Multi-stage precipitation modeling for AA 7050 hole repairs in additive friction stir deposition

A multi-stage precipitation model is formulated to predict the microstructural evolution and explain the high performance of additive friction stir deposited aluminum alloy 7050 (AA 7050) for hole repair. The first stage is the heating process due to the high-temperature thermomechanical process of the stir. In this process, small η precipitates dissolve as they lose their stability with increasing temperature, and this causes the volume fraction of η precipitates to decrease and the concentration of Mg and Zn in the matrix to increase. The second stage is the cooling process at the end of the repair where material feeding ends and the tool is lifted away. Heterogeneous nucleation of η precipitates may occur and as the temperature cools below 250 °C, Guinier–Preston (GP) zones start to form. The final stage is the natural aging process, where the η′ precipitate starts to grow. The volume fraction and precipitate radius are predicted for each type of precipitate. Furthermore, the fine η′ precipitates and GP zones with a decent volume fraction improve the material strength and fatigue life.

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Publication Details

Journal
Journal of Applied Physics
Published
2024-10-23
DOI
https://doi.org/10.1063/5.0221890
Citations
4
Primary Topic
Aluminum Alloy Microstructure Properties
Type
article
Field-Weighted Citation Impact
5.20

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article

Multi-stage precipitation modeling for AA 7050 hole repairs in additive friction stir deposition

Greg D. Hahn, Manoj R. Rajanna, Kendall P. Knight, Alan Timmons et al.
4 citations
Journal of Applied Physics
Aluminum Alloy Microstructure Properties
5.20
article

Multi-stage precipitation modeling for AA 7050 hole repairs in additive friction stir deposition

Greg D. Hahn, Manoj R. Rajanna, Kendall P. Knight, Alan Timmons, Nam Phan, G. A. W. Murray, Jim Lua, B. Feng
article en
4 citations

Abstract

A multi-stage precipitation model is formulated to predict the microstructural evolution and explain the high performance of additive friction stir deposited aluminum alloy 7050 (AA 7050) for hole repair. The first stage is the heating process due to the high-temperature thermomechanical process of the stir. In this process, small η precipitates dissolve as they lose their stability with increasing temperature, and this causes the volume fraction of η precipitates to decrease and the concentration of Mg and Zn in the matrix to increase. The second stage is the cooling process at the end of the repair where material feeding ends and the tool is lifted away. Heterogeneous nucleation of η precipitates may occur and as the temperature cools below 250 °C, Guinier–Preston (GP) zones start to form. The final stage is the natural aging process, where the η′ precipitate starts to grow. The volume fraction and precipitate radius are predicted for each type of precipitate. Furthermore, the fine η′ precipitates and GP zones with a decent volume fraction improve the material strength and fatigue life.

Journal of Applied PhysicsVol. 136(16)
Naval Air Systems Command (US), Global Engineering and Materials (United States) (US), Virginia Tech (US)
Naval Air Systems Command
Openalex Percentile: Top 5%
Aluminum Alloy Microstructure Properties
5.20
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