Title :
Development of technical solutions—structures
Author_Institution :
Messier-Dowty Ltd., France
Abstract :
- Shock absorber system able to identify gas and oil loss giving prognostic capabilityunder representative conditions - Brake wear model validated against flight test data predicted errors below 10% with no extra sensing - Brake cooling prediction successful using modelling techniques - Acousto ultrasonics were the most technically mature for detecting damage on composite structures and cracks in metallic ones - Comparative vacuum monitoring also effective at damage detection of composites
Conference_Titel :
Aircraft Health Management for New Operational and Enterprise Solutions, 2008 IET Seminar on
Conference_Location :
London
Print_ISBN :
978-0-86341-936-2