Fibre reinforced composites in aircraft construction

被引:991
作者
Soutis, C [1 ]
机构
[1] Univ Sheffield, Sheffield S1 3JD, S Yorkshire, England
基金
英国工程与自然科学研究理事会;
关键词
D O I
10.1016/j.paerosci.2005.02.004
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Fibrous composites have found applications in aircraft from the first flight of the Wright Brothers' Flyer 1, in North Carolina on December 17, 1903, to the plethora of uses now enjoyed by them on both military and civil aircrafts, in addition to more exotic applications on unmanned aerial vehicles (UAVs), space launchers and satellites. Their growing use has risen from their high specific strength and stiffness, when compared to the more conventional materials, and the ability to shape and tailor their structure to produce more aerodynamically efficient structural configurations. In this paper, a review of recent advances using composites in modern aircraft construction is presented and it is argued that fibre reinforced polymers, especially carbon fibre reinforced plastics (CFRP) can and will in the future contribute more than 50% of the structural mass of an aircraft. However, affordability is the key to survival in aerospace manufacturing, whether civil or military, and therefore effort should be devoted to analysis and computational simulation of the manufacturing and assembly process as well as the simulation of the performance of the structure, since they are intimately connected. (c) 2005 Elsevier Ltd. All rights reserved.
引用
收藏
页码:143 / 151
页数:9
相关论文
共 23 条
[21]   EFFECTS OF MATRIX CRACKING AND HYGROTHERMAL STRESSES ON THE STRAIN-ENERGY RELEASE RATE FOR EDGE DELAMINATION IN COMPOSITE LAMINATES [J].
ZHANG, J ;
SOUTIS, C ;
FAN, J .
COMPOSITES, 1994, 25 (01) :27-35
[22]   STRAIN-ENERGY RELEASE RATE ASSOCIATED WITH LOCAL DELAMINATION IN CRACKED COMPOSITE LAMINATES [J].
ZHANG, J ;
SOUTIS, C ;
FAN, J .
COMPOSITES, 1994, 25 (09) :851-862
[23]  
[No title captured]