Double-sided fiber laser beam welding process of T-joints for aluminum aircraft fuselage panels: Filler wire melting behavior, process stability, and their effects on porosity defects-Reference-Cited by-同舟云学术

Double-sided fiber laser beam welding process of T-joints for aluminum aircraft fuselage panels: Filler wire melting behavior, process stability, and their effects on porosity defects

Published:2013-11 Issue: Volume:52 Page:1-9
ISSN:0030-3992
Container-title:Optics & Laser Technology
language:en
Short-container-title:Optics & Laser Technology

Author:

Tao Wang,Yang Zhibin,Chen Yanbin,Li Liqun,Jiang Zhenguo,Zhang Yunlong

Funder

National Engineering Research Center of Commercial Aircraft Manufacturing

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Electrical and Electronic Engineering,Atomic and Molecular Physics, and Optics,Electronic, Optical and Magnetic Materials

Reference26 articles.

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2. Neye G, Laserstrahlschweiβkonzept für Rumpfschalen-strukturen, Strahltechnik, Band 5, Bremen: Bias-Verlag; 1997 [Hrsg Sepold G, Jüptner W. ISBN: 3-9805011-5-9], German.

3. Welding process for aeronautics;Mendez;Advanced Materials Proceedings,2001

4. Assessment of fracture and fatigue crack propagation of laser beam and friction stir welded aluminum alloys;Vaidya;Advanced Engineering Materials,2006

5. Brenner B, Standfuβ J, Morgenthal L, Dittrich D, Fux V, Winderlich B, et al., Neue technoloqische aspekte des laserstrahlschweiβens von flugzeugstrukturen, DVS, Düsseldorf; 2004. p. 19–24 [German].

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