Fatigue resistange of turbine blade roots under combined stress

Abstract

The paper presents the results of experimental study of vibration proof of gas turbine engine turbine blade roots made of ZhS30 monocrystal structure alloy under conditions of asymmetric vibration stress. The influence of different kinds of blade root surface hardening on the ultimate strength value was studied. Considerable reduction of ultimate stress after blade running has been found.

About the authors

A. V. Gladkov

"KUZNETSOV", Samara

Author for correspondence.
Email: motor@kuznetsov-motors.ru

Head of GT Engine Component Test Development Laboratory

Russian Federation

V. A. Solyannikov

"KUZNETSOV", Samara

Email: motor@kuznetsov-motors.ru

Doctor of Technical Sciences

Head of Design and Research Department

Russian Federation

A. I. Zhuzhukin

"KUZNETSOV", Samara

Email: motor@kuznetsov-motors.ru

Design Engineer

Russian Federation

References

  1. Serensen, S. V. Fatigue strength under combined stress and symmetry cycle [Text] / S. V. Serensen // Some issues of steel fatigue resistance. - M.: Mashgis, - p.
  2. Stepnov, M. N. Statistical processing of the results of mechanical tests [Text] / M. N. Stepnov. - M.: Mashinostroyeniye, - p.
  3. Forrest, P. Metal fatigue [Text] / P. Forrest. - M.: Mashinostroyeniye, - p.
  4. Kolotnikov, M.Ye. Endurance of turbine blade roots under combined stress [Text] / M. Ye. Kolotnikov, K. G. Svyatyshev, A. N. Davydov. - Kiev, - Part - 68 p.

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