today

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

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

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

17 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Governance Governing Board: 12 industrial leaders + 6 associates + EU Commission Joint Undertaking Executive Team ITD European Parliament Annual discharge Scientific and Tech. Advisory board General Forum ITD: integrated Technology Demonstrator Technology evaluator National States representatives Group Partners ITD Partners

18 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Calls for proposals: some average figures 400 M€ dedicated to calls for proposals 3-4 Calls per year in 2010, 2011,… 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

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

20 Aerospace Technology 2010, Stockholm, 18-19/10/2010 For further information:  Helmut Schwarze SFWA Project Officer  Contact us

21 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Clean Sky Programme Main Technical Achievements

22 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Reduced fuel consumption Reduction of CO 2 and NO X  Engines  Loads & Flow Control  New Aircraft Configurations  Low weight  Aircraft Energy Management  Mission & Trajectory Management External noise reduction „Ecolonomic“ life cycle  Engines  Mission & Trajectory Management  Configurations  Rotorcraft Noise Reduction  Aircraft Life Cycle Smart Fixed Wing Aircraft – Contribution to environmental targets

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

24 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Smart Wing Flight Test Instrumentation

25 Aerospace Technology 2010, Stockholm, 18-19/10/ Integration of the Counter Rotating Open Rotor Concept

26 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Reduced fuel consumption (CO 2 & NOx reduction External noise 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 COup to 20% NO x up to 60% Noiseup to 20 dB Sustainable and Green Engine – Contribution to environmental targets

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

28 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Rotating structure Shafts Modules, sub-systems, nacelle items Design integration, assembly Test Programme Power Turbine items PGB for alternate architecture Airframer requirements and installations Project launch 1 June 2008 Project completion 2013 Prelim. DR June 2011 Interim Review Nov Concept studies Demo spec. Prelim. design Partner selection Detail design Manufacture Build and test Critical DR Dec Open rotor technology development → full-scale engine demonstration Concept DR Sept Nacelle items Pitch Change Mechanism PGB Bearings Sustainable and Green Engine

29 Aerospace Technology 2010, Stockholm, 18-19/10/2010 CROR engine integration concepts

30 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Reduced fuel consumption (CO 2 & NOx reduction) External noise reduction "Ecolonomic" life cycle  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 Green Regional Aircraft – Contribution to environmental targets

31 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Green 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 Box Ground Demonstration Flight Demonstration

32 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Reduced fuel consumption (CO 2 & NOx reduction) External noise reduction "Ecolonomic" life cycle  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 Green Rotorcraft – Contribution to environmental targets

33 Aerospace Technology 2010, Stockholm, 18-19/10/ Innovative Rotor Blades  Active blade devices  Blade stall alleviation, profile drag reduction (tayloring of blade design) Achievements: Baseline reference definition, techno reviews & preliminary selections 2.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-rotor 3.More electrical Helicopter  Elimination of noxious hydraulic fluid; optimised on-board energy ; weight reduction 4.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 Evaluator  Interfacing to the assessment of actual impact of selected technologies for rotorcraft Achievements: 1 st release of the simulated platform (Phoenix) to the TE for integration Green Rotorcraft – Objectives and content

34 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Rotor 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 :

35 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Reduced fuel consumption (CO 2 & NOx reduction) External noise reduction "Ecolonomic" life cycle  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 Contribution to environmental targets Systems for Green Operations - Contribution to environmental targets

36 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Ground Tests Technology Development COPPER Test Rig at Hispano -Suiza PROVEN Test Rig at Airbus Flight Test Aircraft Electrical ECS Electrical Engine Start and Power Generation Electrical WIPS Electrical 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 Objectives and content (1/2) Systems for Green operations - Objectives and content (1/2)

37 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Multi-criteria optimisation Fuel Noise NOx Contrails CO 2 Cruise T/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 taxiing Green FMS Robustness to Weather Technology Development Objectives and content (2/2) Systems - Objectives and content (2/2) SESAR

38 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Eco-Design – Contribution to Environmental Targets Reduced fuel consumption (CO 2 & NOx reduction) External noise reduction "Ecolonomic" life cycle  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

39 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Eco-Design ITD - Objectives and Contents Eco-Design ITD - Objectives and Contents To design airframes for decreasing inputs, outputs and nuisances during A/C design & production and withdrawal phases To design architectures of a/c systems, towards the more/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

40 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Eco-Design ITD

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

42 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Reference vs Clean Sky aircraft and fleet at global level flows & impacts flows & impacts Current technology Aircraft (Reference) Without Clean Sky 2020 / forecast (incl. SESAR) 2000 List of Clean Sky Conceptual Aircraft Promising technologies from ITDs Generic fleet inserted into traffic Performances of technologies Performances of aircraft flows & impacts Environment impacts Deltas With Clean Sky

43 Aerospace Technology 2010, Stockholm, 18-19/10/2010 Thank you for your attention

44 Aerospace Technology 2010, Stockholm, 18-19/10/2010 © 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.