Research Establishments Activities within SFWA-ITD E. COUSTOLS (ONERA) , U. HERRMANN (DLR), C. NAE (INCAS) and J. KOS (NLR) Innovation takes off SFWA-ITD Partnership DLR/INCAS/NLR/ONERA Associate Partners (1/3) • DLR, INCAS, NLR and ONERA were selected by the SFWAITD leaders in a 1st Phase after the “Associate Partners Worskhop” held by AIRBUS @ Toulouse (October 11th, 2006): – DLR – INCAS Cluster: INCAS, ROMAERO, STRAERO & AVIOANE CRAIOVA – NL Cluster: Fokker Aerostructures, NLR, Fokker Elmo, TU Delft, Univ. Twente and 4 SME's. – ONERA – QinetiQ – RUAG • In a 2nd Phase (late 2008/beg. 2009): – AERNNOVA CS Closing Event 22/03/17, Brussels SFWA-ITD Consortium Confidential 2 SFWA-ITD Partnership DLR/INCAS/NLR/ONERA Associate Partners (2/3) • Added values of the four main RECs to participate to CS SFWA -ITD for the benefit of the whole SFWA-ITD partnership are: – Our involvements to fulfil SFWA-ITD objectives: reductions of fuel consumption & external noise; – Our capabilities to support the assessment methodology of investigated innovative technologies; – Our requested expertise to these objectives, in all relevant disciplines; – Our potential to adapt our activities according to some change of strategy in the time life of SFWA-ITD. CS Closing Event 22/03/17, Brussels 3 SFWA-ITD Consortium Confidential SFWA-ITD Partnership DLR/INCAS/NLR/ONERA Associate Partners (3/3) • Illustration of adaptability over the SFWA-ITD duration: Gross Budget (M€) DLR NL-Cluster KOM Mid-2008 12 18 END PROGRAMME 15,9 17,4 • % of Total Budget : – – – – DLR: 4.3% INCAS: 4.3% NLR: 1.8% ONERA: 5.7% NLR INCAS Cluster INCAS 18 6,8 27,4 ONERA 12 16,1 21,0 Main ITD-Leaders Contributors: 16.1% – AIB: 30.0% – SAAB: 6.3% – DASSAULT AVIATION: 6.1% Contribution to Work Breakdown Structure by leading 11 Work Packages (WPx.y.z) over 47 CS Closing Event 22/03/17, Brussels SFWA-ITD Consortium Confidential 4 SFWA-ITD Partnership Illustration of DLR/INCAS/NLR/ONERA Cooperation • Numerical Assessment of CROR configurations – Performance & noise predictions + analysis of installation effects DNW-LLF WT ONERA S1MA WT ONERA CS Closing Event 22/03/17, Brussels SFWA-ITD Consortium Confidential 5 SFWA-ITD Partnership Illustration of DLR Achievement: Infra-Red BLADE Flight Test Year Description 2014 Camera moved from fusel. to FIN: - Small view angle (< 20o) AND - Distance to target area (> 36m) Ground tests in Toulouse & Berlin Wind Tunnel testing (Fin vibr.) pre flight testing on A340 2015 Soft- & hardware development 2016 Surface coating influence on IRmeasurements In-flight camera calibration procedure Soft- & hardware delivered for BLADE Flight Test CS Closing Event 22/03/17, Brussels SFWA-ITD Consortium Confidential 6 SFWA-ITD Partnership Illustration of DLR Achievement: Hot-Films BLADE Flight Test Measuring Transition via hot-film sensor at the wing leading edge Sensors installed in a curved surface, no steps Fast response, remote sensor (75kHz, 50m) Tested, delivered & installed for Flight Test 7 CS Closing Event 22/03/17, Brussels SFWA-ITD Consortium Confidential SFWA-ITD Partnership Illustration of INCAS Achievement Flow Control SHIELD, Ground Based Demonstrator LOSPA, Hardware Manufacturing BizJet-U-Tail HTP interaction CS Closing Event 22/03/17, Brussels SFWA-ITD Consortium Confidential 8 SFWA-ITD Partnership Illustration of NLR Achievement in ‟Smart flap” NLR (aero, structures) in team: Fokker Aerostructures, Dassault, 2 Dutch SMEs Drivers: TLRs: performance, weight, cost, environment Aerodynamics of innovative flap kinematics concept (Fokker patent) Composite design methods building blocks (e.g. lugs) WTTs: INCAS, ONERA Manufacturing simulation for Airborne TE: bizjet Static structural test in innovative set-up Exhibited Paris ‘15, Aerodays ‘15, Farnborough ’16; movie; flyer CS Closing Event 22/03/17, Brussels 9 SFWA-ITD Consortium Confidential SFWA-ITD Partnership Illustration of NLR Achievement in structural panels for Bizjet innovative Aftbody and ‟SHIELD Demonstrator ” Objective: Impact of jet flow thermal & acoustic loads on innovative Aft Body Acoustic fatigue methods for composite structural panels Sizing of panel elements Shaker tests Acoustic fatigue allowables SHIELD test participation and analysis Aviation week, Dec.‘16 CS Closing Event 22/03/17, Brussels Instrumentation of SHIELD panels SFWA-ITD Consortium Confidential Analysis of composite panel 10 SFWA-ITD Partnership Illustration of ONERA Achievement • Flutter Demonstration Tests @ ONERA S2MA Wind Tunnel • Pre-design: 2012 • LDR • Instrumentation • • • • Architecture 2013 def. PDR Final architecture Model Instrument. • • • • CDR 2014 Drawings Manufacturing Test matrix • Manufacturing 2015 • Instrumentation • Struct. Lab tests Design iterative & cooperating process Structural substantiation • Lab 2016 tests • TRR • WTT: 4 weeks High-Quality database Re-usable model Illustration of flutter onset Instrumentation Test set-up: • Excitation / high load capacity • Efficient safety ONERA S2MA WT Model • Highly instrumented • High accuracy machining SFWA-ITD Consortium Confidential SFWA-ITD Partnership Illustration of ONERA Achievement Hz HQ Handling qualities Load Domain Vibration Domain Load Control: Vibration control: • • • • • Gust generation at M~0.7 Response of an aeroelastic model Closed-Loop control (Movable Flap) Dynamical models for vibration restitution Optimization of anti-vibration control laws • Validation: Falcon 7X / Ground Vibration Test • Perfect restitution between F7X A/C data and Control Model control -75% decrease Dynamic Load 42% vibration attenuation SFWA-ITD:CS closing event 22 March 2017, Brussels SFWA-ITD Consortium Confidential SFWA-ITD Partnership DLR/INCAS/NLR/ONERA Summary (1/2) Thus, in the frame of SFWA-ITD, DLR, INCAS, NLR & ONERA: Reinforced existing co-operations or created new ones: COOPERATIONS WITHIN SFWA-ITD ITD Leaders Associate Partners DLR AIRBUS / DASSAULT / FRAUNHOFER / SAAB INCAS AIRBUS / DASSAULT ONERA / INCAS / NLR / RUAG INCAS-Cluster partners / DLR / NLR / ONERA NLR AIRBUS / DASSAULT / FRAUNHOFER / SAAB / EADS CASA NL-CLUSTER partners / DLR / ONERA / INCAS ONERA AIRBUS / DASSAULT / FRAUNHOFER / SAAB / SAFRAN Aircelle / THALES TRT DLR / INCAS / NLR / RUAG CfP Partners TU BRAUNSCHWEIG AVIATION DESIGN / ARA & ULIV / CEDRAT / BIAS / CORSO-MAGENTA / UCAM & Stutt. Uni. Completed 24 Key Deliverables, Released 65 publications (vs 124 whole SFWA-ITD partnership) Submitted 5 patents (vs 41) Participated to several events: Greener Aviation ‘15 & ‘16, Paris Airshow ‘15, Aerodays ‘15, Farnborough Air show ’16…. CS Closing Event 22/03/17, Brussels SFWA-ITD Consortium Confidential 13 SFWA-ITD Partnership DLR/INCAS/NLR/ONERA Summary (2/2) As a final conclusion, DLR, INCAS, NLR & ONERA actively: • Support the preparation of European Future by: – Technology & tool development towards industrial competitiveness (via new/higher performing a/c) – Fostering new aircraft configurations and new technologies towards positive ecologic impact • Solution orientated collaboration (of RE’s) maximizes research acceptance Clean Sky SFWA-ITD has been a success for DLR, INCAS, NLR and ONERA Therefore, Clean Sky2 implements improvements, so…. CS Closing Event 22/03/17, Brussels SFWA-ITD Consortium Confidential 14 ©2014 by the Clean Sky Leading Partners: Airbus, Agusta Westland, Alenia Aermacchi, Dassault Aviation, EADS-CASA, Fraunhofer Institute, LiebbherrAerospace, Rolls-Royce, Saab AB, Safran, Thales & 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. SFWA-ITD Consortium Confidential 15 SFWA-ITD Partnership DLR, INCAS, NLR & ONERA Positioning (1/2) • DLR, INCAS, NLR & ONERA Contributions w.r.t WBS SFWA-ITD CONSORTIUM PLAN TRL 2-3 Work Packages 1.1 1.3 Flow Control TRL 3-4 TRL 4-5 Integrated Flow & Load Control Systems TRL≥6 Integration of 2.1 Smart Wing into OAD Low Drag 3.1 Demonstrator BLADE CS Closing Event 22/03/17, Brussels Description of Work Passive Tech. for Laminar Flow Active Tech. for Lam. Flow & Buffet Control Surface Tech: New Painted Riblet Flow Control for Low Speed / High Lift Adv. Control Sys. Options for A/C Appl. & Int. Adv. Communication Network & field buses Power Network and Management Ground Demonstration Loads & Inertial Sensing Technologies Aerodynamic Sensing Technologies Fluidic Actuators Mechanical Actuators Application of SFWA Technologies Struct. & Syst.: Concepts, Capab. & Int. Numerical Simulations & Ground Testing DLR 1.1.1 1.1.2 1.1.3 1.1.4 1.3.1 1.3.2 1.3.3 1.3.5 1.3.6 1.3.7 1.3.8 1.3.9 2.1.1 2.1.2 2.1.3 3.1.6 Flight Tests Instrumentation X SFWA-ITD Consortium Confidential INCAS NLR ONERA X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X 16 SFWA-ITD Partnership DLR, INCAS, NLR & ONERA Positioning (2/2) • DLR, INCAS, NLR & ONERA Contributions w.r.t WBS TRL 2-3 SFWA-ITD CONSORTIUM PLAN Work Packages 1.2 1.3 TRL 3-4 2.2 Load Control Integrated Flow & Load Control Systems Integration of Other Smart Wing into OAD Low Speed 3.2 Demonstrator 3.5 After-body Demo TRL 4-5 CS Closing Event 22/03/17, Brussels Description of Work Innovative Devices for Load Control Adaptive Wing Advanced Load Control Technologies A/C Load Evaluation & Optimisation Adv. Control Sys. Options for A/C Appl. & Int. Adv. Communication Network & field buses Power Network and Management Ground Demonstration Loads & Inertial Sensing Technologies Aerodynamic Sensing Technologies Fluidic Actuators Mechanical Actuators Investigate Innovative After Body CROR Innovative Power Plant Integration Innovative After Bodies Detailed Design Detailed Simulation and Ground Testing Novel Flap System Load & vibration control - Fatigue testing Manu. of realistic aft bodyshape for Bizjets to 3.5.2 support testing Demonstration of design of new afterbodies wrt 3.5.5 thermal & vibration loads from engine jet Demonstration of aeroelastic stability of new 3.5.7 afterbody configuration 1.2.1 1.2.2 1.2.3 1.2.4 1.3.1 1.3.2 1.3.3 1.3.5 1.3.6 1.3.7 1.3.8 1.3.9 2.2.1 2.2.2 2.2.3 2.2.4 3.2.2 3.2.4 SFWA-ITD Consortium Confidential DLR X INCAS NLR ONERA X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X 17
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