Clean Sky Joint Undertaking. Airframe ITD. Vittorio Selmin Project Officer

Transcription

1 Clean Sky Joint Undertaking Airframe ITD Vittorio Selmin Project Officer

2 Background Greener Airframe Technologies More Electrical a/c architectures More efficient wing Novel Propulsion Integration Strategy Optimized Smart control Fixed surfaces Wing Aircraft Integrated Structures Smart high lift devices Re-think the wing Re-think the a/c architecture Re-think the cabin Re-think the fuselage Re-think the control Step changes in the efficiency of all airframe elements by the means of a systematic re-thinking

3 Key General Objectives More Efficient Airframes Weight Drag Cabin Noise New Materials Maintenance Efficiency of the engineering & manufacturing process Manufacturing Cost Time to Market (lead Time) IADP/Integrated Demonstrators SUPPORT TO IADP: Maturate technologies up to TRL 6 REG High Performance & Energy Efficiency High Versatility & Cost Efficiency FRC Innovative Aircraft Architecture Advanced Laminarity High Speed Airframe Novel Control Novel travel experience Next generation optimized wing Optimized high lift configs. Advanced integrated structures Advanced Fuselage LPA AIR Bizjet REG FRC LPA SAT AIR Bizjet TRANSVERSE Eco-Design for Airframe & Modeling to certification ability SAT FUTURE: De-risk novel generation product in prospect of changing step by the

4 Work Breakdown Structure M - Management & Interface A - High Performance and Energy Efficiency TS A-1: Innovative Aircraft Architecture TS A-2: Advanced Laminarity TS A-3: High Speed Airframe TS A-4: Novel Control TS A-5: Novel travel experience WP M-1 WP A-1.1 WP A-2.1 WP A-3.1 WP A-4.1 WP A-5.1 Overall Management Optimal engine integration on rear fuselage Laminar nacelle Multidisciplinary wing for high & low speed Smart mobile control surfaces WP M-2 WP A-1.2 WP A-2.2 WP A-3.2 WP A-4.2 WP A-5.2 Ergonomic flexible cabin Business Aviation OAD & config. Mgt CROR & UHBR configurations NLF smart integrated wing Tailored front fuselage Active load control Office Centered Cabin WP M-3 WP A-1.3 WP A-2.3 WP A-3.3 LPA OAD & config. Mgt WP M-4 WP A-1.4 Novel high performance configuration Extended laminarity Innovative shapes & structure RotorCraft OAD & configuration Mgt Virtual modelling for certification WP M-5 Regional a/c OAD & config. Mgt B - High Versatility and Cost Efficiency C - Eco-Design TS B-1: Next Generation optimized wing box TS B-2: Optimized high lift configurations TS B-3: Advanced Integrated Structures TS B-4: Advanced Fuselage WP B-1.1 WP B-2.1 WP B-3.1 WP B-4.1 WP C-1 Wing for incremental lift & transmission shaft integration High wing / large Tprop nacelle configuration Advanced Integration of syst. in nacelle Rotor-less tail for Fast Rotorcraft WP B-1.2 WP B-2.2 WP B-3.2 WP B-4.2 WP C-2 (ex A-3.4) More affordable composite structures High lift wing All electrical wing Pressurized fuselage for Fast Rotorcraft WP B-1.3 WP B-3.3 WP B-4.3 WP C-3 (ex B-3.6) More efficient wings technologies Highly integrated cockpit WP B-1.4 WP B-3.4 WP B-4.4 Flow & shape control More affordable small a/c manufacturing More affordable composite fuselage Low weight, low cost cabin Eco-Design TA Link Eco-Design for airframe New materials & manufacturing

5 Share of funding foreseen Participants to date CfP PROJECTS Countries involved to date Leader 16.7% 4* 4 Part. Leaders Core Partners 23.2% 13* % 76* 12 Partners 30.1% 124** 16** *incl. Affiliates and Third Parties ** till CfP04 NEWCORT DISTRACTION BLADEOUT INSCAPE REDISH ERACLE RESET SIMCODEQ CT Ingenieros A.A.I. S.L. Barcelona Supercomputing Centre Testing and Engineering of Aeronautical Materials and Structures SL EUROTECH ARTUS SAS ASPIRE ULTRATECH Sp zoo Ultra Electronics LTD GEVEN Spa LORTEK S.COOP AEROTEX UK LLP NEODAMP SZEL-TECH DEMOS Aero-Magnesium Limited ACS BALANCE INVENT Gesellschaft mit beschränkter Haftung PGA Electronic AERNNOVA ENGINEERING DIVISION SAU (ATP) AERNNOVA Aerospace S.A.U. (ATP) AERNNOVA Aerostructuras ALAVA, S.A. (ATP) SHERLOC QSP AERNNOVA Composites ILLESCAS S.A. (ATP) Internacional de Composites SAU (ATP) TESTCONCERT Fibertecnic SAU (ATP) INTEC-AIR (ATP) Componentes aeronauticos SA (ATP) CIRA Noesis Solutions NV MOTIVATE ALTRAN Deustchland SAS & Co KG INSTYTUT LOTNICTWA OPTIMORPH Polskie Zaklady Lotnicie sp zoo PARTICIPATING LEADERS** SIEMENS Industry Software NV FRCDOORDEMONSTRATOR Stichting Nationaal Lucht- en Ruimtevaartlaboratorium DANOBAT S.Coop Israel Aerospace Industries Ltd. TECHNI-MODUL ENGINEERING University of Sheffield Imperial College of London GE Aviation TU DELFT ZAKLADY LOTNICZE Akzo Noble Car Refinishes BV MARGANSKI & MYSLOWSKI SA HEPODIS MISSP Design Manufactoring Spa Università degli Studi di MAF AERTEC Ingenieria y Desarollos SLU Napoli "Federico II" CRORTET AVIAERTEC LDA Alma Mater Studiorum- CRISTA DILECO Università di Bologna Instituto de Soldadura e ELEMENT Qualidate University of Patras FORMIT University of Nottingham ASTRASY Instituto de Ciencia e Inovacao EM Engenharia Mecanica e Vrije Universiteit Brussel CRO-INSPECT Engenharia Industrial Universitaet Stuttgart RODEO ADD-ON CAETANO AERONAUTIC SA Politecnico di Torino COFRARE 2.0 ALMADESIGN CONCEITO E DESENVOLVIMENTO DE DESIGN LDA Universidad Politécnica de Madrid CORDIAL CRITICAL MATERIALS SA AFPMET Fundación Centro de Tecnologías EDISOFT-EMPRESA DE SERVICOS E OLFITT DESENVOLVIMENTO DE SOFTWARE SA Aeronáuticas COBOMEGA GMVIS SKYSOFT SA AMULET OPTIMAL STRUCTURAL SOLUTIONS Lda Fundación Tecnalia Research & Innovation PILOT PIPS CENTRO PARA A EXCELENCIA EINOVACAO NA INDUSTRIA AUTOMOVEL TEKEVER - TECNOLOGIAS DE INFORMACAO, S.A. Deutsches zentrum fuer Luft und Raumfahrt EV I3PS SMART-LAYUP ASCO Industries N.V. Fundación Andaluza para el Desarrollo Aeroespacial E2S2A2 Meggitt A/S Fundacion para la Investigacion, Desarollo y Aplication de Materiales Compuestos TR4EMACS OASIS INDUCTICE MEGGITT Aerospace LTD FOKKER Aerostructures B.V. HAIRD Precision Micro Limited (ATP) Fokker Technologies Holding B.V. OPTIWIND IMCA INtegrated Aerospace P.W Metrol Dabkowski Dariusz RAMAL srl WIN-TOOL Sciences COrporation INNOHYBOX OLTITA CORIOLIS Composite Technologies TAMI ACUMEN Design Associates Ltd DOVER TRANSITION ADDMAN PRODIGE WINNER PASSPORT ACCURATE CORE PARTNERS LABOR Broad Participation: e.g. AIR DADIYSO COMP (till CfP06) LEADER SPECTRAL MEPAFUS WINBOXTOOL BRIDAS ONERA C-JOINTS PSIDESC RIB-ON AMTRAS ARIESS **incl. Affiliates and Third Parties [Project ] = related to Small Air Transport

6 AIR ITD - CfP Status CfP08 16 Topics 11.5 Meuro Topic nb CfP Title Topic Leader WP/ Task Type of Action Duration (Month) Est. budget [k ] HPE AIR Composite mould tool based on 3D printing. SAAB A-3.1 RIA AIR Investigation of gust loads in a transonic flow based on an innovative test rig. ONERA A-4.2 RIA AIR In-Seat Ventilation & Supply for Personalized Comfort Control on Board an Aircraft AIB A-5.1 IA HVC AIR Full Scale Innovative Integrated Tooling for Composite Material Wing Box (SAT) IAI B-1.2 IA AIR Development and Optimization of Bonding Assembly Technology for a Wingbox (SAT) IAI B-1.2 IA AIR Virtual-Hybrid-Real On Ground demonstration for HVDC & EMA Integration ADS B-3.2 IA AIR Enhanced Low Cost Complex Composite Structures ADS B-2.2 IA AIR Cold Spray of metallic coatings on polymer and composite materials. (SAT) PZL B-3.4 IA AIR Design of special welding head for FSW process with automatic adjustable pin and welding force control system (SAT) PZL B-3.4 IA AIR Evaluation and modelling of comfort driving parameters in a Cabin Demonstrator FhG B-4.4 RIA AIR Model based development of an innovative ECS air distribution system supported by a generic laboratory ECS analogue allowing for piecewise integration of ECS components prototypes for ground testing with a Cabin Demonstrator FhG B-4.4 RIA Eco-Design (ED) AIR Bio contamination survey and tests DAv C-2.1 IA AIR Non destructive control (NDT) of sticking and assemblies focused on tightness DAv C-2.1 IA AIR Sizing for recycled carbon fibres to optimise adhesion in organic/inorganic composite materials. FhG C RIA AIR Development of an anaerobic digester prototype for aircraft use FhG C RIA AIR Development and evaluation of a manufacturing process for a lightweight aircraft wheel made of CFRP FhG C IA

7 Innovation Takes Off Q&A

8 Thank You

9 Backup Slides

10 CfP08 - HPE JU Ref. CfP Title Activity Line WP/Task RIA or IA Duration (Month) Est. budget [k ] JTI-CS CFP08-AIR Composite mould tool based on 3D printing. HPE A-3.1 RIA

11 CfP08 - HPE JU Ref. CfP Title Activity Line WP/Task RIA or IA Duration (Month) Est. budget [k ] JTI-CS CFP08-AIR Investigation of gust loads in a transonic flow based on an innovative test rig. HPE A-4.2 RIA

12 CfP08 - HPE JU Ref. CfP Title Activity Line WP/Task RIA or IA Duration (Month) Est. budget [k ] JTI-CS CFP08-AIR In-Seat Ventilation & Supply for Personalized Comfort Control on Board an Aircraft HPE A-5.1 IA

13 CfP08 - HVC JU Ref. CfP Title Activity Line WP/Task RIA or IA Duration (Month) Est. budget [k ] JTI-CS CFP08-AIR Full Scale Innovative Integrated Tooling for Composite Material Wing Box HVC B-1.2 IA

14 CfP08 - HVC JU Ref. CfP Title Activity Line WP/Task RIA or IA Duration (Month) Est. budget [k ] JTI-CS CFP08-AIR Development and Optimization of Bonding Assembly Technology for a Wingbox HVC B-1.2 IA

15 CfP08 - HVC JU Ref. CfP Title Activity Line WP/Task RIA or IA Duration (Month) Est. budget [k ] JTI-CS CFP08-AIR Enhanced Low Cost Complex Composite Structures HVC B-2.2 IA

16 CfP08 - HVC JU Ref. CfP Title Activity Line WP/Task RIA or IA Duration (Month) Est. budget [k ] JTI-CS CFP08-AIR Cold Spray of metallic coatings on polymer and composite materials. HVC B-3.4 IA

17 CfP08 - HVC JU Ref. CfP Title Activity Line WP/Task RIA or IA Duration (Month) Est. budget [k ] JTI-CS CFP08-AIR Virtual-Hybrid-Real On Ground demonstration for HVDC & EMA Integration HVC B-3.2 IA

18 CfP08 - HVC JU Ref. CfP Title Activity Line WP/Task RIA or IA Duration (Month) Est. budget [k ] JTI-CS CFP08-AIR Designing of special welding head for FSW process with automatic adjustable pin and welding force control system HVC B-3.4 IA

19 CfP08 - HVC JU Ref. CfP Title Activity Line WP/Task RIA or IA Duration (Month) Est. budget [k ] JTI-CS CFP08-AIR Evaluation and modelling of comfort driving parameters in a Cabin HVC B-4.4 RIA Demonstrator 20

20 CfP08 - HVC JU Ref. CfP Title Activity Line WP/Task RIA or IA Duration (Month) Est. budget [k ] JTI-CS CFP08-AIR Model based development of an innovative ECS air distribution system for ground testing with a Cabin Demonstrator HVC B-4.4 RIA

21 CfP08 ECO DESIGN

22 CfP08 ECO DESIGN

23 CfP08 ECO DESIGN

24 CfP08 ECO DESIGN

25 CfP08 ECO DESIGN

26 Key Objectives Validate through demonstration of integrated technologies : To introduce innovative airframe architecture To introduce technologies for more efficient airframe : drag, weight, cost, environmental impact, passenger well-being, maintenance, servicing, To enhance the efficiency of the engineering & manufacturing process : timeto-market and competitiveness against low-cost labour countries, To fully address a technology issue from modeling to certification ability Serve maturity up to TRL 6 of airframe technologies De-risk novel generation product in the prospect of a next game changing step by Support next generation bizjets and general aviation directly Support Large a/c, regional a/c and rotorcraft directly and through IADPS Create Product differentiators Supporting a 5 Product s Segments Strategy Base 27

27 Interfacing & cross interaction management Overall Technical Overview Specifications & Requirements Technology Development & Demonstration Integration Profile Development Integrated Concept demonstrat prototype airframe compon ts IADP RA Concept Analysis HPE Technology Streams Innovative Aircraft Architecture Advanced Laminarity IADP LPA IADP Rcraft High Speed Airframe IADP RA Novel Control IADP LPA Novel Travel Experience IADP Rcraft HVC Next Gen. optimized wing box ITD Systems SAT Transverse act Optimized high lift configurations Advanced Integrated Structures Advanced Fuselage Novel innovation wave TRL <= 5 ITD Engine ITD Systems ECO TE HPE: High Performance and Energy Efficiency HVC: High Versatility and Cost Efficiency