A review: Fibre metal laminates, background, bonding types and applied test methods

SINMAZÇELİK T., AVCU E., BORA M. Ö., ÇOBAN O.

MATERIALS & DESIGN, cilt.32, sa.7, ss.3671-3685, 2011 (SCI-Expanded) identifier identifier

  • Yayın Türü: Makale / Derleme
  • Cilt numarası: 32 Sayı: 7
  • Basım Tarihi: 2011
  • Doi Numarası: 10.1016/j.matdes.2011.03.011
  • Dergi Adı: MATERIALS & DESIGN
  • Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
  • Sayfa Sayıları: ss.3671-3685
  • Anahtar Kelimeler: Sandwich structures, Surface treatments, Mechanical, FATIGUE-CRACK GROWTH, MECHANICALLY FASTENED JOINTS, VELOCITY IMPACT RESPONSE, BOLTED COMPOSITE JOINTS, FIBRE/MATRIX ADHESION, ALUMINUM-ALLOYS, SURFACE PRETREATMENT, DELAMINATION GROWTH, FRACTURE PROPERTIES, CO2-LASER TREATMENT
  • Kocaeli Üniversitesi Adresli: Evet

Özet

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. (C) 2011 Elsevier Ltd. All rights reserved.