Development of fibre metal laminates for advanced aerospace structures

Citation
Lb. Vogelesang et A. Vlot, Development of fibre metal laminates for advanced aerospace structures, J MATER PR, 103(1), 2000, pp. 1-5
Citations number
2
Categorie Soggetti
Material Science & Engineering
Journal title
JOURNAL OF MATERIALS PROCESSING TECHNOLOGY
ISSN journal
09240136 → ACNP
Volume
103
Issue
1
Year of publication
2000
Pages
1 - 5
Database
ISI
SICI code
0924-0136(20000601)103:1<1:DOFMLF>2.0.ZU;2-W
Abstract
Fibre metal laminates offer significant improvements over current available materials for aircraft structures. While weight reduction and improved dam age tolerance characteristics were the prime drivers to develop these new f amily of materials, it turns out that they have additional benefits which b ecome more and more important for today's designers, e.g, cost reduction an d improved safety. The combination of these aspects in one material is an e xtraordinary achievement. It shows that GLARE is a unique material for airc raft applications. Moreover, it makes clear that, through its unique combin ation of properties, GLARE is a strong candidate material for fuselage skin structures of the new generation of aircraft. (C) 2000 Elsevier Science S. A. All rights reserved.