Cyclic Creep Deformation Characteristics Of Single Crystal Of Nickle Basesuperalloy CMSX 3

  • J. Zrník
  • Z. G. Wang
  • Y. Yu
  • J. A. Wang
  • M. Žitňanský
  • P. Horňak
Part of the NATO ASI Series book series (NSSB, volume 355)

Abstract

High temperature components assembled in aircraft turbines are subjected to complex stress, including thermal stress, stress originating from centrifugal force and high frequency vibration stress. Recently increased attention has been paid to the study of creep and fatigue interaction which appears to be an important factor in the prediction of the components’ life1,2.

Keywords

Fatigue Nickel 

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Copyright information

© Plenum Press, New York 1996

Authors and Affiliations

  • J. Zrník
    • 1
  • Z. G. Wang
    • 1
  • Y. Yu
    • 2
  • J. A. Wang
    • 2
  • M. Žitňanský
    • 3
  • P. Horňak
    • 4
  1. 1.Technical University of KošiceSlovakia
  2. 2.Institute of Materials Research Academia SinicaShenyangChina
  3. 3.Dalian University of TechnologyChina
  4. 4.Slovak Technical UniversityBratislavaSlovakia

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