Laser beam welded structures for a regional aircraft: weight, cost and carbon footprint savings-Reference-Cited by-同舟云学术

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Laser beam welded structures for a regional aircraft: weight, cost and carbon footprint savings

Published:2016-04 Issue: Volume:39 Page:38-52
ISSN:0278-6125
Container-title:Journal of Manufacturing Systems
language:en
Short-container-title:Journal of Manufacturing Systems

Author:

Alexopoulos Nikolaos D.,Gialos Anastasios A.,Zeimpekis Vasileios,Velonaki Zaneta,Kashaev Nikolai,Riekehr Stefan,Karanika Alexandra

Funder

European Unio

Extra-Laser project

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Hardware and Architecture,Software,Control and Systems Engineering

Reference30 articles.

1. An integrated systems engineering approach to aircraft design;Price;Prog Aerosp Sci,2006

2. Aircraft primary structure and materials. Workshop on Revolutionary Aircraft for Quiet Communities;Montgomery,2007

3. Application of modern aluminum alloys to aircraft;Starke;Prog Aerosp Sci,1996

4. Assessment of the ability of conventional and advanced wrought aluminum alloys for mechanical performance in light-weight applications;Pantelakis;Mater Des,2008

5. Fatigue behavior of the aeronautical Al–Li (2198) aluminum alloy under constant amplitude loading;Alexopoulos;Int J Fatigue,2013

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3. Research progress on the microstructure, mechanical properties and corrosion resistance of friction stir welded of Al-Li alloy joints;Materials Today Communications;2024-06

4. Bridging microstructure and crystallography with the crack propagation behavior in Ti-6Al-4V alloy fabricated via dual laser beam bilateral synchronous welding;Journal of Materials Science & Technology;2024-03

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