4. SFWA - Research Centres Activities within SFWA

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
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SFWA-ITD Consortium Confidential
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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.
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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
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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
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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
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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
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SFWA-ITD Partnership
Illustration of INCAS Achievement
Flow Control
SHIELD,
Ground Based
Demonstrator
LOSPA, Hardware Manufacturing
BizJet-U-Tail HTP
interaction
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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
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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
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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….
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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….
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©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.
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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
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SFWA-ITD Consortium Confidential
INCAS
NLR
ONERA
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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
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INCAS
NLR
ONERA
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