航天制造技术2024,Issue(2) :25-28.

耐高温树脂及其复合材料性能研究

Study on Properties of High Temperature Resistant Resin and Its Composites

张帆 赵荣 张崇耿 张宁 王领 张海鹏 余泰池
航天制造技术2024,Issue(2) :25-28.

耐高温树脂及其复合材料性能研究

Study on Properties of High Temperature Resistant Resin and Its Composites

张帆 1赵荣 1张崇耿 1张宁 1王领 1张海鹏 1余泰池1
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作者信息

  • 1. 西安长峰机电研究所,西安 710065
  • 折叠

摘要

针对固体火箭发动机复杂管路一体化成型工艺技术要求,进行了TDS型苯并噁嗪树脂的粘度、热重曲线、流变性能以及复合材料的力学性能测试,得到了TDS型苯并噁嗪在注胶温度下粘度小于 0.3 Pa.s,工艺窗口大于 6 h,该树脂在800℃氮气气氛下,残碳率为55.6%,也获得了复合材料的拉伸强度、压缩强度、压缩模量、弯曲强度和层间剪切强度等参数.研究结果表明:TDS型苯并噁嗪耐高温树脂初步满足了固体火箭发动机复杂管路一体化成型工艺技术要求.

Abstract

According to the technical requirements of complex pipetune one-body processing of solid rocket motor,the viscosity,thermo-gravimetric curves,rheological properties and composites properties of TDS benzoxazine resin were studied.The viscosity of less than 0.3 Pa.s of TDS benzoxazine resin at glue injection temperature was obtained by mechanical properties test.Its process operation time was more than 6 h,the resin residual yield was 55.6%under the nitrogen atmosphere at the temperature 800℃,as well as the tensile strength,compressive strength,bending strength,and shear strength properties of the composite materials were also obtained.All these study results show that TDS benzoxazine of high temperature resistant resin can meet the technical requirements of one-body processing of complex pipetune of solid rocket motor.

关键词

耐高温树脂/复合材料/性能研究

Key words

high temperature resistant resin/composite material/performance research

引用本文复制引用

出版年

2024
航天制造技术
首都航天机械公司

航天制造技术

影响因子:0.318
ISSN:
参考文献量3
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