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Vibration characteristics investigation of mistuned blisks with receptance substructure component modal synthesis method

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Abstract

To improve the simulation efficiency of mistuned blisk, a method called receptance substructure component modal synthesis method (RSCMSM) is proposed to reduce its degrees of freedom (DOFs). The advantage of this method is that only the interface DOFs need to be solved, which observably enhances the computational efficiency. The modal frequencies, maximum modal shape and frequency response function are calculated via RSCMSM. It is seen that the smooth frequency band is governed by blade vibration and the steep frequency band is governed by disk or bladed-disk coupling vibration. In addition, a peak is observed for the tuned blisk but many peaks appear for the mistuned blisk and many small wave crests are observed near the peak. To verify validity of this method, the computational time of RSCMSM is compared with high fidelity finite element method (HFFEM) and classical substructure component modal synthesis method (CSCMSM), which manifests that the computational efficiency increases by 32.19 %–80.82 % than that of HFFEM when the mistuned level is 0 %~5 %. Moreover, computational efficiency of RSCMSM is increased by 0.85 %–7.56 % than that of CSCMSM. The validity of RSCMSM is verified for calculating the complex mechanical structure.

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Acknowledgments

The authors gratefully acknowledge the financial supports for this research from the National Key Research and Development Plan Project: Grant No. 2017YFB1301300 and the National Natural Science Foundation of China: Grant Nos. 11772011.

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Authors and Affiliations

  1. State Key Laboratory of Reliability and Intelligence of Electrical Equipment, He Bei University of Technology, Tianjin, 300401, China

    Bin Bai, Junyi Zhang & Han Li

  2. School of Mechanical Engineering, He Bei University of Technology, Tianjin, 300401, China

    Bin Bai, Junyi Zhang & Han Li

  3. Avic Tianjin Aviation Electromechanical Co. LTD, Tianjin, 300308, China

    Yanchao Cui

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  1. Bin Bai
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Correspondence to Bin Bai or Yanchao Cui.

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Recommended by Editor No-cheol Park

Bin Bai is an Associate Professor at He Bei University of Technology, China. His main research interests are system dynamics; aeroengine vibration, strength, reliability and robustness design; reliability assessment of industrial robots. He has published more than 20 papers which are indexed by SCI, such as Aerospace Science and Technology, Journal of Aerospace Engineering, Journal of Sound and Vibration, Journal of Mechanisms and Robotics-ASME, etc.

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Bai, B., Zhang, J., Cui, Y. et al. Vibration characteristics investigation of mistuned blisks with receptance substructure component modal synthesis method. J Mech Sci Technol 34, 2715–2729 (2020). https://doi.org/10.1007/s12206-020-0604-7

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  • DOI: https://doi.org/10.1007/s12206-020-0604-7

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