推进技术 ›› 1998, Vol. 19 ›› Issue (4): 74-77.

• • 上一篇    下一篇

含粘接缺陷固体发动机喷管堵盖受压分析

史宏斌,侯晓,钟伟芳   

  1. 陕西动力机械研究所;陕西动力机械研究所;华中理工大学力学系
  • 发布日期:2021-08-15

NON LINEAR ANALYSIS OF SRM NOZZLE CLOSURE WITH INITIAL COHERE IMPERFECTIONS UNDER DISTRIBUTED LOAD

  1. Shaanxi Inst.of Power Machinery,Xi′an,710025;Shaanxi Inst.of Power Machinery,Xi′an,710025;Huazhong Univ.of Science & Technology,Wuhan,430074
  • Published:2021-08-15

摘要: 利用VonKarman模型,对受内压作用固体火箭发动机喷管堵盖进行了几何大变形分析,考虑了工艺因素对堵盖变形和堵盖与喷管喉衬粘接界面应力的影响,分别对牢靠粘接和3种不同形式的不牢靠粘接进行了计算,结果表明,堵盖与喉衬的粘接面脱粘对界面应力场有很大的影响。

关键词: 固体推进剂火箭发动机;发动机喷管;喷管盖;变形;粘接缺陷

Abstract: Based on Von Karman′s theory,the non linear analysis of SRM nozzle closure under distributed load was conducted.The effects of processing factors on the deformation of the nozzle closure,and the interface stress of the closure and the throat insert were taken into account.Four caculating models,which include one perfect form and three various debond forms were also considered.The results configure out that the debond of the closure and the throat insert play an important part in the interface intensity

Key words: Solid propellant rocket engine;Engine nozzle;Nozzle closure;Deformation;Bonding defect