Volume 12 Issue 4
Oct.  1997
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Article Navigation >  Journal of Aerospace Power  > 1997  >  12(4): 407-409
Xu Qi, Pan Shengcai. FRETTING FATIGUE OF DOVETAIL JOINT UNDER COMBINED CYCLIC LOADING[J]. Journal of Aerospace Power, 1997, 12(4): 407-409.
Citation: Xu Qi, Pan Shengcai. FRETTING FATIGUE OF DOVETAIL JOINT UNDER COMBINED CYCLIC LOADING[J]. Journal of Aerospace Power, 1997, 12(4): 407-409.
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FRETTING FATIGUE OF DOVETAIL JOINT UNDER COMBINED CYCLIC LOADING

  • 1.

    Yancheng Polytechnical Institutel,Yancheng 224003

  • 2.

    5th Dept.Nanjing University of Aeronautics and Astronautics,Nanjing 210016

  • Received Date: 1996-11-01
  • Rev Recd Date: 1997-05-01
  • Publish Date: 1997-10-28
    Abstract
  • The state-of-art in research on fretting fatigue of dovetail joint in aircraft engine at home and abroad was sized up.Stress analysis of dovetail joint part was carried out.Experimental equipment was desiged and set up.A number of tentative experiments was conducted.It is confirmed that the experimental technique and equipment can offer a great deal of data for designing.

     

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      沈阳化工大学材料科学与工程学院 沈阳 110142

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