K-cor 夹层结构制备工艺
DOI:
CSTR:
作者:
作者单位:

南京航空航天大学材料学院

作者简介:

通讯作者:

中图分类号:

基金项目:


Manufacturing Processes of K-cor Sandwich Structure
Author:
Affiliation:

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    K-cor 是应用Z-pin 增强技术的一种新型高性能结构。本文以NHZP-1 树脂为基体研究适合K
    -cor 结构的半固化Z-pin 拉挤工艺,得到固化度为51. 25%的Z-pin 为满足制备要求的最佳参数,并制作悬空
    装置采用两步法进行半固化Z-pin 的植入和压弯,探索出压弯和后固化工艺。在此基础上,对试制的K-cor 夹
    层结构进行平拉和剪切试验研究。结果发现,折弯长度是K-cor 夹层结构的另一重要参数,较长的折弯长度会
    增加Z-pin 与蒙皮的结合面积从而提高结构的拉伸性能

    Abstract:

    The K-cor sandwich construction is a new kind of foam sandwich structure reinforced by Z-pin tech鄄
    nique. There are seldom studies available at present. The NHZP-1 resin was used as matrix for partial鄄cured Z-pin爷
    s pultrusion processing. 51. 25% of the cure degree is the optimum parameter based on a series of experiments. And
    an impending device was made for insertion and flushing for the protruding pin using the two鄄step method. The param鄄
    eters of flushing and post鄄cure were also explored. On the basis of the completion, static shear and stretching tests
    were conducted under different loads. The pin flattened length is also critical for the configuration. The increased
    bonded area between Z-pin and the two skins can enhance the resistance of stretching test behavior

    参考文献
    相似文献
    引证文献
引用本文

段沐枫. K-cor 夹层结构制备工艺[J].宇航材料工艺,2012,42(5).

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2016-11-28
  • 出版日期:
文章二维码