2016
DOI: 10.1063/1.4937829
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Structure of Ti-6Al-4V nanostructured titanium alloy joint obtained by resistance spot welding

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Cited by 5 publications
(4 citation statements)
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“…The elastic modulus of the BM was lower than that of the FZ and HAZ [29,30]. Therefore, fatigue cracks are more likely to initiate in the FZ, considering the microstructure defects and high-stress levels in the FZ [31]. Furthermore, the stress values along the other directions are small and can be neglected concerning the failure of welding joints.…”
Section: Resultsmentioning
confidence: 99%
“…The elastic modulus of the BM was lower than that of the FZ and HAZ [29,30]. Therefore, fatigue cracks are more likely to initiate in the FZ, considering the microstructure defects and high-stress levels in the FZ [31]. Furthermore, the stress values along the other directions are small and can be neglected concerning the failure of welding joints.…”
Section: Resultsmentioning
confidence: 99%
“…Сплавы синтезировали в шести режимах (рис.1б), отличающихся длительностью спада основного сварочного импульса тока. Высота литого ядра во всех случаях составляла около 80-90 % от общей толщины соединяемых пластин (рис.3), что характерно при КТС титановых сплавов из-за их высокого удельного сопротивления [14].…”
Section: материалы и методыunclassified
“…This titanium alloy is used widely in the aerospace industry to produce large-scale welded and prefabricated aircraft constructions, internal pressure capacities in an extensive range of temperatures from − 196 to 450 °C, and many other structural components of the rocket, aviation, and civil engineering [24].…”
Section: Titanium Alloysmentioning
confidence: 99%
“…Fig 24. Load vs displacement plots of the (a) uncoated, and (b) CNT-coated welded samples at the best welding parameters[36] …”
mentioning
confidence: 99%