国产芳纶纤维复合材料用环氧树脂体系
DOI:
作者:
作者单位:

西安航天复合材料研究所

作者简介:

通讯作者:

中图分类号:

基金项目:


Epoxy Formulation System for Domestic Aramid Fiber Reinforced Composite
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:

    研制了一种环氧/ 芳香胺体系,采用DSC、固化反应动力学分析等方法对树脂体系进行了表征,并
    对其浇注体、复合材料NOL 环以及Φ150 mm 压力容器性能进行了研究。结果表明,该树脂体系具有优良的浇
    注体力学及热性能,其拉伸强度为101 MPa,断裂伸长率达4. 1%,弯曲强度为177 MPa,马丁耐热温度为
    142. 2℃;与国产芳纶纤维的界面粘接性能良好,其NOL 环层间剪切强度可以达到52. 1 MPa,制备的复合材料
    Φ150 mm 压力容器PV / W 值可达38. 44 km。

    Abstract:

    An aromatic amine cured epoxy resin formulation system has been developed according to the characteristic
    of the domestic aramid fiber. The curing process of the formulation system was studied by DSC test. Mechanical
    property of the resin casting body was measured by universal testing machine. The interlaminar shear strength (ILSS)
    of NOL-ring samples and explosion properties of Φ150 mm standard pressure vessels prepared by the domestic aramid
    fiber reinforced aromatic amine cured epoxy composite were also investigated. The results indicate that the epoxy formulation
    system provide excellent mechanical properties and heat-resistance performance. The tensile strength,elongation
    rate at break,flexural strength and martin heat resistant temperature of the casting body are 101 MPa,4. 1%,177
    MPa and 142. 2℃ respectively. The interfacial adhesion property of the composite is pretty good. The ILSS of the composite
    and PV / W of Φ150 mm pressure vessels are 52. 1 MPa and 38. 44 km respectively.

    参考文献
    相似文献
    引证文献
引用本文

王百亚.国产芳纶纤维复合材料用环氧树脂体系[J].宇航材料工艺,2013,43(6).

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:
第十一届航天复合材料成形与加工工艺技术中心交流会 征文通知

关闭