Vibration fault detection of fuel pump using Recurrence Quantification Analysis
This research is aimed at investigating the use of a novel technique for monitoring non-linear transient accelerometer data using Recurrence Quantification Analysis (RQA) for use in auxiliary aircraft hardware health monitoring. Identification of premature failure using the RQA technique is explored and investigated for its use in preempting hardware failure of auxiliary fuel pump and forming a new basis for a Mean Time Before Failure (MTBF) for these devices. Authors assume that the use of RQA in combination with traditional methods could indicate early warning of incoming faults and more precise set of MTBF. The question whether the development of this technique is applicable across other aircraft parts may be offered.
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Availability:
- Find a library where document is available. Order URL: http://worldcat.org/issn/23521465
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Supplemental Notes:
- © 2018 Pavol Pecho et al. Published by Elsevier B.V. Abstract reprinted with permission of Elsevier.
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Authors:
- Pecho, Pavol
- Wylie, Mark
- Bugaj, Martin
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Conference:
- 7th International Conference on Air Transport - INAIR 2018
- Location: Donau , Austria
- Date: 2018-11-20 to 2018-11-21
- Publication Date: 2018
Language
- English
Media Info
- Media Type: Web
- Features: Figures; Photos; References;
- Pagination: pp 287-294
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Serial:
- Transportation Research Procedia
- Volume: 35
- Issue Number: 0
- Publisher: Elsevier
- ISSN: 2352-1465
- Serial URL: http://www.sciencedirect.com/science/journal/23521465/
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Publication flags:
Open Access (libre)
Subject/Index Terms
- TRT Terms: Aircraft; Fuel pumps; Monitoring; Vibration
- Uncontrolled Terms: Aircraft maintenance; Aircraft parts; Proactive maintenance; Recurrence quantification analysis
- Subject Areas: Aviation; Maintenance and Preservation; Vehicles and Equipment;
Filing Info
- Accession Number: 01690684
- Record Type: Publication
- Files: TRIS
- Created Date: Jan 8 2019 7:00PM