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<pubDate xmlns="http://apache.org/cocoon/i18n/2.1">Thu, 12 Mar 2026 22:12:25 GMT</pubDate>
<dc:date>2026-03-12T22:12:25Z</dc:date>
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<title>Microstructural and Mechanical Characterization of the Yb: YAG Laser Welding of High-Pressure Die-Casting Mg-Al-Mn Magnesium Alloy</title>
<link>http://hdl.handle.net/10985/19665</link>
<description>Microstructural and Mechanical Characterization of the Yb: YAG Laser Welding of High-Pressure Die-Casting Mg-Al-Mn Magnesium Alloy
OUALLAM, Seddik; PEYRE, Patrice; DJEGHLAL, Lamine; GUITTONNEAU, Fabrice; BOUTAGHOU, Zoheir; KABA, Liamine; MASSE, Jean-Eric
In this work, the Yb:YAG laser beam welding of the magnesium alloy AM60 was studied. A laser power of 2 kW and a welding speed of 3.5 m / min give a different welding quality than that obtained by CO2 laser with the same parameters. The metallurgical characterization, by optical microscopy, showed the formation of four distinct zones : base metal (BM), heat affected zone (HAZ), the partially fusion zone (PFZ) and the fusion zone (FZ), due to the thermal effect produced by the laser welding thermal cycle. Their dimensions are quantified. The microstructural examination using scanning electron microscopy showed the presence of fine dendritic structure in the FZ although the use of electron dispersive spectroscopy analysis confirm that an eutectic Mg17Al12 phase are surrounded by α-Mg solid solution in the HAZ. Electron backscattered diffraction technique revealed an important grain refinement in FZ and considerable twining phenomena in HAZ, but no texture. X-ray diffraction technique has been used, full width at half maximum of diffraction peaks is measured; it also confirmed the grain refinement in FZ in comparison to BM and HAZ. Both microhardness and tensile proprieties of the complete weld joint are similar to those of the BM.
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<pubDate>Wed, 01 Jan 2020 00:00:00 GMT</pubDate>
<guid isPermaLink="false">http://hdl.handle.net/10985/19665</guid>
<dc:date>2020-01-01T00:00:00Z</dc:date>
<dc:creator>OUALLAM, Seddik</dc:creator>
<dc:creator>PEYRE, Patrice</dc:creator>
<dc:creator>DJEGHLAL, Lamine</dc:creator>
<dc:creator>GUITTONNEAU, Fabrice</dc:creator>
<dc:creator>BOUTAGHOU, Zoheir</dc:creator>
<dc:creator>KABA, Liamine</dc:creator>
<dc:creator>MASSE, Jean-Eric</dc:creator>
<dc:description>In this work, the Yb:YAG laser beam welding of the magnesium alloy AM60 was studied. A laser power of 2 kW and a welding speed of 3.5 m / min give a different welding quality than that obtained by CO2 laser with the same parameters. The metallurgical characterization, by optical microscopy, showed the formation of four distinct zones : base metal (BM), heat affected zone (HAZ), the partially fusion zone (PFZ) and the fusion zone (FZ), due to the thermal effect produced by the laser welding thermal cycle. Their dimensions are quantified. The microstructural examination using scanning electron microscopy showed the presence of fine dendritic structure in the FZ although the use of electron dispersive spectroscopy analysis confirm that an eutectic Mg17Al12 phase are surrounded by α-Mg solid solution in the HAZ. Electron backscattered diffraction technique revealed an important grain refinement in FZ and considerable twining phenomena in HAZ, but no texture. X-ray diffraction technique has been used, full width at half maximum of diffraction peaks is measured; it also confirmed the grain refinement in FZ in comparison to BM and HAZ. Both microhardness and tensile proprieties of the complete weld joint are similar to those of the BM.</dc:description>
</item>
<item>
<title>Etude du soudage TIG de l’alliage d’aluminium 2024-T3</title>
<link>http://hdl.handle.net/10985/8421</link>
<description>Etude du soudage TIG de l’alliage d’aluminium 2024-T3
OUALLAM, Seddik; DJEGHLAL, Lamine; KABBA, L; MASSE, Jean-Eric; BARRALLIER, Laurent
Recent programs of aircraft design are characterized in terms of materials, by introducing weldable alloys as alternatives to the traditional technique of riveting, open the way to reduce weight and allow cost reductions in production and maintenance. Understanding the influence of various parameters of TIG welding process applied to the alloy 2024-T3 aluminum should help us to take into account the behavior in service of assemblies, from the design of structures. This work deals with the definition of a weldability operating field of the alloy studied and metallurgical and mechanical consequences of this assembly on the properties of the material.
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<pubDate>Tue, 01 Jan 2013 00:00:00 GMT</pubDate>
<guid isPermaLink="false">http://hdl.handle.net/10985/8421</guid>
<dc:date>2013-01-01T00:00:00Z</dc:date>
<dc:creator>OUALLAM, Seddik</dc:creator>
<dc:creator>DJEGHLAL, Lamine</dc:creator>
<dc:creator>KABBA, L</dc:creator>
<dc:creator>MASSE, Jean-Eric</dc:creator>
<dc:creator>BARRALLIER, Laurent</dc:creator>
<dc:description>Recent programs of aircraft design are characterized in terms of materials, by introducing weldable alloys as alternatives to the traditional technique of riveting, open the way to reduce weight and allow cost reductions in production and maintenance. Understanding the influence of various parameters of TIG welding process applied to the alloy 2024-T3 aluminum should help us to take into account the behavior in service of assemblies, from the design of structures. This work deals with the definition of a weldability operating field of the alloy studied and metallurgical and mechanical consequences of this assembly on the properties of the material.</dc:description>
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