Transcript GRC general overview - Sébastien Dubois

Clean Sky programme
Sébastien DUBOIS,
Project Officer Green RotorCraft
Session d'information CLEAN SKY
1er Février 2011 – Blagnac (France)
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
Outlines
The Green Rotorcraft Project
 Environmental objectives
 Membership
 GRC at a glance
 Next call for proposal
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
Clean Sky / Green Rotorcraft : heading toward
ACARE goals
Halving noise
REACH compliance
Green Life Cycle
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Emissions reduction
Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
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GRC: Participants & Global Shares
160M€ Total Budget: 10% of Clean Sky
ITD-leaders (< 50%)
 Agusta-Westland
(co-leader)
 Eurocopter
(co-leader)
 Liebherr (D)
 Hispano-Suiza (F)
 Thales Avionics
Electrical Systems (F)
Associates (<25%)

DLR
(D)

DLR (D)

(F)(F)
 ONERA
ONERA

PZL Swidnik (Pol)
 PZL Swidnik (Pol)

CIRA-SELEX ATS: cluster (I)

CIRA-SELEX
ATS: (NL,
cluster (I)

IGOR: cluster of 11 members
D)
 B,
IGOR
: cluster of 10 members (NL, B, D)
Airborne Composite, Akustik
Universiteit Twente
Airborne
Composite, Eurocarbon,
Fibre Optic
Sensors and Sensing Systems, LMS; Microflown
Technologies, Micromega Dynamics, NLR,
Technische Universiteit Delft, Universiteit Twente
Partners (>25%)
Main Stakeholders of the domain presents in the ITD GRC:
Helicopoter Manufacturers, Research Institutes, Systems suppliers
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10 members composed of 23 legal entities
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
Green Rotorcraft – Programme Concept
2009
2009
2010
2010
2011
2011
2012
2012
2013
2013
2014
2014
2015
2015
NOISE REDUCTION
OPTIMIZED CONFIGURATIONS
Selection of breakthrough Technologies and
advanced configurations for impact on
Rotorcraft Noise reduction and Greener
Operations.
Design, Build and Integrate the
technologies in ground and flight
Demonstration
Flight Test and
Validation of
rotorcraft
Technologies and
configurations
Criteria definition for Demonstration
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
GRC: Background from Rotorcraft EU-projects
‘90
Field
‘95
‘00
‘05
Avionics
ATM
Systems
‘10
FLYSAFE
‘15
ALICIA
PEGASE
OPTIMAL
ON-WINGS
SESAR
Greening –
CO2, NOx,
External Noise,
ENABLE
FRIENDCOPTER
CLEANSKY
HORTIA
HELINOISE
SILENCER
TEENI
EROS
Aerodynamics
HELISHAPE
-
CFD
ROSAA
DACRO
GOAHEAD
HELIFUSE
ECARP
TRISID
DART
ASETT
Gear / Drive
FACET
RHILP
Flight
Physics
FP2
ON-WINGS
HELIFLOW
FP3
FP4
FP5
Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
ADYN
TILTAERO
ACT-TILT
FP6
NICE-TRIP
FP7
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GRC: Detailed WPs
1. Innovative Rotor Blades
 Active blade devices
 Blade stall alleviation, profile drag reduction (tayloring of blade design)
2. Drag reduction, required power reduction
 Passive and active flow controls for helicopter and tiltorotor components
 Integration of MR pylon, hub, aft body, tail, turboshaft engine installation
3. More electrical Helicopter
 Elimination of noxious hydraulic fluid; optimised on-board energy ; weight reduction
4. Lean powerplant
 installation of a Diesel engine on a light single HC for low CO2 emission
5. Environment-Friendly Flight Path
 Noise abatement with optimized flight procedures in VFR & IFR including ATM constraints
 Fuel consumption and pollutant emissions reduction through a mission profile optimization
6. EcoDesign
 Participation to generic studies +demo on specific rotorcraft technologies & components
7. Technical Evaluator
 Interfacing to the assessment of actual impact of selected technologies for rotorcraft7
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
GRC1- Rotor Blades - Technologies
 Optimized design
 3D blade profile tayloring
 Active control
 active blade deformation
e.g. active twist
(further to Friendcopter) :
 Active control surface
e.g. Gurney flap :
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
GRC1- Rotor Blades Master Plan & demonstration
Demonstrators
 Various levels of component testing for GRC1 developed technologies
 Bench test of full scale active twist blade section (concept progress from
FRIENDCOPTER)
 2D wind tunnel testing of GRC1 developed technologies
 Model rotor testing of active dual speed rotor concepts
 Whirl Tower (full-scale blades) testing for active blades (laminar airfoil or dual
speed rotors) and passive optimised blades
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 Flight tests of existing blades fitted with laminar flow covers
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
On-going projects selected through Calls for
proposals
WP
ACRONYM
CS
Funding
(€)
Starting
date
Duration
(months)
GRC1
MulticompAct
Multilayer Piezocomposites for Active Twist Rotor
Blade
206,250
Jan 10
24
GRC1
LamBlade
Development and provision of a numerical model
to solve laminar turbulent boundary layer transition
and boundary layer velocity profiles for unsteady
flow conditions
92,400
Oct 10
12
GRC1
MORALI
Performance/benefit assessment of advanced
rotor configurations including active and passive
blades
299,880
Nov 10
48
GRC1
PT656
Gurney flap actuator and mechanism for a full
scale helicopter rotor blade
575.000
Under
nego
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Title
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
GRC2- Drag reduction - Technologies
GRC 2.1 – Rotor hub drag
=> Gas emission reduction
GRC 2.2 – Fuselage drag
=> Gas emission reduction
GRC 2.3 – Engine installation
=> emission & noise reduction
GRC2.4 – Optimised design
(H/C & T/R - full airframe)
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
GRC2- Drag reduction
Master Plan & demonstration
Demonstrators
 Rotor hub for light & medium helicopters
 Wind tunnel tests of new hub cap solutions
 Flight tests of the new hub cap
 Fuselage and Empennage optimization for light/medium/heavy helicopters & TiltRotor
Laboratory & Wind tunnel tests
 Flow control devices applied on a blunt helicopter fuselage
 Passive and active devices of blunt light/medium and heavy helicopter fuselages
 Helicopter empennage with movable control surfaces
 Enhanced fuselage components of the common ERICA tilt rotor
 Engine Installation: light/heavy helicopter and the ERICA tilt rotor
 Wind tunnel tests of different engine installation solutions
 Ground and/or flight-test measurements of the optimised engine installation
 Optimised Design: the common helicopter platform
 Wind tunnel tests on the optimised geometries
Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
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On-going projects selected through Calls for
proposals
WP
ACRONYM
Title
CS
Funding
(€)
Starting
date
Duration
(months)
GRC2
TILTOp
Contribution to the study of the air intake and
exhaust integration into a tiltrotor nacelle
286,200
July 10
18
GRC2
CODE-Tilt
Contribution to design optimisation of tiltrotor for
drag (fuselage/wing junction, nose, landing gear,
empennage)
637,200
Oct 10
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GRC2
CARD
Contribution to analysis of rotor hub drag
reduction
375,000
Nov 10
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GRC2
ADHeRo
Contribution to the aerodynamic design
optimisation of a helicopter fuselage including its
rotating rotor head.
618,250
Jan 11
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GRC2
HEAVYcOPTer
Contribution to optimisation of heavy helicopter
engine installation design
439,200
Under
nego
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GRC2
HELIDES
Helicopter hub and fuselage drag investigation by
means of hybrid URANS/LES methods
147,285
Under
nego
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
GRC3 – Integration of Innovative Electrical
Systems
Goals : removal of hydraulic fluid, deletion of engine
bleed air circuit
 Efficient electrical generation,
conversion and distribution
(generic for small aircraft)
 Electromagnetic Actuators for
helicopter flight control (ground
testing)
Electrically driven Tail Rotor
(concept studies)
Efficient power generation and
control for piezoelectric actuation,
esp. active blades
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
GRC3 – Integration of Innovative Electrical
Systems - Master Plan & demonstration
Demonstrators
 EMA system for medium/heavy helicopter flight control
 EMA system for landing gear and for rotor braking
 Energy recovery subsystem
 Management of energy recovery
 Innovative High Voltage Energy Storage System for Advanced Rotorcraft
Integration
 Brushless 28VDC Starter-Generator
 Electrical tail rotor motor
 Piezo Power Supply module ( Active rotor blade demonstration)
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
On-going projects selected through Calls for
proposals
WP
ACRONYM
Title
GRC3
RECYCLE
Innovative energy recovery for electrical use
GRC3
ELETAD
Electric Tail Drive - Modelling, Simulation and Rig
Prototype Development.
GRC3
PPSMPAB
Piezo Power Supply Module
CS
Funding
(€)
Starting
date
Duration
(months)
187,500
July 10
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1,798,496
Oct 10
66
429,350
Mars 11
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
GRC4 - Diesel Engine on a Light Helicopter
 Objectives
To reduce drastically CO2 emission thanks to
the very low fuel consumption of modern
Diesel engine technology
Typically -30% to -40% over full flight envelope
Using regular kerosene fuel (or biodiesel)
To integrate the engine minimising the
potential adverse effects :
• weight penalty ;
• Vibration ;
• Cooling system
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
GRC4 - Diesel Engine on a Light Helicopter
Master Plan & demonstration
Demonstrators
 Flight worthy helicopter demonstrator based on EC120 and modified to
integrate an adapted Diesel engine, to be tested on ground
 Main modified/new components: primary structure, engine installation,
transmission, clutch system, cooling system, control system.
 Aeronautical Diesel power-pack designed for helicopter use (power rating,
weight reduction, FADEC).
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
GRC5- Flight Path – Principles (1/2)
 For helicopter (further OPTIMAL) & Tilt Rotor A/C (further
to NICE-TRIP):
 Low-noise on-board system
 En-route optimised flight paths for the reduction of polluting emissions
Flight guidance
systems
 IFR & VFR approach and departure procedures (noise footprint minimisation)
 Low level VFR & IFR en route navigation (noise impact minimisation)
 SNI shorter routes to minimise fuel emission and gas emission
Operational
Requirements
Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
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GRC5- Flight Path – Technologies (2/2)
First flight test
campaign completed
(June 2010)
with experimental
guidance system
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
GRC5- Flight Path – Technologies (2/2)
Demonstrators
 Validation of On Board Management (of Low Noise Flight Paths)
 Final Flight Test Demonstrations (Operational Demonstration on real area as
airports, heliports and confined helipads)
 Applicability to Different Aircraft Configurations (i.e. Tilt-Rotor)
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
On-going projects selected through Calls for
proposals
ACRONYM
Title
CS
Funding
(€)
Starting
date
Duration
(months)
GRC5
EMICOPTER
Emission analysis: Tools required to perform the
emission analysis and evaluation methodology
296,250
Jan 10
18
GRC5
GARDEN
GNSS-based ATM for Rotorcraft to Decrease
Emissions and Noise
370,231
Jan 10
66
GRC5
MAEM-RO
Emission analysis - Tools required to perform the
emissions analysis and evaluation methodology,
experimental support
July 10
20
288,500
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
GRC6 – EcoDesign Demonstration for Rotorcraft
Airframe
• Doors & Structural
– Recyclable composite parts
– Surface preparation for compositemetallic bonding
– Bonding and painting
– Repair
– testing
Transmission components
Gear Box Housing
 Cd free protection
 Repair AND painting
 testing
 Cr6 free Magnesium protection & touch up AND painting
 Testing
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
Impact assessment of GRC results (for TE) Simulation Framework
PhoeniX: Platform Hosting Operational & ENvironmental Investigations for
Rotorcraft
Helicopter
Mission
Simulation Framework
Noise
Footprints
Image courtesy of Eurocopter
Image courtesy of AgustaWestland
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
Impact assessment of GRC results (for TE) Noise Reduction
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
SAGE ITD – SAGE5, Turboshaft engine
Built and test
Innovative Core
Engine
Airframer
requirements and
installations
Preliminary DR
Jan. 2010
Engine test
Sept 2012
Turboshaft engine development → full-scale engine demonstration
Demo spec.
Project launch
1 Jan. 2009
Prelim. design
Partner selection
Detail design
Manufacture
Critical DR
July 2011
Build and
test
Project completion
2013
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
EDS ITD
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
Call for proposals under negotiation: Call 7th
7th Call: launched
Launched 24-09-2010; Deadline 09-12-2010
Details & information on: www.cleansky.eu
WPs
in the “Calls” section
Title
Gross
Budget (€)
Project Duration
(months)
GRC3
Innovative management of energy recovery for
reduction of electrical power consumption on fuel
consumption
500.000
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GRC3
Adaptation kit design & manufacturing: APU
Driving System
430.000
54
GRC4
Optimised Diesel engine design matching a new
light helicopter architecture
650.000
18
GRC4
Diesel Power-pack Integration on a light
helicopter demonstrator
9.300.000
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GRC5
Tuning of simplified rotorcraft noise models.
Preliminary acoustic measurement test campaign
300.000
8
GRC6
Manufacturing of a Thermoplastic Composite
Feasibility Article for a Helicopter Door
200.000
18
GRC6
Manufacturing of Thermoplastic Structural
Demonstrators (Upper Panel Rear Fuselage,
Sponson Fairing Demonstrator & Radome
Demonstrator)
200.000
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
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Next Call for proposal
8th Call: launched
Launched 08-02-2011; Deadline +3 months
Details & information on: www.cleansky.eu
in the “Calls” section
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
Contact us
For further information:
 www.cleansky.eu
Sébastien DUBOIS
Project Officer
 [email protected]
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
Thank you for your attention
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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)
© 2010 by the CleanSky Leading Partners: Airbus,
AgustaWestland, Alenia Aeronautica, Dassault Aviation,
EADS-CASA, Eurocopter, Fraunhofer Institute, Liebherr
Aerospace, Rolls-Royce, Saab AB, Safran Thales and 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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Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France)