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Reliability assessment of a fault tolerant propulsion system for an electrical helicopter

  • Technical University of Munich

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

14 Scopus citations

Abstract

The paper describes an approach and a methodology of quantitative reliability assessment of fault tolerant propulsion systems for an electrical helicopter. As a comprehensive parameter for the assessment of fault tolerance of the components with a number of degradation states, it is proposed to use the criterion 'degree of fault tolerance'. On the basis of such a parameter the transition probabilities have been defined for the Multi-State System reliability Markov Models. The simulation and assessment results allow concluding, which power train topology complies best with the design requirements on the reliability and the future operational conditions of electrical helicopters.

Original languageEnglish
Title of host publication2017 12th International Conference on Ecological Vehicles and Renewable Energies, EVER 2017
PublisherInstitute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)9781538616925
DOIs
StatePublished - 30 May 2017
Event12th International Conference on Ecological Vehicles and Renewable Energies, EVER 2017 - Monte-Carlo, Monaco
Duration: 11 Apr 201713 Apr 2017

Publication series

Name2017 12th International Conference on Ecological Vehicles and Renewable Energies, EVER 2017

Conference

Conference12th International Conference on Ecological Vehicles and Renewable Energies, EVER 2017
Country/TerritoryMonaco
CityMonte-Carlo
Period11/04/1713/04/17

Keywords

  • Multi-State Markov Model
  • electrical helicopter
  • fault tolerance
  • multilevel inverter
  • reliability
  • traction multi-phase motor

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