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Interval analysis of rotor dynamic response based on Chebyshev polynomials

  • Collaborative Innovation Center for Advanced Aero-Engine
  • Beihang University

Research output: Contribution to journalArticlepeer-review

Abstract

Uncertainty is extensively involved in the rotor systems of rotating machinery, which may cause an unstable vibrational response. To take the uncertainty into consideration for the uncertain rotor-bearing system, an improved unified interval analysis method based on the Chebyshev expansion is established in this paper. Firstly, the Chebyshev Interval Method (CIM) to calculate not only the critical speeds but also the dynamic response of rotor with uncertain parameters is introduced. Then, the numerical investigation is carried out based on the developed double disk rotor model and computation procedure, and the results demonstrate the validity. But when the uncertainty is sufficiently large to influence critical speeds, the upper and lower bounds are far from the actual bounds. In order to overcome the defects, a Bound Correction Interval analysis Method (BCIM) is proposed based on the Chebyshev expansion and the modal superposition. In use of the improved method, the bounds of the interval responses, especially the upper bound, are corrected, and the comparison with other methods demonstrates that the higher accuracy and a wider application range.

Original languageEnglish
Pages (from-to)2342-2356
Number of pages15
JournalChinese Journal of Aeronautics
Volume33
Issue number9
DOIs
StatePublished - Sep 2020

Keywords

  • Aero-engine
  • Chebyshev expansion
  • Interval analysis methods
  • Rotor dynamics
  • Uncertainty

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