2018
DOI: 10.1007/s00170-018-1996-8
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Comparative study on successive and simultaneous double-sided laser beam welding of AA6056/AA6156 aluminum alloy T-joints for aircraft fuselage panels

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Cited by 17 publications
(6 citation statements)
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“…It can be observed that, for both of the two hybrid welded joints, the micro-hardness values of the fusion zone and the heat affected zone decreased compared with that of the base material. Some existing research results show that the vaporization of alloying element and the grain size became larger, while the precipitates became less leaded to the reduction of the micro-hardness of the fusion zone and the heat affected zone, respectively [24,25,26]. As shown in Figure 8a,b, two distinct softening regions were identified in the heat affected zone of the two hybrid welded joints: one was in the partially melted zone because the partial melting of the grain boundaries resulted in the diffusion of strengthening alloying elements from solid phase to liquid phase with greater solubility [27]; the other was at a distance away from the fusion line (2.4–4.2 mm for laser-CMT hybrid welded joint and 5.8–8.8 mm for plasma-CMT hybrid welded joint), which, due to the obvious dissolution of β″ strengthening phases and the number of β″ phases, decreases substantially in this region [28].…”
Section: Resultsmentioning
confidence: 99%
“…It can be observed that, for both of the two hybrid welded joints, the micro-hardness values of the fusion zone and the heat affected zone decreased compared with that of the base material. Some existing research results show that the vaporization of alloying element and the grain size became larger, while the precipitates became less leaded to the reduction of the micro-hardness of the fusion zone and the heat affected zone, respectively [24,25,26]. As shown in Figure 8a,b, two distinct softening regions were identified in the heat affected zone of the two hybrid welded joints: one was in the partially melted zone because the partial melting of the grain boundaries resulted in the diffusion of strengthening alloying elements from solid phase to liquid phase with greater solubility [27]; the other was at a distance away from the fusion line (2.4–4.2 mm for laser-CMT hybrid welded joint and 5.8–8.8 mm for plasma-CMT hybrid welded joint), which, due to the obvious dissolution of β″ strengthening phases and the number of β″ phases, decreases substantially in this region [28].…”
Section: Resultsmentioning
confidence: 99%
“…There were two main reasons for the microhardness decrease in the weld seam: firstly, the microhardness of the filler wire was lower than that of the base material; secondly, the alloying elements were burned and lost during the welding process [1,36]. That the grain size became larger and the precipitates became fewer were the causes of the microhardness decrease in the heat-affected zone [37]. Overall, the microhardness values of each zone for the LPMHW joint were lower than that of the LCHW joint, and the microhardness values of the arc zone were also lower than that of the laser zone.…”
Section: Microhardness Distributionmentioning
confidence: 99%
“…By comparison, the width of the heat-affected zone of the LPMHW joint was larger than that of the LCHW joint. It was found that there were two softening regions in the affected zone of the two joints: one was in the partially melted zone because of the loss of strengthening alloying elements in this area [37,38], and the other was at a distance away from the fusion line due to the strengthening phases (β") being dissolved and substantially decreased in this area [39]. Furthermore, the second softening region was more prominent in the arc zone, and was also wider for the LPMHW joint compared with that of the LCHW joint.…”
Section: Mechanical Propertiesmentioning
confidence: 99%
“…The T-joints welding is currently gaining a lot of attention as an alternative to replace riveting as the primary fabrication method of skin-stringer formation [3][4]. The disadvantages of skin-stringer joints formation using rivets include increased weight, relatively high cost, and low productivity [5][6].…”
Section: Introductionmentioning
confidence: 99%