Structure-property investigations on a laser beam welded dissimilar joint of aluminium AA6056 and titanium Ti6Al4V for aeronautical applications Part I: Local gradients in microstructure, hardness and strength

Author:

Vaidya W.V.,Horstmann M.,Ventzke V.,Petrovski B.,Koçak M.,Kocik R.,Tempus G.

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science

Reference42 articles.

1. K.-H. Rendigs: Aluminium structures used in aerospace- status and prospects, Mater. Sci. Forum, 1997, 242, 11.

2. R. Kocik, S. Kaschel, M. Kreimeyer, J. Schumacher, F. Vollertsen: Development of a new joining technology for hybrid metal aircraft structures, in ICALEO 2004, Proc. 23rd Int. Conf. on Application of Lasers and Electro-Optics 2004, San Francisco, California, USA, 04-07 Oct. 2004, Laser Institute of America (LIA) Congr. Proc., CD-ROM 597, LIA, Orlando, Florida, USA, 2004.

3. R. Kocik, T. Vugrin, T. Seefeld: Laser beam welding in airframe structures, status and future applications, (in German), in 5. Laser-Anwendungforum, 13-14. Sept., 2006, Bremen, Laserstrahlfügen: Prozesse, Systeme, Anwendungen, Trends, (ed. F. Vollertsen und T. Seefeld), Strahltechnik, Band 28, Bremen, Germany, BIAS-Verlag, 2006, 15.

4. N. Bailey: Review of metallurgical problems in dissimilar metal welding, in Welding Dissimilar Metals, (ed. N. Bailey), The Welding Institute, Cambridge, Great Britain, 1986, 1.

5. K. Bing, B. Eigenmann, B. Scholtes, E. Macherauch: Brazing residual stresses in components of different metallic materials, Mater. Sci. Engng. A, 1994, A174, 95.

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