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Hot Deformation Behavior and Processing Map Considering Strengthening Effect for Al-10.0Zn-3.0Mg-2.8Cu Alloy
Si-Qi Wang1, Xi Zhao1, Xian-Wei Ren2
1School of Aerospace Engineering, North University of China, Taiyuan 030051, China.
Optimizing hot processing for Al-10.0Zn-3.0Mg-2.8Cu alloy enhances aging effects by refining insoluble phases. The ideal processing window is identified for improved performance in aerospace and defense applications.
Area of Science:
- Materials Science
- Metallurgy
- Mechanical Engineering
Background:
- High-performance aluminum alloys are critical for aerospace and defense.
- Understanding hot deformation behavior is key to optimizing alloy properties.
- Al-10.0Zn-3.0Mg-2.8Cu alloy requires precise processing for desired mechanical outcomes.
Purpose of the Study:
- To optimize the hot processing map for Al-10.0Zn-3.0Mg-2.8Cu alloy.
- To investigate the influence of insoluble phase behavior on strengthening.
- To determine optimal processing parameters for enhanced aging effects.
Main Methods:
- Hot deformation experiments using compression testing (0.001–1 s-1 strain rates, 380–460 °C).
- Establishment of a hot processing map at 0.9 strain.
- Real-time Electron Backscatter Diffraction (EBSD) and Energy Dispersive Spectroscopy (EDS) detection.
Main Results:
- Optimal hot processing region identified: 431–456 °C and 0.004–0.108 s-1 strain rate.
- Insoluble phase refinement and dissolution were observed to enhance work hardening consumption.
- Strain rates around 0.1 s-1 promote better insoluble phase dissolution for superior aging effects.
Conclusions:
- The study refines the optimal hot processing strain rate to approximately 0.1 s-1 for Al-10.0Zn-3.0Mg-2.8Cu alloy.
- Optimized processing parameters provide theoretical support for engineering applications in aerospace and defense.
- Understanding insoluble phase evolution is crucial for maximizing alloy strengthening potential.
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