2020
DOI: 10.1002/mawe.201900113
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Microstructure and fatigue performance of friction stir welded joints of 2A12‐T4 and 7075‐T6 dissimilar aluminum alloy

Abstract: The objective of this work is to investigate the microstructure and fatigue performance of friction stir welding joint of 2A12‐T4 and 7075‐T6 dissimilar aluminum alloy. Microstructure shows that the grain growth of heat‐affected zone in both sides of joint is noticeable; the grain size of thermo‐mechanically affected zone in both sides of joint is deformed and distorted in various degrees; nugget zone is fine equiaxed grain with uniform distribution. Microhardness of joint presents an approximate “W” types dis… Show more

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Cited by 4 publications
(3 citation statements)
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“…Wang et al [7] analyzed the microstructure and properties of the friction stir joining zone of 2195-T8/2219-T87 dissimilar aluminum alloy and obtained that the joining zone showed a basin shape, the grain size of the heat-affected zone of the joining zone dramatically changed, and the hardness of the joining zone was the highest on the side of 2195-T8 aluminum alloy and the lowest. fang et al [8] studied the friction stir lap of 2a12-T4/7a09-T6 aluminum alloy and obtained that the interface curve between the lap plates was curved when the lap was from 2a12-T4 (1.2 mm) to 7a09-T6 (4 mm). Moreover, when the lap is from 7a09-T6 (4 mm) to 2a12-T4 (1.2 mm), the surface curve between the lap plate bending is small in a horizontal state.…”
Section: Introductionmentioning
confidence: 99%
“…Wang et al [7] analyzed the microstructure and properties of the friction stir joining zone of 2195-T8/2219-T87 dissimilar aluminum alloy and obtained that the joining zone showed a basin shape, the grain size of the heat-affected zone of the joining zone dramatically changed, and the hardness of the joining zone was the highest on the side of 2195-T8 aluminum alloy and the lowest. fang et al [8] studied the friction stir lap of 2a12-T4/7a09-T6 aluminum alloy and obtained that the interface curve between the lap plates was curved when the lap was from 2a12-T4 (1.2 mm) to 7a09-T6 (4 mm). Moreover, when the lap is from 7a09-T6 (4 mm) to 2a12-T4 (1.2 mm), the surface curve between the lap plate bending is small in a horizontal state.…”
Section: Introductionmentioning
confidence: 99%
“…Aluminum and aluminum alloys were widely used in automation areas and aerospace industries because of its excellent characteristics that include lower density, high strength properties and easy molding 1–3 . As an aviation material, 2024 aluminum alloy was widely used in aircraft fuselages.…”
Section: Introductionmentioning
confidence: 99%
“…Aluminum and aluminum alloys were widely used in automation areas and aerospace industries because of its excellent characteristics that include lower density, high strength properties and easy molding. [1][2][3] As an aviation material, 2024 aluminum alloy was widely used in aircraft fuselages. Aircraft located at coastal airports flew or parked in high humidity, high salt marine environments, where seawater or the humid marine atmosphere had caused serious corrosion damage to the aluminum alloy components of the aircraft.…”
Section: Introductionmentioning
confidence: 99%