Abstract

Low cycle fatigue (LCF) of a low-carbon (LC) directionally-solidified (DS) nickel-base superalloy, CM247 LC DS, was investigated using both experimental and computational methods. Strain-controlled LCF tests were conducted at 850°C, with a loading direction either parallel or perpendicular to the solidification direction. Trapezoidal loading-waveforms with 2s and 200s dwell times imposed at the minimum and the maximum strains were adopted for the testing. A constant strain range of 2% was maintained throughout the fully-reversed loading conditions (strain ratio R = −1). The observed fatigue life was shorter when the loading direction was perpendicular to the solidification one, indicating an anisotropic material response. It was found that the stress amplitude remained almost constant until final fracture, suggesting limited cyclic hardening/softening. Also, stress relaxation was clearly observed during the dwell period. Scanning Electron Microscopy fractographic analyses showed evidence of similar failure modes in all the specimens. To understand deformation at grain level, crystal plasticity finite element modelling was carried out based on grain textures measured with EBSD. The model simulated the full history of cyclic stress-strain responses. It was particularly revealed that the misorientations between columnar grains resulted in heterogeneous deformation and localised stress concentrations, which became more severe when the loading direction was normal to a solidification direction, explaining the shorter fatigue life observed.

Highlights

  • Nickel based superalloys are widely used as turbine blades and discs in gas turbines operating at high temperatures

  • It was revealed that the misorientations between columnar grains resulted in heterogeneous deformation and localised stress concentrations, which became more severe when the loading direction was normal to a solidification direction, explaining the shorter fatigue life observed

  • 4.1 Low cycle fatigue behaviour For the specimens considered in this study, the LCF life measured in our tests showed considerably high orientation and strain-rate dependencies

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Summary

Introduction

Nickel based superalloys are widely used as turbine blades and discs in gas turbines operating at high temperatures. Moore and Neu [19] reported that the rate of loading and the imposition of a dwell at maximum/minimum load significantly affected fatigue life at higher temperatures Such effects were found for specimens loaded in parallel to the solidification direction. In this paper, we presented a study of fatigue behaviour of a DS nickel-based superalloy, by employing a combination of testing, microstructural characterisation and numerical modelling. Characterisations using EBSD was carried out to establish grain structures and textures, which allowed us, for the 1st time, to consider abnormal grains formed during material processing (a cluster of smaller grains with orientations distinctively different from those of the major columnar grains) These EBSD data were used as input into the finite element (FE) study, and the simulation results were employed to elucidate anisotropic fatigue behaviour observed in the tested specimens. Grain orientations were defined using Euler angles established with EBSD

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