Innovation Takes Off Not legally binding
Clean Sky 2 Information Day dedicated to the 1 st Call for Proposals (CFP01) Innovation Takes Off Engine ITD François Mirville, SAFRAN/Snecma Keith Nurney, Rolls-Royce Peter Taferner, MTU Aero Engines Paris, 3 February 2015
Overview of the ITD/IADP From Clean Sky towards Clean Sky 2 Clean Sky, through SAGE (Sustainable And Green Engines), is delivering significant step changes in key engine technologies along the following themes: Open Rotor, Composites, Lean Burn combustors, high power gearboxes, enhanced turbines and compressors, advanced materials and improved structures Clean Sky 2 is about providing and demonstrating new engine technology for the whole of the civil market The Clean Sky 2 engines ITD will build on Clean Sky and demonstrate technology at a whole engine level
Overview of the ITD/IADP High-Level Objectives Environmental objectives for the engines ITD are to demonstrate at TRL6 the following: 20-30% reduction in CO2* Significant contribution to ACARE 2020 NOx reduction target (-80%*) Upto -11EPNdB per operation reduction in noise* *relative to year 2000 baseline Industrial objectives are to ensure future competitiveness of European Aero Engine industry, securing trade, employment and high technology knowledge and skills
Engine ITD timelines Overview of the ITD/IADP WP1 WP2 WP3 WP4 WP5 WP6 Open Rotor Flight Test UHPE demonstrator Business Aviation Regional Turboprop Geared engine Configuration (HPC-LPT) VHBR Turbofan Middle of Market VHBR Turbofan Long Range SNECMA SNECMA TM MTU RR RR 2014 2016 2018 2020 2022 Flight Demonstrator Ground Demonstrator Technology Demonstrator Ground Demonstrator Ground Demonstrator Flight Demonstrator WP7 Small Aircraft Engine SMA Several demonstrators
Overview of the ITD/IADP WP1- SNECMA Clean Sky 2 activities: Contra Rotating Open Rotor for Flight Test Demo This WP is now integrated in IADP_LPA Large Passenger Aircraft WP1.1.- CROR Engine Demonstrator FTD See IADP_LPA presentation from Cleansky 2 - Paris infoday feb 3 rd, 2015 Open Rotor engine Snecma proprietary data
Overview of the ITD/IADP WP2 SNECMA Clean Sky 2 activities: Ultra High Propulsive Efficiency for SMR aircraft Main Technology Objectives from design to ground test of an engine demo to validate LP modules & nacelle technologies UHBR turbofan for SMR aircraft Key Technologies Low pressure ratio fan / variable area fan nozzle Low weight / low drag fixed or rotating structures and nacelle. High power gear box High efficiency LP turbine & LP compressor Engine / aircraft specific integration Potential Partner participation: : Fixed structures in propulsive system, low pressure turbine components, controls and systems components, shafts, bearings Snecma proprietary data
Overview of the ITD/IADP WP3 Turbomeca Clean Sky 2 activities: Main Technology Objectives From design to ground test of a new turboprop engine demo (1800-2000 shp) for business aviation and short range regional. Improvement of advanced core engine ARDIDEN3 Key Technologies HP core small size (high pressure ratio, low NOx combustor, advanced materials on HP turbine) Capability to hybridise the core engine Advanced propeller / air inlet / gear box Controls, lub & hybrid actuation systems ARDIDEN 3 Existing turboshaft to be modified for CS2 TP Potential Partner Participation : Propeller Power gear box and accessory gear box Air inlet & Nacelle Innovative accessories (oil, bleed, starter,..)
Overview of the ITD/IADP WP4 MTU Clean Sky 2 activities: Advanced Geared Engine Configurations Main Technology Objectives Rig and Engine Testing and Validation of Compressor and Turbine Technology to further reduce Emissions Key Technologies Aerodynamic Integration Material Technologies Manufacturing Technologies Timeframe: 2015-2021
Overview of the ITD/IADP Rolls-Royce Clean Sky 2 activities are split into two work packages: WP5: underlying technologies for VHBR engines with focus on the Middle-of- Market short range aircraft WP6: VHBR technologies for the long range airliner market with Engine Demonstrator Composites Integration Turbines Transmissions UltraFan TM Externals & Structures Control & Power Systems
Overview of the ITD/IADP WP7.1 SMA Clean Sky 2 activities Light weight & Efficient Jet-fuel reciprocating engine Main Technology Objectives Existing technologies power density improvement Research on very high power density (target 2.5 kw/kg) Optimization of the engine integration on an aircraft Key Technologies Material Technologies Manufacturing Technologies Turbochargers Propellers systems, dampers Heat exchangers Timeframe: 2015-2018
Overview of the CFP01 topics
SAFRAN_Snecma CfP - Mounts Engine Mounting System (EMS) for Ground Test Demo Design, manufacture, assembly and instrumentation of an Engine Mounting System for UHPE Ground Test Demo ; EMS Set for characterization and validation through Partials tests : manufacture, assembly and instrumentation, mechanical tests. Structural Part linking the Engine to the pylon Partner is expected to provide Contribution to the EMS specifications Technology proposals in order to challenge the mass of the EMS a qualified EMS for demonstrator testing Type of action: IA Programme Area: ENG JTP Ref.: WP2 Ultra High Propulsive Efficiency Indicative Funding Topic Value: 1500 k Duration: 72 month Start Date: 09-2015
MTU CfP - CMC Development & Manufacture of an all-oxide Ceramic Matrix Composite (CMC) Interturbine Duct Component CMC materials show considerable potential towards weight and cooling air reduction due to lower specific weight and higher temperature resistance compared to metallic components Part provides flow path between HPT outlet and LPT inlet Partner is expected to provide codes, optimization strategies and mechanical simulation for the design of such a component characterization of the chosen material including material testing a qualified part for demonstrator testing Type of action: RIA Programme Aerea: ENG JTP Ref.: WP4 Geared Engine Configuration Indicative Funding Topic Value: 3.000 k Duration: 48 month Start Date: 07-2015
Overview of Rolls-Royce CfP packages To support the technology programme defined by Rolls- Royce in Clean Sky 2, four initial CfPs have been launched: Advanced bearing technology Crack growth in TiAl Prediction of low emissions core noise Characterisation of Thermo-mechanical crack growth The Rolls-Royce CS2 programme is focussed on demonstration of the UltraFan TM engine The CfPs are aimed technologies that will underpin the UltraFan TM programme and will be essential to its success Not legally binding
Overview of Rolls-Royce CfP packages Advanced Bearings Key technology to support the main engine and the power gearbox Thermomechanical crack growth UltraFan TM Low Emissions Noise Prediction TiAl Crack Growth Key technology for the new lightweight, high-speed IPT Core engine technology enablers Supporting CS2 and ACARE goals: Improved life, reduced weight and noise Not legally binding
Engines ITD Any questions on the 1 st Call for Proposals or the Engines topics can be addressed to the following mailbox: Info-Call-CFP-2014-01@cleansky.eu Thank you!
Thank You Disclaimer The selection of Partners will be based on Horizon 2020 Rules for Participation, the rules for submission of proposals, evaluation and selection of Partners as adopted by the Governing Board of Clean Sky 2 JU and will apply to the calls for Proposals The content of this presentation is not legally binding. This presentation wishes to provide a preliminary overview of these rules. The proposed content/approach is based on the consultation with the National States Representative Group and the Task Force of the Clean Sky 2 Programme Programme 18