Aircraft Gas Turbine Rotating Compressor Disk Vibration PUBLIC ACCESS

[+] Author Affiliations
R. F. French

General Electric Company, Cincinnati, OH

Paper No. 65-WA/GTP-11, pp. V001T01A005; 12 pages
  • ASME 1965 Winter Annual Meeting: GT Papers
  • ASME 1965 Winter Annual Meeting: GT Papers
  • Chicago, Illinois, USA, November 7–11, 1965
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-8008-1
  • Copyright © 1965 by ASME


This paper is concerned with the experimental investigation of vibration in aircraft jet-engine rotating compressor disks of two different configurations. The blades in the first configuration were small, with relatively low mass, and had an insignificant effect on the disk vibration except for centrifugal loading. The second configuration had relatively large blades which resulted in combined blade and disk modes. The test techniques, test results, and examples of some known phenomenon as they occur in lightweight aircraft jet-engine disks are discussed.

Copyright © 1965 by ASME
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