复合材料科学与工程 ›› 2013, Vol. 0 ›› Issue (3): 39-42.

• 基础研究 • 上一篇    下一篇

缝合泡沫夹层复合材料的滚筒剥离性能

潘利剑*, 刘卫平, 陈萍, 戚方方   

  1. 中国商飞上海飞机制造有限公司,上海 200436
  • 收稿日期:2012-06-20 出版日期:2013-05-28 发布日期:2022-03-16
  • 作者简介:潘利剑(1980-) ,男,博士,主要从事树脂基复合材料及其液体成型工艺方面的工作研究,xiaopanhrb@163.com。
  • 基金资助:
    上海市科技人才计划项目(11PJ1430900)

THE CLIMBING DRUM PEEL BEHAVIOR OF STITCHED FOAM-CORE SANDWICH COMPOSITES

PAN Li-jian*, LIU Wei-ping, CHEN Ping, QI Fang-fang   

  1. Shanghai Aircraft Manufacturing Co.,Ltd.,Shanghai 200436,China
  • Received:2012-06-20 Online:2013-05-28 Published:2022-03-16

摘要: 制备了改进锁式缝合、临缝式缝合、双线链式缝合等三种缝合方式下不同缝合密度、缝线直径的缝合泡沫夹层复合材料,并对其滚筒剥离性能进行了测试。结果表明,未缝合泡沫夹层复合材料的剥离载荷上升到一定高度后便趋于稳定,而缝合泡沫夹层复合材料的剥离载荷上升到一定高度后呈正弦曲线变化; 缝合后最大剥离载荷的平均值得到大幅度的提高,可增加到原有的1. 6 ~ 4. 7 倍左右;缝合参数相同,缝合方式不同的缝合泡沫夹层复合材料的剥离载荷存在一定的差异,同样的缝合方式下,缝合密度、缝线直径越大,剥离载荷越大。

关键词: 复合材料, 缝合, 泡沫夹层, 滚筒剥离

Abstract: The stitched foam core sandwich composites with different parameter under three stitch formation lockstitch,stuffing stitch and double chain stitch were produced. And the climbing drum peel tests were performed.The experimental results show that the peel load of unstitched sandwich composites increased to a peak value and then drove to stabilization,while the peel load of stitched foam-core sandwich composites increased to a peak value and then varies in sine-shaped mode. The average value of the max peel load increased remarkably by stitching.The average value of the max peel load of stitched foam-core sandwich composites increased to 1. 6 ~ 4. 7 times of that unstitched. The peel load of the stitched foam-core sandwich composites with different stitch formation was different under the same stitch parameters. The greater of stitch density and stitch diameter was,the greater of the peel load was under the same stitch formation.

Key words: composites, stitching, foam core sandwich panel, climbing drum peel

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