Sustainable And Green Engines –ITD

Michel GOULAIN, SAGE PO

Clean Sky Info Day on 8th Call for proposals Toulouse, 1st February 2011

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

Content

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SAGE: the 5 demonstrators SAGE : objectives SAGE 1 to 5: actors and challenges Call 8: the topics

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

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SAGE ITD – 5 Concepts, 5 Demonstrations

Clean Sky Info Day on 7th call for proposals, 11 October 2010, Brussels Geared Drive Counter rotating Open Rotor

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SAGE Objectives

2000 Clean Sky Engine Sector Environmental Targets and Achievements ACARE

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SAGE ITD Steering Committee Rolls-Royce SAFRAN MTU AVIO ITP Volvo Aero Corporation Airbus Alenia Clean Sky Joint Undertaking

CO2 Baseline -14 % to – 20 % TRL 6 -20 % NOx Noise (EPNdB) Cumulative Baseline -60 % to – 80 % TRL 6 -80 % Baseline -16 to – 20 TRL 6 -20

* NOx baseline is roughly consistent with 80% of CAEP2 ** Noise baseline is roughly ICAO Stage3 – 10 EPNdB 4 4/16

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

SAGE ITD – SAGE1, Geared Open Rotor

BR715 core gas generator core Open rotor assembly Test Programme Concept DR Airframer requirements and installations Intercase, inc. mount Rear rotating structure Critical DR Open rotor technology development → full-scale engine demonstration Concept studies Demo spec.

Prelim. design Partner selection Detail design Manufacture Build and test Project launch 1 June 2008 Prelim. DR Project completion

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

Low Pressure Compressor Booster 5 5/16

SAGE ITD – SAGE2, Geared Open Rotor

Nacelle rotating parts Composite blades Rotating frames M88 gas generator Power Turbine Power gear box

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

Pitch Control Mechanism rotating parts 6 6/16

Pusher Counter-Rotating Open Rotor Challenges

Propellers

Pitch Change Control Noise & Vibration A/C Installation and wake interaction Protective Air Intake Certificability & Reliability Counter-rotating propellers, noise optimised De-icing Rotating Nacelle Parts Operability & Power Management Power gearbox Communications via rotating systems Power Turbine

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

SAGE ITD – SAGE3, Large 3-shaft Demonstrator

Trent 1000 core engine Composite fan system Integrated installations Test programme Concept DR Dec. 2009 Concept studies Technology selection for demonstration Project launch 1 June 2009 Prelim. Design Process development Partner selection Detail design Manufacture Rig testing Prelim. DR March 2011 Lightweight intercase structures, material characterisation and manufacturing technologies Critical DR August 2011 Phased build and technology demonstration Build 1 engine test 2012 Build 2 engine test 2013

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

Low Pressure Turbine and structures 8 8/16

Advanced Large 3-Shaft Turbofan Challenges

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

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SAGE ITD – SAGE4, Geared Turbo Fan

High-Speed Low Pressure Turbine Mid Turbine Frame PW1000G Donor Engine High Pressure Compressor Concept DR Mar. 2010 Critical DR Sep. 2011 Initial Concept Design Concept Definition & Concept Studies Concept Optimization Detail Design Manufacture Assy and Test Fan Drive Gear System Project launch 1 June 2008 Prelim. DR Dec. 2010 Project completion 2014 Turbine Exhaust Case 10 10/16

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

Advanced Geared Turbo Fan Challenges

New High Efficient High Pressure Compressor Efficiency & Performance Mid Turbine Frame with aggressive Interduct Innovative Designs & Mfg Processes Advanced Fan Drive Gear System Weight & Mech. Integration New High Speed Low Pressure Turbine Engine Control & Power System Temps & Materials New Lightweight Exhaust Frame

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

SAGE ITD – SAGE5, Turboshaft engine

Innovative Core Engine Preliminary DR Feb. 2009 Airframer requirements and installations Engine test Sept 2012 Turboshaft engine development → full-scale engine demonstration Demo spec.

Prelim. design Partner selection Detail design Manufacture Build and test Project launch 1 Sept 2009 Critical DR July 2011 Project completion 2014

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

Built and test 12 12/16

Call 8 Topics

JTI-CS-SAGE

JTI-CS-SAGE-01

JTI-CS-2011-1-SAGE-01-001

JTI-CS-SAGE-02

JTI-CS-2011-1-SAGE-02-08 JTI-CS-2011-01-SAGE2-02-06 JTI-CS-2011-1-SAGE2-2011-07

JTI-CS-SAGE-03

JTI-CS-2011-1-SAGE-03-009 JTI-CS-2011-01-SAGE-03-010 JTI-CS-2011-01-SAGE-03-011

JTI-CS-SAGE-04

JTI-CS-2011-01-SAGE-04-009 JTI-CS-2011-01-SAGE-04-010 JTI-CS-2011-01-SAGE-04-011 JTI-CS-2011-01-SAGE-04-012 JTI-CS-2011-01-SAGE-04-013 JTI-CS-2011-01-SAGE-04-014 JTI-CS-2011-01-SAGE-04-015

JTI-CS-SAGE-05

JTI-CS-2011-1-SAGE-05-013 JTI-CS-2011-1-SAGE-05-014 JTI-CS-2011-1-SAGE-05-015

Clean Sky - Sustainable and Green Engines

Area-01 - Geared Open Rotor

Lean Burn Control System Verification Rig

Area-02 - Direct Drive Open Rotor

Propellers electrical de-icing system: reliability assessment of key technologies for high temperature electrical machines Pitch Change Mechanism key technologies maturation PCM kinematic demonstration

Area-03 - Large 3-shaft turbofan

Large 3 shaft Demonstrator – Aeroengine intake acoustic liner technology development Steel casting process advancement Advanced press forming and hardening of high strength steels

Area-04 - Geared Turbofan

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 High temperature Ni-based super alloy casting process advancement

Area-05 - Turboshaft

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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1.300.000

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

Contact us For further information: www.cleansky.eu

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

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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.

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

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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 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 Cast ability Steel casting process advancement 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 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

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

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