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Conclusion ! Flexible, Modular Operation ! Small / Large Channel Count ! Stand-alone / Integrated ! Performant Data-acquisition ! Time / Frequency / Order / Octave ! High Throughput Rate ! Visualization with Added-Value ! Time data, Frequency Data, Order data ! Level w.r.t. Warning/Alarm level ! Maintainable ! Maximal use of Standard Software & Hardware ! Interchangeable Hardware components ! Safe operation ! Data Integrity ! Data Storage / Archiving ! Process-centric ! Centralized and User-friendly Acquisition Set-up, Control and Monitoring ! De-centralized visualization ! Cost-effective 40 Aerospace Testing Expo 2005
Thank you for your attention LMS Users Conference, March 22th 2006 Jan Debille
Page 1 and 2: AERO-ENGINE DYNAMIC TESTING tacklin
Page 3 and 4: Jet engines: powered by a turbine e
Page 5 and 6: Jet Engine Jet engine = turbine + t
Page 7 and 8: Outline ! Introduction to Jet Engin
Page 9 and 10: Traditional aero-engine dynamic dat
Page 11 and 12: Challenges for the future Quality !
Page 13 and 14: Challenges for the future Multi-cha
Page 15 and 16: Processing Storage The ideal aero-e
Page 17 and 18: Networked data acquisition system w
Page 19 and 20: The LMS SCADAS III family The indus
Page 21 and 22: LMS SCADAS III: a wide range of sig
Page 23 and 24: New conditioner: PQDCA ! Programmab
Page 25 and 26: Dynamic strain measurements ! Stand
Page 27 and 28: IRIG-B ! GPS based time encoding fo
Page 29 and 30: Test laboratory concept Embedded wo
Page 31 and 32: Scalable Storage NAS or SAN Gibabit
Page 33 and 34: Data organization and retrieval Tes
Page 35 and 36: Example 1: 200 channel recording an
Page 37 and 38: Example 2: Physical infrastructure
Page 39: Outline ! Introduction to Jet Engin

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