Research Establishments Activities within SFWA-ITD...SFWA-ITD Consortium Confidential •...
Transcript of Research Establishments Activities within SFWA-ITD...SFWA-ITD Consortium Confidential •...
Research Establishments
Activities within SFWA-ITD
Innovation takes off
E. COUSTOLS (ONERA) , U. HERRMANN (DLR),
C. NAE (INCAS) and J. KOS (NLR)
SFWA-ITD Consortium Confidential
• DLR, INCAS, NLR and ONERA were selected by the SFWA-
ITD 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 2
SFWA-ITD PartnershipDLR/INCAS/NLR/ONERA Associate Partners (1/3)
SFWA-ITD Consortium Confidential
• 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.
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SFWA-ITD PartnershipDLR/INCAS/NLR/ONERA Associate Partners (2/3)
SFWA-ITD Consortium Confidential
• Illustration of adaptability over the SFWA-ITD duration:
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SFWA-ITD PartnershipDLR/INCAS/NLR/ONERA Associate Partners (3/3)
• % of Total Budget :– DLR: 4.3%
– INCAS: 4.3%
– NLR: 1.8%
– ONERA: 5.7%
16.1%
Main ITD-Leaders Contributors:– AIB: 30.0%
– SAAB: 6.3%
– DASSAULT AVIATION: 6.1%
DLR NL-Cluster NLR INCAS Cluster INCAS ONERA
KOM Mid-2008 12 18 18 12
END PROGRAMME 15,9 17,4 6,8 27,4 16,1 21,0
Gross Budget (M€)
� Contribution to Work Breakdown Structure by
leading 11 Work Packages (WPx.y.z) over 47
SFWA-ITD Consortium Confidential
SFWA-ITD PartnershipIllustration of DLR/INCAS/NLR/ONERA Cooperation
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• Numerical Assessment of CROR configurations– Performance & noise predictions + analysis of installation effects
ONERA
ONERA S1MA WT
DNW-LLF WT
SFWA-ITD Consortium Confidential
SFWA-ITD PartnershipIllustration of DLR Achievement: Infra-Red
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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 IR-
measurements
In-flight camera calibration procedure
Soft- & hardware delivered for BLADE
Flight Test
BLADE Flight Test
SFWA-ITD Consortium Confidential
SFWA-ITD PartnershipIllustration of DLR Achievement: Hot-Films
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BLADE Flight TestMeasuring Transition via hot-film sensor at the wing leading edgeSensors installed in a curved surface, no stepsFast response, remote sensor (75kHz, 50m)Tested, delivered & installed for Flight Test
SFWA-ITD Consortium Confidential
SFWA-ITD PartnershipIllustration of INCAS Achievement
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Flow ControlLOSPA, Hardware Manufacturing
BizJet-U-Tail HTP
interaction
SHIELD,
Ground Based
Demonstrator
SFWA-ITD Consortium Confidential
SFWA-ITD PartnershipIllustration of NLR Achievement in ‟Smart flap”
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NLR (aero, structures) in team: Fokker Aerostructures, Dassault, 2 Dutch SMEs
Drivers:
TLRs:
performance,
weight,
cost,
environment
Exhibited Paris ‘15, Aerodays ‘15, Farnborough ’16; movie; flyer
Static structural test in innovative set-up
Manufacturing simulation for Airborne
Composite design methods building blocks (e.g. lugs)
Aerodynamics of innovative flap kinematics concept (Fokker patent)
WTTs:
INCAS,
ONERA
TE: bizjet
SFWA-ITD Consortium Confidential
SFWA-ITD PartnershipIllustration of NLR Achievement in structural panel s for Bizjetinnovative Aftbody and ‟SHIELD Demonstrator ”
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Objective: Impact of jet flow thermal & acoustic loads on innovative Aft Body
SHIELD test participationand analysis
Acoustic fatigue methods for composite structural panels
Instrumentation of SHIELD panels
Analysis of composite panel
Acoustic fatigue allowables
Sizing of panel elements Shaker tests
Aviation week, Dec.‘16
SFWA-ITD Consortium Confidential
2012 2013 2014 2015 2016• Pre-design:• LDR• Instrumentation
• CDR• Drawings• Manufacturing• Test matrix
• Manufacturing• Instrumentation• Struct. Lab tests
• Architecture def.• PDR• Final architecture• Model Instrument.
• Lab tests•TRR• WTT: 4 weeks
Structuralsubstantiation
High-Quality databaseRe-usable model
Instrumentation
Model
• Highly instrumented
• High accuracy machining
Test set-up:
• Excitation / high load capacity
• Efficient safety
Design iterative & cooperating process
Illustration of flutter onset
SFWA-ITD PartnershipIllustration of ONERA Achievement• Flutter Demonstration Tests @ ONERA S2MA Wind Tunnel
ONERA S2MA WT
SFWA-ITD Consortium ConfidentialSFWA-ITD:CS closing event 22 March 2017, Brussels
HQ Handling qualities Load Domain Vibration DomainHz
-75% decrease Dynamic Load
Load Control: • Gust generation at M~0.7• Response of an aeroelastic model
• Closed-Loop control (Movable Flap)
Vibration control: • 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
42% vibration attenuation
SFWA-ITD PartnershipIllustration of ONERA Achievement
SFWA-ITD Consortium Confidential
Thus, in the frame of SFWA-ITD, DLR, INCAS, NLR & ONERA:
� Reinforced existing co-operations or created new ones:
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SFWA-ITD PartnershipDLR/INCAS/NLR/ONERA Summary (1/2)
ITD Leaders Associate Partners CfP Partners
DLR AIRBUS / DASSAULT / FRAUNHOFER / SAAB
ONERA / INCAS / NLR / RUAG
INCAS AIRBUS / DASSAULTINCAS-Cluster partners /
DLR / NLR / ONERATU BRAUNSCHWEIG
NLRAIRBUS / DASSAULT / FRAUNHOFER /
SAAB / EADS CASANL-CLUSTER partners / DLR / ONERA / INCAS
ONERAAIRBUS / DASSAULT / FRAUNHOFER / SAAB / SAFRAN Aircelle / THALES TRT
DLR / INCAS / NLR / RUAG
AVIATION DESIGN / ARA & ULIV / CEDRAT / BIAS / CORSO-MAGENTA / UCAM & Stutt. Uni.
COOPERATIONS WITHIN SFWA-ITD
� 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….
SFWA-ITD Consortium ConfidentialCS Closing Event 22/03/17, Brussels 14
SFWA-ITD PartnershipDLR/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….
SFWA-ITD Consortium Confidential
©2014 by the Clean Sky Leading Partners: Airbus, Agusta Westland, Alenia
Aermacchi, Dassault Aviation, EADS-CASA, Fraunhofer Institute, Liebbherr-
Aerospace, 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.
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SFWA-ITD Consortium Confidential
SFWA-ITD PartnershipDLR, INCAS, NLR & ONERA Positioning (1/2)
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• DLR, INCAS, NLR & ONERA Contributions w.r.t WBST
RL 2-3
TR
L 3-4T
RL 4-5
TR
L ≥6
Description of Work DLR INCAS NLR ONERA1.1.1 Passive Tech. for Laminar Flow X X1.1.2 Active Tech. for Lam. Flow & Buffet Control X X X X1.1.3 Surface Tech: New Painted Riblet X X1.1.4 Flow Control for Low Speed / High Lift X X X X1.3.1 Adv. Control Sys. Options for A/C Appl. & Int. X X1.3.2 Adv. Communication Network & field buses X1.3.3 Power Network and Management X1.3.5 Ground Demonstration X X1.3.6 Loads & Inertial Sensing Technologies X1.3.7 Aerodynamic Sensing Technologies X X X1.3.8 Fluidic Actuators X X X1.3.9 Mechanical Actuators X X2.1.1 Application of SFWA Technologies X2.1.2 Struct. & Syst.: Concepts, Capab. & Int. X X2.1.3 Numerical Simulations & Ground Testing X X X X
Low Drag Demonstrator
BLADE3.1 3.1.6 Flight Tests Instrumentation X XX
1.3
Work Packages SFWA-ITD CONSORTIUM PLAN
Flow Control1.1
Integrated Flow & Load
Control Systems
2.1Integration of Smart Wing into OAD
SFWA-ITD Consortium Confidential
SFWA-ITD PartnershipDLR, INCAS, NLR & ONERA Positioning (2/2)
CS Closing Event 22/03/17, Brussels 17
TR
L 2-3T
RL 3-4
TR
L 4-5
• DLR, INCAS, NLR & ONERA Contributions w.r.t WBS
Description of Work DLR INCAS NLR ONERA1.2.1 Innovative Devices for Load Control X X1.2.2 Adaptive Wing X1.2.3 Advanced Load Control Technologies X X X1.2.4 A/C Load Evaluation & Optimisation X X X1.3.1 Adv. Control Sys. Options for A/C Appl. & Int. X X1.3.2 Adv. Communication Network & field buses X1.3.3 Power Network and Management X1.3.5 Ground Demonstration X X1.3.6 Loads & Inertial Sensing Technologies X1.3.7 Aerodynamic Sensing Technologies X X X1.3.8 Fluidic Actuators X X X1.3.9 Mechanical Actuators X X2.2.1 Investigate Innovative After Body X2.2.2 CROR Innovative Power Plant Integration X X X X2.2.3 Innovative After Bodies Detailed Design X X2.2.4 Detailed Simulation and Ground Testing X X X X3.2.2 Novel Flap System X3.2.4 Load & vibration control - Fatigue testing X
3.5.2Manu. of realistic aft bodyshape for Bizjets to
support testing X
3.5.5Demonstration of design of new afterbodies wrt
thermal & vibration loads from engine jet X
3.5.7Demonstration of aeroelastic stability of new
afterbody configuration X
2.2
Integrated Flow & Load
Control Systems
Integration of Other Smart
Wing into OAD
Work Packages SFWA-ITD CONSORTIUM PLAN
Load Control1.2
1.3
3.5
Low Speed Demonstrator
3.2
After-body Demo