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Research on dynamic model of rotors with bearing misalignment

  • Beihang University

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

Based on the structural and mechanics analysis of aero-engines rotor system, the dynamic model of the flexible rotor system with multi-supports are presented in order to solve the bearing misalignment problem of rotor system in aero-engines. The motion equations are derived through Lagrange method. The relationship between structural and mechanics characteristics parameters are built up. Finally, the dynamic influence of bearing misalignment on rotor system is divided into three kinds: additional rotor bending rigidity, additional bearing misalignment excitation force and additional imbalance. The equations suggest that additional imbalance excitation force activates the nonlinearity on rotor system and an additional 2× excitation force might appear.

Original languageEnglish
Title of host publicationAdvanced Engineering Solutions
PublisherTrans Tech Publications Ltd
Pages3-8
Number of pages6
ISBN (Print)9783038350507
DOIs
StatePublished - 2014
Event4th International Conference on Intelligent Structure and Vibration Control, ISVC 2014 - Chongqing, China
Duration: 25 Jul 2014 → 28 Jul 2014

Publication series

NameApplied Mechanics and Materials
Volume539
ISSN (Print)1660-9336
ISSN (Electronic)1662-7482

Conference

Conference4th International Conference on Intelligent Structure and Vibration Control, ISVC 2014
Country/TerritoryChina
CityChongqing
Period25/07/14 → 28/07/14

Keywords

  • Dynamic model
  • Lagrange method
  • Misalignment
  • Rotor

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