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Design and Realization of Aero-Engine Status Monitor System Platform Based on Various Information

  • Conference paper
  • First Online:
Proceedings of the First Symposium on Aviation Maintenance and Management-Volume II

Part of the book series: Lecture Notes in Electrical Engineering ((LNEE,volume 297))

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Abstract

After collection and classification of aero-engine information, the paper used such technologies as trend analysis and reliability assessment to assess the working status of aero-engines. On this basis, the aero-engine status monitor system platform was designed and applied into reality.

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References

  1. Kejun X, Xinnong Y (2006) Study on assessment method of comprehensive flight conversion ratio for aeroengine. J Propul Technol 17(1):24–29 (in Chinese)

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Author information

Authors and Affiliations

  1. Naval Aeronautical Engineering Institute Qingdao School, Qingdao, 266041, China

    Hongwei Li, Kai Zhang, Shufeng Li & Yan Feng

Authors
  1. Hongwei Li
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  2. Kai Zhang
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  3. Shufeng Li
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  4. Yan Feng
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Corresponding author

Correspondence to Hongwei Li .

Editor information

Editors and Affiliations

  1. Northwestern Polytechnical University, Xi'an, China

    Jinsong Wang

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© 2014 Springer-Verlag Berlin Heidelberg

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Cite this paper

Li, H., Zhang, K., Li, S., Feng, Y. (2014). Design and Realization of Aero-Engine Status Monitor System Platform Based on Various Information. In: Wang, J. (eds) Proceedings of the First Symposium on Aviation Maintenance and Management-Volume II. Lecture Notes in Electrical Engineering, vol 297. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-54233-6_14

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  • DOI: https://doi.org/10.1007/978-3-642-54233-6_14

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  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-54232-9

  • Online ISBN: 978-3-642-54233-6

  • eBook Packages: EngineeringEngineering (R0)

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