Low velocity impact response of basalt-aluminium fibre metal laminates

被引：61
|
作者：
Ferrante, L. [1 ,3 ]
Sarasini, F. [1 ]
Tirillo, J. [1 ]
Lampani, L. [2 ]
Valente, T. [1 ]
Gaudenzi, P. [2 ]
机构：
[1] Univ Roma La Sapienza, Dept Chem Engn Mat Environm, Via Eudossiana 18, I-00184 Rome, Italy
[2] Univ Roma La Sapienza, Dept Mech & Aerosp Engn, Via Eudossiana 18, I-00184 Rome, Italy
[3] Politecn Torino, Dept Appl Sci & Technol DISAT, Corso Duca Abruzzi 24, I-10129 Turin, TO, Italy
来源：
MATERIALS & DESIGN | 2016年 / 98卷
关键词：
Polymer matrix composites; Fibre metal laminates; Basalt fibres; Low velocity impact; MECHANICAL-BEHAVIOR; DAMAGE TOLERANCE; AEROSPACE STRUCTURES; FRACTURE PROPERTIES; AIRCRAFT STRUCTURES; COMPOSITES; GLARE; FATIGUE; APPLICABILITY; RESISTANCE;
D O I：
10.1016/j.matdes.2016.03.002
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
This work reports on a preliminary study to assess the response of fibre metal laminates (FMLs) made of stacked layers of basalt fabric epoxy prepreg and aluminium sheets to low velocity impact and, through comparison with published results for Glare materials, benchmark their impact performance. Comparison is also made with results from plates of monolithic aluminium with comparable thickness. The effect of impactor size is also investigated whilst the impact energies were selected with the aim of inducing first crack (FC) and through the thickness crack (TTT) on the FML samples. Optical microscopy and profilometry were used to elucidate fracture mechanisms and the dent depth. The response of basalt fibre metal laminates was found to be both significantly influenced by the impactor size and fairly positive, proving to be competitive with monolithic aluminium plates although some issues about the aluminium basalt interface have been raised. (C) 2016 Elsevier Ltd. All rights reserved.
引用
收藏
页码：98 / 107
页数：10
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