W. Zink

Differentially built up aluminium structures, using riveting and bonding processes have been proven successfully on aircraft structures over the last decades. This design has nearly permitted the highest degree of required performance level and automation in production so that further weight and cost reduction is largely exhausted. Further improvements can only be obtained by a fundamental different design approach. EADS Airbus Germany has worked out within a government funded technology project new concepts for integrally stiffened fuselage structures using Laser Beam Welding technique. This challenge needs a highly interdisciplinary proceeding with respect to material, process, stress, design and quality assurance aspects.

19th European Conference on Materials for Aerospace Applications, Munich, Germany, 2000

Book Chapter

englisch

14,8 x 21,0 cm, 8 Seiten

DGLR-Bericht, 2001, 2001-02, Advanced Aerospace Materials - Proceedings 2000 ; S.25-32; 2001; Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn

NA

fuselages, structural design, aeronautics

Bibliothek

2001