Paper Title:
Vibration Analysis of Aeroengine Compressor Blade-Disc Coupling System
  Abstract

This paper introduces the FEA method for cyclic symmetric structures and makes an vibration characteristics analysis to a certain aeroengine compressor blade-disc coupling system based on this method. According to the anslysis results the dynamic characteristics of the blade-disc coupling system are discussed. The analysis method and results in this paper can be used for further study on optimal design and vibration safety verification for the blade-disc coupling system.

  Info
Periodical
Edited by
Kai Cheng, Yongxian Liu, Xipeng Xu and Hualong Xie
Pages
264-268
DOI
10.4028/www.scientific.net/AMM.16-19.264
Citation
W. Q. Zhao, Y. X. Liu, M. W. Lu, "Vibration Analysis of Aeroengine Compressor Blade-Disc Coupling System", Applied Mechanics and Materials, Vols. 16-19, pp. 264-268, 2009
Online since
October 2009
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Price
$32.00
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