Seeded Planetary Bearing Fault in a Helicopter Gearbox—A Case Study

Linghao Zhou, Fang Duan, Elasha Faris, David Mba

Research output: Chapter in Book/Report/Conference proceedingChapter

1 Citation (Scopus)

Abstract

Helicopters have been extensively employed as a versatile tool in modern society, thus guaranteeing operation safety and flightworthiness has always been our top-tier concerns. However, many accidents indicate that current helicopter health and usage monitoring system (HUMS) are not accurate and effective enough to fulfil this goal, especially for detecting an imminent planetary bearing fault (CAA Authority 2006). To study this case and address such issues, an experiment was undertaken with a special rig, comprising of real helicopter main gearbox (MGB) and dynamometer as a variable load. Defects of different sizes were seeded at the outer race of bearings inside second epicyclic planetary module. Vibration signals of different test conditions (input speed, load and defect sizes) were recorded for post-processing. Measured vibration data contains overwhelming background noise and planetary gear meshes, making it cumbersome to identify the bearing defect. Various signal processing techniques are applied to identify the bearing defect, including signal pre-whitening, gear/bearing signal separation, kurtogram, envelope analysis, high-order spectral analysis and so on. The comparative results suggest that certain combinations of aforementioned methods are more effective than single process techniques. One case of successful detection is demonstrated in this paper. This study potentially benefits improving HUMS effectiveness and supports helicopter maintenance decision-making.
Original languageEnglish
Title of host publication Proceedings of the 7th Conference on Design and Modeling of Mechanical Systems, CMSM'2017, March 27–29, Hammamet, Tunisia
Subtitle of host publicationDesign and Modeling of Mechanical Systems—III
EditorsMohamed Haddar, Fakher Chaari, Abdelmajid Benamara, Mnaouar Chouchane, Chafik Karra, Nizar Aifaoui
Place of PublicationCham
PublisherSpringer Verlag
Pages495-505
Number of pages11
ISBN (Print)978-3-319-66697-6
DOIs
Publication statusPublished - 25 Nov 2017
EventInternational Conference and Modeling of Mechanical Systems - Hammane, Tunisia
Duration: 27 Mar 201729 Mar 2017

Conference

ConferenceInternational Conference and Modeling of Mechanical Systems
Abbreviated titleCMSM 2017
CountryTunisia
CityHammane
Period27/03/1729/03/17

Keywords

  • Planetary bearing
  • Seeded defect
  • HUMS
  • Advanced signal processing
  • Fault diagnosis

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    Zhou, L., Duan, F., Faris, E., & Mba, D. (2017). Seeded Planetary Bearing Fault in a Helicopter Gearbox—A Case Study. In M. Haddar, F. Chaari, A. Benamara, M. Chouchane, C. Karra, & N. Aifaoui (Eds.), Proceedings of the 7th Conference on Design and Modeling of Mechanical Systems, CMSM'2017, March 27–29, Hammamet, Tunisia: Design and Modeling of Mechanical Systems—III (pp. 495-505). Cham: Springer Verlag. https://doi.org/10.1007/978-3-319-66697-6_48