Skip to main content

2014 | OriginalPaper | Buchkapitel

2. Trend Prognosis of Aero-Engine Abrupt Failure Based on Affinity Propagation Clustering

verfasst von : Limin Li, Zhongsheng Wang, Zhenbao Liu, Shuhui Bu

Erschienen in: Proceedings of the First Symposium on Aviation Maintenance and Management-Volume II

Verlag: Springer Berlin Heidelberg

Aktivieren Sie unsere intelligente Suche, um passende Fachinhalte oder Patente zu finden.

search-config
loading …

Abstract

This paper presented a new method for trend prognosis of aero-engine abrupt failure which was based on clustering analysis. We used affinity propagation method to cluster vibration data from aero-engine rotating machinery to find the failure trend by means of features extracted from it. This system could remind rapidly which failure will happen next. It is possible to be applied to trend prognosis of aero-engine abrupt failure in airlines.

Sie haben noch keine Lizenz? Dann Informieren Sie sich jetzt über unsere Produkte:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

  • über 102.000 Bücher
  • über 537 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Maschinenbau + Werkstoffe
  • Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 390 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Maschinenbau + Werkstoffe




 

Jetzt Wissensvorsprung sichern!

Literatur
1.
Zurück zum Zitat Silveira E, Atxaga Irisarri G (2010) Failure analysis of two sets of aircraft blades. Eng Fail Anal 17(3):641–647CrossRef Silveira E, Atxaga Irisarri G (2010) Failure analysis of two sets of aircraft blades. Eng Fail Anal 17(3):641–647CrossRef
2.
Zurück zum Zitat Etemadi AR, Behjati P, Madaah Hosseini HR, Kokabi AH (2010) Failure analysis of brazed air passages of an aircraft fuel system. Eng Fail Anal 17(6):1495–1499CrossRef Etemadi AR, Behjati P, Madaah Hosseini HR, Kokabi AH (2010) Failure analysis of brazed air passages of an aircraft fuel system. Eng Fail Anal 17(6):1495–1499CrossRef
3.
Zurück zum Zitat Ukil A, Zivanovic R (2007) The detection of abrupt changes using recursive identification for power system fault analysis. Electr Power Syst Res 77(3–4):259–265CrossRef Ukil A, Zivanovic R (2007) The detection of abrupt changes using recursive identification for power system fault analysis. Electr Power Syst Res 77(3–4):259–265CrossRef
4.
Zurück zum Zitat Baker A, Rajic N, Davis C (2009) Towards a practical structural health monitoring technology for patched cracks in aircraft structure. Appl Sci Manuf 40(9):1340–1352CrossRef Baker A, Rajic N, Davis C (2009) Towards a practical structural health monitoring technology for patched cracks in aircraft structure. Appl Sci Manuf 40(9):1340–1352CrossRef
5.
Zurück zum Zitat Sathiya Naarayan S, Pavan Kumar DVTG, Chandra S (2009) Implication of unequal rivet load distribution in the failure the and damage tolerant design of metal and composite civil aircraft riveted lap joints. Eng Fail Anal 16(7):2255–2273CrossRef Sathiya Naarayan S, Pavan Kumar DVTG, Chandra S (2009) Implication of unequal rivet load distribution in the failure the and damage tolerant design of metal and composite civil aircraft riveted lap joints. Eng Fail Anal 16(7):2255–2273CrossRef
6.
Zurück zum Zitat Smith Cary, Akujuobi Cajetan M, Hamory Phil, Kloesel Kurt (2007) An approach to vibration analysis using wavelets in an application of aircraft health monitoring. Mech Syst Signal Process 21(3):1255–1272CrossRef Smith Cary, Akujuobi Cajetan M, Hamory Phil, Kloesel Kurt (2007) An approach to vibration analysis using wavelets in an application of aircraft health monitoring. Mech Syst Signal Process 21(3):1255–1272CrossRef
7.
Zurück zum Zitat Pecht M, Jaai R (2010) A prognostics and health management roadmap for information and electronics-rich systems. Microelectron Reliab 50(3):317–323CrossRef Pecht M, Jaai R (2010) A prognostics and health management roadmap for information and electronics-rich systems. Microelectron Reliab 50(3):317–323CrossRef
8.
Zurück zum Zitat Yiakopoulos CT, Gryllias KC, Antoniadis IA (2011) Rolling element bearing fault detection in industrial environments based on a K-means clustering approach. Expert Syst with Appl 38(3):2888–2911CrossRef Yiakopoulos CT, Gryllias KC, Antoniadis IA (2011) Rolling element bearing fault detection in industrial environments based on a K-means clustering approach. Expert Syst with Appl 38(3):2888–2911CrossRef
9.
Zurück zum Zitat Ypma A, Pajunen P (1999) Rotating machine vibration analysis with second-order independent component analysis. In: Proceedings of the first international workshop on independent component analysis and signal separation, pp 37–42 Ypma A, Pajunen P (1999) Rotating machine vibration analysis with second-order independent component analysis. In: Proceedings of the first international workshop on independent component analysis and signal separation, pp 37–42
10.
Zurück zum Zitat Luo M (2006) Data-driven fault detection using trending analysis. PhD Dissertation, Louisiana State University Luo M (2006) Data-driven fault detection using trending analysis. PhD Dissertation, Louisiana State University
Metadaten
Titel
Trend Prognosis of Aero-Engine Abrupt Failure Based on Affinity Propagation Clustering
verfasst von
Limin Li
Zhongsheng Wang
Zhenbao Liu
Shuhui Bu
Copyright-Jahr
2014
Verlag
Springer Berlin Heidelberg
DOI
https://doi.org/10.1007/978-3-642-54233-6_2

Neuer Inhalt