航空学报 > 1996, Vol. 17 Issue (2): 196-201

动载与静载作用下残余应力对ARALL层板裂纹孔边分层影响的实验研究

仲伟虹1, 陈昌麒1, 寇长河1, 郑瑞琪2   

  1. 1. 北京航空航天大学104教研室,北京,100083;2. 北京航空材料研究所八室,北京,100095
  • 收稿日期:1994-07-07 修回日期:1994-12-21 出版日期:1996-04-25 发布日期:1996-04-25

EXPERIMENTAL STUDY ON EFFECTS ON DELAMINATION NEAR CRACK OF ARALL BY RESIDUAL STRESS UNDER FATIGUE AND STATIC LOADS

Zhong Weihong1, Chen Changqi1, Kou Changhe1, Zheng Ruiqi2   

  1. 1. Beijing Institute of Aeronautical Materials, Beijing,100095;2. Faculty 104, Beijing University of Aeronautics and Astronautics Beijing, 100083
  • Received:1994-07-07 Revised:1994-12-21 Online:1996-04-25 Published:1996-04-25

摘要: 研究了疲劳载荷与静态拉伸条件下 ARALL层板孔边分层的状态 ,分析了不同残余应力对该层板孔边分层损伤的影响。结果表明 ,两种载荷条件下的分层破坏是完全不同的。疲劳载荷下裂纹扩展过程中伴随分层的典型的情况是呈对称双椭圆形 ,静态拉伸作用下层板边缘效应更加明显。给层板施加适当的预应力可以提高其抵抗分层损伤的能力

关键词: 复合材料, 层压板, 层离, 残余应力

Abstract: The delamination near the centre crack of ARALL under fatigue load and static load is investigated, and the effects on delamination of different residual stresses are analyzed. The results show that the situations under the two kinds of loads are different. Under the fatigue load, the typical delamination with crack growth is symmetrical bi\|ellipse. But under the condition of static tensile, the edge\|effects become more evident. Applying a proper pre\|stress to the laminate can increase the ability of anti\|delamination damage.

Key words: composite laminates, delaminating, residual stress

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