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Effect of pre-tensile treatments on the mechanical properties and deformation mechanism of a novel Ni-based superalloy

Stacking fault energy can be reduced by adding Co to Ni-based superalloys. In this work, a novel Ni-based superalloy was developed with 20 wt% Co content to reduce the stacking fault energy. After pre-tensile treatments, the alloy formed substructures with numerous dislocations, slip bands, and stac...

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Bibliographic Details
Published in:Materials science & engineering. A, Structural materials : properties, microstructure and processing Structural materials : properties, microstructure and processing, 2023-05, Vol.874, p.145063, Article 145063
Main Authors: Yang, Cheng, Hu, Rui, Wang, Xingmao, Du, Jinhui, Luo, Xian, Bi, Zhongnan, Gan, Bin
Format: Article
Language:English
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Summary:Stacking fault energy can be reduced by adding Co to Ni-based superalloys. In this work, a novel Ni-based superalloy was developed with 20 wt% Co content to reduce the stacking fault energy. After pre-tensile treatments, the alloy formed substructures with numerous dislocations, slip bands, and stacking faults. When the deformation reached 6%, stacking faults in different directions intersected, forming Lomer-Cottrell locks (L-C locks) at the intersections. Mechanical properties were tested at 760 °C. Compared to the standard heat-treated alloy, the yield strength of the alloy with 3% pre-tensile deformation increased by 16.2%, while the stress rupture life maintained 64.2% at 760 °C/480 MPa. The yield strength of the alloy with 6% pre-tensile deformation increased by 29.8%, and the stress rupture life maintained 74.1% at 760 °C/480 MPa. During the tensile process, the densities of stacking faults and deformation twins in the pre-tensile alloys increased, leading to increased hindrance to dislocations and consequently an increase in yield strength. The grain boundaries of the pre-tensile alloy have high dislocation density, and the dislocation recovery and recrystallization softening mechanism occurred during the stress rupture process, resulting in a lower stress rupture life than that of standard heat-treated alloy. As the deformation was increased to 6%, the simultaneous presence of M23C6 and stacking faults enhanced the pinning of dislocations and grain boundaries, improving the stress rupture life of the pre-tensile alloy.
ISSN:0921-5093
1873-4936
DOI:10.1016/j.msea.2023.145063