材料科学
复合材料
芳纶
铝
眩光
损伤容限
复合材料层合板
胶粘剂
复合数
金属
环氧树脂
玻璃纤维
纤维增强塑料
纤维
图层(电子)
冶金
作者
Tamer Sınmazçelik,Egemen Avcu,Mustafa Özgür Bora,Onur Çoban
出处
期刊:Materials in engineering
[Elsevier]
日期:2011-03-13
卷期号:32 (7): 3671-3685
被引量:833
标识
DOI:10.1016/j.matdes.2011.03.011
摘要
During the past decades, increasing demand in aircraft industry for high-performance, lightweight structures have stimulated a strong trend towards the development of refined models for fibre-metal laminates (FMLs). Fibre metal laminates are hybrid composite materials built up from interlacing layers of thin metals and fibre reinforced adhesives. The most commercially available fibre metal laminates (FMLs) are ARALL (Aramid Reinforced Aluminium Laminate), based on aramid fibres, GLARE (Glass Reinforced Aluminium Laminate), based on high strength glass fibres and CARALL (Carbon Reinforced Aluminium Laminate), based on carbon fibres. Taking advantage of the hybrid nature from their two key constituents: metals (mostly aluminium) and fibre-reinforced laminate, these composites offer several advantages such as better damage tolerance to fatigue crack growth and impact damage especially for aircraft applications. Metallic layers and fibre reinforced laminate can be bonded by classical techniques, i.e. mechanically and adhesively. Adhesively bonded fibre metal laminates have been shown to be far more fatigue resistant than equivalent mechanically bonded structures.
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