Fire resistance of aircraft composite laminates

被引：21

作者：

Mouritz, AP ^{[1
]}

机构：

[1] Royal Melbourne Inst Technol, Sch Aerosp Mech & Mfg Engn, Melbourne, Vic 3001, Australia

来源：

JOURNAL OF MATERIALS SCIENCE LETTERS | 2003年 / 22卷 / 21期

关键词：

D O I：

10.1023/A:1026103231041

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

A study was conducted on the fire resistance of aircraft composite laminates. The scanning electron microscopy was used to study the effect of fire on the mechanical properties of the composite materials. A model for estimating the residual flexural properties of aircraft composite after being thermally degraded in a fire, was also presented. It was found that the carbon fibers were not damaged in the fire test, where as the epoxy matrix had decomposed to a carbonaceous char.

引用

页码：1507 / 1509

页数：3