ENGINE Demonstration Programmes in Clean Sky & Clean Sky 2
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2 ENGINE Demonstration Programmes in Clean Sky & Clean Sky 2 Jean-François BROUCKAERT SAGE & ENGINES ITD Project Officer Aerodays 2015, London, October 2015 Innovation Takes Off
3 Outline 1. Open-Rotor Architectures CS1-SAGE1 RRUK CS1-SAGE2 SNECMA CS2-LPA-(ENG-WP1) - SNECMA 2. Large VHBR Turbofans Architectures LR Aircraft CS1-SAGE3 RRUK CS1-SAGE6 RRUK (Lean Burn) CS2-ENG-WP5 RRUK CS2-ENG-WP6 RRUK 3. VHBR Turbofans SMR Aircraft CS2-ENG-WP2 SNECMA - UHPE 4. Geared Turbofans SMR Aircraft CS1-SAGE4 MTU CS2-ENG-WP4 MTU 5. Turboshaft Engines - Helicopters CS1-SAGE5 - TURBOMECA 6. TurboProp Engines Regional/SAT CS2-ENG-WP3 TURBOMECA CS2-ENG-WP8 GE Avio 7. Small Piston Engines Small Air Transport (SAT) CS2-ENG-WP7 - SMA
4 1. Open Rotor Architectures
5 CS1 SAGE 2 Snecma Objective : to build and ground test a full-scale Geared Pusher Open Rotor engine Main benefit of the Open Rotor concept : 30 % CO2 emissions reduction compared to the CFM56 * engine Open Rotor GTD will run in 2016 on a brand new Safran Open Air Test Bench. Plus several CfP partners Snecma proprietary information * CFM56 engines are a product of CFM International, a 50/50 joint company between Snecma (Safran) and GE.
6 CS2 LPA (ENG-WP1) Snecma Flight Test Demonstrator_Contra rotating Open Rotor for SMR aircraft : a breakthrough to reach the optimal performance Top objectives Performance Architecture & Technologies Aircraft/Propulsion System Integration Data Exploitation Snecma proprietary data
7 2. Large Turbofan Architectures
![[EPNdB]](/docs-images/91/105929517/images/8-8.jpg "Composite fan")
8 CS1 SAGE3 Rolls-Royce Delivered both Ground and Flight Tests Subsystem Environmental targets (wrt reference) CO2 [%] Noise [EPNdB] Composite fan system -1 to -3-1 to -3 Advanced integrated externals -0.5 to Low weight low pressure turbine -1 to -2 0 A wealth of Hardware delivered through the Rolls-Royce led SAGE 3 Advanced Low Pressure System engine programme
9 CS1 SAGE6 Rolls-Royce NO X Emissions Targets NOx LTO <40% CAEP6 Cruise EINOx <12g/kg Advanced/Active Control System Hardware being delivered for both Ground and Flight Tests of the Advanced Low Emissions Combustion System Engine programme 2016 to deliver both Ground and Flight Tests
10 CS2 ENG-WP5 & 6 Rolls-Royce Aim: System integration and delivery of whole-engine demonstration through ground and flight-based testing Composite Containment Casing Optimised Powerplant & Nacelles Lean Burn Combustor Lightweight High Efficiency Compressors Controls, EHM & Systems Integration Advance Core Architecture Lightweight Cti Fan blades Lightweight Externals Power gear box Lightweight High Efficiency Turbines Enabling Technologies Demonstrators Building on the success of the ALPS Engine from Clean Sky SAGE 3 Advance3 Core for the UltraFan TM Demonstration planned for 2016 Efficiency relative to Trent %+ Rolls-Royce Ultrafan TM Demonstrator Planned EIS Efficiency relative to Trent %+ ByPass Ratio 15+
11 3. VHBR Turbofans
12 CS2 ENG-WP2 Snecma Ultra High Propulsive Efficiency for SMR aircraft : towards enhanced performance Main Technology Objectives to validate LP modules & nacelle technologies 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 UHBR turbofan for SMR aircraft Potential Partner participation: Fixed structures in propulsive system, low pressure turbine components, controls and systems components, shafts, bearings Snecma proprietary data
13 4. Geared Turbofans
14 CS1 SAGE4 MTU Clean Sky SAGE 4 Demonstrator is ready to test h All-electric VGV-Aktuator (SENER) Life leightweight TEC db Acoustic liner Turbine Technology h Integrated Drive System Technology tested on a specific transmission test bench Compressor Technology η Surface treament Life Erosion protection new Materials (CFRP) Additive Maufacturing New measurement methods h h h h h h lb lb Life improved outer cavity design advanced case design new IAS designs smart ACC optimized airfoil shape improved trim balancing frequency mistuned airfoils CMC segments TiAl blade technology
15 CS2 ENG-WP4 MTU BPR 5 OPR 36 V % BPR 12 Technology maturation for future engine generations Performance Parameters h lb Life db Clean Sky 2 Notional Engine Concept WP 4 Partners SFC % CO 2 % 1st gen GTF BPR OPR 60+ Source: - 25% Future Geared Fan Engines ENOVAL Clean Sky 2 Advanced Technology Projects Compression System Expansion System Design Materials Manufacturing Proof of technology maturity in Clean Sky 2 validation vehicles LPC 2 shaft compressor rig ICD Engine demonstrator MTF ITD LPT TEC Mix HPC
16 5. Turboshaft Engines
17 CS1 SAGE5 Turbomeca Design a totally new core engine called for kw range allowing to : Reduce by 15% Fuel Consumption Reduce overall dimension and weight Highlight possible production and maintenance cost reduction axis SAGE 5 demonstrates new technologies for compressor, combustor, HP turbine, LP turbine and innovative architecture through : partial testing campaign of innovative technologies separately Core engine demonstrator Reach a TRL level 6 for each technology Preliminary DR Feb Engine test Feb 2013 Turboshaft engine development full-scale engine demonstration Demo spec. Prelim. design Partner selection Detail design Manufacture Build and test Project launch 1 Sept 2009 Critical DR July % Fuel consumption reduction demonstrated
18 6. Turboprop Engines
19 CS2 ENG-WP3 Turbomeca Ground demonstration of a full Integrated Power Plant System Including Air Intake & nacelle Taking advantage of the FADEC for enhanced system controls capabilities The core generator is derived from the ARDIDEN 3 Turboshaft engine Engine adaptations will be studied for matching TP usage New propeller and Power Gear Box will be designed
20 CS2 ENG-WP8 GE Avio Integrated Collaborative Partnership to Strengthen European Competitiveness in Small Air Transport Turboprop Engines Market High Level Objectives (vs 2014 ref. engine) + 15% Fuel Efficiency - 10% Total Operating Costs - 10 db Noise Reduction (contrib.) Sub-systems Technology Development and Validation on Advanced Core with High OPR Low Re Turbine Design Integrated Low Noise Propulsive System Affordable Low Emission Combustor
21 7. Small Piston Engines
22 CS2 ENG-WP7 SMA Light weight and efficient Jet-fueled reciprocating engine ( kw ) 1. Engine power density challenge a. Improvement of existing architectures & manufacturing (WP7.1.1) b. Research for breakthrough technologies - Target 2.5 kw/kg (WP7.1.4) c. Turbocharger - Key equipment (WP7.1.2) 2. Powerplant optimization a. Propeller for compression ignition engine (WP7.1.3) b. Aircraft engine installation / heat exchangers (WP7.1.5)
23 Visit us at the Expo: Clean Sky Booth Contact us at: Thank You for your Attention
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