2014
DOI: 10.1007/s40430-014-0175-6
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Mechanical and microstructural characterization of laser-welded joints of 6013-T4 aluminum alloy

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Cited by 22 publications
(9 citation statements)
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“…AA 6013 aluminum alloy, also known as an aluminum-magnesium-silicon-copper alloy is widely used in aerospace applications, automotive and aircraft industries [1][2][3]. AA 6013 is evaluated to be a promising aluminum alloy in producing fuselage panels, leading and trailing edges, and engine cowlings due to its improved formability feature, high corrosion resistance and low density [4,5].…”
Section: Introductionmentioning
confidence: 99%
“…AA 6013 aluminum alloy, also known as an aluminum-magnesium-silicon-copper alloy is widely used in aerospace applications, automotive and aircraft industries [1][2][3]. AA 6013 is evaluated to be a promising aluminum alloy in producing fuselage panels, leading and trailing edges, and engine cowlings due to its improved formability feature, high corrosion resistance and low density [4,5].…”
Section: Introductionmentioning
confidence: 99%
“…The ability of a steel body structure to deliver weight savings is limited, so the use of aluminium in auto body structures is increasing, and is projected to expand further in the next decade [3]. Owing to their low density and good mechanical properties, aluminium alloys are increasingly being employed in many important manufacturing areas, such as the automobile industries, aeronautics and the military [4][5][6]. Friction-stir welding (FSW) and laser beam welding (LBW) are noteworthy for their present use in commercial aircraft manufacturing [7][8][9][10][11].…”
Section: Introductionmentioning
confidence: 99%
“…Friction-stir welding (FSW) and laser beam welding (LBW) are noteworthy for their present use in commercial aircraft manufacturing [7][8][9][10][11]. LBW has accounted for a 5% reduction in the weight of Airbus A300 series structures and has also been employed to join some parts of the fuselage [4]. LBW was used to join critical parts in the fuselage in order to mitigate possible materials problems.…”
Section: Introductionmentioning
confidence: 99%
“…As trincas de solidificação podem ocorrer em ligas de alumínio com adição de elementos de liga como Mg, Si e Cu [10]. Muitas ligas tratáveis termicamente, por exemplo, aquelas das classes AA2000 e AA6000, são susceptíveis ao surgimento de trincas durante a soldagem [11]. Este tipo de trinca ocorre quando a fração de líquido interdendrítico não suporta as tensões atuantes durante os últimos estágios de solidificação, resultando nas chamadas trincas do tipo "linha de centro" ou "de cratera", oriundas do meio da zona de fusão.…”
Section: Introductionunclassified