基于动态模块的CMDB推进剂的疲劳损伤演变模型
Li Yao1, Xu Jinsheng2, Zhou Changsheng1
1School of Mechanical Engineering, Key Laboratory of Special Engine Technology, Ministry of Education, Nanjing University of Science and Technology, Nanjing, 210094, China.
Scientific reports
|December 4, 2025
概括
温度上升会延长复合改性双基推进剂 (CMDB) 的疲劳寿命. 一个三阶段损害演化模型准确地预测了在周期性负荷下材料的行为,这对于固体火箭推进系统至关重要.
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:
- 复合改性双基推进剂 (CMDB) 对于固体火箭推进来说至关重要.
- 了解其在循环负荷下疲劳行为对于安全和性能至关重要.
- 温度显著影响材料的性能和降解.
研究的目的:
- 系统地研究CMDB推进剂在应变控制的循环负荷下疲劳行为.
- 量化疲劳寿命演变和机械响应在各种温度和应变幅度.
- 分析疲劳前调节对推进剂损伤的影响.
主要方法:
- 压力控制的循环负荷测试在各种温度范围内进行.
- 量化了疲劳寿命和机械反应.
- 进行了疲劳前测试,以分析损伤的演变.
- 基于损伤力学和粘性弹性理论,开发了一种三阶段疲劳损伤演变模型.
主要成果:
- 随着温度的升高,CMDB推进剂的疲劳寿命会增加.
- 应激反应表现出明显的三阶段演变:最初的软化,稳定的发展和加速.
- 建立的三阶段模型与实验数据有很好的一致性.
结论:
- 开发的疲劳损伤模型有效地描述了周期性加载期间的CMDB推进剂行为.
- 该框架为评估性能和预测固体火箭推进系统的使用寿命提供了机制基础.
- 温度是影响CMDB推进剂疲劳寿命和损伤机制的关键因素.
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