Stress-dependent χ phase transformation in a Ni-based superalloy

Abstract The ongoing push to elevate operating temperatures in aerospace gas turbine engines – driven by goals of enhanced fuel efficiency and reduced CO 2 emissions – mandates advancements in the creep resistance of Ni- and Co-based superalloys, which are integral for critical engine components. This study elucidates the role of stress assisted localized phase transformations in the creep properties of these alloys. By leveraging chemo-mechanical coupling, self-healing γ ′ precipitates are designed to immobilize planar defects, thereby increasing creep resistance. Employing advanced characterization techniques such as high-resolution Scanning Transmission Electron Microscopy (HR-STEM), in conjunction with atomistic simulations and thermodynamic calculations, novel deformation pathways facilitated by χ local phase transformation (LPT) strengthening have been uncovered; notably, the formation of χ nano-laths through microtwinning and superlattice intrinsic stacking fault (SISF) shearing. This study highlights critical insights into the compositional boundaries necessary for optimizing LPT strengthening while avoiding deleterious bulk formation of η / χ phases. These advancements will guide the design of new alloys maximizing high-temperature creep strength for advanced aerospace applications.

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Publication Details

Journal
Communications Materials
Published
2025-08-14
DOI
https://doi.org/10.1038/s43246-025-00895-z
Citations
1
Primary Topic
High Temperature Alloys and Creep
Type
article
Field-Weighted Citation Impact
0.71

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article

Stress-dependent χ phase transformation in a Ni-based superalloy

N. S. Harsha Gunda, Yunzhi Wang, Longsheng Feng, Maryam Ghazisaeidi et al.
1 citations
Communications Materials
High Temperature Alloys and Creep
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article

Stress-dependent χ phase transformation in a Ni-based superalloy

N. S. Harsha Gunda, Yunzhi Wang, Longsheng Feng, Maryam Ghazisaeidi, Sammy Tin, Ashton J. Egan, Michael J. Mills
article en
1 citations

Abstract

Abstract The ongoing push to elevate operating temperatures in aerospace gas turbine engines – driven by goals of enhanced fuel efficiency and reduced CO 2 emissions – mandates advancements in the creep resistance of Ni- and Co-based superalloys, which are integral for critical engine components. This study elucidates the role of stress assisted localized phase transformations in the creep properties of these alloys. By leveraging chemo-mechanical coupling, self-healing γ ′ precipitates are designed to immobilize planar defects, thereby increasing creep resistance. Employing advanced characterization techniques such as high-resolution Scanning Transmission Electron Microscopy (HR-STEM), in conjunction with atomistic simulations and thermodynamic calculations, novel deformation pathways facilitated by χ local phase transformation (LPT) strengthening have been uncovered; notably, the formation of χ nano-laths through microtwinning and superlattice intrinsic stacking fault (SISF) shearing. This study highlights critical insights into the compositional boundaries necessary for optimizing LPT strengthening while avoiding deleterious bulk formation of η / χ phases. These advancements will guide the design of new alloys maximizing high-temperature creep strength for advanced aerospace applications.

Communications MaterialsVol. 6(1)
Lawrence Livermore National Laboratory (US), University of Arizona (US), Friedrich-Alexander-Universität Erlangen-Nürnberg (DE), The Ohio State University (US), Indian Institute of Technology Delhi (IN)
National Science Foundation, U.S. Department of Energy, Alexander von Humboldt-Stiftung, Ohio State University, Lawrence Livermore National Laboratory
Openalex Percentile: Top 27%
High Temperature Alloys and Creep
0.71
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