节点文献

航天复合材料压力容器研制技术

Development Technique of Composite Overwrapped Pressure Vessel for Aerospace System

  • 推荐 CAJ下载
  • PDF下载
  • 不支持迅雷等下载工具,请取消加速工具后下载。

【作者】 于斌刘志栋靳庆臣程彬陈威石晓强吴学彬

【Author】 YU Bin,LIU Zhi-dong,JIN Qing-chen,CHENG Bin,CHEN Wei, SHI Xiao-qiang,WU Xue-bin(Lanzhou Institute of Physics,Lanzhou 73000,Gansu,China)

【机构】 兰州空间技术物理研究所

【摘要】 分析了航天复合材料压力容器技术指标特点。提出了容器金属内衬、增强纤维和树脂基体的选材要求。讨论了金属内衬全金属承压区、薄膜区、封头过渡区、封头/筒体界面、焊接区的结构设计方法,以及圆柱形、球形、近球形、椭球形、环形、锥形容器纤维缠绕复合材料壳体结构特点。简述了结构设计算法,以及包括疲劳寿命、应力断裂寿命、爆破前先泄漏(LBB)安全失效模式等容器安全设计的分析和试验方法。

【Abstract】 The specification features of aerospace composite overwrapped pressure vessel were analyzed in this paper.The material selection requirement of metal liner,reinforced fiber and resin system for vessel was proposed.The structure design methods for metal pressure bearing region,membrane region,head transition region,interface between head and cylinder,weld region were described.The fiber overwrapped structure characteristics of cylinder,sphere,near-sphere,ellipse,toroidal and conical shape were discussed.The structure design method was introduced.The analysis and test of fatigue life,stress rupture life and leak before burst(LBB) mode were presented.

  • 【文献出处】 上海航天 ,Aerospace Shanghai , 编辑部邮箱 ,2012年05期
  • 【分类号】V229.7;TH49
  • 【被引频次】8
  • 【下载频次】316
节点文献中: 

本文链接的文献网络图示:

本文的引文网络