4.7 Article

Studies on high-temperature fatigue behaviour and mechanism for conventionally cast and directed energy deposited forms of Alloy 625

Journal

INTERNATIONAL JOURNAL OF FATIGUE
Volume 178, Issue -, Pages -

Publisher

ELSEVIER SCI LTD
DOI: 10.1016/j.ijfatigue.2023.108005

Keywords

Alloy 625; Directed energy deposition; Conventionally cast; Microstructure; Low cycle fatigue

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The aim of this study is to investigate the behavior of low cycle fatigue (LCF) and creep-fatigue interaction (CFI) in two product forms of Alloy 625. The results showed that the materials produced using additive manufacturing process have better fatigue life compared to those produced by conventional casting. Microstructural analysis revealed the generation of alternating strain within the microstructure and the occurrence of strain incompatibility in the partitioned regions of fine and neighboring coarser grains. At higher temperatures, additional phenomena such as dynamic strain ageing, oxidation, and creep led to earlier fatigue failure.
The aim of the present work is to study the low cycle fatigue (LCF) and creep-fatigue interaction (CFI) behaviour of two product forms of Alloy 625. Experiments were performed under total strain control mode using triangular and trapezoidal waveforms under complete reverse loading with R = -1, with a total strain amplitude of +/- 0.25 %, +/- 0.4 % and +/- 0.6 % employing a constant strain rate of 3 x 10-3 s- 1 over a temperature range of 298 to 973 K. The additive manufacturing process using the directed energy deposition (DED) technique resulted in an improved fatigue life as compared with the conventional casting (CCA) route. Microstructural analysis using electron back scatter diffraction indicated that an alternating strain got generated within the microstructure and the damage was observed as a strain incompatibility within the partitioned regions of fine and neighbouring coarser grains. The preferred columnar growth occurred in the 001 direction. Inter-dendritic decohesions were attributed to the Mo, Nb and Ti enrichments. While at ambient temperature, an inter-dendritic de-cohesion and strain incompatibility was the cause for final failure, the occurrence of additional time dependent phenomena such as dynamic strain ageing (DSA), oxidation and creep triggered an earlier fatigue failure at elevated temperatures.

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