Statistical data and literature from academia, industry, and other government agencies were reviewed and analyzed to establish requirements for fixture work in detection, diagnosis, prognosis, and mitigation for IVHM related hardware and software. Around 15 to 20 percent of commercial aircraft accidents between 1988 and 2003 involved inalftfnctions or failures of some aircraft system or component. Engine and landing gear failures/malfunctions dominate both accidents and incidents. The IVI vl Project research technologies were found to map to the Joint Planning and Development Office's National Research and Development Plan (RDP) as well as the Safety Working Group's National Aviation Safety Strategic. Plan (NASSP). Future directions in Aviation Technology as related to IVHlvl were identified by reviewing papers from three conferences across a five year time span. A total of twenty-one trend groups in propulsion, aeronautics and aircraft categories were compiled. Current and ftiture directions of IVHM related technologies were gathered and classified according to eight categories: measurement and inspection, sensors, sensor management, detection, component and subsystem monitoring, diagnosis, prognosis, and mitigation.
Commercial Aircraft Integrated Vehicle Health Management Study
01.02.2010
Report
Keine Angabe
Englisch
Integrated Utilities Management System for Commercial Aircraft
British Library Conference Proceedings | 1997
|Applicable Aircraft Integrated Vehicle Health Management (IVHM) Regulations, Policy, and Guidance
SAE Technical Papers | 2019
Integrated thermal management system for commercial vehicle
Europäisches Patentamt | 2023
|