Innovation Takes Off. Not legally binding

Transcription

1 Innovation Takes Off Not legally binding

2 Clean Sky 2 Information Day AIRFRAME ITD Pedro L. Rubio EADS CASA HO R&T Development Madrid, 12ve of February 2014

3 From Clean Sky towards Clean Sky 2 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

4 High Level Objectives

5 From the From the Impact Perspective Expected Impacts Environmental Perspective More resource efficient aircraft : challenging targets for up to 30% cumulative CO 2 10 EPNdB Eco responsible industrial capabilities Smart & Efficient Mobility Perspective Industrial Leadership Perspective Increased operational flexibility (flight domain) Access to dense populated areas : low noise and low speed performances Access to remote areas performances : short take off and landing, reduced a/c ground infrastructure, remote repairing Travelling Time not as a wasted Time : passenger well-being Sustainable traffic growth Cost efficient Products Strong Product Differentiators Cost efficient engineering, manufacturing & life cycle support processes (up to recycling) Reduced time to market Sustainable industrial capability

6 Key Objectives Validate through demonstration of integrated technologies : To introduce innovative airframe architecture To introduce techonogies for more efficient airframe : drag, weight, cost, environmental impact, passager 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

7 Setup and Implementation

8 The Leadership : who are we? Key world player in the aerospace industry. More than 8,000 aircraft delivered, RAFALE FALCON representing some 28 million of hours of flight Falcon in operation. Omnirole BizJets Only group in the world to design, manufacture and support both combat aircraft and business jets. neuron UCAV Demonstrator Saab serves the global market of governments, authorities and corporations with products, services and solutions ranging from military defence to commercial aeronautics. The product portfolio includes the Gripen combat aircraft, Unmanned Aerial Systems (UAS) and large aero-structures for OEM s such as Airbus and Boeing. More than 70 years in business and more than 4000 aircraft manufactured, among them 500 airliners. World leader in turboprop aircraft with full capabilities from design, manufacturing, aircraft integration, certification and services. Product portfolio includes: full proven family of transport aircraft: A400M, C295, CN235 & C212; Eurofighter, Unmanned Aerial Systems (UAS), world leader in Air Refuelling Systems & Aircraft; large aero-structures for OEM s such as Airbus and Boeing. More than 90 years in business and more than 6,000 aircraft delivered to more than 140 operators in 70 countries.

9 The Overall Partnerships Airbus, ALENIA, EUROCOPTER, AGUSTA WESTLAND, SAT Core Team and Fraunhofer Institute have a central role to AIRFRAME ITD The role of industrial core partners, REs and Academia will be major in three main direction: Development of main technologies and elements of OEM defined demonstrators => direct contributions at models, design, development, manufacture & testing level to demonstrator components Development of other industrial core partner defined major demonstrators, in line with the defined demonstrations objectives and technology routes Development of lower TRL / longer term technologies The AIRFRAME ITD work scope is still under a consolidation process : it is expected to be adjusted and tuned against The final outcomes from the regulation adoption process The recommendations from the expert panel of the Technical Evaluation The suggestions arising from the current Information Process

10 Transverse Enabling Capability Focused Integrated Demonstrations Investigate advanced engine integration & novel overall architecture Laminar nacelles; NLF smart integrated wing fitting the industrial environment High efficient multi-disciplinary flexible wing; fuselage changes in shapes, & structure Smart multi-function control surfaces & load & flutter alleviation Passenger friendly cabin; ergonomic & flexible, new volume utilisation Low cost composite structures Efficient architectural concept for turbopropeller high wing composite nacelle & adaptative wing New structural paradigm for optimised integration of systems in airframe, electrical wing Novel composite fuselage & cabin; tailless or pressurized fuselage for rotorcraft Overall Technical Overview High Performance & Energy Efficiency High Versatility & Cost Efficiency 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 Novel Certificat Eco Design Extended Laminarity More Efficient Wing Flow & shape Control Advanced Manufact.

11 Interfacing & cross interaction management Specifications & Requirements Technology Development & Demonstration Integration Profile Development Integrated Concept demonstrat prototype airframe compon ts IADP RA Concept Analysis 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 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

12 High Performance & Energy Efficiency- WBS High Performance & 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 Leader : Dassault Aviation Co leader : SAAB Management & Interfacing WP A-1.1: Optimal engine integration on rear fuselage WP A-2.1: Laminar nacelle WP A-3.1: Multidisciplinary wing for high & low speed WP A-4.1: Smart mobile control surfaces Innovative Aircraft Architecture WP A-5.1: Ergonomic flexible cabin Advanced Laminarity Novel Control Novel Travel Experience WP A-1.2: CROR configuration WP A-2.2: NLF smart integrated wing WP A-3.2: Tailored front fuselage WP A-4.2: Active load control WP A-5.2: Office Centered Cabin WP A-1.3: Novel high speed configuration WP A-2.3: Laminarity for high lift wing WP A-3.3: Innovative shapes & structure WP A-1.4: Novel certification processes WP A-2.4: Extended laminarity WP A-3.4: Optimized cockpit structure WP A-1.5: Eco Design

13 TS A-1 : Innovative Aircraft Architecture High Performance & Energy Efficiency TS A-1: Innovative Aircraft Architecture WP A-1.1: Optimal engine integration on rear fuselage WP A-1.2: CROR configuration WP A-1.3: Novel high speed configuration WP A-1.4: Novel certification processes WP A-1.5: Eco Design Objectives Demonstrate viability & assess potentiality of advanced aircraft configurations : explore concepts, identify potential showstoppers & confirm solutions Engine integration on rear fuselage, CROR, High Speed Facilitate certification : cost-effectiveness and time to market for innovations insertion Eco design for Airframe : green life cycle Means & Enablers Large Wind Tunnel Test Sample and structural parts demonstrator for Eco Design Partnership Framework Engine Supplier, Research Institute, PLM & engineering software provider, Aero-Structure Industry with track record in Eco Design, Material & Coating provider Timescale Highly optimised configurations: In-rupture configurations: Gross Budget (activities) : 140/145 M

14 TS A-2 : Advanced Laminarity High Performance & Energy Efficiency TS A-2: Advanced Laminarity WP A-2.1: Laminar nacelle WP A-2.2: NLF smart integrated wing WP A-2.3: Laminarity for high lift wing WP A-2.4: Extended laminarity Objectives Demonstrate aero-shape concepts and architecture revision of N(H)LF Nacelles Demonstrate a NLF wing concept that can be manufactured, produced and maintained in an industrial environment Explore laminarity potential for adverse configuration: high lift wing Progress on advanced laminarity techniques in design (e.g. active shock control, hybrid flow ), production and maintainability to extended application domain and operability Means & Enablers Nacelle demonstrators flight test Large scale NLF smart wing ground demonstrator Partnership Framework Research Institute & Academia, Aero-Structure Industry, Nacelle Supplier Timescale Gross Budget (activities) : 85/90 M

15 TS A-3 : High Speed Airframe High Performance & Energy Efficiency TS A-3: High Speed Airframe WP A-3.1: Multidisciplinary wing for high & low speed WP A-3.2: Tailored front fuselage WP A-3.3: Innovative shapes & structure WP A-3.4: Optimized cockpit structure Objectives Progress on the wing, fuselage and cockpit in an integrated approach for high performing aircraft (enlarged flight domain) Achieving new aero-structural design optima of composite wing by steering (i.e. shape/structure coupled optimization) Reshaping & and optimized system integration of front fuselage Efficiency of metallic fuselage: architecture with low density & multifunctional materials, multidisciplinary optimization (e.g. structure & noise), new volumes Cockpit setup capable to accommodate all next generation cockpit features Means & Enablers Representative wing box demonstrator Wind Tunnel Tests Dedicated structural components & partial fuselage demonstrator Partnership Framework Research Institute & Academia, Aero-Structure Industry, Material Provider, Equipment Supplier Timescale Optimization/Local demonstrators: Radical concepts/sub scale demonstrators: Gross Budget (activities) : 70/75 M

16 TS A-4 : Novel Control High Performance & Energy Efficiency TS A-4: Novel Control WP A-4.1: Smart mobile control surfaces WP A-4.2: Active load control Objectives Develop enhanced load alleviation function for gust loads Develop anti-flutter control law to gain flutter margin Develop efficient concept for multifunction control surfaces Develop integrated mobile surface Means & Enablers Flight test of new control laws Full scale ground demonstrator of smart mobile surfaces Partnership Framework Research Institute & Academia, Mobile part manufacturer, Equipment provider Timescale Short term demonstration batch: Extended demonstration batch: Gross Budget (activities) : ~ 25 M

17 TS A-5 : Novel Travel Experience (Cabin) High Performance & Energy Efficiency TS A-5: Novel travel experience WP A-5.1: Ergonomic flexible cabin WP A-5.2: Office Centered Cabin Objectives Passenger cabins have not been addressed within Clean Sky. Improve passenger comfort and ergonomy, safety and services, but also significant fuel efficiency through weight reduction & ecological benefit with environmental friendly materials Human engineering approach New seat arrangement and furniture & equipment concepts Purpose focused functionalities of cabin areas Local environment tailoring Means & Enablers Dedicated digital and mock up studies Local/partial cabin items demonstrators Partnership Framework Cabin system provider, Research Institute & Academia, Material Providers, Equipment Suppliers, Design centers, Social behavior analysts Timescale Gross Budget (activities) : ~ 25 M

18 High Versatility & Cost Efficiency- WBS High Versatility & Cost Efficiency 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 Leader : EADS CASA Management & Interfacing WP B-1.1: Wing for incremental lift & transmission shaft integration WP B-1.2: More affordable composite structures WP B-1.3: More efficient wings technologies WP B-1.4: Flow & shape control WP B-2.1: High wing / large Tprop nacelle configuration WP B-2.2: Optimized integration of Tprop nacelles WP B-2.3: High lift wing WP B-3.1: Advanced integration of system in nacelle WP B-3.2: All electrical wing WP B-3.3: Highly integrated cockpit WP B-3.4: Advanced integration of systems in small a/c WP B-3.5: More affordable small a/c manufacturing WP B-4.1: Rotor-less tail for Fast Rotorcraft Innovative Aircraft Architecture WP B-4.2: Pressurized fuselage for Fast Rotorcraft WP B-4.3: More affordable composite fuselage WP B-4.4: Affordable low weight, human centered Cabin Advanced Laminarity Novel Control Novel Tra Experien WP B-3.5: New materials & manufacturing

19 TS B-1 : Next Generation Optimized Wing Box High Versatility & Cost Efficiency TS B-1 : Next Generation optimized wing box WP B-1.1: Wing for incremental lift & transmission shaft integration WP B-1.2: Optimized composite structures WP B-1.3: More efficient wing technologies WP B-1.4: Flow & shape control Objectives Structural improvements for wing Better use of composite materials Optimization of the wing efficiency Morphing technologies Active load control Means & Enablers Full scale wing, including components for IADPs Full range of calculation and simulation tools (CFD, FEM, dynamics) Sample, sub-components and full component ground tests Partnership Framework Research Institute & Academia, Aero-Structure Industry, Material Provider Timescale Item to be delivered to IADPs: Large scale demonstrators : Gross Budget (activities) : 60/65 M

20 TS B-2 : Optimized high lift configurations High Versatility & Cost Efficiency TS B-2 : Optimized high lift configurations WP B-2.1: High wing / large Tprop nacelle configuration WP B-2.2: High lift wing WP B-2.3: Optimized integration of Tprop nacelles Objectives Global aero structural optimizations Enhanced nacelle/engine integration Advanced high lift systems Progress on drag and integration for high wing with large turbo propulsors Means & Enablers Wind Tunnel test Full scale wing and flap including components for IADP Sample, sub-components and full component ground tests Partnership Framework Research Institute & Academia, Aero-Structure Industry, Nacelle suppliers, Engine suppliers Timescale Gross Budget (activities) : 45/50 M

21 TS B-3 : Advanced Integrated Structures High Versatility & Cost Efficiency TS B-3 : Advanced Integrated Structures WP B-3.1: Advanced integration of system in nacelle WP B-3.2: All electrical wing WP B-3.3: Higly integrated cockpit WP B-3.4: Advanced integration of systems in Small A/C WP B-3.5: More Affordable Manufacturing for Small A/C WP B-3.6: New materials & manufacturing Objectives More affordable, weight optimized structural components Native, optimized integration of equipment & systems in the structural design Manufacturing & assembly technology base Means & Enablers Full scale hybrid integrated cockpit demonstrator with cockpit system integration Electrical wing demonstrator at bench facilities and delivery to IADP Anti-icing WT / Anechoic chamber testing, component manufacturing demontrator Ground demonstrators consisting of central fuselage airframe subassemblies of metal fuselage and wing sections. System integration demonstrator for small a/c Partnership Framework Research Institute & Academia, Aero-Structure Industry, Material Provider, Equipment Supplier Timescale Gross Budget (activities) : 100/105 M

22 TS B-4 : Advanced Integrated Structures High Versatility & Cost Efficiency TS B-4: Advanced Fuselage WP B-4.1: Rotor-less tail for Fast Rotorcraft WP B-4.2: Pressurized fuselage for Fast Rotorcraft WP B-4.3: More Affordable composite fuselage WP B-4.4: Affordable low weight, human centered cabin Objectives New concept of fuselage to support future generation of fast rotorcraft Integrated structural concept for composite fuselage with more global aero structural optimizations Optimized passenger cabin environment Means & Enablers Full scale, flightworthy tail assembly fast rotorcraft demonstrator Fast rotorcraft pressurized fuselage demonstrator structurally tested on dedicated benches Full scale fuselage barrel demonstrator Small scale cabin set-ups & virtual demonstrators Partnership Framework Research Institute & Academia, Aero-Structure Industry, Material Provider, Equipment Supplier Timescale Gross Budget (activities) : 140/145 M

23 Major demonstration validations or components to be delivered to IADPs Technology Streams Innovative Aircraft Architecture Optimized CROR configurations Laminar wing (NFL/Hybrid) concept IADP LPA Advanced Laminarity Cabin arrangement concepts More electrical wing integration High Speed Airframe IADP Rcraft Novel Control Wing components Fuselage components Novel Travel Experience Next Gen. optimized wing box Optimized high lift configurations Advanced Integrated Structures Nacelle integration concept Wing concept Wing items Fuselage concept demonstrated Cabin Technologies IADP RA Advanced Fuselage More electrical wing integration

24 Further Information Göran Bengtsson - Saab AB Yvon Ollivier Dassault Aviation Miguel Llorca Sanz EADS CASA