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Interval analysis of rotor dynamic response based on Chebyshev polynomials

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

科研成果: 期刊稿件文章同行评审

摘要

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.

源语言英语
页(从-至)2342-2356
页数15
期刊Chinese Journal of Aeronautics
33
9
DOI
出版状态已出版 - 9月 2020

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