2022
DOI: 10.1016/j.matchar.2022.111871
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Microstructure and corrosion behavior of linear friction welded TA15 and TC17 dissimilar joint

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Cited by 14 publications
(3 citation statements)
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“…Specifically, considering a pressure-resistant hull of marine parts with bulged flanges, the flanges do not require as high a strength as the pressure-resistant hull because the pressures on either side of them are equivalent. Therefore, parts serving in the marine environment tend to require composite connections of dissimilar titanium alloys so as to achieve a property balance between the structures [6][7][8].…”
Section: Introductionmentioning
confidence: 99%
“…Specifically, considering a pressure-resistant hull of marine parts with bulged flanges, the flanges do not require as high a strength as the pressure-resistant hull because the pressures on either side of them are equivalent. Therefore, parts serving in the marine environment tend to require composite connections of dissimilar titanium alloys so as to achieve a property balance between the structures [6][7][8].…”
Section: Introductionmentioning
confidence: 99%
“…It was clearly observed that, when temperature increases gradually from 585 °C to 700 °C, the fracture morphology of welded zone transforms from intergranular fracture to ductile-brittle mixed fracture and dimple fracture with increasing fracture toughness. Caimei Wang et al [8] joined TA15 and TC17 titanium alloys using friction welding, studied the properties. The TC17 side welding zone (WZ) was composed of coarse β phases, α phase at grain boundaries and martensite α' phase at the grain interior, while the TA15 side WZ consisted of abundant acicular martensite α' phases and few retained β phases.…”
Section: Introductionmentioning
confidence: 99%
“…This alloy has also been widely used in the key load-bearing components and engine structure parts of aerospace applications [1][2][3]. However, titanium alloy has high activity, low thermal conductivity, and high deformation resistance [4][5][6][7], which makes it very difficult to manufacture by traditional manufacturing methods, such as casting [8,9], forging [10,11], and welding [12][13][14]. In addition, aerospace parts tend to be functional, lightweight, and have a structural integrated design [15][16][17][18][19][20][21][22][23].…”
Section: Introductionmentioning
confidence: 99%