CS2 - Airframe

Clean Sky 2
Eco Design – ITD Airframe
Jérôme Lery – Dassault Aviation
April 2013
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Clean Sky 2: Global
Objectives of ITD Airframe
• Validate:
Moving one step beyond CS …
– Introduction of innovative airframe architecture
– Introduction of technologies
for more efficient airframe : drag, weight, cost,
environmental impact (eco design for the complete life cycle),
operational flexibility including mobility to all airports, passenger comfort,
maintenance, servicing, …
– Enhancing of the efficiency of the engineering & manufacturing process : timeto-market and competitiveness against low-cost labour countries
– full addressing of technology issue from modelling to certification ability
• Serve:
– Maturity up to TRL 6 of airframe technologies
– De-risking of next generation products:
• Support next generation bizjets and general aviation directly
• Support Large aircraft, regional and rotorcraft directly and through IADPs
• Create:
– Product differentiators
This document is the property of one or more Parties to the Clean Sky Eco-Design ITD consortium and shall not
be distributed or reproduced without their formal approval
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Clean Sky 2: Global
Objectives of ITD Airframe
• Validate:
– Introduction of innovative airframe architecture
– Introduction of technologies
for more efficient airframe : drag, weight, cost,
Moving one step beyond CS …
environmental impact (eco design for the complete life cycle),
operational flexibility including mobility to all airports, passenger comfort,
maintenance, servicing, …
– Enhancing of the efficiency of the engineering & manufacturing process : time-tomarket and competitiveness against low-cost labour countries
– full addressing of technology issue from modelling to certification ability
• Serve:
BUILDING ON ECO DESIGN
– Maturity up to TRL
6 of airframe
technologies
CLEAN
SKY EXPERIENCE
– De-risking of next generation products:
• Support next generation bizjets and general aviation directly
• Support Large aircraft, regional and rotorcraft directly and through IADPs
• Create:
– Product differentiators
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This document is the property of one or more Parties to the Clean Sky Eco-Design ITD consortium and shall not
be distributed or reproduced without their formal approval
Clean Sky: Eco-Design Airframe (EDA) Objectives
• Development of A/C technologies to reduce environmental
impacts during out-of-operation phases of the A/C lifecycle
Reduction of
inputs and
outputs
WP 2.4
WP 2.1
Technology
areas along
the lifecycle
WP 2.3
This document is the property of one or more Parties to the Clean Sky Eco-Design ITD consortium and shall not
be distributed or reproduced without their formal approval
WP 2.2
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EDA: Technology Clusters WP 2.1 and 2.2
Technology Clusters
High Level Cluster
A – Low Energy Cluster
I – CFRP
B - Light Alloys/Green metallics
II - Metallics
C - Composites for high temperatures
III - Biomaterials
D - Green PU foams for seating
IV - Thermoplastics
E - Thermoplastic composites for interior applications
F - Thermoplastic a/c structures
V - Special polymers
applications
G - Electrostatic Functionality of organic Materials
VI - Electronics
H - Aerospace alloys, processes, surface treatments and coatings suitable for reducing lifecycle
environmental impact
I - Biocomposites for cabin interior applications
J - Materials for electronics
K – Mg alloys
Technologies
• Materials
• Manufacturing
Processes
Technology
Clusters
• Materials
• Manufacturing
Processes
• Applications
(A/C parts)
• Materials
• Manufacturing
Processes
Demonstrators
i.e. A/C parts • Testing
• Dismantling /
Recycling 5
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This document is the property of one or more Parties to the Clean Sky Eco-Design ITD consortium and shall not
be distributed or reproduced without their formal approval
EDA: LCA Platform
Interface
Tools
Databases
Non-expert
Non-expert
GaBi
ATALYS
Expert
Commercial (GaBi,
Ecoinvent, etc.)
Aerospace
(CS EDA developed)
This document is the property of one or more Parties to the Clean Sky Eco-Design ITD consortium and shall not
be distributed or reproduced without their formal approval
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EDA: Overall LCA Logic
Technologies
Eco-Statement
A/C Reference
parts
(current & innovative)
LCA on
Reference
parts
Material & Process
Technologies
Combination
for A/C
extrapolation
A/C Level EcoStatement
A/C modularization
and BOM per
module
A/C
Part A
Material
a
Material
…
(current & innovative)
available
Material b
Part B
Material
a
Material
…
Not available
Link to S2-S5
to complement
information
Data
on
Sub-module
Information
Material b
Part C
Material
a
Material
…
S2,
S3,
S4,
S5
available
Material b
Part D
Material
a
Material
…
Not available
Link to S2-S5
to complement
information
Material cake
on part level
Material
a
Material cake on submodule level
Process
data
Required
information
Information on
Sub-module level
Miscellaneous:
Copper, bronze,
synthetic
5%
Titanium
3%
Material
…
Material b
Material b
Information on
part level
Composite
10%
Reference
aircraft
AL-ALY
STL-ALY
CRES
TITANIUM
MG-ALY
KV/EP
PLASTIC
COPPER
FILM ADH
NOMEX
SEALING
EQUIPMENT
GL/EP
RUBBER
PAINT
GR/PH
LEAD
OIL
Steel
1%
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be distributed or reproduced without their formal approval
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Aluminium
81%
Eco Design in ITD Airframe
Cross-Interaction Management.
(Concept Analysis)
Eco Design Synthesis at a/c level - Interfacing
3 Directions / 7 Technology Streams
Eco Design
activities
Applicability & impact
This document is the property of one or more Parties to the Clean Sky Eco-Design ITD consortium and shall not
be distributed or reproduced without their formal approval
Fuselage test Case
Innovative Cabin
Advanced Control
Systems
Advanced Laminarity
Advanced Fuselage
& Cockpit
Fuselage with optimized usage of
volume and minimized weight,
cost and environmental impact
More efficient wings
Next Generation
Opt. Wing box
Novel Nacelles
Innovative a/c
Architecture
Innovative / disruptive
configurations
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Eco-Design Global Ojectives
• To make available to the aerospace industry and its supply chain a set of
new technologies reducing the environmental footprint of the aircraft
production from the global life cycle point of view (continuation of CS EDA
activities)
– Reduction of resource consumption (from raw material to water & energy)
– Individual processes development toward a global positive environmental
impact throughout an integrated LCA approach
– Development not only environmentally wise but also cost-efficient for:
• Production
• Maintenance
• Disposal
• The metallic & composite fuselage demonstrator will be the reference
cases for the LCA.
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This document is the property of one or more Parties to the Clean Sky Eco-Design ITD consortium and shall not
be distributed or reproduced without their formal approval
Eco-Design Work Breakdown Structure
TS 6
Advanced Fuselage & Cockpit
WP 6.1 to 6.5
WP 6.6 to 6.8
Efficient fuselage and
cockpit
More affordable, more
eco-efficient (MAMEF)
WP 6.9
Eco-Design (*)
WP 6.10
New materials & manufacturing
and assembly
WP 6.9.1
WP 6.9.2
WP 6.9.3
WP 6.9.4
WP 6.9.5
WP 6.9.6
Green
Manufacturing
Technologies
Green
Maintenance
Technologies
Long Life
Structure
Technologies
End Of Life
Life Cycle
Assessment
Lifecycle
Demonstration
Leader: TBD
Leader: TBD
Leader: TBD
Leader:
DAv
Leader: TBD
Leader: FhG
(*): Technologies development focused on fuselage as primary goal (but also
applicable to the other modules of A/C). Test case bizjet and/or regional fuselage
demo (TBC). Synthesis at configuration(s) level within WP0 and ED coordination
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This document is the property of one or more Parties to the Clean Sky Eco-Design ITD consortium and shall not
be distributed or reproduced without their formal approval
WP 6.9.4 End Of Life: Scope of Work
• Development of technologies for dismantling
and recycling (continuation of CS EDA
activities)
• Implementation of Design for Dismantling
(DfD) / Recycling (DfR) approach (link to be
made with Eco Design transversal activity for
Design for Environment or DfE)
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This document is the property of one or more Parties to the Clean Sky Eco-Design ITD consortium and shall not
be distributed or reproduced without their formal approval
WP 6.9.5 LCA: Scope of Work
• LCA studies to quantify environmental benefit
brought by Clean Sky 2 technologies vs. Clean
Sky (EDA) technologies
• LCA tools and database development (starting
from Clean Sky EDA developments and EDA
LCA platform)
• Consolidation / validation of extrapolation
methodology from parts to complete A/C
• Tracking of Substances all along the life cycle12
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This document is the property of one or more Parties to the Clean Sky Eco-Design ITD consortium and shall not
be distributed or reproduced without their formal approval
Spare
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This document is the property of one or more Parties to the Clean Sky Eco-Design ITD consortium and shall not
be distributed or reproduced without their formal approval
ITD Airframe
AIRFRAME ITD
Technology Demonstrations
(Technology Streams)
Small Air
Transport
concepts
Regional a/c
concepts
Large
Passenger
a/c concepts
Rotorcraft
concepts
TE
Innovative Aircraft Arch.
Novel Nacelles
Next Gen Opt. Wing Box
Advanced Laminarity
TRL 5/6 at Airframe Level
BizJet
concepts
IADP LPA
IADP RA
IADP Rcraft
Others
Products
portfolio
• Concepts & Technologies
• Major airframe components
for further integration
testing in IADPs
Advanced Control Systems
Adv. Fuselage & Eco-Design
Innovative Cabine
ITD Engine
TRL < 5
Interfacing & cross interaction management
Technology insertion
in future a/c concepts
analysis
ITD
Systems
This document is the property of one or more Parties to the Clean Sky Eco-Design ITD consortium and shall not
be distributed or reproduced without their formal approval
Novel innovation
wave
longer term insertion
for FP 2050
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TS 1: Innovative
Aircraft
Architecture
WP 6.2:
Innovative shapes
& structure of
cockpit & fuselage
WP 6.3:
Rotor-less tail for
Fast Rotorcraft
WP 5.3:
Flow & shape
control
integration
WP 5.4:
Integration of all
electrical systems
WP 6.4:
Pressurized
fuselage for Fast
Rotorcraft
This document is the property of one or more Parties to the Clean Sky Eco-Design ITD consortium and shall not
be distributed or reproduced without their formal approval
WP 6.10: New
materials &
manufacturing &
assembly
Eco-friendly & low cost
processes & technologies
WP 6.9:
Eco Design
More affordable, more Eco-Efficient
WP 6.6:
MAME2
composite
fuselage
WP 6.8:
MAME2 cockpit
DIRECTION 2:
More efficient wings
WP 7.2:
Low weight, Low
cost Cabin
WP 7.3:
Advanced flying
office
ServicesCentric
WP 6.5:
Optimized cockpit
structure
WP 6.7:
MAME2 metallic
fuselage
DIRECTION :
Innovative / disruptive
configurations
WP 7.1:
Ergonomic flexible
cabin
Optimized
WP 5.2:
Active load
control
TS 7: Novel travel
experience
Efficient fuselage & cockpit
WP 6.1:
Tailored front
fuselage
Control
WP 4.2:
Extended
laminarity
TS 6: Advanced
Fuselage & Cockpit
WP 5.1:
Multifunctional
control surfaces
Technologies
& processes
WP 3.5:
More efficient
wing technologies
WP 4.2:
aminarity for high
lift wing
Technologies
WP3.4:
Optimized
composite
structures
WP 4.1:
NLF smart
integrated wing
TS 5: Advanced
control Systems
Efficient wing
WP 3.2: Wing for
incremental lift &
transmission shaft
integration
More affordable,
more Eco-Friendly
Processes
WP 1.5:
Novel certification
processes
WP 3.1:
Multidisciplinary
wing for high &
low speed
WP3.3:
High lift wing
TS 4: Advanced
laminarity
New structural design
WP 1.4:
Novel high speed
configuration
WP 2.2:
Advanced
integration of
system in nacelle
Novel overall
architecture
WP 1.3: CROR
configuration
WP 2.1:
Laminar nacelle
Nacelles
WP 1.2: High wing
/ large Tprop
nacelle
configuration
Advanced engine
integration
WP 1.1:
Tail plane engine
integration
TS 3: Next
Generation
optimized wing box
TS 2: Novel
Nacelles
DIRECTION 3:
Fuselages
with
optimized
usage of
volume and
minimized
weight, cost
and
environ15
-mental.
impact
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