玻璃钢/复合材料 ›› 2019, Vol. 0 ›› Issue (6): 90-94.

• 应用研究 • 上一篇    下一篇

芳纶纤维/碳纤维复层结构复合材料变形研究

吴思保1,2,3, 礼嵩明1,2,3*, 鹿海军1,2,3   

  1. 1.中航复合材料有限责任公司,北京101300;
    2.航空工业复合材料技术中心,北京101300;
    3.先进复合材料重点实验室,北京100095
  • 收稿日期:2019-02-26 出版日期:2019-06-25 发布日期:2019-06-28
  • 通讯作者: 礼嵩明(1986-),男,硕士研究生,主要从事结构功能一体化复合材料方面的研究,lisongming860206@126.com。
  • 作者简介:吴思保(1991-),男,硕士研究生,主要从事结构功能一体化复合材料方面的研究。

STUDY ON DEFORMATION OF COMPOSITES OF ARAMID FIBER/CARBON FIBER COMPOUND STRUCTURE

WU si-bao1,2,3, LI song-ming1,2,3*, LU hai-jun1,2,3   

  1. 1.AVIC Composite Corporation Ltd., Beijing 101300, China;
    2.AVIC Composite Technology Center, Beijing 101300, China;
    3.National Key Laboratory of Advanced Composites, Beijing 100095, China
  • Received:2019-02-26 Online:2019-06-25 Published:2019-06-28

摘要: 在不同种类的树脂基复合材料复合的热历程中,由于材料热膨胀系数存在差异,复层结构会产生内应力,发生一定的变形。研究了复合工艺(复合温度和压力)、复合方式(二次胶接和共胶接)和芳纶纤维复合材料的预变形对芳纶纤维/碳纤维复层结构复合材料变形的影响,结果表明:降低复合温度可以明显地减小复层结构的变形,当复合温度由180 ℃降至120 ℃时,复层结构的变形减小了80%;随着复合压力的增加,复层结构的变形减小,当压力达到0.3 MPa时,变形不再减小;与芳纶纤维-碳纤维干-湿共胶接相比,采用二次胶接和碳纤维-芳纶纤维干-湿共胶接的复合方式有利于减小复层结构的变形;芳纶纤维复合材料的预变形处理是控制复层结构变形的有效方法。

关键词: 复层结构, 变形, 复合工艺, 二次胶接, 共胶接, 预变形

Abstract: Resin matrix composites possess the advantages of high specific strength, high specific modulus, high designability, strong corrosion resistance and integration molding, which have been widely used in the fields of aerospace, vehicles, ships, electronics, etc. In some practical application fields, different resin matrix composites need to be compound to obtain functional composites with excellent comprehensive properties that single resin matrix composites don′t possess. When different kinds of resin matrix composites are combined, their respective degree of size change with the change of temperature is different during the compound thermal process because of the difference of their thermal expansion coefficient, which creates the internal stress of the compound structure and eventually lead to a certain deformation. In this paper, the influence of compound process (compound temperature and compound pressure), compound methods (secondary bonding and co-bonding), the pre-deformation of aramid fiber composite on the deformation of the composite of aramid fiber/carbon fiber compound structure were studied. The results show that the deformation of the compound structure can be decreased obviously with the decrease of compound temperature. When the compound temperature drops from 180 ℃ to 120 ℃, the deformation of the compound structure decreases by 80%. Appropriate increase of compound pressure contributes to decrease the deformation of the compound structure, whereas the deformation is no longer decreased when compound pressure reaches 0.3 MPa. Aramid fiber-carbon fiber secondary bonding (aramid fiber composite and carbon fiber composite both have been cured completely before they are combined) and carbon fiber-aramid fiber dry-wet co-bonding (carbon fiber composite have been cured completely, while aramid fiber is not cured before they are combined) are beneficial to decrease the deformation of compound structure compared by aramid fiber-carbon fiber dry-wet co-bonding (aramid fiber composite have been cured completely, while carbon fiber is not cured before they are combined). The pre-deformation of aramid fiber composite is an effective way of the deformation control of compound structure.

Key words: compound structure, deformation, compound process, secondary bonding, co-bonding, pre-deformation

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