研究加载速度对CMDB推进剂动态启动断裂性的影响
Jian Zheng1, Xuan Wu2, Zhengwei Sun2
1School of Mechanical Engineering, Key Laboratory of Special Engine Technology, Ministry of Education, Nanjing University of Science and Technology, Nanjing, 210094, People's Republic of China. zhengjian@njust.edu.cn.
Scientific reports
|December 31, 2024
概括
这项研究确定了在高发射负载下复合改性双基 (CMDB) 推进剂的动态断裂性. 结果显示,加载速度影响性,微观结构分析揭示了故障机制.
科学领域:
- 材料科学 材料科学 材料科学
- 机械工程 机械工程
- 航空航天工程 航空航天工程
背景情况:
- 火箭推进剂颗粒必须承受极端的发射负载和点火压力.
- 在动态应力下评估推进剂的结构完整性对于火箭性能和安全至关重要.
研究的目的:
- 为了研究复合改性双基 (CMDB) 推进剂的动态启动断裂性.
- 建立一种可靠的方法,在动态负载条件下预测推进剂的结构完整性.
主要方法:
- 动态机械性能被测试使用破裂直径通过平的巴西圆盘 (CSTFBD) 标本与修改的Split Hopkinson压力杆 (SHPB).
- 进行了数值模拟,并与实验数据进行比较.
- 扫描电子显微镜 (SEM) 用于分析断裂表面和微观结构演变.
主要成果:
- 动态断裂启动性可以通过准静态理论和时间到断裂来确定.
- 该ZWT构成模型准确地预测动态负载下的推进剂行为,与实验结果保持一致.
- SEM分析显示,断裂模式和甲 (AP) 颗粒破裂显著影响动态负载下推进剂的故障机制.
结论:
- 该ZWT构成模型适用于在动态负载下模拟推进剂的结构完整性.
- 负载率显著影响CMDB推进剂的动态断裂启动性.
- 了解微结构性故障机制为在动态条件下推进剂设计和分析提供了理论基础.
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