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采用混杂复合材料的止裂设计及其剩余强度分析
引用本文:陶梅贞,张元明.采用混杂复合材料的止裂设计及其剩余强度分析[J].宇航学报,1990(4):88-93.
作者姓名:陶梅贞  张元明
作者单位:西北工业大学 (陶梅贞,张元明),飞机强度研究所 (沈真),飞机强度研究所(刘俊石)
摘    要:本文用理论分析和试验研究证实了混杂复合材料构成的软化带可用以控制碳/环层板中的裂纹扩展,以较小的重量代价,提高其剩余强度。文章还分析了裂纹尺寸和软化带的材料、参数对碳/环层压板的损伤容限特性的影响。

关 键 词:混杂复合材料  裂纹扩展  剩余强度

DESIGN FOR CRACK ARRESTMENT OF HYBRID COMPOSITE AND THE ANALYSIS OF RESIDUAL STRENGTH
Tao Meizhen Zhang Yuanming.DESIGN FOR CRACK ARRESTMENT OF HYBRID COMPOSITE AND THE ANALYSIS OF RESIDUAL STRENGTH[J].Journal of Astronautics,1990(4):88-93.
Authors:Tao Meizhen Zhang Yuanming
Institution:Tao Meizhen Zhang Yuanming(Northwestern Polytechnical University)Shen Zhen Liu Junshi (Aircraft Structural Strength Research Institute)
Abstract:This paper presents a softening strip design of hybrid composite material. It is proved by means of theoretical analysis and experimental investigation that the softening strip can be used to prevent the crack propagation and to increase the residual strength of graphite/epoxy laminated composite plate. The influence of the crack size and the paramen-ters of the softening strips on the damage tolerance capability are also analysed.
Keywords:Hybrid composite  Softening strip  Crack propagation  Residual strength  
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