Using aligned nanofibres for identifying the toughening micromechanisms in nanofibre interleaved laminates

被引:73
作者
Daelemans, Lode [1 ]
van der Heijden, Sam [1 ]
De Baere, Ives [2 ]
Rahier, Hubert [3 ]
Van Paepegem, Wim [2 ]
De Clerck, Karen [1 ]
机构
[1] Univ Ghent, Dept Text, Technol Pk Zwijnaarde 907, B-9052 Zwijnaarde, Belgium
[2] Univ Ghent, Dept Mat Sci & Engn, Technol Pk Zwijnaarde 903, B-9052 Zwijnaarde, Belgium
[3] Vrije Univ Brussel, Dept Mat & Chem, Pl Laan 2, B-1050 Brussels, Belgium
关键词
Nano particles; Delamination; Fibre bridging; Damage tolerance; Electro-spinning; INTERLAMINAR FRACTURE-TOUGHNESS; MODE-I; COMPOSITE-MATERIALS; CARBON/EPOXY COMPOSITES; ELECTROSPUN FIBERS; DAMAGE RESISTANCE; PHASE-SEPARATION; DELAMINATION; INTERLAYERS; MECHANISM;
D O I
10.1016/j.compscitech.2015.11.021
中图分类号
TB33 [复合材料];
学科分类号
摘要
The susceptibility to delamination is one of the main concerns in many advanced laminated composite applications. Laminates interleaved with electrospun nanofibrous veils provide a potential solution in order to increase the material's resistance to interlaminar fracture. Previous studies have shown that nanofibres are able to bridge microcracks in the laminates resulting in an increased interlaminar fracture toughness (IFT). However, the exact micromechanisms resulting in these nanofibre bridging zones are still unclear. In this article, aligned nanofibrous structures are used to identify and study the different micromechanisms which take place during Mode II crack propagation. Three nanofibrous veil morphologies with a distinct orientation of the nanofibres are used: (1) a random deposition of nanofibres, (2) nanofibres oriented parallel to the crack growth direction, and (3) nanofibres oriented perpendicular to the crack growth direction. A thorough analysis of the fracture surface of tested specimens and crack path behaviour is performed in order to determine the micromechanisms associated with the development of nanofibre bridging zones. A strong effect of the nanofibre orientation distribution on the Mode II IFT and the underlying toughening mechanisms was observed: different micromechanisms were observed depending on the nanofibre orientation. (C) 2015 Elsevier Ltd. All rights reserved.
引用
收藏
页码:17 / 26
页数:10
相关论文
共 33 条
[1]   Effect of Nylon-66 nano-fiber interleaving on impact damage resistance of epoxy/carbon fiber composite laminates [J].
Akangah, Paul ;
Lingaiah, Shivalingappa ;
Shivakumar, Kunigal .
COMPOSITE STRUCTURES, 2010, 92 (06) :1432-1439
[2]   A new method for determining mode II R-curve by the End-Notched Flexure test [J].
Arrese, A. ;
Carbajal, N. ;
Vargas, G. ;
Mujika, F. .
ENGINEERING FRACTURE MECHANICS, 2010, 77 (01) :51-70
[3]  
ASTM International, 2014, D790514 ASTM
[4]   Mode I and Mode II interlaminar fracture toughness of composite laminates interleaved with electrospun nanofibre veils [J].
Beckermann, Gareth W. ;
Pickering, Kim L. .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2015, 72 :11-21
[5]   Global and local nanofibrous interlayer toughened composites for higher in-plane strength [J].
Bilge, K. ;
Venkataraman, S. ;
Menceloglu, Y. Z. ;
Papila, M. .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2014, 58 :73-76
[6]   Structural composites hybridized with epoxy compatible polymer/MWCNT nanofibrous interlayers [J].
Bilge, K. ;
Ozden-Yenigun, E. ;
Simsek, E. ;
Menceloglu, Y. Z. ;
Papila, M. .
COMPOSITES SCIENCE AND TECHNOLOGY, 2012, 72 (14) :1639-1645
[7]   The determination of the mode II adhesive fracture resistance, GIIC, of structural adhesive joints:: an effective crack length approach [J].
Blackman, BRK ;
Kinloch, AJ ;
Paraschl, M .
ENGINEERING FRACTURE MECHANICS, 2005, 72 (06) :877-897
[8]   Hybrid multi-scale composites developed from glass microfiber fabrics and nano-epoxy resins containing electrospun glass nanofibers [J].
Chen, Qi ;
Zhang, Lifeng ;
Zhao, Yong ;
Wu, Xiang-Fa ;
Fong, Hao .
COMPOSITES PART B-ENGINEERING, 2012, 43 (02) :309-316
[9]   Correlation of damage resistance under low velocity impact and Mode II delamination resistance in CFRP laminates [J].
Chou, I ;
Inutake, T ;
Namba, K .
ADVANCED COMPOSITE MATERIALS, 1999, 8 (02) :167-176
[10]   Nanofibre bridging as a toughening mechanism in carbon/epoxy composite laminates interleaved with electrospun polyamide nanofibrous veils [J].
Daelemans, Lode ;
van der Heijden, Sam ;
De Baere, Ives ;
Rahier, Hubert ;
Van Paepegem, Wim ;
De Clerck, Karen .
COMPOSITES SCIENCE AND TECHNOLOGY, 2015, 117 :244-256