| 注册
首页|期刊导航|含能材料|温度对HTPB推进剂疲劳特性的影响

温度对HTPB推进剂疲劳特性的影响

梁蔚 吕庆山 陈雄 许进升 童心 闫晓晶

含能材料2017,Vol.25Issue(3):184-190,7.
含能材料2017,Vol.25Issue(3):184-190,7.DOI:10.11943/j.issn.1006-9941.2017.03.002

温度对HTPB推进剂疲劳特性的影响

Effect of Temperature on Fatigue Properties of HTPB Propellant

梁蔚 1吕庆山 2陈雄 1许进升 1童心 1闫晓晶3

作者信息

  • 1. 南京理工大学机械工程学院,江苏南京210094
  • 2. 中国兵器工艺导航与控制技术研究所,北京100089
  • 3. 晋西工业集团技术研发中心,山西太原030027
  • 折叠

摘要

Abstract

To study the fatigue properties of hydroxyl terminated polybutadiene (HTPB) propellant at different temperatures,the constant stress control fatigue cyclic loading tests at different temperatures were carried out.Taking peak strain as damage factor,based on damage mechanics and viscoelastic theory,a three-stage model of fatigue damage with temperature effect of HTPB propellant was established.The results show that with increasing temperature,the fatigue life of materials decreases,the fracture strain increases.The peak strain in the process of fatigue obviously has three stages of evolution:initial deformation stage,stable development stage and acceleration stage,which is the macro-behavior of material damage.The three-stage model established overcomes the shortcomings of two-phase model that can't consider macroscopic crack propagation.By fitting the model parameters,the theoretical results of 213 K and 333 K are predicted by linear regression method,which are in good agreement with the experimental results,therefore it can be used to characterize the damage evolution law of materials very well.

关键词

端羟基聚丁二烯(HTPB)推进剂/应力控制/疲劳寿命/损伤因子/损伤模型

Key words

hydroxyl terminated poly-butadiene(HTPB) propellant/stress control/fatigue life/damage factor/damage model

分类

军事科技

引用本文复制引用

梁蔚,吕庆山,陈雄,许进升,童心,闫晓晶..温度对HTPB推进剂疲劳特性的影响[J].含能材料,2017,25(3):184-190,7.

基金项目

国家自然科学基金(51606098),江苏省自然科学基金(BK20140772),中央高校基本科研业务费专项资金(30915011301) (51606098)

含能材料

OA北大核心CSCDCSTPCD

1006-9941

访问量0
|
下载量0
段落导航相关论文