Clean SkySustainable and Green Engine ITD

TAKE OFF

Informationsveranstaltung

zu Ausschreibungen

nationaler und europäischer

Luftfahrtforschungsprogramme

Michel GOULAIN, SAGE

Project Officer

June 1st, 2010, Vienna

2

Clean Sky JTI – Activities & DeliveriesClean Sky JTI – Activities & Deliveries

Impact

Assessment

Concept

Studies

Technology

Demonstration

3

Clean Sky JTI – Engine related Activities& DeliveriesClean Sky JTI – Engine related Activities& Deliveries

ATMS T-Dem.

Engine T-Dem.

A/C T-Dem.

A/C S/S T-Dem.

Engine Concepts

A/C Concepts

A/C S/S Concepts

ATMS Concepts

A/C Techno.

A/C S/S Techno.

Engine Techno.

ATMS Techno.

Impacts

Engine C-Stud.

A/C S/S C-Stud.

ATMS C-Stud.

A/C C-Stud.

Impact Assess.

Note : CS supporting processes (tools development, …) supposed as included in represented processes

4

Clean Sky JTI – Engines Activities over ITDs & TE Clean Sky JTI – Engines Activities over ITDs & TE

Smart

Fixed

Wing

Aircraft

(SFWA)

Green

Rotor-

Craft

(GRC)

Sustainable

And

Green

Engine

(SAGE)

System

for

Green

Operations

(SGO)

Eco-

Design

(ED)

Clean Sky Technical Bodies

Technology

Evaluator

(TE)

Green

Regional

Aircraft

(GRA)

5

SAGE Integrated TechnologyDemonstrator (ITD) SAGE Integrated TechnologyDemonstrator (ITD)

Smart

Fixed

Wing

Aircraft

(SFWA)

Green

Rotor-

Craft

(GRC)

Sustainable

And

Green

Engine

(SAGE)

System

for

Green

Operations

(SGO)

Eco-

Design

(ED)

Clean Sky Technical Bodies

Technology

Evaluator

(TE)

Green

Regional

Aircraft

(GRA)

6

SAGE ITD – 4 Engine Concepts, 5 DemonstrationsSAGE ITD – 4 Engine Concepts, 5 Demonstrations

Geared Pusher

Counter-Rotating Open Rotor

Direct Drive Pusher

Counter-Rotating Open Rotor

Advanced

Large 3-shaft Turbofan

Advanced

Geared Turbofan

Advanced

Turboshaft

SA

GE

5

SAGE 1 SAGE 2

SA

GE

3

SAGE 4

7

SAGE ITD – Time ScheduleSAGE ITD – Time Schedule

Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4

SAGE1

Geared Open Rotor

SAGE2

Direct Drive Open Rotor

SAGE3

Large 3-shaft Turbofan

SAGE4

Geared Turbofan

SAGE5

Turboshaft

2014 20152008 2009 2010 2011 2012 2013

Concept Studies

Preliminary Design

Detail Design

Build/Test

Manufacturing

Concept Studies

Prel.

Detail

Build/Test

Manufacturing

Concept

Preliminary Design

Detail

Test 1

Manufacturing

Test 2

Concept Studies

Prel.Design

Detail Design

Build/Test

Manufacturing

Preliminary Design

Detail Design

Build/Test

M‘ing

PDRPDR

PDRPDR

PDRPDR

PDRPDR

PDRPDR

CDRCDR

CDRCDR

CDRCDR

CDRCDR

CDRCDR

CoDRCoDR

CoDRCoDR

CoDRCoDR

CoDRCoDR

RigTest

Int.DRInt.DR

8

SAGE ITD – MembershipSAGE ITD – Membership

� Clean Sky Members

�Clean Sky Leaders :

�Clean Sky Associates :

� Clean Sky Partners

�From Call for Proposals (CfP) #1 :

�From coming CfPs : …

9

SAGE ITD – SAGE1, Geared Open Rotor SAGE ITD SAGE ITD –– SAGE1, SAGE1, GearedGeared Open Rotor Open Rotor

Intercase, inc, mount

Rear rotating structure

BR715 core gas

generator core

Open rotor assemblyTest Programme

LPC BoosterAirframer requirements

and installations

Project launch1 June 2008

Project completion2014

Prelim. DRJune 2011

Concept DRNov. 2009

Concept studies

Demo spec.

Prelim. design

Partner selection

Detail design

Manufacture

Build and

test

Critical DRSept. 2012

Open rotor technology development → full-scale engine demonstration

10

SAGE ITD – SAGE2, Direct Drive Open Rotor SAGE ITD SAGE ITD –– SAGE2, Direct Drive Open SAGE2, Direct Drive Open Rotor Rotor

Rotating structure

Shafts

Modules, sub-systems, nacelle

items

Design integration, assembly

Test Programme

Power Turbine items

PGB for alternate

architecture

Airframer requirements

and installations

Project launch1 June 2008

Project completion2013

Prelim. DRJune 2011

Interim ReviewNov. 2009

Concept studies

Demo spec.

Prelim. design

Partner selection

Detail design

Manufacture

Build and

test

Critical DRDec. 2011

Open rotor technology development → full-scale engine demonstration

Concept DRSept. 2010

Nacelle items

Pitch Change

Mechanism

PGB

Bearings

11

SAGE ITD – SAGE3, Large 3-shaftDemonstratorSAGE ITD SAGE ITD –– SAGE3, Large 3SAGE3, Large 3--shaftshaftDemonstratorDemonstrator

Lightweight intercase

structures, material

characterisation and

manufacturing technologies

Trent 1000 core engine

Composite fan system

Integrated installations

Test programme

LP Turbine and

structures

Project launch1 Jan. 2009

Build 2 engine test

2013

Prelim. DRMarch 2011

Concept DRDec. 2009

Concept studiesTechnology

selection for demonstration

Prelim. DesignProcess

developmentPartner selection

Detail designManufacture

Rig testing

Phased build and technology

demonstration

Critical DRSept. 2011

Build 1 engine test

2012

12

SAGE ITD – SAGE4, Geared Turbo Fan SAGE ITD SAGE ITD –– SAGE4, SAGE4, GearedGeared Turbo Fan Turbo Fan

Mid Turbine

Frame

Project launch1 June 2008

Project completion2013

Prelim. DRDec. 2010

Concept DRMar. 2010

Initial Concept Design

Concept Definition & Concept Studies

Detail DesignManufacture

Assy and

Test

Critical DRSept. 2011

HPCFan Drive

Gear SystemHigh-Speed

LPT

Concept

Optimization

existing commercial

Geared Turbo Fan

13

SAGE ITD – SAGE5, Turboshaft engineSAGE ITD SAGE ITD –– SAGE5, Turboshaft SAGE5, Turboshaft engineengine

Innovative Core Engine

Project launch1 Jan. 2009

Project completion2013

Critical DRJuly 2011

Preliminary DRJan. 2010

Demo spec.Prelim. design

Partner selection

Detail design

Manufacture

Build and

test

Engine testSept 2012

Turboshaft engine development → full-scale engine demonstration

Built and testAirframer requirements

and installations

14

SAGE ITD Associates – Volvo AeroSAGE ITD Associates – Volvo Aero

SAGE 1 SAGE 2 SAGE 3 SAGE 4

Manufacturing process simulation of welding

�Volvo Aero focus on design,

development and manufacturing of

complex lightweight static and rotating structures.

�Advanced manufacturing and

manufacturing process simulation technologies developed in FP5 and FP6

projects are a key to success.

Intermediate Compressor

Case

Mid Turbine Frame

Complex rotating parts

Rear Rotating StructureIntermediate

Case

15

SAGE ITD Associates - ITP SAGE ITD Associates - ITP

SAGE 1 SAGE 3

�ITP’s contribution in SAGE 1 is design,

development and manufacturing of the ORD booster.

�In SAGE3 ITP contributes in technology

development for Low Weight Efficient Low Pressure turbines.

ORD booster

Low Pressure Turbine

16

SAGE ITD Associates - AVIO SAGE ITD Associates - AVIO

�AVIO’s key contribution to SAGE is technology

development focused to highly efficient and

reliable Lower Pressure Turbine and Power Gearbox, both considered core items of future

engine architectures

�Technological effort is based on FP5, FP6 and FP7 projects, continuous improvement and

excellence partnership network

SAGE 2 SAGE 4

Low Pressure Turbine

Fan DriveGear System

Power Gearbox

17CleanSky SFWA-ITD, Vienna 01st June 2010

SAGE-ITD Call for Proposal Topics OverviewSAGESAGE--ITD ITD CallCall forfor ProposalProposal Topics Topics OverviewOverview

In the total project lifetime the SAGE-ITD expect to contribute in CleanSkyCall for Proposals (CfP) on

�100 – 200 topics

�Total value of topics ~ 100M€

In the current calls Industry, Research Establishments and Universitiesare invited to check your interest and to reply upon

Call #2 – 2010 (30.March 2010 – 30.June 2010 (17:00))

�0 topic

Call #3 – 2010 (28.April 2010 – 20.July 2010 (17:00))

�4 topics

�Total value of topics ~ 12.5 M€

18

SAGE-ITD Call for Proposal Topics in Call#3 2010SAGESAGE--ITD ITD CallCall forfor ProposalProposal Topics in Call#3 2010Topics in Call#3 2010

JTI-CS-SAGE 4 12.500.000 9.375.000

JTI-CS-SAGE-01

JTI-CS-SAGE-02

JTI-CS-SAGE-03 10.000.000

JTI-CS-2010-3-SAGE-03-002 10.000.000JTI-CS-SAGE-04

JTI-CS-SAGE-05 2.500.000

JTI-CS-2010-3-SAGE-05-002 1.200.000

JTI-CS-2010-3-SAGE-05-003 1.100.000

JTI-CS-2010-3-SAGE-05-004 200.000

Development of a Wasted Heat Regeneration System (WHRS)

Area-01 - Geared Open Rotor

Clean Sky - Sustainable and Green Engines

Area-02 - Direct Drive Open Rotor

Development of exhaust noise attenuation technologies

Development of an advanced system for pollutant measurement

Area-05 - Turboshaft

Aeroengine intake technology development

Area-03 - Large 3-shaft turbofan

Area-04 - Geared Turbofan

Identification topics VALUE MAX FUNDITD - AREA - TOPIC

19

CleanSky SFWA-ITD, Vienna 01st June 2010

JTI CleanSkyJTI JTI CleanSkyCleanSky

Vielen Dank für Ihre

Aufmerksamkeit

20

CleanSky SFWA-ITD, Vienna 01st June 2010

JTI CleanSkyJTI JTI CleanSkyCleanSky

© 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.