Sustainable and Green Engine ITD

Sustainable and Green Engine ITD

Annual Implementation Plan

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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



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2 / 24 AIP 2009 SAGE 0 17.07.2009


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



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3 / 24 AIP 2009 SAGE 1.1 17.07.2009


SAGE1.1 Open Rotor Assembly

WP No. SAGE1.1 WP Title Open Rotor Assembly


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



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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


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



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SAGE1.2 Core Engine

WP No. SAGE1.2 WP Title Core Engine


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


partner Due Date

1.2.1 Core engine down selection Rolls-Royce M12



(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



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SAGE1.3 Integration and Test

WP No. SAGE1.3 WP Title Integration and Test


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


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



(WP/Task) Due date

1.3.1 Performance bids 1.1, 1.2 M8

1.3.2 Structural models 1.1, 1.2 M10



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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



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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


Partner

2.0.1 Support to planning and steering activities Snecma



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partner Due Date

2.0B SAGE 2 Interim Review Snecma M18


(WP/Task) Due date

2.0B SAGE2 WPs reports WP2.i.j M19



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



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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


partner Due Date

2.1D Interim review Snecma M18



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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


(WP/Task) Due date

2.1A SAGE2 Demonstration Requirements Document 2.0 M16



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



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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


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


partner Due Date

M2.2B Interim reviews Snecma M18



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(WP/Task) Due date

2.2C Demonstrator sub-systems URD’s (v0 versions) WP2.1 M18



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



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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


partner Due Date

Out of the period


(WP/Task) Due date

Out of the period



Due date

Out of the period



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SAGE3.1 Turbomachinery

WP No. SAGE3.1 WP Title Turbomachinery


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


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



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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



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SAGE3.2 Structures and Systems

WP No. SAGE3.2 WP Title Structures and Systems


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


partner Due Date

3.2.1 Demonstrator technology selection Volvo/Rolls-Royce

M19



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SAGE3.3 Integration and Test

WP No. SAGE3.3 WP Title Integration and Test


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


partner Due Date

3.3.1 Demonstrator technology selection Rolls-Royce M19



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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


(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



Due Date

4.1.3 Initial Modules and Engine Modifications Concept MTU 4.3 Nov-09



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SAGE 4.2 Structures & Systems

WP No. 4.2 WP Title Structures & Systems


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


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


(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



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



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SAGE 4.3 Integration & Test

WP No. 4.3 WP Title Integration & Test


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


Partner

4.3.1 Support to planning, steering and monitoring activities MTU


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



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



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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


partner Due Date

M 5.1a Kick-off meeting (end of preliminary study phase) TM M9



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



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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


partner Due Date

M 5.2a Kick-off meeting (end of preliminary study phase) TM M9


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



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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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Sustainable and Green Engine ITD