复合材料科学与工程 ›› 2025, Vol. 0 ›› Issue (9): 125-134.DOI: 10.19936/j.cnki.2096-8000.20250928.016

• 工程应用 • 上一篇    下一篇

复合材料无缝衬套挤压强化仿真及其疲劳寿命预测研究

孙卓伟, 袁国青*   

  1. 同济大学 航空航天与力学学院,上海200092
  • 收稿日期:2024-11-18 发布日期:2025-10-23
  • 通讯作者: 袁国青(1967—),男,博士,硕士生/博士生导师,研究方向为复合材料,92002@tongji.edu.cn。
  • 作者简介:孙卓伟(1997—),男,硕士研究生,研究方向为复合材料孔挤压。

Simulation study on grommet hole reinforcement technology for composite structure and its fatigue life prediction

SUN Zhuowei, YUAN Guoqing*   

  1. School of Aerospace Engineering and Applied Mechanics, Tongji University, Shanghai 200092, China
  • Received:2024-11-18 Published:2025-10-23

摘要: 孔挤压强化是一种广泛用于提高航空结构疲劳寿命的技术。对于复合材料开孔结构,将无缝衬套通过挤压安装于开孔中可以有效提高开孔层合板的疲劳寿命。基于有限元软件ABAQUS,研究了无缝衬套孔挤压复合材料带孔层合板工艺,并提出了预测挤压后层合板疲劳寿命的方法,研究了挤压量对层合板疲劳寿命的影响规律。结果表明:挤压强化可以在层合板孔边和无缝衬套上产生一定的残余应力场,层合板内各层残余应力情况有一定差异,无缝衬套挤压出口面上的残余压应力最大;存在最佳挤压量,在该挤压量下进行强化不会对层合板产生损伤,在结构中产生的残余压应力场可有效提升开孔层合板的疲劳寿命,对于本文的研究对象,该最佳挤压量为2%,疲劳寿命可提升103%;若挤压量较大,孔挤压会在孔边造成损伤,以基体压缩损伤为主,这将影响甚至降低层合板的疲劳寿命。

关键词: 复合材料, 无缝衬套挤压强化, 疲劳寿命预测

Abstract: Cold expansion technology is a technique widely used to improve the fatigue life of aerostructures. For composite open-hole structures, the grommet can be expanded into the hole to effectively improve the fatigue life of the laminate. Based on the FEA software ABAQUS, this paper simulates the process flow of grommet hole reinforcement technology of composite laminate, predicts the fatigue life of the laminate after hole reinforcement, and studies the influence of different degrees of cold expansion (DCE) on the fatigue life of the laminate. The results show that: grommet hole reinforcement can generate a certain residual stress field on the hole edge of the laminate and the grommet. There are certain differences in the residual stress field of each layer, and the compressive residual stress on the extrusion outlet surface of the grommet is the highest; there is an optimal DCE , under which the reinforcement will not damage the laminate, and can also generate a suitable residual stress field in the structure, which can maximize the fatigue life of the laminate. The optimal DCE is 2% for the research object in this paper; if the DCE is too large, the grommet hole reinforcement will cause damage at the edge of the hole, mainly the matrix compression damage, which will affect or even reduce the fatigue life of the laminate.

Key words: composites, grommet hole reinforcement, fatigue life prediction

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