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1 1/16 Clean Sky Info Day on 7th call for proposals, 11 October 2010, Brussels Sustainable And Green Engines –ITD Michel GOULAIN, SAGE PO Clean Sky Info.

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Presentation on theme: "1 1/16 Clean Sky Info Day on 7th call for proposals, 11 October 2010, Brussels Sustainable And Green Engines –ITD Michel GOULAIN, SAGE PO Clean Sky Info."— Presentation transcript:

1 1 1/16 Clean Sky Info Day on 7th call for proposals, 11 October 2010, Brussels Sustainable And Green Engines –ITD Michel GOULAIN, SAGE PO Clean Sky Info Day on 8th Call for proposals Toulouse, 1st February 2011

2 2 2/16 Clean Sky Info Day on 7th call for proposals, 11 October 2010, Brussels Content SAGE: the 5 demonstrators SAGE : objectives SAGE 1 to 5: actors and challenges Call 8: the topics

3 3 3/16 Clean Sky Info Day on 7th call for proposals, 11 October 2010, Brussels SAGE ITD – 5 Concepts, 5 Demonstrations Geared Drive Counter rotating Open Rotor

4 4 4/16 Clean Sky Info Day on 7th call for proposals, 11 October 2010, Brussels 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 CO2NOxNoise (EPNdB) Cumulative 2000Baseline Clean Sky -14 % to – 20 % TRL % to – 80 % TRL to – 20 TRL 6 ACARE-20 %-80 %-20 * NOx baseline is roughly consistent with 80% of CAEP2 ** Noise baseline is roughly ICAO Stage3 – 10 EPNdB

5 5 5/16 Clean Sky Info Day on 7th call for proposals, 11 October 2010, Brussels Intercase, inc. mount Rear rotating structure BR715 core gas generator core Open rotor assembly Test Programme Low Pressure Compressor Booster Airframer requirements and installations Project launch 1 June 2008 Project completionPrelim. DR Concept DR Concept studies Demo spec. Prelim. design Partner selection Detail design Manufacture Build and test Critical DR Open rotor technology development → full-scale engine demonstration SAGE ITD – SAGE1, Geared Open Rotor

6 6 6/16 Clean Sky Info Day on 7th call for proposals, 11 October 2010, Brussels M88 gas generator Composite blades Power gear box Power Turbine Rotating frames Nacelle rotating parts Pitch Control Mechanism rotating parts SAGE ITD – SAGE2, Geared Open Rotor

7 7 7/16 Clean Sky Info Day on 7th call for proposals, 11 October 2010, Brussels Power Turbine Propellers Pitch Change Control Propellers Pitch Change Control Protective Air Intake Protective Air 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 Counter-rotating propellers, noise optimised De-icing Communications via rotating systems Power gearbox Pusher Counter-Rotating Open Rotor Challenges

8 8 8/16 Clean Sky Info Day on 7th call for proposals, 11 October 2010, Brussels Lightweight intercase structures, material characterisation and manufacturing technologies Trent 1000 core engine Composite fan system Integrated installations Test programme Low Pressure Turbine and structures Project launch 1 June 2009 Build 2 engine test 2013 Prelim. DR March 2011 Concept DR Dec Concept studies Technology selection for demonstration Prelim. Design Process development Partner selection Detail design Manufacture Rig testing Phased build and technology demonstration Critical DR August 2011 Build 1 engine test 2012 SAGE ITD – SAGE3, Large 3-shaft Demonstrator

9 9 9/16 Clean Sky Info Day on 7th call for proposals, 11 October 2010, Brussels Technologies for lightweight, efficient intercase structures Composite fancase Composite fan blades Novel intake with optimised aero and acoustic liners Advanced integrated dressings Lightweight, high efficiency LPT Improved controls heat management Advanced sealing technologies Lightweight annulus fillers Intake optimised to composite fan system Advanced Large 3-Shaft Turbofan Challenges

10 10 10/16 Clean Sky Info Day on 7th call for proposals, 11 October 2010, Brussels Mid Turbine Frame Fan Drive Gear System High Pressure Compressor High-Speed Low Pressure Turbine PW1000G Donor Engine Project launch 1 June 2008 Project completion 2014 Prelim. DR Dec Concept DR Mar Initial Concept Design Concept Definition & Concept Studies Detail Design Manufacture Assy and Test Critical DR Sep Concept Optimization Turbine Exhaust Case SAGE ITD – SAGE4, Geared Turbo Fan

11 11 11/16 Clean Sky Info Day on 7th call for proposals, 11 October 2010, Brussels New High Efficient High Pressure Compressor Mid Turbine Frame with aggressive Interduct New High Speed Low Pressure Turbine New Lightweight Exhaust Frame Advanced Fan Drive Gear System Temps & Materials Weight & Mech. Integration Innovative Designs & Mfg Processes Efficiency & Performance Engine Control & Power System Advanced Geared Turbo Fan Challenges

12 12 12/16 Clean Sky Info Day on 7th call for proposals, 11 October 2010, Brussels Innovative Core Engine Project launch 1 Sept 2009 Project completion 2014 Critical DR July 2011 Preliminary DR Feb 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 SAGE ITD – SAGE5, Turboshaft engine

13 13 13/16 Clean Sky Info Day on 7th call for proposals, 11 October 2010, Brussels Call 8 Topics

14 14 14/16 Clean Sky Info Day on 7th call for proposals, 11 October 2010, Brussels For further information: Contact us

15 15 15/16 Clean Sky Info Day on 7th call for proposals, 11 October 2010, Brussels © 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.

16 16 16/16 Clean Sky Info Day on 7th call for proposals, 11 October 2010, Brussels 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


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