MAGNA STEYR Aerospace. October 2012

Transcription

1 MAGNA STEYR Aerospace Presentation October 2012

2 Managementstructure MAGNA International Don Walker Chief Executive Officer Vince Galifi Jim Tobin Herbert Demel Burkhard Goeschel Tom Skudutis Guenther Apfalter Mike Sinnaeve Chief Financial Officer Chief Marketing Officer, President Magna Asia Chief Strategy Officer Chief Technology Officer COO Magna Interiors, Exteriors, Seating, Mirrors, Closures and Cosma President Magna Europe VP Operational Improvement & Quality Joe Pittel President Frank Seguin President Tom Skudutis President Jake Hirsch President Guenther Apfalter President Mike Bisson President Albert Lidauer President EU Bob Brownlee President Americas / Asia MAGNA SEATING MAGNA EXTERIORS & INTERIORS MAGNA MIRRORS & MAGNA CLOSURES COSMA INTERNATIONAL MAGNA POWERTRAIN & MAGNA ELECTRONICS MAGNA STEYR Seating Systems Exterior & Interior Systems Vision, Closure & Lighting Systems Body & Chassis Systems Powertrain & Electronic Systems Vehicle Engineering & Contract Manufacturing Fuel, Battery & Roof Systems 2

3 Worldwide Presence MAGNA Int. (Status Q3 2012) Canada 19,075 Aurora (Headquarters) Mexico 20, USA Westeuropa Austria Belgium England France Germany Irland Italy Schweden Spain Osteuropa Czech Republic Hungary Poland Russia Slowak Republic Turkey Asia 9,050 China Korea Japan India Thailand South America 4,975 Brazil Argentina Africa 100 South Africa ~ 115,000 employees 26 countries 296 manufacturing operations 88 product development / engineering / sales centers $28.7 billions (Sales 2011) 3

4 We offer Vehicle Engineering Engineering services including complete vehicle engineering Fuel- & Batterysystems Innovative fuel & battery systems Aerospace Contract Manufacturing Flexible solutions from niche to volume production Roof systems Entire range of roof systems 4

5 Aerospace and Diversified Industries Feed lines for launchers Cryogenic storage systems Satellite components Aviation components Aviation services 25. Oktober 2012 Serial production for the upper stage and main stage Lightweight storage systems and lines for liquid hydrogen and liquid helium Devices and structural components for satellites Development and production of propulsion subsystems Development and production of structural components Engineering services, supply chain management and development of ground support equipment MAGNA STEYR Marketing & Communications 5

6 Feed Lines for Launchers Past Today Future Ariane 5 Main Stage EPC Ariane 5 Uppers Stage ESC-A Ariane 5 Midlife Evolution Production: Seamless and welded tubes, provided with flanges, expansion joints, supports and insulation. Production: tubing system for liquid hydrogen and liquid oxygen from tank to vulcaine engine System Supplier (development phase) for the complete tubing systems for the new upper stage; development in cooperation with Astrium 6

7 Cryogenic Storage Systems Past Today Future BMW Clean Energy Automotive Doublewall Hydrogen Tanks Scientific Satellites Space LH2 storage system Technology transferred from space into automotive application Double wall cryogenic composite storage tank for LH2 Research project in cooperation with Airbus for LH2 supply system for fuel cells on airplanes Double wall cryogenic composite storage tank for LHe: Project for European Space Agency (ESA) for future satellites missions 7

8 Satellite Components Past Today Future Devices and structural components for satellites Development and manufacturing of blades for the ROSETTA Platform Louvres (in flight reaching destination by 2014). Antenna Hold-Down and Release Mechanism for large deployable antennas (pyrotechnical separation) MAGNA STEYR Part in EXPERT Re-entry Demonstrator, development and production of several components Development of micro technologies for Louvres to be used for satellites thermal control 8

9 Aviation Components Past Today Future Development and production of propulsion subsystems Development and production of structural components Relocation Project: Airbus FALC & SCT (Final Assembly Line China Small Components Transportation) Airbus A 320 Manufacturing of ACC Active Clearance Control Systems for A/C Engines (GP 7200 A380) Relocation Project: Airbus FAL US (Final Assembly Line US Components Transportation) A320 & A350 9

10 Aviation Services Past Today Future Engineering services, supply chain management development of ground support equipment Turbine test stands (aviation & power) Design, analysis and production including verification Engineering & testing support for satellite and aviation programs Development programs for aviation and space Components 10

11 Synergies between Automotive and Aerospace Astrium Projects: Ariane 5 Feedlines Development Production Optimisation competence for different industries: Space Aeronautics Automotive Railway Medical others BMW Clean Energy Cryotank Public- Bus Cryotank StorHy Cryotank H2 Tank Aeronautics Flat & CFRP Cryotank ESA Projects: LHe Double wall cryogenic composite storage tank FLPP Cryogenic CFRP pressure line technology demonstrator for LHe, LH2 and LOX 11

12 Accreditation acc. DIN EN ISO/IEC Phase 1 Implementation 2011 Phase 2 Implementation 2012 Dye penetration testing (PT) X-Ray testing (RT) Visual inspection testing (VT) Ultrasonic testing (UT) Hydraulic pressure test, up to bar (incl. Climatic conditioning) Hydraulic burst test, up to bar Hydraulic pressure cycling test, up to bar (incl. Climatic conditioning) Drop test, hydraulic pressurised, up to bar (incl. Climatic conditioning) Thermal aging test Accelerated stress rupture test Fatigue test Permeation test, up to 900 bar Gas test, up to 900 bar (Function, Gas cycles) Gas thightness test, up to 900 bar (incl. Climatic conditioning) Impact test, pneumatic pressurised, up to 900 bar Impact test, hydraulic pressurised, up to bar Drop test, pneumatic pressurised, up to 900 bar (on external terrain) Bullet test, up to 900 bar (on external terrain) Bonfire test, up to 900 bar (on external terrain) Dynamic durability test, vibration table,, hydraulic pressurised, up to bar or pneumatic pressurised, up to 900 bar Chemical resistance test 12

13 H2 & FC Standardization for Aerospace MAGNA STEYR is a member of the SAE/EURO CAE WG 80/AE7 AFC Hydrogen Fuel Cells Task Group for FC/H2 use on future commercial aircraft Summary of Purpose To develop guidelines to support qualification and certification of Hydrogen Fuel Cell Systems in the various intended applications for civil aircraft. Fuel (LH2 and GH2), fuel storage, fuel distribution and appropriate electrical systems into the aircraft. The duration of WG-80 activity is initially scheduled to be complete by first draft end of Members Airbus Operations GmbH, QinetiQ, Liebherr-Aerospace, Michelin, Diehl Aerospace, Parker Aerospace, Embraer, Boeing, Cessna, General Electric, JSJ Technologies LLC, Dassault Aviation, US FCC 13

14 Management Systems & Human Resources Certified according EN 9100 Quality management system for Aerospace EN Quality management system for welding ISO 14001, EMAS II Environmental management system ISO/IEC Data security management system OHSAS Operational safety management system ISO/IEC Testing laboratory (pressure, leakage testing, physical laboratory, ) Personnel Qualification Quality Manager for EN9100 and EASA (Airworthiness directives POA, DOA) Welding supervisor acc. EN 719 and DVS NDI personnel (PT, VT, RT, UT, LT) acc. EN473 and EN4179 Welding personnel EN287-1, ISO9609-2, EN1418 Master of Engineer in the fields of mechanics, aeronautics and composites 14

15 References Customers & Partners 15