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Sustainable and Green Engine ITD
Annual Implementation Plan
Page 1 of 24
1 / 24 AIP 2009 SAGE 0 17.07.2009
European Commission Research Directorates
Call for Proposal Topics under 2008 Annual Implementation Plan
For reference, in addition to the work outlined in the remainder of this Annual Implementation Plan for 2009, the following Calls for Proposal topics that were committed in the 2008 Annual Implementation Plan will be launched.
Excluded Tasks (for call for proposals), SAGE2 No Description Est. Cost [k€] Due Date SAGE2-2008-1
Pitch Change Mechanism – Conceptual & preliminary design activities
2500 2010
SAGE2-2008-4
Power GearBox (PGB) advanced planet bearings development
600 2012
Excluded Tasks (for call for proposals), SAGE5 No Description Est. Cost [k€] Due Date SAGE5-2009-1
Development of a thermoelectricity generator for the supply of the engine control system
1000 2011
SAGE5-2009-2
Development of a high pressure fuel pump with integrated metering system
1500 2011
SAGE5-2009-3
Development of high accuracy, low weight “Smart” sensors for pressure, position, temperature measurement
800 2011
SAGE5-2009-4
Development of sensor for the measurement of turbine engine temperature
800 2011
SAGE5-2009-5
Development of high temperature survival electronic devices for engine control systems
2000 2011
SAGE5-2009-6
Development of high power density electrical actuators with Smart electrical interfaces in severe environment
2000 2011
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 2 of 24
2 / 24 AIP 2009 SAGE 0 17.07.2009
European Commission Research Directorates
SAGE0 ITD Coordination
WP No. SAGE0 WP Title ITD Coordination
Leader Rolls-Royce Contact Mark Pacey
Statement of Work (Tasks) Description Leading partner Start End • Coordinate ITD draft budgeting Rolls-Royce M8 M9 • Coordinate ITD reporting for 2008 Rolls-Royce M8 M9 • Manage ITD interfaces to Joint Undertaking Rolls-Royce M8 M19 • Organisation and management of Consortium
Management Committee Rolls-Royce M8 M19
• Administer JU financial contributions and maintain records and financial accounts
Rolls-Royce M8 M19
• Coordinate preparation of 2010 Annual Implementation Plan
Rolls-Royce M14 M16
• Coordinate 2010 Grant Agreement Annex 1b preparation.
Rolls-Royce M15 M18
Milestones No. Title Leading
partner Due Date
0.1 Deliver reports for 2008 Grant Agreement. Rolls-Royce M9
0.2 Deliver draft ITD budget for 2010. Rolls-Royce M9
0.3 Deliver Annual Implementation Plan for 2010 Rolls-Royce M16
0.4 Deliver 2010 SAGE Grant Agreement Annex 1b Rolls-Royce M18
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 3 of 24
3 / 24 AIP 2009 SAGE 1.1 17.07.2009
European Commission Research Directorates
SAGE1.1 Open Rotor Assembly
WP No. SAGE1.1 WP Title Open Rotor Assembly
Leader Rolls-Royce Contact Mark Pacey
Statement of Work (Tasks) Description Leading partner Start End • Integrate and manage planning of the open rotor
assembly development. Rolls-Royce M8 M19
• Continue transmissions system trade studies and develop specifications for sub-systems.
Rolls-Royce M8 M19
• Initial studies to understand capability requirements for propeller system.
Rolls-Royce M8 M19
• Complete initial hot rotating plug studies. Rolls-Royce M8 M19 • Continue development of noise prediction methods
for open rotor engines. Rolls-Royce M8 M19
• Determine need for rig testing and develop rig testing strategy. Complete strip and inspection of Rig 145 open rotor aerodynamic rig.
Rolls-Royce M8 M19
Subcontract Tasks No. Title Responsible
Partner
1.1.1 Analytical methods development to predict open rotor noise Rolls-Royce
1.1.2 Strip and inspection of Rig 145 open rotor aerodynamic rig Rolls-Royce
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 4 of 24
4 / 24 AIP 2009 SAGE 1.1 17.07.2009
European Commission Research Directorates
Excluded Tasks (for call for proposals) No Description Est. Cost [k€] Due Date 1.1.1.5 Open rotor assembly bearings manufacture 1000 2011
1.1.2.1 Propeller system development 9000 2011
Milestones No. Title Leading
partner Due Date
1.1.1 Issue rig test strategy Rolls-Royce M12
1.1.2 Issue noise measurement system specifications Rolls-Royce M13
1.1.3 Propeller system critical capability acquisition review Rolls-Royce M16
1.1.4 Outline overall transmissions concept. Rolls-Royce/ Volvo
M17
1.1.5 Outline transmissions manufacturing concepts. Rolls-Royce/ Volvo
M17
1.1.6 Concept Design Review Rolls-Royce M19
Inputs needed (Deliverables from other WP/Tasks) No. Title From
(WP/Task) Due date
1.1.1 Basic flight cycle loads, local proof / ultimate loads, fatigue loads, component deflections, component stiffness.
1.3 M10
1.1.2 Confirmation of concept engine architecture 1.3 M13
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 5 of 24
5 / 24 AIP 2009 SAGE1.2 17.07.2009
European Commission Research Directorates
SAGE1.2 Core Engine
WP No. SAGE1.2 WP Title Core Engine
Leader Rolls-Royce Contact Mark Pacey
Statement of Work (Tasks) Description Leading partner Start End • Confirm selection of suitable donor core engine Rolls-Royce M8 M11 • Define necessary modifications to donor core and outline
design solutions Rolls-Royce/ITP/Volvo
M8 M19
• Define requirement specification for low pressure turbine and outline design solutions
Rolls-Royce M8 M19
• Define requirement specification for integrated demonstrator control system and develop controls concept
Rolls-Royce M8 M19
Milestones No. Title Leading
partner Due Date
1.2.1 Core engine down selection Rolls-Royce M12
1.2.2 Concept Design Review Rolls-Royce M19
Inputs needed (Deliverables from other WP/Tasks) No. Title From
(WP/Task) Due date
1.2.1 Basic flight cycle loads, local proof / ultimate loads, fatigue loads, component deflections, component stiffness.
1.3 M10
1.2.2 Gas temperatures in zones around the core engine 1.3 M10
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 6 of 24
6 / 24 AIP 2009 SAGE1.3 17.07.2009
European Commission Research Directorates
SAGE1.3 Integration and Test
WP No. SAGE1.3 WP Title Integration and Test
Leader Rolls-Royce Contact Mark Pacey
Statement of Work (Tasks) Description Leading partner Start End • Provide engine performance related specification
and requirements for FTB demonstrator Airbus M8 M10
• Develop specification for the demonstrator Rolls-Royce M8 M10 • Develop whole engine design concept Rolls-Royce M8 M19 • Develop and maintain whole engine models,
distribute loads and temperatures to work packages Rolls-Royce M8 M19
• Define externals interfaces and mount system Rolls-Royce M8 M19 • Develop initial test and instrumentation
requirements and demonstrator test strategy Rolls-Royce M8 M19
• Perform preliminary integration studies for regional aircraft
Alenia, Rolls-Royce M12 M19
Milestones No. Title Leading
partner Due Date
1.3.1 Define performance model Rolls-Royce M9
1.3.2 Test requirements review Rolls-Royce M12
1.3.3 Define whole engine general arrangement Rolls-Royce M14
1.3.5 Concept Design Review Rolls-Royce M19
Inputs needed (Deliverables from other WP/Tasks) No. Title From
(WP/Task) Due date
1.3.1 Performance bids 1.1, 1.2 M8
1.3.2 Structural models 1.1, 1.2 M10
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 7 of 24
7 / 24 AIP 2009 SAGE1.3 17.07.2009
European Commission Research Directorates
Deliverables (Outputs to other WP/Tasks) No. Title Leading
partner To (WP/Task)
Due date
1.3.1 Demonstrator general arrangement Rolls-Royce 1.1, 1.2 M10
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 8 of 24
8 / 24 AIP SAGE2.0 17.07.2009
European Commission Research Directorates
SAGE2.0 Project Management
WP No. SAGE2.0 WP Title Project Management
Leader Snecma Contact Arnaud Lebrun
Statement of Work (Tasks) Description Leading partner Start End • Project Planning
? Implementation Agreements follow-up
? Demonstration set-up
? Development Plan set-up
? Steering tools implementation
? Technical documentation set-up
? Interim Review set-up
Snecma M8 M19
• Project Steering
? Project coordination
? Deliveries management
? Milestones management
? Risk management
? Technical requirements management
? Technical design management
? Reporting
Snecma M8 M19
Subcontract Tasks No. Title Responsible
Partner
2.0.1 Support to planning and steering activities Snecma
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 9 of 24
9 / 24 AIP SAGE2.0 17.07.2009
European Commission Research Directorates
Milestones No. Title Leading
partner Due Date
2.0B SAGE 2 Interim Review Snecma M18
Inputs needed (Deliverables from other WP/Tasks) No. Title From
(WP/Task) Due date
2.0B SAGE2 WPs reports WP2.i.j M19
Deliverables (Outputs to other WP/Tasks) No. Title Leading
partner To (WP/Task)
Due date
2.0F SAGE2 Management Plan Snecma SAGE2 M13
2.0G SAGE2 Demonstration Requirements Document Snecma WP2.1 M16
2.0H SAGE 2 Annual report Snecma SAGE Coordinator
M19
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 10 of 24
10 / 24 AIP SAGE2.1 17.07.2009
European Commission Research Directorates
SAGE2.1 Demonstrator Integration & Systems Development
WP No. SAGE2.1 WP Title Demonstrator Integration & Systems Development
Leader Snecma Contact Alain Mazelet
Statement of Work (Tasks) Description Leading partner Start End • Work Package management Snecma M8 M19 • Prosecution of Demonstrator & Demonstrator sub-
systems design processes & tools implementation Snecma M8 M19
• Prosecution of Demonstrator models construction (Performance model, WEM, …)
Snecma M8 M19
• Demonstrator requirements specification Snecma & Airbus France
M8 M19
• FTB – Demonstrator integration Snecma & Airbus France
M8 M19
• Prosecution of Demonstrator conceptual design Snecma M8 M19
• Demonstrator sub-systems & modules requirements specification
Snecma M8 M19
• Prosecution of sub-systems conceptual design Snecma, Hispano-Suiza, Techspace Aero
M16 M19
• Prosecution of sub-systems equipments requirements specification
Snecma, Hispano-Suiza, Techspace Aero
M14 M19
• Regional aircraft - CROR integration Snecma & Alenia Aeronautica
M17 M19
Milestones No. Title Leading
partner Due Date
2.1D Interim review Snecma M18
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 11 of 24
11 / 24 AIP SAGE2.1 17.07.2009
European Commission Research Directorates
Excluded Tasks (for call for proposals) No Description Est. Cost [k€] 2.1.1 Pitch Actuation System equipments, motor & sensor design activities 400
2.1.2 Pitch Actuation System equipments, reductor design activities 800
2.1.3 Design, computation and drawing of lubrication system equipment 660
2.1.4 Performance and qualification tests of lubrication system equipment 240
2.1.5 Manufacturing and Participation to detailed design and test of heat exchanger 400
Inputs needed (Deliverables from other WP/Tasks) No. Title From
(WP/Task) Due date
2.1A SAGE2 Demonstration Requirements Document 2.0 M16
Deliverables (Outputs to other WP/Tasks) No. Title Leading
partner To (WP/Task)
Due date
2.1F Demonstrator URD (v0 version) Airbus France
2.0 & 2.1 M16
2.1G Demonstrator SRD (v0 version) Snecma 2.0, 2.1 & 2.2 M18
2.1H Demonstrator SDD (v0 version) Snecma 2.0, 2.1 & 2.2 M18
2.1I Demonstrator sub-systems URD’s (v0 versions) Snecma 2.0, 2.1 & 2.2 M18
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 12 of 24
12 / 24 AIP SAGE2.2 17.07.2009
European Commission Research Directorates
SAGE2.2 Engine Modules & Nacelle Development
WP No. SAGE2.2 WP Title Engine Modules & Nacelle Development
Leader Snecma Contact Jean-Marc Cailleau
Statement of Work (Tasks) Description Leading partner Start End • Work package management Snecma M8 M19 • Prosecution of Demonstrator modules & nacelle
design processes & tools implementation Snecma, Aircelle, Avio, Volvo Aero, Alenia Aermacchi, CfP Partners
M8 M19
• Support to Demonstrator conceptual design Snecma, Aircelle, Avio, Volvo Aero, Alenia Aermacchi, CfP Partners
M8 M19
• CRT initial overall assessment Snecma, Avio M8 M19 • Prosecution of PGB conceptual design Avio M8 M19 • Prosecution of Demonstrator modules & nacelle
components conceptual design Snecma, Aircelle, Avio, Volvo Aero, Alenia Aermacchi, CfP Partners
M8 M19
• PGB components technology development Avio, CfP Partners M8 M19
Subcontract Tasks No. Title Responsible
Partner
2.2.1 Demonstrator concepts technical assessments (behaviour and features) Snecma
2.2.2 Demonstrator sub-systems technical assessments (behaviour and features) Snecma
2.2.3 PGB technology development and concept technical assessment Avio
2.2.4 Turbine concept technical assessment Avio
Milestones No. Title Leading
partner Due Date
M2.2B Interim reviews Snecma M18
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 13 of 24
13 / 24 AIP SAGE2.2 17.07.2009
European Commission Research Directorates
Inputs needed (Deliverables from other WP/Tasks) No. Title From
(WP/Task) Due date
2.2C Demonstrator sub-systems URD’s (v0 versions) WP2.1 M18
Deliverables (Outputs to other WP/Tasks) No. Title Leading
partner To (WP/Task)
Due date
2.2E Demonstrator sub-systems SDD & CDD’s (v0 versions)
Snecma, Aircelle, Avio, Volvo Aero, Alenia Aermacchi, CfP Partners
2.0 & 2.1 M18
2.2F WP’s annual reports Snecma, Aircelle, Avio, Volvo Aero, Alenia Aermacchi, CfP Partners
2.0 M19
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 14 of 24
14 / 24 AIP 2009 SAGE2.3 17.07.2009
European Commission Research Directorates
SAGE2.3 Ground Tests
WP No. SAGE2.3 WP Title Ground Tests
Leader Snecma Contact Alain Mazelet
Statement of Work (Tasks) Description Leading partner Start End Not starting in 2009 Snecma M49 M60
Milestones No. Title Leading
partner Due Date
Out of the period
Inputs needed (Deliverables from other WP/Tasks) No. Title From
(WP/Task) Due date
Out of the period
Deliverables (Outputs to other WP/Tasks) No. Title Leading
partner To (WP/Task)
Due date
Out of the period
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 15 of 24
15 / 24 AIP 2009 SAGE3.1 17.07.2009
European Commission Research Directorates
SAGE3.1 Turbomachinery
WP No. SAGE3.1 WP Title Turbomachinery
Leader Rolls-Royce Contact Mark Pacey
Statement of Work (Tasks) Description Leading partner Start End • Develop a specification for low weight, low cost LPT for
high bypass ratio turbofans. ITP/Rolls-Royce M8 M11
• Manufacturing and mechanical evaluation of titanium aluminide for turbine blades
ITP/Rolls-Royce M8 M19
• Develop LPT concepts to deliver specification. ITP M12 M15 • Identify technology demonstration requirements necessary
to deliver LPT concepts. ITP M12 M15
• Select LPT concepts for demonstration applicable to selected demonstrator engine.
ITP/Rolls-Royce M16 M18
Milestones No. Title Leading
partner Due Date
3.1.1 Capability review for titanium aluminide turbine blades Rolls-Royce M14
3.1.2 Machining review for titanium aluminide turbine blades Rolls-Royce M19
3.1.3 Demonstrator technology selection ITP/Rolls-Royce
M19
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 16 of 24
16 / 24 AIP 2009 SAGE3.1 17.07.2009
European Commission Research Directorates
Subcontract Tasks No. Title Responsible
Partner
3.1.1 TiAl casting development Rolls-Royce
3.1.2 TiAl casting process modelling Rolls-Royce
3.1.3 Refractory development for TiAl casting Rolls-Royce
3.1.4 Development of a TiAl casting process model for centrifugal casting Rolls-Royce
3.1.5 TiAl fatigue threshold and crack growth rate measurement Rolls-Royce
3.1.6 TiAl batch to batch variation assessment Rolls-Royce
3.1.7 Machining of TiAl testbars for mechanical evaluation Rolls-Royce
3.1.8 Hot isostatic pressing and heat treatment of TiAl blades and testbars Rolls-Royce
3.1.9 TiAl machining capability assessment Rolls-Royce
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 17 of 24
17 / 24 AIP 2009 SAGE3.2 17.07.2009
European Commission Research Directorates
SAGE3.2 Structures and Systems
WP No. SAGE3.2 WP Title Structures and Systems
Leader Rolls-Royce Contact Mark Pacey
Statement of Work (Tasks) Description Leading partner Start End • Develop a specification for a low weight, aerodynamically
efficient intercase integrated within the compression system for high bypass ratio turbofans.
Volvo/Rolls-Royce
M8 M11
• Develop intercase concepts to deliver specification. Volvo M12 M15 • Identify technology demonstration requirements necessary
to deliver intercase concepts. Volvo M12 M15
• Select intercase concepts for demonstration applicable to selected demonstrator engine.
Volvo/Rolls-Royce
M16 M18
Milestones No. Title Leading
partner Due Date
3.2.1 Demonstrator technology selection Volvo/Rolls-Royce
M19
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 18 of 24
18 / 24 AIP 2009 SAGE3.3 17.07.2009
European Commission Research Directorates
SAGE3.3 Integration and Test
WP No. SAGE3.3 WP Title Integration and Test
Leader Rolls-Royce Contact Mark Pacey
Statement of Work (Tasks) Description Leading partner Start End • Select baseline engine and conduct baseline engine
modelling and assessment Rolls-Royce M8 M14
• Develop potential requirements of a large engine demonstrator
Rolls-Royce M8 M10
• Develop range of demonstrator concepts to fulfil requirements
Rolls-Royce /Volvo/ITP
M10 M14
• Undertake whole engine performance and mechanical modelling of concepts
Rolls-Royce M14 M19
• Review concepts and select technologies for demonstration Rolls-Royce M18 M19
Milestones No. Title Leading
partner Due Date
3.3.1 Demonstrator technology selection Rolls-Royce M19
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 19 of 24
19 / 24 AIP 2009 SAGE4.1 17.07.2009
European Commission Research Directorates
SAGE4.1 Engine Modules
WP No. 4.1 WP Title Engine Modules
Leader MTU Contact Peter Taferner
Statement of work (Tasks) Description Leading partner Start End • Plan, manage and coordinate provision of new HPC,
LPT and adaptation of the donor engine MTU Jan-09 Dec-09
• Provide HPC concept design MTU Mar-09 Dec-09 • Provide HS-LPT concept design MTU Jan-09 Dec-09 • Provide Engine Modifications Concept MTU Jan-09 Dec-09
Milestones No. Title Leading partner Due
Date
4.1.3 Initial Modules and Engine Modifications Concept Design Review
MTU Nov-09
Inputs needed (Deliverables from other WP/Tasks) No. Title From
(WP/Task) Due Date
4.3.1 Geared fan demonstrator requirements study 4.3 Jul-09 4.3.2 Initial geared fan demonstrator concept 4.3 Sep-09
Deliverables (Outputs to other WP/Tasks) No. Title Leading
partner To (WP/Task)
Due Date
4.1.3 Initial Modules and Engine Modifications Concept MTU 4.3 Nov-09
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 20 of 24
20 / 24 AIP 2009 SAGE4.3 17.07.2009
European Commission Research Directorates
SAGE 4.2 Structures & Systems
WP No. 4.2 WP Title Structures & Systems
Leader MTU Contact Peter Taferner
Statement of work (Tasks) Description Leading partner Start End • Plan, manage and coordinate provision of new fan
drive gear system, mid turbine frame and controls and power system
MTU Jan-09 Dec-09
• Initiation of Fan Drive Gear System (FDGS)Concept Design AVIO May-09 Dec-09
• Provide Mid Turbine Frame Concept Design VAC Jan-09 Dec-09
Milestones No. Title Leading partner Due
Date 4.2.1 Initial Advanced Fan Drive Gear System assessment AVIO Dec-09
4.2.2 Initial MTF Concept Design Review VAC Nov-09
Inputs needed (Deliverables from other WP/Tasks) No. Title From
(WP/Task) Due Date
4.3.1 Geared fan demonstrator requirements study 4.3 Jul-09 4.3.2 Initial geared fan demonstrator concept 4.3 Sep-09
Deliverables (Outputs to other WP/Tasks) No. Title Leading
partner To (WP/Task)
Due Date
4.2.1 Initial FDGS Concept Design and documentation AVIO 4.3 Dec-09
4.2.2 Initial MTF Concept Design and documentation VAC 4.3 Nov-09
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 21 of 24
21 / 24 AIP 2009 SAGE4.3 17.07.2009
European Commission Research Directorates
SAGE 4.3 Integration & Test
WP No. 4.3 WP Title Integration & Test
Leader MTU Contact Peter Taferner
Statement of work (Tasks) Description Leading partner Start End
• Plan, manage and coordinate whole engine design, geared fan demonstrator test and build & strip and test evaluation
MTU Jan-09 Dec-09
• Provide Geared fan demonstrator requirements MTU Jan-09 Dec-09 • Provide geared fan demonstrator concept MTU Jan-09 Dec-09
Subcontract Tasks No. Title Responsible
Partner
4.3.1 Support to planning, steering and monitoring activities MTU
Milestones No. Title Leading partner Due
Date
4.3.1 Geared fan demonstrator requirements study review MTU Jul-09
4.3.2 Initial geared fan demonstrator Concept Design Review MTU Sept-09
Deliverables (Outputs to other WP/Tasks) No. Title Leading
partner To (WP/Task)
Due Date
4.3.1 Geared fan demonstrator requirements study MTU 4.1, 4.2 July-09
4.3.2 Initial geared fan demonstrator concept and technology development plan
MTU 4.1, 4.2 Dec-09
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 22 of 24
22 / 24 AIP SAGE5.1 17.07.2009
European Commission Research Directorates
SAGE 5.1 Core Study
WP No. SAGE 5.1 WP Title Core Study
Leader Turbomeca Contact Brigitte CHEFTEL
Statement of Work (Tasks) Description Leading partner Start End
T5.1.1: Compressor, casing, IGV and air flow path design, rig test design. New coating characterisation
TM M9 M12
T5.1.2: Combustion chamber and injector (position and type) design. Rig test design study.
TM M9 M12
T5.1.3: HP turbine blades and disk design. Rig test design. New blade material characterisation
TM M9 M12
T5.1.4: LP turbine blades and disk design. Rig test design TM M9 M12
T5.1.5: Management TM M9 M12
Excluded Tasks (for call for proposals) No Description Est. Cost [k€] T5.1.1 Oxidation/corrosion resistant coatings for titanium aluminides for using on low
pressure turbine blades between 650 and 850°C 230
Milestones No. Title Leading
partner Due Date
M 5.1a Kick-off meeting (end of preliminary study phase) TM M9
Deliverables (Outputs to other WP/Tasks) No. Title Leading
partner To (WP/Task)
Due date
D5.1.1a Preliminary report on the selection of compressor TM T5.1.1 M12
D5.1.2a Preliminary report on the selection of combustors TM T5.1.2 M12
D5.1.3a Preliminary report on the selection of HP turbine TM T5.1.3 M12
D5.1.4a Preliminary report on the selection of LP turbine TM T5.1.4 M12
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 23 of 24
23 / 24 AIP SAGE5.2 17.07.2009
European Commission Research Directorates
SAGE 5.2 Whole engine study
WP No. SAGE 5.2 WP Title Whole engine study
Leader Turbomeca Contact Brigitte CHEFTEL
Statement of Work (Tasks) Description Leading partner Start End
T5.2.1: Oil system - Parts study TM M9 M12
T5.2.2: Transmission - Parts study and material choice TM M9 M12
T5.2.3: Low noise device - Parts study TM M9 M12
T5.2.4: More electrical AGB - Parts study TM M9 M12
T5.2.5: Control system - Parts study TM / partners? M9 M12
T5.2.6: Exhaust - Parts study TM M9 M12
T5.2.7: Contra rotative architecture - Parts design TM M9 M12
T5.2.8: Management TM M9 M12
Excluded Tasks (for call for proposals) No Description Est. Cost [k€] T5.2.1 Design and feasibility of air intake and gear box static parts made of organic matrix
composite 230
Milestones No. Title Leading
partner Due Date
M 5.2a Kick-off meeting (end of preliminary study phase) TM M9
Deliverables (Outputs to other WP/Tasks) No. Title Leading
partner To
(WP/Task) Due date
D5.2.1a Preliminary study report on the oil system TM T5.2.1 M12
D5.2.2a Preliminary study report on the transmission TM T5.2.2 M12
D5.2.3a Preliminary study report on the Low noise device TM T5.2.3 M12
D5.2.4a Preliminary study report on the More electrical AGB TM T5.2.4 M12
Sustainable and Green Engine ITD
Annual Implementation Plan
Page 24 of 24
24 / 24 AIP SAGE5.2 17.07.2009
European Commission Research Directorates
No. Title Leading partner
To (WP/Task)
Due date
D5.2.5a Preliminary study report on the Control system TM T5.2.5 M12
D5.2.6a Preliminary study report on the Exhaust TM T5.2.6 M12
D5.2.7a Preliminary study report on the Contra rotative architecture
TM T5.2.7 M12
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