Clean Sky at a Glance - SUNJET II · Clean Sky at a Glance SUNJET II - Clean Sky at Le Bourget 21...
-
Upload
nguyenthuy -
Category
Documents
-
view
219 -
download
0
Transcript of Clean Sky at a Glance - SUNJET II · Clean Sky at a Glance SUNJET II - Clean Sky at Le Bourget 21...
Clean Sky – (2008-2016) – 1.6 billion (800 mil from FP7, industry in kind)Clean Sky 2 – (2014-2024) - 4 billion (1755 mil from H2020, industry in kind)
CS1 organisation (2008-2016)
EUROCONTROLEASA
Smart Fixed Wing AircraftAirbus (F, D, UK, E)SAAB (SE)
Green Regional Aircraft Alenia Aeronautica (I)EADS CASA (E)
Green Rotorcraft AgustaWestland (I, UK)Eurocopter (F, D)
Sustainable and Green Engines Rolls-Royce (UK, D)Safran (F)
Systems for Green Operation Thales (F)Liebherr (D)
Ecodesign Dassault Aviation (F)Fraunhofer Gesellschaft (D)
Technology EvaluatorThalesDLR
CS1 financial contribution and allocation
Maximum Overall EC Contribution:
800 M€
Partners(min 200 M€
i.e.25%)
Call
for
Proposals
Members
(max. 600 M€ i.e. 75%)
ITD Leaders(max 400 M€ i.e. 50%)
Associates(max 200 M€
i.e. 25%)
match EC contribution
50% (in-kind)
match EC
contribution 50%
(in-kind)
Maximum Overall EC Contribution:
800 M€
Partners(min 200 M€
i.e.25%)
Call
for
Proposals
Members
(max. 600 M€ i.e. 75%)
ITD Leaders(max 400 M€ i.e. 50%)
Associates(max 200 M€
i.e. 25%)
match EC contribution
50% (in-kind)
match EC
contribution 50%
(in-kind)
Development strategy
• Technologies are selected, developed and monitored in terms of maturity or ‘technology readiness level’ (TRL). They were identified as the most promising in terms of potential impact on the environmental performance of future aircraft.
• Concept aircraft are design studies dedicated to integrating technologies into a viable conceptual configuration. Clean Sky’s results are measured and reported by comparing these concept aircraft to existing aircraft and aircraft incorporating ‘evolutionary technology’ in the world fleet.
• Demonstration Programmes include physical demonstrators that integrate several technologies at a larger ‘system’ or aircraft level, and validate their feasibility in operating conditions. This supports the evaluation of the actual potential of the technologies. The ultimate goal of Clean Sky is to achieve successful demonstrations in a relevant operating environment, i.e. up to TRL 6.
9
Conceptual aircraft and demonstratorsTechnologies and configurations:
Advanced Metallic Material
Advanced Composite Materials
Structure Health Monitoring
Low Noise Landing Gear
Low Noise & High Efficiency High Lift Devices
Advanced Electrical Power Generation and Distribution System
Electrical Environmental Control System
EMA for Primary Flight Control System Actuation
EMA for Landing Gear Actuation
Mission Trajectory Management
optimization
Green Regional Turboprop
10
Conceptual aircraft and demonstrators
GRA ATR first flight, Crown Panel 9 July 2015, TRL 5/6
Test campaign # 1
Innovative CFRP fuselage “crown” panel
Contributions from ALENIA (design), ATR
(installation and operation; test aircraft); Fraunhofer
(panel instrumentation)
Aim of Flight test campaign was to support the
development of innovative CFRP panel with
embedded layer to provide additional acoustic
damping
The expected benefits concern weight, internal
noise, assembly costs and structural health
monitoring
Test Campaign # 2 : AEA (All Electric Aircraft) February 2016
E-ECS (Environmental Control System 35 kW vs. 70)
EPGDS (electrical power generation and distribution system)
E-EM Electric management
EMA LG/FCS (Cabin installation of additional electrical loads)
FTI
ElectricECS
Electrical Energy
Management
270 HVDCnetwork
demo channelEMAs E-Loads
https://www.youtube.com/watch?v=5CuJ
9kgoNGU
Conceptual aircraft and demonstrators
Conceptual aircraft and demonstrators
featuring
• SFWA Natural laminar flow (NLF) wing
• SNECMA conceptual Counter Rotating
Open Rotor (CROR)engines
• SGO MTM Optimized trajectories, in the FMS
Short/medium-range (SMR) aircraft, [APL2]
This concept aircraft includes both the ‘smart’ laminar-flow wing and the incorporation of the contra-rotating open rotor (CROR) engine concept, developed within the Clean Sky programme.• The Flight-testing of a A340 demonstrator aircraft with representative Laminar Wing
is planned Sept 2017, although still part of the CS1 framework; • the CROR engine demonstrator on ground is scheduled by Q4-16, while the flight
testing is moved to CS2.• Advanced systems and new flight trajectories already matured to appropriate level
are included in the architecture.
Conceptual aircraft and demonstrators
The Ground Based Demonstrator (GBD) is a full scale partial wingbox demonstration of the
structure and systems needed to produce a leading edge solution to meet the strict requirements to
achieve Natural Laminar Flow (NLF) Wing.
Contributors were GKN as Partner, and Airbus together with the Manufacturing Technology Centre at
Coventry for the assembly and testing of the integrated product.
Main features: The GBD is a 4.5m long by 1m wide section of flight-representative wing leading edge attached to
a partial wing box assembly. The leading edge accommodates a Krueger flap in two sections. This
split has allowed GKN Aerospace engineers to investigate two very different design philosophies.Major outcomes are: Ground Based Demonstrator (full scale Leading edge) fully functional Installation of electro-thermal anti-ice system, moveable Krueger flaps, bird strike and lightening
protection) Numerous manufacturing & assembly lessons learnt (esp. wrt. accessibility)
Conceptual aircraft and demonstrators
Objective: to demonstrate in flight thatthe Natural Laminar Flow (NLF) wingproduced at ‘industrial scales’ will confersignificant performance, with lowmaintenance and operational costs
Main features:
Advanced passive laminar wingaerodynamic design
Two alternative integrated structuralconcepts for a laminar wing
High quality, low tolerancemanufacturing and repair techniques
Anti-contamination surface coating Shielding Krueger high lift device
Expected benefits: fuel burn saving onshort and mid-range aircraft comparedwith an equivalent aircraft with aconventional wing
Counter-Rotating Open Rotor- Joint certification group with engine and airframers
and airworthiness authorities.- Definition of the applicable regulations (propeller vs.
turbofan)- Assessment of critical aspects, like blade release
containment; impact on fuselage design (shielding)- Noise assessment progressed.- Ground Tests in preparation.
Main engine demonstrator
Rotorcraft demonstratorsGRC Demonstration of Helicopter Low Noise IFR and
VFR Procedures
May 2015 TRL 6
H175 helicopter flying low-noise IFR approaches to the heliport of Toulouse-Blagnac airport.
The approach procedures were flown using accurate lateral and vertical guidance provided by EGNOS (European Geostationary Navigation Overlay Service), the European Satellite-Based Augmentation System (SBAS), and in the presence of airplane traffic simultaneously approaching and departing to/from airport runways.These helicopter-specific procedures allow achieving the Simultaneous Non Interfering (SNI) aircraft and rotorcraft IFR operations at a medium-size commercial airport.
The low-noise procedures demonstrated noise footprint reductions of up to 50 per cent.
Detailed design and integration of the procedures in Toulouse airspace was achieved by GARDEN, a partner project with expertise in Air Traffic Management (ATM).
For the VFR tests, an AW139 was used as part of another Partner's projects MANOUVERS
Addressing the H2020 (societal) Challenges
• “Smart Green and Integrated Transport”
Resource efficient transport that respects the environment
Ensuring safe and seamless mobility
Building industrial leadership in Europe
Enhancing and leveraging innovation capability across Europe, with a strong emphasis on SME participation
Leveraging private sector initiatives, and (important!) building on MS national and regional efforts
Aviation R&I in H2020
Long termresearch
Greening and competitiveness
ATM
Clean Sky 2 SESAR
Basic research
ERC
Alternative fuels
Security
Fuel cells
FCH 2
Access to financing
RSFF
ICTMaterials
SME support
Research infrastructures
H2020 – CS2 (2014-2024)
Clean Sky 2 Programme Set-up
Large
Systems
ITDs
Vehicle
IADPs
Tech
no
logy
Eva
luat
or
(TE)
Ger
man
Aer
osp
ace
Cen
ter
(DLR
)
Regional AircraftLeonardo
FastRotorcraft
Leonardo Airbus
Helicopters
Engines ITD
Safran – Rolls-Royce – MTU
Systems ITD
Thales – Liebherr
Airframe ITD
Dassault – Airbus D&S – Saab
Smal
l Air
Tra
nsp
ort
Evek
tor
–P
iagg
io
Large Passenger
AircraftAirbus
EU Funding Decision 1.755bn€1.716bn€ “net” (after running costs)
Eco
-Des
ign
Frau
nh
ofe
rG
ese
llsch
aft
Up to 40% of EU funding available for CS2 Leaders
At least 60% of EU funding open to competition:
Up to 30% for Core Partners (becoming Members once selected)
At least 30% for CfP (i.e. Partners as in CS) plus CfTs
Meaning >1bn€ of EU funding in play, via open Calls
CS2 Participation
Industry, SMEs, Academia, and Research Organizations eligible both forparticipation as Core Partners or Partners.
Participation may also take place via suitable Clusters / Consortia.
800 - 1000 Participants expected across all tiers of the industrial supplychain and “R&I Chain”, with large investment leverage effect
Final remarks1. The Clean Sky original scope aimed at improving the
environmental impact of aviation through insertion oftechnologies in future aeronautical products.
2. In H2020, CS2 complements this environmental target withmobility and competitiveness.
3. The JU is addressing new aspects, like the involvement ofAcademia, the link with Structural Funds, an increasedcollaboration with SESAR and EASA and the potential new typeof Calls.
4. CS is also potentially contributing to the future InternationalCooperation via the involvement by DG-RTD
5. This paves the way to the evolution of Clean Sky in the nextfuture.