Clean Sky 2 AIRFRAME ITD Call for Proposals #6 Brussels, 22 nd February 2017 This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
From Clean Sky towards Clean Sky 2 • Greener Airframe Technologies • More efficient wing • Integrated Structures • More Electrical a/c architectures • Novel Propulsion Integration Strategy • Smart high lift devices S mart F ixed W ing A ircraft • Optimized control surfaces Re-think Re-think the wing the cabin Re-think the Re-think the a/c fuselage architecture Re-think the control Step changes in the “efficiency” of all airframe elements by the means of a systematic “re - thinking” 2 This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
AIRFRAME Key General Objectives New Materials Maintenance Noise Weight Drag Cabin More Efficient Airframes Efficiency of the engineering & manufacturing process Time to Market Manufacturing Cost (lead Time) IADP/Integrated SUPPORT TO IADP : Maturate technologies up to TRL 6 Demonstrators REG High Performance & Energy Efficiency High Versatility & Cost Efficiency Next Innovative Novel Optimized Advanced FRC Advanced High Speed Novel generation Advanced Aircraft travel high lift integrated Laminarity Airframe Control optimized Fuselage Archi tecture experience configs. structures wing REG FRC LPA AIR Bizjet LPA SAT AIR Bizjet TRANSVERSE Eco-Design for Airframe & Modeling to certification ability SAT FUTURE : De-risk novel generation product in the prospect of changing step by 2030+ This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
AIRFRAME ITD Interfaces Overview with other SPDs Leonardo Airbus Leonardo Helicopters IADPs AIRFRAME ITD Dassault – SAAB - Airbus DS IADPs & SAT provide General Requirements Airframe technologies development up to TRL5/6 TRL6+ demonstrations in IADPs and SAT 4 This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
Overall WBS and participants A - High Performance and Energy B - High Versatility and Cost Efficiency Efficiency TS A-1: TS B-1: Next TS B-2: TS B-3: TS A-0: TS A-2: TS A-5: Novel TS B-0: TS B-4: Innovative TS A-3: High TS A-4: Novel Generation Optimized high Advanced Management & Advanced travel Management & Advanced Aircraft Speed Airframe Control optimized wing lift Integrated Interface Laminarity experience Interface Fuselage Architecture box configurations Structures WP A-0.1 WP A-1.1 WP A-2.1 WP A-3.1 WP A-4.1 WP A-5.1 WP B-0.1 WP B-1.1 WP B-2.1 WP B-3.1 WP B-4.1 Wing for Optimal engine Multidisciplinary High wing / large Advanced Overall Smart mobile Ergonomic flexible Overall incremental lift & Rotor-less tail for integration on Laminar nacelle wing for high & Tprop nacelle Integration of Management control surfaces cabin Management transmission shaft Fast Rotorcraft rear fuselage low speed configuration syst. in nacelle integration WP A-0.2 WP A-1.2 WP A-2.2 WP A-3.2 WP A-4.2 WP A-5.2 WP B-0.2 WP B-1.2 WP B-2.2 WP B-3.2 WP B-4.2 Business Aviation SAT More affordable Pressurized CROR & UHBR NLF smart Tailored front Active load Office Centered OAD & config. OAD & composite High lift wing All electrical wing fuselage for Fast configurations integrated wing fuselage control Cabin Mgt configuration Mgt structures Rotorcraft WP A-0.3 WP A-1.3 WP A-2.3 WP A-3.3 WP B-0.3 WP B-1.3 WP B-3.3 WP B-4.3 More affordable LPA Novel high More efficient Extended Innovative shapes RotorCraft OAD & Highly integrated composite OAD & config. performance wings laminarity & structure configuration Mgt cockpit fuselage Mgt configuration technologies WP A-0.4 WP A-1.4 WP A-3.4 WP B-0.4 WP B-1.4 WP B-3.4 WP B-4.4 Regional a/c More affordable Eco-Design TA Virtual modelling Eco-Design for Flow & shape Low weight, low OAD & config. small a/c Link for certification airframe control cost cabin Mgt manufacturing WP B-0.5 WP B-3.5 Advanced Eco-Design TA integration of Link syst. in small a/c WP B-3.6 New materials & manufacturing 4 Technology Streams 5 Technology Streams Co-Leaders: Airbus D&S S.A.U. (CASA) Co-Leaders: DAv, SAAB Leaders: Airbus, FNM-VEL, FNM-HD/AW, Leaders: Airbus, Fraunhofer AH, Fraunhofer, SAAB, Evektor, Piaggio CP : NACOR, GAINS, ecoTECH, CASTLE, MANTA CP : NACOR, OUTCOME, ASTRAL, SHERLOC, OPTICOMS, PASSARO, SAT-AM, CASTLE, LIFTT(?) 5 This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
Share of Participants Countries AIR ITD Family funding to date involved foreseen to date Leader 16.7% 4* 4 Part. 23.2% 13* 6 Leaders Core 30.0% 76* 12 Partners Partners 30.1% 124 16 *incl. Affiliates and Third Parties This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
AIRFRAME ITD - CfP Status – CfP06 Identificatio CfP Title WP/Task n Code Project HPE AIR-01-25 Improvement of the aerodynamic loads prediction at high Reynolds number A-1.4 AIR-01-26 Development of innovative and optimized stiffeners run-out for overall panel weight saving A-3.1 AIR-01-27 Innovative solutions for metallic ribs or fittings introduced in a composite box to optimally deal with thermo- A-3.1 mechanical effects Bigger cockpit windshields and associated trade- off between “plugged” design and “load - bearing” design A-3.2 AIR-01-28 A-3.3 AIR-01-29 Optimisation of Friction Stir Welding (FSW) and Laser Beam Welding (LBW) for assembly of structural aircraft parts Project HVC AIR-01-39 Ice tunnel Model & test for Induction system + Ice tunnel Model & test for Heat Transport system B-2.1/B- 3.2 AIR-01-40 Infusion manufacturing methodolodies for Aircraft complex composite components. B-2.2 AIR-01-41 All Electric Wing: Integrated electronics for actuator data and power management for Morphing Leading Edge B-1.4 / B- 3.2 activities AIR-01-42 Lay-up tools for Helicopter Shells B-3.3.10 B-3.3.2 AIR-01-43 Materials & Process : Low Cost Optical Wave Guide for Damage Detection & Data Transfer AIR-01-44 Adjustable high loaded rod B-3.3.2 AIR-01-45 Development and deployment of PLM Tools for A/C Ground Functional testing with Eco-design criteria. B-3.6 AIR-01-46 Auto testing technologies and more automated factories for Aircraft validation test process B-3.6 AIR-01-47 Part specific process optimization in SLM B-3.6 B-4.3 AIR-01-48 Development and validation of a portable, automated and jigless system for drilling and assembly of fuselage joints B-4.3 AIR-01-49 Development and validation of a self-adaptive system for automated assembly of major composite aerostructures AIR-01-50 Design and manufacturing of innovative toolings for large curved fuselage panel B-4.3 7 This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
AIRFRAME ITD - CfP Status – CfP06 TS A-1: Innovative Aircraft Architecture AIB WP A-1.1 WP A-1.2 WP A-1.3 WP A-1.4 Optimal engine Novel high UHBR & CROR Virtual modelling integration on performance configuration for Certification rear fuselage configuration 8 This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
AIRFRAME ITD - CfP Status – CfP06 BJ COMPOSITE WING ROOT TS A-3: High Speed Airframe DAV WP A-3.1 WP A-3.2 WP A-3.3 WP A-3.4 Multidisciplinary Tailored front Innovative shapes & wing for high & low Eco-Design for Airframe fuselage structure speed 9 This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
AIRFRAME ITD - CfP Status – CfP06 BJ COMPOSITE WING ROOT TS A-3: High Speed Airframe DAV WP A-3.1 WP A-3.2 WP A-3.3 WP A-3.4 Multidisciplinary Tailored front Innovative shapes & wing for high & low Eco-Design for Airframe fuselage structure speed 10 This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
AIRFRAME ITD - CfP Status – CfP06 TS A-3: High Speed Airframe DAV WP A-3.1 WP A-3.2 WP A-3.3 WP A-3.4 Multidisciplinary Tailored front Innovative shapes & wing for high & low Eco-Design for Airframe fuselage structure speed 11 11 This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
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