4.7 Article

Effect of microstructure on fatigue resistance of Inconel 740H and Haynes 282 nickel-based alloys at high temperature

Journal

MATERIALS CHARACTERIZATION
Volume 203, Issue -, Pages -

Publisher

ELSEVIER SCIENCE INC
DOI: 10.1016/j.matchar.2023.113095

Keywords

Fatigue crack growth; Fatigue threshold; Dislocation; Oxidation; & gamma;' phase

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The fatigue crack growth behavior of Inconel 740H and Haynes 282 nickel-based alloys was investigated at different temperatures. The results showed an increased fatigue crack growth rate for both alloys, with Inconel 740H exhibiting an increased fatigue threshold at high temperatures. The presence of MC carbides, serrated grain boundaries, and twins affected the crack growth path. The interaction between the strengthening ?' phase and dislocations was different in the two alloys, with Haynes 282 exhibiting shear mechanisms and Inconel 740H exhibiting Orowan bypass mechanisms at elevated temperatures. The resistance of dislocation movement was reduced by cross slip, dislocation climbing, and entanglement, leading to accelerated damage accumulation. The different Cr content in the two alloys promoted the formation of different carbides and oxide layers, which played a role in the fatigue threshold at elevated temperatures.
Fatigue crack growth behavior of Inconel 740H and Haynes 282 nickel-based alloys at 20 C-?, 700 C-? and 750 C-? was studied. Results showed increased fatigue crack growth rate for both the two alloys, while increased fatigue threshold in Inconel 740H at high temperatures. The size and distribution of MC carbides, serrated grain boundaries and twins deflected crack growth path. The strengthening ?' phase was interacted with dislocations by Orowan bypass and shear mechanisms at room temperature, while ?' was sheared in Haynes 282 and Orowan bypassed in Inconel 740H alloy at elevated temperatures. The cross slip, dislocation climbing and entanglement reduced the resistance of dislocation movement and accelerated the accumulation of damage. The higher content of Cr in Haynes 282 alloy promoted formation of M(23)C(6 )carbide while the lower content in Inconel 740H alloy promoted thicker oxide layer. The Cr content needed careful tuning as it was superior to microstructural factors for higher fatigue threshold at elevated temperatures.

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