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dc.contributor.authorOUALLAM, Seddik
dc.contributor.author
 hal.structure.identifier
DJEGHLAL, Lamine
27672 École nationale polytechnique [Alger, Algérie] [ENP]
dc.contributor.authorBARRALLIER, Laurent
dc.contributor.author
 hal.structure.identifier
KABBA, L
27672 École nationale polytechnique [Alger, Algérie] [ENP]
dc.contributor.author
 hal.structure.identifier
MASSE, Jean-Eric
211915 Mechanics surfaces and materials processing [MSMP]
dc.date.accessioned2014
dc.date.available2014
dc.date.issued2013
dc.date.submitted2014
dc.identifier.urihttp://hdl.handle.net/10985/8421
dc.description.abstractRecent 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.language.isofr
dc.publisherCongrès Français de Mécanique
dc.rightsPost-print
dc.subjectsoudage
dc.subjectaluminium 2024
dc.subjectTIG
dc.titleEtude du soudage TIG de l’alliage d’aluminium 2024-T3
dc.typdocCommunication avec acte
dc.localisationCentre de Aix en Provence
dc.subject.halSciences de l'ingénieur: Matériaux
ensam.audienceNon spécifiée
ensam.conference.titleCongrès français de mécanique (21; 2013; Bordeaux (Gironde))
ensam.conference.date2013-08-26
ensam.countryFrance
ensam.title.proceeding21ème Congrès Français de Mécanique
ensam.page1-6
hal.identifierhal-01059323
hal.version1
hal.statusaccept


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