2022
DOI: 10.1016/j.addma.2022.103276
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Additive manufacturing-based repair of IN718 superalloy and high-cycle fatigue assessment of the joint

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Cited by 4 publications
(5 citation statements)
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“…Overall, there was a significant improvement in terms of the material strength in the IN718/TiB 2 deposits in comparison with the IN718 alone; however, the ductility was drastically reduced. The material strength of IN718/TiB 2 is comparable to the solution treated and aged DED IN718 [49].…”
Section: Tensile Propertiesmentioning
confidence: 75%
“…Overall, there was a significant improvement in terms of the material strength in the IN718/TiB 2 deposits in comparison with the IN718 alone; however, the ductility was drastically reduced. The material strength of IN718/TiB 2 is comparable to the solution treated and aged DED IN718 [49].…”
Section: Tensile Propertiesmentioning
confidence: 75%
“…Additive manufacturing metal materials include titanium alloys [ 16 , 17 ], aluminum alloys [ 18 , 19 ], high-temperature alloys [ 20 , 21 , 22 , 23 ], steel [ 24 , 25 , 26 ], and magnesium alloys [ 27 , 28 ]. The raw material forms used in metal additive manufacturing include metal powders and wires [ 29 ], the most widely used of which is metal powder.…”
Section: Metal Additive Manufacturing Formation Processmentioning
confidence: 99%
“…d) Schematics of LDED repaired IN718 superalloy block, grain orientation maps showing the grain morphology and distribution in the LDED repaired joint for the e) direct aged (DA) and f) solution treated and aged (STA) conditions, g) Power‐law‐type S‐N curves, Reproduced with permission. [ 189 ] Copyright 2022, Elsevier. The comparison of S‐N curves of the AMed and wrought IN718 superalloys at h) room temperature (RT) and i) 650 °C, Reproduced with permission.…”
Section: Fatigue Performance Of Amed Metalsmentioning
confidence: 99%
“…Thus, post-heat treatment is mandatory to improve fatigue property. Sarkar et al [189] assessed the high-cycle fatigue property of the IN718 superalloy joint repaired through LDED, and the joint was the region between the substrate and the deposited metal, as shown in Figure 14d. The samples had two conditions, i.e., one was solution-treated and aged (STA), and another was direct aged (DA) only.…”
Section: Fatigue Performancementioning
confidence: 99%
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