Clean Sky Smart Fixed Wing Aircraft ITD

Transcription

1 TAKE OFF Informationsveranstaltung zu Ausschreibungen nationaler und europäischer Luftfahrtforschungsprogramme Clean Sky Smart Fixed Wing Aircraft ITD Michel GOULAIN, SAGE Project Officer June 1st, 2010, Vienna

2 SFWA-ITD Organisation and Setup 2

3 SFWA- ITD Participants and Global Shares 393M Total Budget ITD-Leaders Associate Partners Airbus SAAB Dassault EADS-CASA Thales Fraunhofer SAFRAN Rolls-Royce DLR ONERA INCAS -Cluster NL-Cluster QinetiQ RUAG Aernnova 25% of Total Budget Partners Partner participation based on Call for Proposals CfP 50% of Total Budget 25% of Total Budget 3

4 Key Technologies for SFWA Input connecting to: SAGE ITD - CROR engine SGO ITD - Systems for Green Operation Smart Wing Technologies Technology Development Technology Integration Large Scale Flight nstration Natural Laminar Flow (NLF) Innovative Powerplant Integration Technology Integration Large Scale Flight nstration Impact of airframe flow field on Propeller design (acoustic, aerodynamic, vibration) Hybrid Laminar Flow (HLF) Active and passive load control Novel enabling materials Innovative manufacturing scheme Impact of open rotor configuration on airframe (Certification capabilities, structure, vibrations...) Innovative empennage design TE Output providing data to: SFWA technologies for a Green ATS 4

5 SFWA- ITD Technology WBS SFWA 0: Airbus / SAAB Dassault SFWA1: Smart Wing Technology Technologies enter at TRL 2 or 3 SFWA1.1 Airbus Flow Control Airbus SFWA1.2 Load Control SFWA1.3 Integrated Flow & Load Control Systems NL-Cluster Selected Technologies developed at TRL 4 SAAB SFWA2: New Configuration Airbus SFWA2.1 Integration of Smart Wing into OAD Dassault SFWA2.2 Integration of Other Smart Components into OAD Airbus SFWA2.3 Interfaces & Technology Assessment Selected Technologies integrated at TRL 4 or 5 Airbus SFWA3: Flight nstration Airbus SFWA3.1 High Speed Smart Wing Flight nstrator Selected technologies validated in large scale flight demos at TRL > 6 SFWA3.2 Dassault Low Speed Smart Wing Flight nstrator Airbus SFWA3.3 Innovative Engine nstrator Flying Test Bed Airbus SFWA3.4 Long Term Technology Flight nstrator Technology Development Technology Integration Airbus SFWA3.5 Innovative Empenage Flight Design Flight nstration 5

6 The Smart Fixed Wing Aircraft Concepts A major contribution to the maturing, integration and large scale demonstration of Smart Fixed Wing Aircraft - technologies is delivered through eight SFWA- Aircraft concepts by Defining or providing the operational environment to mature a technology to high TRLs Providing an evaluation platform Setting a scenario for a potential target application.? 1. High Speed nstrator Passive (HSDP) 2. Low Speed nstrator (LSD) 3. Short Range Aircraft Concept (SRA) 4. Low Sweep Bizjet Concept (LSBJ) 5. High Speed nstrator Active (HSDA) 6. Long Range Aircraft Concept (LRA) 7. High Sweep Bizjet Concept (HSBJ) 8. CROR Engine FTB 6

7 SFWA ITD Flight nstrator Options 1. High Speed Flight nstrator Objective: Large scale flight test of passive and active flow and loads control solutions on all new innovative wing concepts to validate low drag solutions at representative Mach and Reynolds Numbers. Envisaged to be used at least in two major phases of the project. Selected in April 2009 Option 1: UAV Option 2: Alpha-Jet Option 3: Airbus A340 with modified wing 2. Low Speed Flight nstrator Objective: Validation flight testing of High Lift solution to support / enable the innovative wing low drag concepts with a full scale demonstrator. Option 1: Dassault Falcon Option 2: Airbus A Innovative Engine nstrator Flying Testbed Objective: nstrate viability of full scale innovative engine concept in operational condition Options under investigation Selection scheduled for 2010 Status: Preferred solution 4. Long Term Technology Flight nstrator Objective: Validation of durability and robustness of Smart Wing technologies in operational environment Option 1: In Service Transport Aircraft Option 2: Airbus A300 Beluga Option 2: Airbus A320 Selection(s) part of technology roadmap 7

8 The SFWA- High Speed nstrator Passive (HSDP) Smart Passive Laminar Flow Wing Laminar Wing Ground test demonstrator to address structural, system and manufacturing aspects Design of an all new natural laminar wing Proof of natural laminar wing concept in wind tunnel tests Use of novel materials and structural concepts Exploitation of structural and system integration together with tight tolerance / high quality manufacturing methods in a large scale ground test demonstrator Large scale flight test demonstration of the laminar wing in operational conditions Starboard wing Laminar wing structure concept option 1 Port wing Laminar wing structure concept option 2 Laminar Wing aerdynamic layout and performance 8

9 SFWA-ITD HSDP preparation Worksharing 9

10 SFWA-ITD Integration of the CROR Engine Concept CROR Aero -Acoustic experimental characterization with / without pylon. Example of the RR - CROR (Dream, Dowty Design) Innovative Power-Plant Integration Design of innovative CROR blades and pylon CROR installation effects: aero, noise, vibrations, handling qualities CROR propeller kinematics, study of fragment impact depending on size and propeller and fuselage materials Structural technologies for armour and shielding Feasibility study of a full scale CROR engine in a Flying Testbed nstration (FTB) CROR design study with new blade and engine design CROR integration study for a full scale test of a CROR engine on-board a modified Airbus A Flying Test Bed. 10

11 SFWA-ITD Call for Proposal Topics Overview In the total project lifetime the SFWA-ITD expect to contribute in CleanSky Call for Proposals (CfP) on topics Total value of topics ~ 100M In the current calls Industry, Research Establishments and Universities are invited to check your interest and to reply upon Call # (30.March June 2010 (17:00)) 4 topics Total value of topics ~ 5.90M Call # (28.April July 2010 (17:00)) 8 topics Total value of topics ~ 4.04M 11

12 The Smart Fixed Wing Aircraft Concepts Topics 3rd CfP? 1. High Speed nstrator Passive (HSDP) 2. Low Speed nstrator (LSD) 3. Short Range Aircraft Concept (SRA) 4. Low Sweep Bizjet Concept (LSBJ) 5. High Speed nstrator Active (HSDA) 6. Long Range Aircraft Concept (LRA) 7. High Sweep Bizjet Concept (HSBJ) 8. CROR Engine FTB 9. Multiple Aircraft Concepts / Technology Streams

13 SFWA-ITD Call for Proposal Topics in Call# Identification ITD - Area - Topic No. topics Value Start Date End Date JTI-CS-SFWA-01 Area01 - Smart Wing Technoilogy JTI-CS SFWA MEMS accelerometer for wing behaviour measurement JTI-CS SFWA MEMS gyrometer for wing behaviour measurement JTI-CS-SFWA-02 Area02 - New Configuration 0 0 JTI-CS-SFWA-03 Area03 - Flight nstrator JTI-CS SFWA Starbord leading edge and upper cover design and manufacturing JTI-CS SFWA Krueger flaps design and manufacture totals : SFWA High Speed nstrator Passive HSDP SFWA Low Speed nstrator LSD SFWA CROR Engine FTB SFWA Application in different aircraft concepts SFWA Low Sweep Bizjet Concept LSBJ For a complete description of the topics, please refer to the published text of the call in CleanSky SFWA-ITD, Vienna 01 st June

14 The Smart Fixed Wing Aircraft Concepts Topics 2nd CfP? 1. High Speed nstrator Passive (HSDP) 2. Low Speed nstrator (LSD) 3. Short Range Aircraft Concept (SRA) 4. Low Sweep Bizjet Concept (LSBJ) 5. High Speed nstrator Active (HSDA) 6. Long Range Aircraft Concept (LRA) 7. High Sweep Bizjet Concept (HSBJ) 8. CROR Engine FTB 9. Multiple Aircraft Concepts / Technology Streams

15 SFWA-ITD Call for Proposal Topics in Call# SFWA High Speed nstrator Passive HSDP SFWA Low Speed nstrator LSD SFWA CROR Engine FTB SFWA Application in different aircraft concepts SFWA Low Sweep Bizjet Concept LSBJ 15

16 JTI CleanSky Vielen Dank für Ihre Aufmerksamkeit 16

17 JTI CleanSky 2010 by the CleanSky Leading Partners: Airbus, AgustaWestland, Alenia Aeronautica, Dassault Aviation, EADS- CASA, Eurocopter, Fraunhofer Institute, Liebherr-Aerospace, Rolls-Royce, Saab AB, Safran, Thales and the European Commission. Permission to copy, store electronically, or disseminate this presentation is hereby granted freely provided the source is recognized. No rights to modify the presentation are granted. 17