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1 1 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) Clean Sky programme Sébastien DUBOIS, Project Officer Green RotorCraft Session.

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Presentation on theme: "1 1 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) Clean Sky programme Sébastien DUBOIS, Project Officer Green RotorCraft Session."— Presentation transcript:

1 1 1 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) Clean Sky programme Sébastien DUBOIS, Project Officer Green RotorCraft Session d'information CLEAN SKY 1 er Février 2011 – Blagnac (France)

2 2 2 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

3 3 3 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) Clean Sky / Green Rotorcraft : heading toward ACARE goals REACH compliance Halving noise Emissions reduction Green Life Cycle

4 4 4 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) ITD-leaders (< 50%)  DLR (D)  ONERA (F)  PZL Swidnik (Pol)  CIRA-SELEX ATS : cluster (I)  IGOR : cluster of 11 members (NL, B, D) Airborne Composite, Akustik Universiteit Twente 160M€ Total Budget: 10% of Clean Sky  Agusta-Westland (co-leader)  Eurocopter (co-leader)  Liebherr (D)  Hispano-Suiza (F)  Thales Avionics Electrical Systems (F)  DLR (D)  ONERA (F)  PZL Swidnik (Pol)  CIRA-SELEX ATS : cluster (I)  IGOR : cluster of 10 members (NL, B, D) Airborne Composite, Eurocarbon, Fibre Optic Sensors and Sensing Systems, LMS; Microflown Technologies, Micromega Dynamics, NLR, Technische Universiteit Delft, Universiteit Twente Partners (>25%) Associates (<25%) Main Stakeholders of the domain presents in the ITD GRC: Helicopoter Manufacturers, Research Institutes, Systems suppliers 10 members composed of 23 legal entities GRC: Participants & Global Shares

5 5 5 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) Green Rotorcraft – Programme Concept

6 6 6 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) GRC: Background from Rotorcraft EU-projects Field ‘90‘95‘00‘05‘10‘15 Avionics ATM Systems Greening – CO2, NOx, External Noise, Aerodynamics - CFD Gear / Drive Flight Physics ROSAA EROS CLEANSKY FRIENDCOPTER SILENCER TEENI GOAHEAD HELINOISE HELISHAPE DACRO ECARP HELIFUSE HELIFLOW HORTIA ENABLE SESAR FLYSAFE ALICIA ON-WINGS OPTIMAL PEGASE ON-WINGS NICE-TRIP RHILP ACT-TILT TILTAERO DART TRISID ADYN ASETT FACET FP6FP7FP4FP5 FP3 FP2

7 7 7 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) 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 rotorcraft

8 8 8 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 :

9 9 9 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 Flight tests of existing blades fitted with laminar flow covers

10 10 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) On-going projects selected through Calls for proposals WPACRONYMTitleCS Funding (€) Starting date Duration (months) GRC1MulticompAct Multilayer Piezocomposites for Active Twist Rotor Blade 206,250Jan 1024 GRC1LamBlade Development and provision of a numerical model to solve laminar turbulent boundary layer transition and boundary layer velocity profiles for unsteady flow conditions 92,400Oct 1012 GRC1MORALI Performance/benefit assessment of advanced rotor configurations including active and passive blades 299,880Nov 1048 GRC1PT656 Gurney flap actuator and mechanism for a full scale helicopter rotor blade Under nego 58

11 11 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) GRC2- Drag reduction - Technologies GRC 2.3 – Engine installation => emission & noise reduction GRC 2.1 – Rotor hub drag => Gas emission reduction GRC 2.2 – Fuselage drag => Gas emission reduction GRC2.4 – Optimised design (H/C & T/R - full airframe)

12 12 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 & Tilt- Rotor 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

13 13 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) On-going projects selected through Calls for proposals WPACRONYMTitleCS Funding (€) Starting date Duration (months) GRC2TILTOp Contribution to the study of the air intake and exhaust integration into a tiltrotor nacelle 286,200July 1018 GRC2CODE-Tilt Contribution to design optimisation of tiltrotor for drag (fuselage/wing junction, nose, landing gear, empennage) 637,200Oct 1036 GRC2CARD Contribution to analysis of rotor hub drag reduction 375,000Nov 1036 GRC2ADHeRo Contribution to the aerodynamic design optimisation of a helicopter fuselage including its rotating rotor head. 618,250Jan 1142 GRC2HEAVYcOPTer Contribution to optimisation of heavy helicopter engine installation design 439,200Under nego 24 GRC2HELIDES Helicopter hub and fuselage drag investigation by means of hybrid URANS/LES methods 147,285Under nego 24

14 14 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) GRC3 – Integration of Innovative Electrical Systems  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 Goals : removal of hydraulic fluid, deletion of engine bleed air circuit

15 15 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)

16 16 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) On-going projects selected through Calls for proposals WPACRONYMTitleCS Funding (€) Starting date Duration (months) GRC3RECYCLE Innovative energy recovery for electrical use 187,500July 1029 GRC3ELETAD Electric Tail Drive - Modelling, Simulation and Rig Prototype Development. 1,798,496Oct 1066 GRC3PPSMPAB Piezo Power Supply Module 429,350Mars 1149

17 17 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) GRC4 - Diesel Engine on a Light Helicopter  Objectives  To reduce drastically CO 2 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

18 18 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).

19 19 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 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 Flight guidance systems

20 20 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) GRC5- Flight Path – Technologies (2/2) First flight test campaign completed (June 2010) with experimental guidance system First flight test campaign completed (June 2010) with experimental guidance system

21 21 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)

22 22 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) On-going projects selected through Calls for proposals ACRONYMTitleCS Funding (€) Starting date Duration (months) GRC5EMICOPTER Emission analysis: Tools required to perform the emission analysis and evaluation methodology 296,250Jan 1018 GRC5GARDEN GNSS-based ATM for Rotorcraft to Decrease Emissions and Noise 370,231Jan 1066 GRC5MAEM-RO Emission analysis - Tools required to perform the emissions analysis and evaluation methodology, experimental support 288,500 July 1020

23 23 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 composite- metallic bonding – Bonding and painting – Repair – testing  Gear Box Housing Cr6 free Magnesium protection & touch up AND painting Testing  Transmission components Cd free protection Repair AND painting testing

24 24 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 Image courtesy of Eurocopter Helicopter Mission Noise Footprints Image courtesy of AgustaWestland Simulation Framework

25 25 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) Impact assessment of GRC results (for TE) - Noise Reduction

26 26 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) SAGE ITD – SAGE5, Turboshaft engine Innovative Core Engine Project launch 1 Jan Project completion 2013 Critical DR July 2011 Preliminary DR Jan Demo spec. Prelim. design Partner selection Detail design Manufacture Build and test Engine test Sept 2012 Turboshaft engine development → full-scale engine demonstration Built and test Airframer requirements and installations

27 27 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) EDS ITD

28 28 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) WPsTitleGross Budget (€) Project Duration (months) GRC3 Innovative management of energy recovery for reduction of electrical power consumption on fuel consumption GRC3 Adaptation kit design & manufacturing: APU Driving System GRC4 Optimised Diesel engine design matching a new light helicopter architecture GRC4 Diesel Power-pack Integration on a light helicopter demonstrator GRC5 Tuning of simplified rotorcraft noise models. Preliminary acoustic measurement test campaign GRC6 Manufacturing of a Thermoplastic Composite Feasibility Article for a Helicopter Door GRC6 Manufacturing of Thermoplastic Structural Demonstrators (Upper Panel Rear Fuselage, Sponson Fairing Demonstrator & Radome Demonstrator) Call for proposals under negotiation: Call 7 th 7th Call: launched Launched ; Deadline Details & information on: the “Calls” sectionwww.cleansky.eu

29 29 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) Next Call for proposal 8th Call: launched Launched ; Deadline +3 months Details & information on: the “Calls” sectionwww.cleansky.eu

30 30 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) For further information:  Sébastien DUBOIS Project Officer  Contact us

31 31 Clean Sky – Session d’information/ 2 février 2011 à Blagnac (France) Thank you for your attention

32 32 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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