在各种负载条件下,对具有内部空洞的固体推进剂的故障模式进行数值模拟
Kai Liu1,2, Qingchun Yang3, Liang Cao4
1National Graduate College for Elite Engineers, Beihang University, Beijing 100191, China.
Polymers
|February 13, 2026
概括
基终结聚乙烯 (HTPB) 推进剂的内部空隙危及固体火箭发动机的安全性. 这项研究模拟了HTPB推进剂的行为,揭示了空腔大小和工程参数如何影响故障模式,增强结构完整性和安全性.
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:
- 固体火箭发动机的可靠性取决于推进剂的结构完整性.
- 基终结聚乙烯 (HTPB) 推进剂中的内部空洞降低了机械性能,并构成安全风险.
- 了解空腔效应对于推进剂设计和发动机安全至关重要.
研究的目的:
- 开发和验证一个包含损坏的HTPB推进剂的组成模型.
- 以数值研究初始模量,冲击速率和限制压力对具有内部空洞的推进剂故障模式的影响.
- 建立一个基础,优化推进剂的结构安全性关于空腔大小和工程参数.
主要方法:
- 使用通用增量压力-应变损伤模型 (GISSMO) 开发了一种HTPB推进剂的构成模型.
- 通过在各种拉伸速率下进行单轴拉伸试验验证实模型的有效性.
- 在不同的条件下,进行数值模拟来分析具有空洞 (40-100毫米半径) 的推进剂的故障机制.
主要成果:
- 经验证的模型准确地预测了力位移曲线,并捕获了取决于速率的材料行为 (弹性-塑料到弹性).
- 大型腔 (80-100毫米) 导致应力度,内壁损伤,挤出,崩和潜在的骨折.
- 较小的腔 (40-60毫米) 显示出更大的稳定性,损伤主要局限于体积压缩.
结论:
- 初始模量显著影响损伤的传播;较高的模量 (>24 MPa) 抑制了大腔的损伤.
- 撞击下的空洞行为随着速度和限制压力而变化,影响结构稳定性和损伤定位.
- 优化与腔体大小相关的工程参数是提高推进剂结构安全性的关键.
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