Aluminum alloys are widely used in the aircraft industries even if such materials present lower ductility with respect to steels, anisotropy phenomena and, more important, they are often 'difficult' to be welded or even 'non-weldable'. In the last years the friction stir welding process (FSW) was proposed and applied in order to get good mechanical and technological performances of the joints. In this paper, an experimental and numerical investigation on the lap joining of AA2198-T4 aluminum alloy blanks by FSW is presented. In particular the joints strength and metallurgical properties are investigated by varying the joint configuration and the tool geometry and rotational speed. It is found that the use of cylindrical-conical pin tools and the correct choice of the relative sheet positioning increase the welded nugget extension and integrity improving the mechanical performances of the obtained joints.
Friction stir welding of lap joints: Influence of process parameters on the metallurgical and mechanical properties
2009
8 Seiten, 29 Quellen
Article (Journal)
English
Aluminiumlegierung , Anwendung in der Luft- und Raumfahrt , Finite-Elemente-Methode , geometrischer Parameter , Luftfahrzeug , mechanische Festigkeit , Metallurgie , Rotationsgeschwindigkeit , Rührreibschweißen , Schweißlinse , Schweißwerkzeug , Theorie-Experiment-Vergleich , Überlappstoß , Verfahrensparameter , Werkzeuggeometrie
Friction stir welding of T-joints
Tema Archive | 2003
|Metallurgical and corrosion features of friction stir welding of AA5O83-H111
Tema Archive | 2006
|Friction stir welding process goes commercial
Tema Archive | 1997
|