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Innovation Takes Off
Clean Sky 2 Information Day
AIRFRAME ITD
Yvon OLLIVIER Dassault Aviation
Brussels, 28th of March 2014
From Clean Sky towards Clean Sky 2
Step changes in the “efficiency” of all airframe elements by the means of a systematic “re-thinking”
Re-think the a/c architecture
Re-think the fuselage
Re-think the wing
Re-think the control
Re-think the cabin
Smart Fixed Wing Aircraft
• Greener Airframe Technologies • More Electrical a/c architectures
• More efficient wing • Novel Propulsion Integration Strategy • Optimized control surfaces
• Integrated Structures • Smart high lift devices
3
High Level Objectives
4
From the Impact Perspective
From the Expected Impacts
Environmental Perspective • More resource efficient aircraft : challenging targets for up to • 30% cumulative CO2 • 10 EPNdB
• Eco responsible industrial capabilities
Smart & Efficient Mobility 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
Industrial Leadership Perspective
• Cost efficient Products • Strong Product Differentiators • Cost efficient engineering, manufacturing & life cycle support
processes (up to recycling) • Reduced time to market • Sustainable industrial capability
5
Key Objectives • Validate through demonstration of integrated technologies :
• To introduce innovative airframe architecture
• To introduce technologies for more efficient airframe : drag, weight, cost, environmental impact, passager well-being, maintenance, servicing, …
• To enhance the efficiency of the engineering & manufacturing process : time-to-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 2030+
• 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 6
Setup and Implementation
7
The Leadership : who are we ?
• Key world player in the aerospace industry. • More than 8,000 aircraft delivered,
representing some 28 million of hours of flight. • 1900 Falcon in operation. • Only group in the world to design, manufacture and support both combat aircraft and business jets.
RAFALE Omnirole
FALCON BizJets
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.
8
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
9
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
Inve
stig
ate
adva
nce
d e
ngi
ne
inte
grat
ion
& n
ove
l ove
rall
arch
itec
ture
Lam
inar
nac
elle
s; N
LF s
mar
t in
tegr
ated
win
g fi
ttin
g th
e in
du
stri
al e
nvi
ron
men
t
Hig
h e
ffic
ien
t m
ult
i-d
isci
plin
ary
flex
ible
win
g; f
use
lage
ch
ange
s in
sh
apes
, &
str
uct
ure
Smar
t m
ult
i-fu
nct
ion
co
ntr
ol
surf
aces
& lo
ad &
flu
tter
al
levi
atio
n
Pass
enge
r fr
ien
dly
cab
in;
ergo
no
mic
& f
lexi
ble
, new
vo
lum
e u
tilis
atio
n
Low
co
st c
om
po
site
str
uct
ure
s
Effi
cien
t ar
chit
ectu
ral c
on
cep
t fo
r tu
rbo
pro
pel
ler
hig
h w
ing
– co
mp
osi
te n
acel
le &
ad
apta
tive
w
ing
New
str
uct
ura
l par
adig
m f
or
op
tim
ised
inte
grat
ion
of
syst
ems
in a
irfr
ame,
ele
ctri
cal w
ing
No
vel c
om
po
site
fu
sela
ge &
ca
bin
; tai
lless
or
pre
ssu
rize
d
fuse
lage
fo
r ro
torc
raft
Tran
sve
rse
En
ablin
g C
apab
ility
Focu
sed
Inte
grat
ed
D
em
on
stra
tio
ns
Novel Certificat°
Eco Design
Extended Laminarity
More Efficient Wing
Advanced Manufact.
Flow & shape Control
Overall Technical Overview
10
Concept
Analysis
Technology Streams
Innovative Aircraft Architecture
Advanced Laminarity
High Speed Airframe
Next Gen. optimized wing box
IADP LPA
IADP RA
IADP Rcraft
ITD Engine ITD Systems
Novel Control
Advanced Fuselage
Novel Travel Experience
Optimized high lift configurations
Advanced Integrated Structures
IADP LPA
IADP RA
IADP Rcraft
SAT Transverse
act°
ITD Systems
TEECO
Specifications & Requirements
Technology Development & Demonstration
Integration Profile Development Integrated
Concept demonstrat°
prototype airframe componts
Inte
rfac
ing
& c
ross
in
tera
ctio
n m
anag
emen
t
Novel innovation
waveTRL <= 5
11
High Performance & Energy Efficiency
Innovative Aircraft Architecture
Advanced Laminarity
Novel ControlNovel Travel Experience
Management & Interfacing
Leader : Dassault AviationCo leader : SAAB
High Performance & Energy Efficiency- WBS
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
TS A-2:Advanced Laminarity
WP A-2.1:Laminar nacelle
WP A-2.2:NLF smart
integrated wing
WP A-2.4:Extended laminarity
WP A-2.3:Laminarity for high lift wing
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
WP A-3.5:Eco Design
TS A-4:Novel Control
WP A-4.1: Smart mobile
control surfaces
WP A-4.2:Active load
control
TS A-5:Novel travel experience
WP A-5.1: Ergonomic
flexible cabin
WP A-5.2:Office Centered
Cabin
12
High Performance &
Energy Efficiency 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
Means & Enablers
• Large Wind Tunnel Test
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: 2014-2018 • In-rupture configurations: 2017-2022
Gross Budget (activities) : 85/90 M€
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
TS A-1 : Innovative Aircraft Architecture
13
High Performance &
Energy Efficiency
TS A-2 : Advanced 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
• 2014-2018
Gross Budget (activities) : 85/90 M€
TS A-2: Advanced Laminarity
WP A-2.1: Laminar nacelle
WP A-2.2: NLF smart integrated
wing
WP A-2.4: Extended laminarity
WP A-2.3: Laminarity for high lift
wing
14
High Performance &
Energy Efficiency
TS A-3 : High Speed Airframe
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 • Eco design for Airframe : green life cycle
Means & Enablers
• Representative wing box demonstrator • Wind Tunnel Tests
• Dedicated structural components & partial fuselage demonstrator • Sample and structural parts demonstrator for Eco Design
Partnership Framework • Research Institute & Academia, Aero-Structure Industry with track record in Eco
Design, Material Provider, Equipment Supplier
Timescale • Optimization/Local demonstrators: 2014-2018 • Radical concepts/Sub scale demonstrators: 2018-2023
Gross Budget (activities) : 120/125 M€
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
WP A-3.5: Eco Design 15
High Performance &
Energy Efficiency
TS A-4 : Novel 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: 2014-2017 • Extended demonstration batch: 2016-2022
Gross Budget (activities) : ~ 25 M€
TS A-4: Novel Control
WP A-4.1: Smart mobile control
surfaces
WP A-4.2: Active load control
16
TS A-5 : Novel Travel Experience (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
• 2014-2020
Gross Budget (activities) : ~ 25 M€
TS A-5: Novel travel experience
WP A-5.1: Ergonomic flexible cabin
WP A-5.2: Office Centered Cabin
High Performance &
Energy Efficiency
17
High Versatility & Cost Efficiency
Innovative Aircraft Architecture
Advanced Laminarity
Novel ControlNovel Travel Experience
Management & Interfacing
Leader : EADS CASA
TS B-1 :Next Generation
optimized wing box
WP B-1.1:Wing for incremental
lift & transmissionshaft integration
WP B-1.2:More affordable
composite structures
WP B-1.3:More efficient wings
technologies
WP B-1.4:Flow & shape control
TS B-2:Optimized high lift
configurations
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
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: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-3.5:New materials & manufacturing
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
High Versatility & Cost Efficiency- WBS
18
High Versatility & Cost
Efficiency 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: 2014-2018 • Large scale demonstrators : 2014-2022
Gross Budget (activities) : 60/65 M€
TS B-1 : Next Generation Optimized Wing Box
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
19
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
• 2014-2018
Gross Budget (activities) : 45/50 M€
TS B-2 : Optimized high lift configurations
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
High Versatility & Cost
Efficiency
20
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
• 2014-2020
Gross Budget (activities) : 100/105 M€
TS B-3 : Advanced Integrated Structures
TS B-3 : Advanced Integrated
Structures
WP B-3.3: Higly integrated cockpit
WP B-3.1: Advanced integration of system in nacelle
WP B-3.2: All electrical wing
WP B-3.6: New materials & manufacturing
WP B-3.5: More Affordable Manufacturing for Small
A/C
WP B-3.4: Advanced integration of systems in Small
A/C
High Versatility & Cost
Efficiency
21
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
• 2014-2018
Gross Budget (activities) : 140/145 M€
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
22
Major demonstration validations or components to be delivered to IADPs
Technology Streams
Innovative Aircraft Architecture
Advanced Laminarity
High Speed Airframe
Next Gen. optimized wing box
IADP LPA
IADP RA
IADP Rcraft
Novel Control
Advanced Fuselage
Novel Travel Experience
Optimized high lift configurations
Advanced Integrated Structures
• Fuselage components
• Fuselage concept demonstrated
• Cabin Technologies
• Optimized CROR configurations
• Laminar wing (NFL/Hybrid) concept
• Cabin arrangement concepts
• More electrical wing integration
• Wing components
• Wing items
• More electrical wing integration
• Nacelle integration concept
• Wing concept
23
[email protected] Göran Bengtsson - Saab AB Miguel Llorca Sanz – EADS CASA Yvon Ollivier– Dassault Aviation
Further Information
24
