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Clean Sky Info Day on 7th call for proposals, 11 October 2010, Brussels
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Sustainable And Green Engines –ITD Michel GOULAIN, SAGE PO
Clean Sky Info Day on 8th Call for proposals
Toulouse, 1st February 2011
Clean Sky Info Day on 7th call for proposals, 11 October 2010, Brussels
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Content
• SAGE: the 5 demonstrators• SAGE : objectives• SAGE 1 to 5: actors and challenges• Call 8: the topics
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SAGE ITD – 5 Concepts, 5 Demonstrations
Geared Drive Counter rotating
Open Rotor
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SAGE Objectives
SAGE ITD Steering Committee • Rolls-Royce• SAFRAN• MTU• AVIO• ITP• Volvo Aero Corporation• Airbus• Alenia• Clean Sky Joint Undertaking
Engine Sector Environmental Targets and Achievements
CO2 NOx Noise (EPNdB) Cumulative
2000 Baseline Baseline Baseline
Clean Sky -14 % to –20 %TRL 6
-60 % to –80 %TRL 6
-16 to –20TRL 6
ACARE -20 % -80 % -20
* NOx baseline is roughly consistent with 80% of CAEP2** Noise baseline is roughly ICAO Stage3 – 10 EPNdB
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Intercase, inc. mountRear rotating structure
BR715 core gas generator core
Open rotor assemblyTest Programme
Low Pressure Compressor
Booster
Airframer requirements and installations
Project launch1 June 2008
Project completionPrelim. DR
Concept DR
Concept studiesDemo spec.
Prelim. designPartner selection
Detail designManufacture
Build and test
Critical DR
Open rotor technology development → full-scale engine demonstration
SAGE ITD – SAGE1, Geared Open Rotor
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M88 gas generator
Composite blades
Power gear boxPower Turbine
Rotating frames
Nacelle rotating parts
Pitch Control Mechanism rotating parts
SAGE ITD – SAGE2, Geared Open Rotor
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Power TurbinePower Turbine
PropellersPitch Change Control
PropellersPitch Change Control
ProtectiveAir Intake ProtectiveAir Intake
Rotating Nacelle Parts
Rotating Nacelle Parts
Noise& Vibration
Noise& Vibration
Operability & Power Management
Operability & Power Management
Certificability& Reliability
Certificability& Reliability
A/C Installation and wake interaction
A/C Installation and wake interaction
Counter-rotating propellers, noise optimised
Counter-rotating propellers, noise optimised
De-icingDe-icing
Communications via rotating systems
Communications via rotating systems
Power gearboxPower gearbox
Pusher Counter-Rotating Open Rotor Challenges
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Lightweight intercase structures, material characterisation and
manufacturing technologies
Trent 1000 core engineComposite fan systemIntegrated installations
Test programme
Low Pressure Turbine and structures
Project launch1 June 2009
Build 2 engine test
2013
Prelim. DRMarch 2011
Concept DRDec. 2009
Concept studiesTechnologyselection for
demonstration
Prelim. DesignProcess
developmentPartner selection
Detail designManufactureRig testing
Phased build and technology
demonstration
Critical DRAugust 2011
Build 1 engine test
2012
SAGE ITD – SAGE3, Large 3-shaft Demonstrator
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Technologies for lightweight, efficient intercase structures
Technologies for lightweight, efficient intercase structures
Composite fancaseComposite fancase
Composite fan bladesComposite fan blades
Novel intake with optimised aero and
acoustic liners
Novel intake with optimised aero and
acoustic liners
Advanced integrated dressings
Advanced integrated dressings
Lightweight, high efficiency LPT
Lightweight, high efficiency LPT
Improved controls heat managementImproved controls heat management
Advanced sealing technologies
Advanced sealing technologies
Lightweight annulus fillers
Lightweight annulus fillers
Intake optimised to composite fan system
Intake optimised to composite fan system
Advanced Large 3-Shaft Turbofan Challenges
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Mid Turbine Frame
Fan Drive Gear System
High Pressure Compressor
High-Speed Low Pressure Turbine
PW1000G Donor Engine
Project launch1 June 2008
Project completion2014
Prelim. DRDec. 2010
Concept DRMar. 2010
Initial Concept Design
Concept Definition & Concept Studies
Detail DesignManufacture
Assy and Test
Critical DRSep. 2011
Concept Optimization
Turbine Exhaust Case
SAGE ITD – SAGE4, Geared Turbo Fan
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New High Efficient High Pressure Compressor
New High Efficient High Pressure Compressor
Mid Turbine Frame with aggressive Interduct
Mid Turbine Frame with aggressive Interduct
New High Speed Low Pressure Turbine
New High Speed Low Pressure Turbine
New Lightweight Exhaust Frame
New Lightweight Exhaust Frame
Advanced Fan Drive Gear System
Advanced Fan Drive Gear System
Temps & MaterialsTemps & Materials
Weight & Mech. Integration
Weight & Mech. IntegrationInnovative Designs
& Mfg ProcessesInnovative Designs & Mfg Processes
Efficiency & PerformanceEfficiency & Performance
Engine Control & Power System
Engine Control & Power System
Advanced Geared Turbo Fan Challenges
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Innovative Core Engine
Project launch1 Sept 2009
Project completion2014
Critical DRJuly 2011
Preliminary DRFeb. 2009
Demo spec. Prelim. designPartner selection
Detail designManufacture
Build and test
Engine testSept 2012
Turboshaft engine development → full-scale engine demonstration
Built and testAirframer requirements
and installations
SAGE ITD – SAGE5, Turboshaft engine
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Call 8 TopicsJTI-CS-SAGE 6.600.000JTI-CS-SAGE-01 1.000.000
JTI-CS-2011-1-SAGE-01-001 1.000.000JTI-CS-SAGE-02 4.200.000
JTI-CS-2011-1-SAGE-02-08200.000
JTI-CS-2011-01-SAGE2-02-06 2.000.000JTI-CS-2011-1-SAGE2-2011-07 2.200.000
JTI-CS-SAGE-03 1.300.000
JTI-CS-2011-1-SAGE-03-009 5.000.000JTI-CS-2011-01-SAGE-03-010 800.000JTI-CS-2011-01-SAGE-03-011 500.000
JTI-CS-SAGE-04 5.300.000
JTI-CS-2011-01-SAGE-04-009 600.000JTI-CS-2011-01-SAGE-04-010 400.000JTI-CS-2011-01-SAGE-04-011 1.300.000JTI-CS-2011-01-SAGE-04-012 1.000.000JTI-CS-2011-01-SAGE-04-013 1.000.000JTI-CS-2011-01-SAGE-04-014 500.000JTI-CS-2011-01-SAGE-04-015 500.000
JTI-CS-SAGE-05 2.300.000
JTI-CS-2011-1-SAGE-05-013 450.000JTI-CS-2011-1-SAGE-05-014 750.000JTI-CS-2011-1-SAGE-05-015 1.100.000
Area-01 - Geared Open RotorClean Sky - Sustainable and Green Engines
High temperature Ni-based super alloy casting process advancementArea-05 - Turboshaft
Area-02 - Direct Drive Open Rotor
Integrating forging- and process-simulation into SAGE4 GTF LPT rotor design
Area-04 - Geared Turbofan
Electric Smart Engine ActuatorHigh temperature Ni-based alloy forging process advancement
Feasibility study and prototypes manufacturing of oil tank in thermoplastic for Helicopter EngineHot environment unsteady pressure sensorsDevelopment of Quiet exhaust noise attenuation technologies
Lean Burn Control System Verification Rig
Propellers electrical de-icing system: reliability assessment of key technologies for high temperature electrical machines
Pitch Change Mechanism key technologies maturationPCM kinematic demonstration
Casting process optimization and validation of hollow multivane clusters with thin walls and trailing edges
Total Measurement System for Geometry and Surface Inspection of bladed Disks (TOMMI)Implementation of Carbon-Nanotube Rein-forced Aluminum for Aerospace Heat Ex-changer Applications
Large 3-shaft Demonstrator – Aeroengine intake acoustic liner technology developmentSteel casting process advancementAdvanced press forming and hardening of high strength steels
Area-03 - Large 3-shaft turbofan
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For further information:
www.cleansky.eu
Contact us
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© 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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Info sur SAGE topics
Lean Burn control system verification rig
Pitch Change mechanisms key technologies maturation
PCM Kinematic demonstration
key technology maturation for electric de-icing machines
Intake liner
Cast ability
Press performing sheet
Casting process optimization and validation of hollow multivane clusters with thin walls and trailing edges
Integrating forging- and process-simulation into SAGE4 GTF LPT rotor design
Total Measurement System for Geometry and Surface Inspection of bladed Disks (TOMMI)
Implementation of Carbon-Nanotube Rein-forced Aluminum for Aerospace Heat Ex-changer Applications
Electric Smart Engine Actuator
High temperature Ni-based alloy forging process advancement
Intake liner
Steel casting process advancement
Feasibility study and prototypes manufacturing of “oil tank in thermoplastic” for Helicopter Engine
Hot environment unsteady pressure sensors
Development of Quiet exhaust noise attenuation technologies