Sustainable and Green Engine ITD -...

Sustainable and Green Engine ITD

2010 Annual Implementation Plan

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1 / 31 AIP 2009 SAGE 0 27.01.2010

European Commission Research Directorates

SAGE0 ITD Coordination

WP No. SAGE0 WP Title ITD Coordination

Leader Snecma Contact Arnaud Lebrun

Statement of Work (Tasks) Description Leading

partner Start End

• Coordinate ITD draft budgeting Snecma Jan. 2010 Feb. 2010 • Coordinate ITD reporting for 2009 Snecma Jan. 2010 Feb. 2010 • Manage ITD interfaces to Joint Undertaking Snecma Jan. 2010 Dec. 2010 • Organisation and management of Consortium

Management Committee Snecma Jan. 2010 Dec. 2010

• Administer JU financial contributions and maintain records and financial accounts

Snecma Jan. 2010 Dec. 2010

• Coordinate preparation of 2011 Annual Implementation Plan

Snecma Jan. 2010 Mar. 2010

• Coordinate 2011 Grant Agreement Annex 1b preparation.

Snecma Feb. 2010 May. 2010

Milestones No. Title Leading

partner Due Date

0.1 Deliver reports for 2009 Grant Agreement. Snecma Feb. 2010

0.2 Deliver draft ITD budget for 2011. Snecma Feb. 2010

0.3 Deliver Annual Implementation Plan for 2011 Snecma Mar. 2010

0.4 Deliver 2011 SAGE Grant Agreement Annex 1b Snecma May 2010


Annual Implementation Plan

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2 / 31 AIP 2009 SAGE 1.1 27.01.2010


SAGE1.1 Open Rotor Assembly

WP No. SAGE1.1 WP Title Open Rotor Assembly

Leader Rolls-Royce Contact Mark Pacey


partner Start End

• Integration and management of open rotor assembly development.

Rolls-Royce Jan. 2010 Dec. 2010

• Propeller system concept selection, preparation and management of Call for Proposal topic

Rolls-Royce Jan. 2010 June 2010

• Preliminary design, analysis and lifing of front rotating structure. Initial manufacturing trials and procurement of long lead forgings and manufacturing tooling.

Rolls-Royce Jan. 2010 Oct. 2010

• Preliminary design, analysis and lifing of rear rotating structure.

VAC Jan. 2010 Oct. 2010

• Development of near field and en route noise prediction methods.

Rolls-Royce Jan. 2010 Dec. 2010

• Complete strip and inspection of open rotor aerodynamic rig.

Rolls-Royce Sep. 2010 Dec. 2010

• PCM (Pitch Control Mechanism) rig concept design

Rolls-Royce Jan 2010 June 2010

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 open rotor blade aerodynamic rig Rolls-Royce



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Indicative Excluded Tasks (for call for proposals) No Description SAGE-01-001 CROR Rotor blade and hub system development

SAGE-01-002 Open rotor assembly bearings manufacture

SAGE-01-003 Thin-walled and shell structures

SAGE-01-004 Cold rotating structures

SAGE-01-005 Communications components for dynamic interfaces in harsh high altitude environments

SAGE-01-006 Sensor and effector components for harsh high altitude environments

SAGE-01-007 Integrated multi-function sensors


partner Due Date

1.1.1 Preliminary Design Review Rolls-Royce Oct. 2010

1.1.2 Open rotor near field source assessment Rolls-Royce May 2010

1.1.3 Open rotor duct path validation rig Rolls-Royce June 2010

1.1.4 Blade aero rig strip complete Rolls-Royce Dec. 2010

1.1.5 Pitch Control Mechanism rig concept defined Rolls-Royce July 2010

1.1.6 Deliver and machine forgings for trial manufacture (FRS) Rolls-Royce July 2010

Inputs needed (Deliverables from other WP/Tasks) No. Title From

(WP/Task) Due date

1.1.1 Preliminary flight cycle loads, local proof / ultimate loads, fatigue loads, component deflections, component stiffness.

1.3 Aug. 2010

1.1.2 Open rotor duct path definition 1.3 Mar. 2010

Deliverables (Outputs to other WP/Tasks) No. Title Leading

partner To (WP/Task)

Due date

1.2.1 Open rotor assembly preliminary design Rolls-Royce 1.3 May 2010

1.2.2 Preliminary propeller system control requirements

Rolls-Royce 1.2 May 2010



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4 / 31 AIP 2009 SAGE1.2 27.01.2010


SAGE1.2 Core Engine

WP No. SAGE1.2 WP Title Core Engine



partner Start End

• Procure and assess condition of donor core engine. Develop repair and refurbishment plan.

Rolls-Royce Jan. 2010 June 2010

• Preliminary design of core engine modifications and procurement of long lead materials.

Rolls-Royce, Volvo

Jan. 2010 Sep. 2010

• Preliminary design and analysis of core engine booster. Planning for procurement and manufacture.

ITP Jan. 2010 Oct. 2010

• Control system architecture definition, modelling and preliminary safety case assessment.



partner Due Date

1.2.1 Core engine procurement Rolls-Royce June 2010



(WP/Task) Due date

1.2.1 Preliminary propeller system control requirements 1.1 May 2010 1.2.2 Preliminary core engine interface loads and temperature

predictions 1.3 Aug. 2010



Due date

1.2.1 Core engine preliminary design including initial modification definitions




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6 / 31 AIP 2009 SAGE1.3 27.01.2010


SAGE1.3 Integration and Test

WP No. SAGE1.3 WP Title Integration and Test



partner Start End

• Integrate and manage the demonstrator project Rolls-Royce Jan. 2010 Dec. 2010 • Definition of ground test requirements to support

future flight clearance, including interface load limits, slave system interfaces and flight test instrumentation requirements.

Airbus Operations

Jan. 2010 June 2010

• Preliminary performance cycle and whole engine mechanical modelling and behaviour prediction

Rolls-Royce Jan. 2010 June. 2010

• Engine installation vibration studies and suppression system concepts

Alenia Jan. 2010 Dec. 2010

• Refinement of test and instrumentation requirements and demonstrator test strategy



partner Due Date

1.3.1 Preliminary load cycle predictions Rolls-Royce April 2010

1.3.2 Complete definition of ground test requirements to support flight clearance

Airbus Operations

June 2010


1.3.4 Complete initial open rotor engine mount studies Alenia Dec. 2010


(WP/Task) Due date

1.3.1 Preliminary open rotor assembly and core engine designs 1.1, 1.2 May 2010



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Due date

1.3.1 Preliminary flight cycle loads, local proof / ultimate loads, fatigue loads, component deflections, component stiffness

Rolls-Royce 1.1, 1.2 Aug. 2010



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8 / 31 AIP SAGE2.0 27.01.2010


SAGE2.0 Project Management

WP No. SAGE2.0 WP Title Project Management

Leader Snecma Contact Arnaud Lebrun


partner Start End

• Project Planning

○ Conceptual design phase steering

○ Preliminary design phase detailed planning

○ Subsequent phase planning

○ Reviews set-up


• Project Steering

○ Contracts management

○ Project coordination

○ Deliveries management

○ Milestones management

○ Risk management

○ Technical requirements management

○ Technical design management

○ Reporting



Partner

SC2.0.1 Support to steering, planning and steering activities Snecma


partner Due Date

M2.0C SAGE2 Concept Reviews Snecma Sep. 2010



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(WP/Task) Due date

2.0C&D SAGE2 WPs reports 2.i.j Dec. 2010



Due date

D2.0I SAGE2 Demonstration Requirements Document (update)

Snecma SAGE2 Mar. 2010

D2.0J SAGE2 Development Plan (update) Snecma SAGE2 Sep. 2010

D2.0H SAGE 2 Annual report Snecma SAGE Coordinator

Dec. 2010



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10 / 31 AIP SAGE2.1 27.01.2010


SAGE2.1 Demonstrator Integration & Systems Development

WP No. SAGE2.1 WP Title Demonstrator Integration & Systems Development

Leader Snecma Contact Alain Mazelet


partner Start End

• Work Package management Snecma Jan. 2010 Dec. 2010 • Prosecution of Demonstrator models construction

(Performance model, WEM, …) Snecma Jan. 2010 Dec. 2010

• Demonstrator requirements specification Snecma, Airbus Operations

Jan. 2010 Nov. 2010

• FTB – Demonstrator integration Snecma, Airbus Operations

Jan. 2010 Dec. 2010

• Prosecution of Demonstrator conceptual design Snecma Jan. 2010 Sep. 2010

• Initiation of Demonstrator preliminary design Snecma Sep. 2010 Dec. 2010

• Demonstrator sub-systems & modules requirements specification

Snecma Jan. 2010 Nov. 2010

• Prosecution of sub-systems conceptual design Snecma, Hispano-Suiza, Techspace Aero

Jan. 2010 Sep. 2010

• Initiation of sub-systems preliminary design Snecma, Hispano-Suiza, Techspace Aero

Sep. 2010 Dec. 2010

• Prosecution of sub-systems equipment requirements specification

Snecma, Hispano-Suiza, Techspace Aero

Jan. 2010 Nov. 2010

• Regional aircraft - CROR integration Snecma, Alenia Aeronautica

Jan. 2010 Dec. 2010



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Partner

SC2.1.1 Support to design activities Snecma

SC2.1.2 Support to design activities Hispano-Suiza


partner Due Date

M2.1E Concept Reviews Snecma Sep. 2010


(WP/Task) Due date

2.1A SAGE2 Demonstration Requirements Document 2.0 Mar. 2010



Due date

D2.1C WP’s Annual Reports Snecma 2.0 Dec. 2010

D2.1H Demonstrator SDD (v1 version) Snecma 2.0 Sep. 2010

D2.1I Demonstrator sub-systems URDs (v1 versions)

Snecma 2.0, 2.1 & 2.2 Sep. 2010

D2.1J Demonstrator CPMS SDD (v1 version) Snecma 2.0 & 2.1 Sep. 2010

D2.1K Demonstrator CPMS Equipments URDs (v1 versions)

Snecma 2.0 & 2.1 Sep. 2010

D2.1L Demonstrator LCS SDD (v1 version) Techspace Aero

2.0 & 2.1 Sep. 2010

D2.1M Demonstrator LCS Equipments URDs (v1 versions)

Techspace Aero

2.0 & 2.1 Sep. 2010

D2.1N Demonstrator PAS SDD (v1 version) Hispano-Suiza 2.0 & 2.1 Sep. 2010

D2.1O Demonstrator PAS Equipments URDs (v1 versions)

Hispano-Suiza 2.0 & 2.1 Sep. 2010



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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


partner Start End

• Work package management Snecma Jan. 2010 Dec. 2010 • Prosecution of Demonstrator modules & nacelle

design processes & tools implementation Snecma, Aircelle, Avio, Volvo Aero, Alenia Aermacchi, CfP Partners

Jan. 2010 Dec. 2010

• Support to Demonstrator conceptual design Snecma, Aircelle, Avio, Volvo Aero, Alenia Aermacchi, CfP Partner

Jan. 2010 Sep. 2010

• Support to Demonstrator preliminary design Snecma, Aircelle, Avio, Volvo Aero, Alenia Aermacchi, CfP Partner

Sep. 2010 Dec. 2010

• Prosecution of PGB conceptual design for alternate demo architecture

Avio Jan. 2010 Sep. 2010

• PGB design follow-on to support technology development

Avio Sep. 2010 Dec. 2010

• Prosecution of Demonstrator modules & nacelle components conceptual design

Snecma, Aircelle, Avio, Volvo Aero, Alenia Aermacchi, CfP Partner

Jan. 2010 Sep. 2010

• Initiation of Demonstrator modules & nacelle components preliminary design

Snecma, Aircelle, Avio, Volvo Aero, Alenia Aermacchi, CfP Partner

Sep. 2010 Dec. 2010



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Description Leading partner

Start End

• Initiation of Propellers technology development Snecma Jan. 2010 Dec. 2010 • Development of improved tools for PGB gears

reliability and innovative materials application for fatigue limits enhancement

Avio, CfP Partner

Jan. 2010 Dec. 2010


Partner


SC2.2.6 Support to design and technical assessment AVIO


partner Due Date

M2.2C Concept Reviews Snecma, Aircelle, Avio, Volvo Aero, Alenia Aermacchi, CfP Partners

Sep. 2010

Indicative Excluded Tasks (for call for proposals) No Description SAGE-02-003 PAS equipment, motor and sensor design activities

SAGE-02-004 PAS equipment reductor design activities

SAGE-02-005 Design, computation and drawing of LCS equipment

SAGE-02-006 Performance and qualification tests of LCS equipment

SAGE-02-007 Test bench for heat exchanger

SAGE-02-008 Demonstrator module development

SAGE-02-009 Development of propellers technology


(WP/Task) Due date

2.2C Demonstrator sub-systems URD’s (v1 versions) 2.1 Sep. 2010



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Due date

D2.2G Demonstrator sub-systems SRD & sub-systems parts CRD’s (v1 versions)

Snecma, Aircelle, Avio, Volvo Aero, Alenia Aermacchi, CfP Partners

2.0 & 2.1 Sep. 2010

D2.2E Demonstrator sub-systems SDD & sub-systems parts CDD’s (v1 versions)

Snecma, Aircelle, Avio, Volvo Aero, Alenia Aermacchi, CfP Partners

2.0 & 2.1 Sep. 2010

D2.2F WP’s annual reports Snecma, Aircelle, Avio, Volvo Aero, Alenia Aermacchi, CfP Partners

2.0 Dec. 2010



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SAGE2.3 Ground Tests

WP No. SAGE2.3 WP Title Ground Tests

Leader Snecma Contact Alain Mazelet


partner Start End

• Work package management Snecma Sep. 2010 Dec. 2010 • Initiation of GTB conceptual design Snecma Sep. 2010 Dec. 2010


Partner



partner Due Date

M2.3A GTB Concept Review Snecma Nov. 2010


(WP/Task) Due date

2.3A SAGE2 Demonstration Requirements Document 2.0 Mar. 2010

2.3B Demonstrator SDD (v1 version) 2.1 Sep. 2010



Due date

D2.3A GTB SRD (v0 version) Snecma 2.0 Nov. 2010

D2.3B GTB SDD (v0 version) Snecma 2.0 Nov. 2010



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16 / 31 AIP 2009 SAGE3.1 27.01.2010


SAGE3.1 Turbomachinery

WP No. SAGE3.1 WP Title Turbomachinery



partner Start End

• Concept design and studies of composite fancase, including structural and acoustic design.

Rolls-Royce Jan. 2010 May 2010

• Preparation of a Call for Proposal topic description for the delivery of a composite fancase

Rolls-Royce Jan. 2010 March 2010

• Aerodynamic and structural design and analysis of composite fan annulus fillers


• Develop a specification for composite fan annulus fillers and prepare a CfP topic description.

Rolls-Royce Jan. 2010 March 2010

• Develop instrumentation concepts for composite fan system

Rolls-Royce Aug. 2010 Dec. 2010

• Support to Call for Proposal evaluations Rolls-Royce Oct. 2010 Oct. 2010 • Develop LPT concept selected for the

demonstrator to support stage 1 exit.. ITP Jan. 2010 Nov. 2010

• Select LPT final concept for demonstrator engine. ITP/Rolls-Royec

Nov. 2010 Nov. 2010

• Strategic planning for the technologies to be validated through rig testing.

ITP Jan. 2010 Dec. 2010

• Develop an improved blade-row interaction criteria to improve turbine efficiency through rig testing.

ITP Jan. 2010 Dec. 2010


Partner

3.1.1 Manufacturing of the rig parts ITP

3.1.2 Assembly and rig testing to develop a blade-row interaction criteria ITP



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Indicative Excluded Tasks (for call for proposals) No Description SAGE-03-001 Manufacture of complex composite fan annulus fillers

SAGE-03-002 Manufacture of a composite fancase incorporating acoustic treatment


(WP/Task) Due date

3.1.1 Initial demonstrator interface definitions 3.3 Jan. 2010



Due date

3.1.1 Composite fan system performance and weight predictions


3.1.2 Composite fan system instrumentation requirements

Rolls-Royce 3.3 Nov. 2010

3.1.3 Fan system initial interface definition to inlet Rolls-Royce 3.2 July 2010

3.1.4 Initial LPT performance and weight predictions

ITP 3.3 May 2010

3.1.5 LPT instrumentation requirements ITP 3.3 Nov. 2010


partner Due Date

3.1.1 Launch of composite fancase manufacture CfP topic Rolls-Royce March 2010

3.1.2 Launch of composite fan annulus filler manufacture CfP topic Rolls-Royce March 2010

3.1.3 Provide LPT concept for demonstrator engine ITP July 2010

3.1.4 Multistage rig Pass to Test for improved blade-row interaction ITP July 2010

3.1.5 Selection of fancase and annulus filler Partners Rolls-Royce Sept. 2010

3.1.6 Concept Design Review Rolls-Royce Nov. 2010



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SAGE3.2 Structures and Systems

WP No. SAGE3.2 WP Title Structures and Systems



partner Start End

• Aerodynamic, acoustic and structural design of integrated inlet optimised to composite fan system.


• Preparation of Call for Proposal topic description for inlet detail design and manufacture

Rolls-Royce June 2010 July 2010

• Initial design of leaf seal for application to donor core engine and integration with donor engine hardware

Rolls-Royce March 2010 June 2010

• Develop validation plan for low weight, aerodynamically efficient intercase

VAC Jan. 2010 May 2010

• Preliminary design of intercase incorporating technologies for validation.

VAC Jan. 2010 Dec. 2010

Indicative Excluded Tasks (for call for proposals) No Description SAGE-03-003 Development of inlet optimised to composite fancase


(WP/Task) Due date

3.2.1 Fan system initial interface definition 3.1 July 2010



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Due date

3.2.1 Leaf seal initial interface definition proposal Rolls-Royce 3.3 May 2010

3.2.2 Dynamic characteristics of leaf seal proposal


3.2.3 Predictions of inlet impact on performance and weight


3.2.4 Intercase performance and weight predictions

VAC 3.3 May 2010


partner Due Date

3.2.1 Launch of optimised inlet Call for Proposal topic Rolls-Royce March 2010

3.2.2 Selection of inlet Partner Rolls-Royce Sept. 2010

3.2.3 Concept Design Review Rolls-Royce/ VAC

Nov. 2010



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SAGE3.3 Integration and Test

WP No. SAGE3.3 WP Title Integration and Test



partner Start End

• Integrate and manage the demonstrator project, including planning, risk management and reporting

Rolls-Royce/ ITP/VAC

Jan. 2010 Dec. 2010

• Create General Assembly of demonstrator Rolls-Royce Jan. 2010 July 2010 • Whole engine performance and structural

modelling of demonstrator and initial assessments of change impact

Rolls-Royce May 2010 Nov. 2010

• Define top level demonstrator build and test bed plan, including instrumentation and tooling requirements

Rolls-Royce June 2010 Dec. 2010

• Project review and steering Rolls-Royce/ ITP/VAC

Jan. 2010 Dec. 2010


(WP/Task) Due date

3.3.1 Performance and structural characteristic predictions for all demonstrated technologies

3.1, 3.2 May 2010



Due date

3.3.1 Donor core engine initial interface definitions

Rolls-Royce 3.1, 3.2 Jan. 2010

3.3.2 Demonstrator General Assembly Rolls-Royce 3.1, 3.2 Nov. 2010



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partner Due Date

3.3.1 Concept Design Review Rolls-Royce Nov. 2010



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22 / 31 AIP 2009 SAGE4.3 27.01.2010


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. 2010 Dec. 2010

• Provide HPC concept definition and study MTU Jan. 2010 Dec. 2010 • Provide HS-LPT concept definition and study MTU Jan. 2010 Dec. 2010 • Provide Engine Modifications concept definition

and study MTU Jan. 2010 Dec. 2010

Indicative Excluded Tasks (for call for proposals) No Description SAGE-04-001 Turbine materials development

SAGE-04-002 Alternate Designs of Turbine components


partner Due Date

4.1.1 Initial Modules and Engine Modifications Concept Design Review

MTU March 2010

4.1.2 Modules and Engine Modifications Concept Definition and Study Review

MTU Nov. 2010


(WP/Task) Due Date

4.3.1 Initial Geared Fan Demonstrator Concept 4.3 Jan. 2010



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Due Date

4.1.1 Initial Modules and Engine Modifications Concept Design

MTU 4.3 March 2010

4.1.2 Modules and Engine Modifications Concept Definition and Study

MTU 4.3 Nov. 2010



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SAGE 4.2 Structures & Systems

WP No. 4.2 WP Title Structures & Systems



partner Start End

• Plan, manage and coordinate provision of new fan drive gear system, mid turbine frame and controls and power system

MTU Jan. 2010 Dec. 2010

• Provide Demonstrator Concept Definition and Study to Structures & Systems

MTU Jan. 2010 Dec. 2010

• Provide Fan Drive Geared System Concept Definition and Study AVIO Jan. 2010 Dec. 2010

• Provide Mid Turbine Frame Concept Definition and Study

VAC Jan. 2010 Dec. 2010


partner Due Date

4.2.1 Structures & Systems Concept Definition and Study Review MTU Nov. 2010 4.2.2 Fan Drive Geared System Definition and Study Assessment AVIO Nov. 2010 4.2.3 Mid Turbine Frame Concept Definition and Study Review VAC Nov. 2010


(WP/Task) Due Date

4.3.1 Initial Geared Fan Demonstrator Concept 4.3 Jan. 2010



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Due Date

4.2.1 Structures & Systems Concept Definition and Study

MTU 4.3 Nov. 2010

4.2.2 Fan Drive Geared System Definition, Study and Documentation

AVIO 4.3 Nov. 2010

4.2.3 Mid Turbine Frame Concept Definition, Study and Documentation

VAC 4.3 Nov. 2010



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SAGE 4.3 Integration & Test

WP No. 4.3 WP Title Integration & Test



partner Start End

• Plan, manage and coordinate whole engine design, geared fan demonstrator test and build & strip and test evaluation

MTU Jan. 2010 Dec. 2010

• Provide Initial Geared Fan Demonstrator Concept and Technology Development Plan

MTU Jan. 2010 March 2010

• Provide Geared Fan Demonstrator Concept Definition

MTU March 2010 Aug. 2010

• Provide Geared Fan Demonstrator Concept Study MTU Sep. 2010 Dec. 2010 • Provide Geared Fan Demonstrator Concept

Selection MTU Jan. 2010 Dec. 2010


Partner

4.3.1 Support to planning, steering and monitoring activities MTU


partner Due Date

4.3.1 Initial Geared Fan Demonstrator Concept Design Review MTU Jan. 2010

4.3.2 Geared Fan Demonstrator Concept Selection Assessment MTU Dec. 2010



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Due Date

4.3.1 Initial Geared Fan Demonstrator Concept and Technology Development Plan

MTU 4.1, 4.2 March 2010

4.3.2 Geared Fan Demonstrator Concept Selection

MTU 4.1, 4.2 Dec. 2010



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SAGE 5.1 Core Study

WP No. SAGE 5.1 WP Title Core Study

Leader Turbomeca Contact Brigitte CHEFTEL


partner Start End

T5.1.1: Compressor, casing, IGV and air flow path design, rig test design. New coating characterisation

Turbomeca Jan. 2010 Dec. 2010

T5.1.2: Combustion chamber and injector (position and type) design. Rig test design study.


T5.1.3: HP turbine blades and disk design. Rig test design. New blade material characterisation


T5.1.4: LP turbine blades and disk design. Rig test design


T5.1.5: Management Turbomeca Jan. 2010 Dec. 2010

Indicative Excluded Tasks (for call for proposals) No Description SAGE-05-010 Oxidation/corrosion resistant coatings for titanium aluminides for using on low pressure

turbine blades between 650 and 850°C


partner Due Date

M 5.1b Design Review Turbomeca June 2010



Due date

D5.1.1b Report on the selection of compressor Turbomeca T5.1.1 Dec. 2010

D5.1.2b Report on the selection of combustors Turbomeca T5.1.2 Dec. 2010

D5.1.3b Report on the selection of HP turbine Turbomeca T5.1.3 Dec. 2010

D5.1.4b Report on the selection of LP turbine Turbomeca T5.1.4 Dec. 2010



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30 / 31 AIP SAGE5.2 27.01.2010


SAGE 5.2 Whole engine study

WP No. SAGE 5.2 WP Title Whole engine study

Leader Turbomeca Contact Brigitte CHEFTEL


partner Start End

T5.2.1: Oil system - Parts study Turbomeca Jan. 2010 Dec. 2010

T5.2.2: Transmission - Parts study and material choice


T5.2.3: Low noise device - Parts study Turbomeca Jan. 2010 Dec. 2010

T5.2.4: More electrical AGB - Parts study Turbomeca Jan. 2010 Dec. 2010

T5.2.5: Control system - Parts study Turbomeca and partners

Jan. 2010 Dec. 2010

T5.2.6: Exhaust - Parts study Turbomeca Jan. 2010 Dec. 2010

T5.2.7: Contra rotative architecture - Parts design Turbomeca Jan. 2010 Dec. 2010

T5.2.8: Management Turbomeca Jan. 2010 Dec. 2010

Indicative Excluded Tasks (for call for proposals) No Description SAGE-05-011 Design and feasibility of air intake and gear box static parts made of organic matrix

composite

SAGE-05-012 Design and feasibility of a casing in organic composite materials


partner Due Date

M 5.2b Design review Turbomeca June 2010



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partner To

(WP/Task) Due date

D5.2.1b Study report on the oil system Turbomeca T5.2.1 Dec. 2010

D5.2.2b Study report on the transmission Turbomeca T5.2.2 Dec. 2010

D5.2.3b Study report on the Low noise device Turbomeca T5.2.3 Dec. 2010

D5.2.4b Study report on the More electrical AGB Turbomeca T5.2.4 Dec. 2010

D5.2.5b Study report on the Control system Turbomeca T5.2.5 Dec. 2010

D5.2.6b Study report on the Exhaust Turbomeca T5.2.6 Dec. 2010

D5.2.7b Study report on the Contra rotative architecture

Turbomeca T5.2.7 Dec. 2010

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