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Research on vibration problem of integral mistuned bladed disk assemblies at home and abroad

  • Bin Bai*
  • , Guang Chen Bai
  • , Xiao Chen Tong
  • , Zhe Xu
  • , Xiao Ying Li
  • *Corresponding author for this work
  • Beihang University
  • State Intellectual Property Office of the Peoples Republic of China
  • Hebei United University

Research output: Contribution to journal › Article › peer-review

Abstract

Mistuned integral bladed disk assemblies, including the mode, the vibration transmission localization and the localization factors, were elaborated. Besides, the modeling and solving methods of mistuned bladed disk assemblies were discussed. The mainly related hot topics, the latest research methods and their achievements in recent 10years, were reviewed and investigated in detail, including: nonlinearity, flutter, sensitivity, pneumatic and structure coupling, mistuning identification and prediction, mistuning optimization, intentionally mistuning, multi-stage and multi-component disks coupling, Coriolis forces, reliability and robustness etc. Finally, potential topics for future research work were proposed, for instance, building a more effective and applicative model with higher precision, verifying theoretical simulation with the test method, impact on multi-stage and multi-component integral bladed disk assemblies of pneumatic and structure coupling as well as the shroud tip and friction coupling, the principle of Coriolis forces, insensitivity and robustness to the mistuning of bladed disk assemblies and so on.

Original languageEnglish
Pages (from-to)91-103
Number of pages13
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume29
Issue number1
DOIs
StatePublished - Jan 2014

Keywords

  • Integral bladed disk assemblies
  • Localization
  • Mistuned vibration
  • Reliability
  • Robustness

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