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Creep Behavior and Its Influencing Factors in High-Entropy Superalloys: A Molecular Dynamics Simulation Study
Kangning Han1, Qiuju Wang1,2, Yaxin Zhu1,3
1Department of Engineering Mechanics, School of Aerospace Engineering, Huazhong University of Science and Technology, Wuhan 430074, China.
High-entropy superalloys show excellent creep resistance for turbine blades. Molecular dynamics reveal temperature, stress, and microstructure significantly influence deformation mechanisms and performance.
Area of Science:
- Materials Science
- Mechanical Engineering
- Computational Materials Science
Background:
- Turbine blades in aero-engines require materials with exceptional mechanical performance under extreme thermomechanical cyclic loading.
- High-entropy superalloys (HESAs) with a stable dual-phase γ/γ' microstructure offer promising high-temperature structural material properties, particularly superior creep resistance.
Purpose of the Study:
- To systematically investigate the creep behaviors of high-entropy superalloys.
- To explore the influence of stress, temperature, γ/γ' lattice misfit, and γ' volume fraction on creep deformation mechanisms using molecular dynamics simulations.
Main Methods:
- Molecular dynamics (MD) simulations were employed to study creep deformation.
- Systematic variation of stress, temperature, lattice misfit, and volume fraction of the γ' phase.
- Microstructural analysis and atomic diffusion data were utilized to understand creep mechanisms.
Main Results:
- Temperature has a more dominant effect on creep behavior than stress.
- Increasing stress shifts the dominant creep mechanism from atomic diffusion to dislocation nucleation/motion and phase transformation.
- Creep resistance is critically dependent on γ/γ' lattice misfit and γ' volume fraction; negative misfit and increased γ' volume fraction enhance creep resistance.
- Structural stability of the γ/γ' dual-phase system is closely linked to creep resistance.
Conclusions:
- High-entropy superalloys exhibit tunable creep resistance influenced by operational conditions and microstructural parameters.
- Optimizing lattice misfit and γ' volume fraction is crucial for enhancing the high-temperature performance of these alloys.
- Findings provide insights for designing advanced high-entropy superalloys for demanding aero-engine applications.
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