4.7 Article

Thermomechanical fatigue failure investigation on a single crystal nickel superalloy turbine blade

Journal

ENGINEERING FAILURE ANALYSIS
Volume 66, Issue -, Pages 284-295

Publisher

PERGAMON-ELSEVIER SCIENCE LTD
DOI: 10.1016/j.engfailanal.2016.04.016

Keywords

Turbine blade failure; Fatigue testing; Fatigue crack; Finite element analysis

Funding

  1. National Natural Science Foundation of China (NSFC) [51375031, 51305012]
  2. Aviation Science Fund of China [2014ZB51]

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A thermomechanical fatigue (TMF) test rig was developed consisting of the loading, heating, synchronizing, cooling and monitoring systems. Moreover, the specimen was particularly designed to provide adequate load-bearing capability at the blade tip in order to simulate the actual turbine blade loads in laboratory. TMF test on a single crystal nickel superalloy turbine blade was conducted. Then the specimen was segmented in a novel way to preserve the crack surface to investigate the TMF mechanism of the turbine blade. Visual examination together with the metallographic analysis indicated that the most severe TMF damage occurred at the pin-fin fillet on the suction side near the trailing edge. Furthermore, finite element simulation results were compared to the experiment, in which a viscoplastic constitutive model was employed. (C) 2016 Elsevier Ltd. All rights reserved.

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