FSW of T joints in overlap configuration: process optimization in joining dissimilar aluminium alloys for the aeronautic application

Authors


Correspondence to: S. Ciliberto, Department of Materials and Production Engineering, University of Napoli Federico II, Piazzale Tecchio 80, 80126 Napoli, Italy.

E-mail: stefano.ciliberto@unina.it

Abstract

The effect of welding parameters on the mechanical properties of friction stir-welded dissimilar aluminium alloys in overlap joint configuration was studied. Both the welding configuration and the materials chosen were a typical skin-stringer configuration, widely used for aeronautical fuselage panels. Mechanical properties were evaluated by means of both hoop stress and T-pull test. Results show that there is a great dependence of the hoop stress resistance from welding parameters; conversely, T-pull tests do not show the same dependence. The present work demonstrates the suitability of the x in lap configuration for joining dissimilar aluminium alloys. Copyright © 2013 John Wiley & Sons, Ltd.

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