A self-healing carbon fibre reinforced polymer for aerospace applications

被引：404

作者：

Williams, G. ^{[1
]}

Trask, R. ^{[1
]}

Bond, I. ^{[1
]}

机构：

[1] Univ Bristol, Dept Aerosp Engn, Bristol BS8 1TR, Avon, England

来源：

COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING | 2007年 / 38卷 / 06期

基金：

英国工程与自然科学研究理事会;

关键词：

carbon fibre; mechanical testing; strength; self-healing;

D O I：

10.1016/j.compositesa.2007.01.013

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

Self-healing is receiving increasing interest worldwide as a technology to autonomously address the effects of damage in composite materials. This paper describes the results of four point bend flexural testing (ASTM-D6272-02) of T300/914 carbon fibre reinforced epoxy with resin filled embedded hollow glass fibres (HGF) which provided a self-healing functionality. The study investigated the effect of the embedded HGF on the host CFRP mechanical properties and also the healing efficiency of the laminates. after they were subjected to quasi-static impact. Specimens were tested in the undamaged, damaged and heated conditions using a commercial two-part epoxy healing agent (Cytec Cycom 823). Microscopic characterisation of the embedded HGF was also undertaken to characterise the effect on the host laminate fibre architecture. (c) 2007 Elsevier Ltd. All rights reserved.

引用

页码：1525 / 1532

页数：8

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