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基于干法缠绕的高温环氧/国产T800碳纤维复合材料壳体性能

惠雪梅 张光喜 包艳玲 洪星星 鲁建军 阮英波

固体火箭技术2025,Vol.48Issue(5):714-722,9.
固体火箭技术2025,Vol.48Issue(5):714-722,9.DOI:10.7673/j.issn.1006-2793.2025.05.009

基于干法缠绕的高温环氧/国产T800碳纤维复合材料壳体性能

Properties of the high temperature epoxy/domestic T800 carbon fiber composite case based on dry winding

惠雪梅 1张光喜 1包艳玲 1洪星星 1鲁建军 2阮英波1

作者信息

  • 1. 西安航天复合材料研究所,西安 710025||陕西省航天复合材料重点实验室,西安 710025
  • 2. 西安航天复合材料研究所,西安 710025
  • 折叠

摘要

Abstract

Based on the characteristics of the dry winding process,a high-temperature epoxy resin system(GWE-1)suitable for the dry winding of domestic T800 carbon fiber was developed.The curing reaction kinetics,rheological behavior,storage period and mechanical properties of GWE-1 were studied.The micro-morphology characteristics of the resin fracture surface were observed.The domestic T800 carbon fiber/GWE-1 composites of ϕ150 mm and ϕ480 mm standard cases were prepared by the dry winding process,and the dry winding adaptability were verified.The internal pressure bearing capacity of the two standard cases was also tested.The results show that the epoxy system exhibits high strength and toughness,high temperature resistance,long storage time under room temperature and good winding adaptability with domestic T800 carbon fiber.The burst pressures of ϕ150 mm andϕ480 mmstandard cases are 42.9 MPaand 23.0 MPa,respectively,and the characteristic coefficients of the vessels are 55.1 km and 51.6 km,respectively.The ratio of strength transformation of domestic T800 carbon fiber is more than 90%.Therefore,the domestic T800 carbon fiber/GWE-1composites demonstrates excellent internal pressure bearing capacity and has the application potential for solid rocket motor.

关键词

干法缠绕/T800碳纤维/高温环氧树脂/容器特性系数/纤维强度转化率/缠绕适配性

Key words

dry winding/T800 carbon fiber/high-temperature epoxy resin/vessel characteristic coefficient/ratio of strength transformation of fiber/winding adaptability

分类

航空航天

引用本文复制引用

惠雪梅,张光喜,包艳玲,洪星星,鲁建军,阮英波..基于干法缠绕的高温环氧/国产T800碳纤维复合材料壳体性能[J].固体火箭技术,2025,48(5):714-722,9.

基金项目

国家级项目. ()

固体火箭技术

OA北大核心

1006-2793

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