2019
DOI: 10.1016/j.vacuum.2019.108888
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Laser additive manufacturing of TA15 - Inconel 718 bimetallic structure via Nb/Cu multi-interlayer

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Cited by 35 publications
(10 citation statements)
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“…Bobbio et al [14] used the directed energy deposition (DED) to form linearly graded Ti-6Al-4V/Invar 36 FGM; however, the samples prepared in his work had macroscopic cracks, which were assumed to be caused by the mismatches of the secondary phases in thermal expansion and elastic modulus. Shang et al [15] fabricated a TA15-Inconel 718 bimetallic structure via Nb/Cu multi-interlayers via laser additive manufacturing, and reported that Ti, Nb, Cu, and Ni elements diffused due to the heat effect of the laser and high-temperature gradient during the deposition process, which effectively prevented the formation of brittle phases while also strengthening the metallurgical bonds between both alloys.…”
Section: Introductionmentioning
confidence: 99%
“…Bobbio et al [14] used the directed energy deposition (DED) to form linearly graded Ti-6Al-4V/Invar 36 FGM; however, the samples prepared in his work had macroscopic cracks, which were assumed to be caused by the mismatches of the secondary phases in thermal expansion and elastic modulus. Shang et al [15] fabricated a TA15-Inconel 718 bimetallic structure via Nb/Cu multi-interlayers via laser additive manufacturing, and reported that Ti, Nb, Cu, and Ni elements diffused due to the heat effect of the laser and high-temperature gradient during the deposition process, which effectively prevented the formation of brittle phases while also strengthening the metallurgical bonds between both alloys.…”
Section: Introductionmentioning
confidence: 99%
“…The formation of Ti–Ni IMCs was inhibited successfully. In order to limit the formation of brittle phases, the Nb/Cu composite transition layer [15] and Ta/Cu composite transition layer [16] were selected with the same thickness (about 2.0 mm) by LDM. The results showed that the Ti–Ni brittle phase was inhibited and the bimetallic structure without metallurgical defects was obtained.…”
Section: Introductionmentioning
confidence: 99%
“…The results showed that the Ti–Ni brittle phase was inhibited and the bimetallic structure without metallurgical defects was obtained. The tensile strength of the Ta/Cu transition layer [16] was higher (about 369 MPa) compared to the Nb/Cu transition layer [15]. Therefore, Ta/Cu is an ideal material for the transition layer of the titanium and nickel-based alloy bimetallic structure.…”
Section: Introductionmentioning
confidence: 99%
“…Lightweight is a vital assessment index in the selection of materials in the aerospace field [1][2][3]. Titanium alloys and aluminum alloys have become the primary structural materials in the aerospace field due to their characteristics of lightweight and high strength [4,5]. Their composite components combine the respective advantages of the two materials.…”
Section: Introductionmentioning
confidence: 99%