Mixed Mode delamination in carbon nanotube/nanofiber interlayered composites

被引:43
作者
Kaynan, Ozge [1 ,3 ]
Atescan, Yagmur [2 ,3 ,5 ]
Ozden-Yenigun, Elif [1 ,3 ,4 ]
Cebeci, Hulya [2 ,3 ]
机构
[1] Istanbul Tech Univ, Dept Text Engn, TR-34469 Istanbul, Turkey
[2] Istanbul Tech Univ, Dept Aeronaut Engn, TR-34469 Istanbul, Turkey
[3] ITU Aerosp Res Ctr, TR-34469 Istanbul, Turkey
[4] Royal Coll Art, Sch Design, Text, London SW7 2EU, England
[5] Penn State Univ, Dept Aerosp Engn, 229 Hammond, University Pk, PA 16802 USA
关键词
Carbon nanotubes; Nanofibers; Electrospinning; Interlaminar fracture toughness; Mixed-Mode delamination; INTERLAMINAR FRACTURE-TOUGHNESS; ELECTROSPUN NANO-INTERLAYERS; REINFORCED EPOXY COMPOSITES; MECHANICAL-PROPERTIES; ENERGY-ABSORPTION; STRUCTURAL COMPOSITES; SURFACE-MORPHOLOGY; FIBER COMPOSITES; LAMINATED GLASS; STRESS-DRIVEN;
D O I
10.1016/j.compositesb.2018.07.032
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Laminated composites mostly suffer from layer separation and/or delamination, which may affect the stiffness, strength and lifetime of structures. In this study, we aim to produce micron-scale thin carbon nanotubes (CNTs) reinforced adhesive nanofibrous interleaves and to explore their effectiveness when incorporated into structural composites. Neat polyvinyl butyral (PVB) and solutions containing low fractions of CNTs from 0.5 to 2 wt.% were electrospun directly onto carbon fiber prepregs. These interlayered laminates were cured above the glass transition temperature (T-g) of PVB to achieve strong interlaminar binding and also to resist crack re-initiation. The effect of CNTs presence and their mass fractions both on total Mixed-Mode I + II fracture toughness (G(c)) and crack length was investigated under Mixed-Mode I + II loading. Almost 2-fold increase in G(c) was reported in interlayered composites compared to non-interlayered laminates, associated to toughening effect of adhesive PVB/CNTs nanofibrous interlayers. Furthermore, the post-fracture analysis revealed the aid of CNTs interleaves in retarding delamination and afterward stabilization of crack propagation.
引用
收藏
页码:186 / 194
页数:9
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