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...

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Published inTransportation research procedia (Online) Vol. 35; pp. 287 - 294
Main Authors Pecho, Pavol, Bugaj, Martin
Format Journal Article
LanguageEnglish
Published Elsevier B.V 2018
Subjects
Aircraft
Health Monitoring
Maintenance
MTBF
Reccurance Quantification Analysis
Vibrations
Vibrations
Health Monitoring
Maintenance
Reccurance Quantification Analysis
Aircraft
MTBF
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Abstract 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 use Recurrence quantification analysis its 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.
AbstractList 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 use Recurrence quantification analysis its 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.
Author Bugaj, Martin
Pecho, Pavol
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CitedBy_id crossref_primary_10_4028_www_scientific_net_KEM_904_161
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Cites_doi 10.1109/TIM.2014.2313034
10.1007/BF02829139
10.1109/AERO.2012.6187370
10.1007/978-3-662-45317-9_4
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Keywords Vibrations
Health Monitoring
Maintenance
Reccurance Quantification Analysis
Aircraft
MTBF
Language English
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SubjectTerms Aircraft
Health Monitoring
Maintenance
MTBF
Reccurance Quantification Analysis
Vibrations
Title Vibration fault detection of fuel pump using Recurrence Quantification Analysis
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