| METALS AND METAL MATRIX COMPOSITES |
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| Effect of Single-stage Aging on Precipitates and Fatigue Properties of Spray-deposited 7055 Aluminum Alloy |
| GUO Hongfei, WU Jiafang, HOU Xiaohu*, ZHAO Min, ZENG Chao
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| College of Materials Science and Engineering, Inner Mongolia University of Technology, Hohhot 010051, China |
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Abstract Spray deposited 7055 aluminum alloy is widely used in aerospace and defense fields due to its light weight, high strength, good corrosion resistance and toughness. With the development of science and technology, there is a higer requirement for the comprehensive properties of aluminum alloys, especially for fatigue properties. Under the action of long-term strain and alternating load, long-term accumulation of damage will eventually leads to material fracture. In order to improve the fatigue failure, it is necessary to study the influence of different heat treatment processes on the alloy to improve the application performance of the alloy. The microstructure and precipitated phase fatigue fracture morphology of spray deposited 7055 aluminum alloy under three states of under-aging ( 120 ℃×1 h ), peak-aging ( 120 ℃×10 h ) and over-aging ( 120 ℃×44 h ) were analyzed here. The results show that the three aged alloys are under the stress amplitude of 300 MPa. The over-aged alloy shows better fatigue performance, and the fatigue life is 222 000 times. With the extension of aging time, the precipitated phase in the matrix obviously coarsens and grows, and the precipitated phase evolves from GP zone and η′ phase to η′ phase and η phase.
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Published: 10 November 2025
Online: 2025-11-10
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