导弹筒盖系统的故障复现及结构改进

Fault Replay and Design Modification of Missile Cover System

  • 摘要: 采用分系统独立建模方法分别构建筒盖-U型架系统和轴承基座系统的动力学有限元模型,分析结果不仅提取了轴承基座的承载状况,同时再现了系统实验所出现的故障;借助轴承基座系统的静力学模型对轴承基座结构进行改进设计,得到符合使用条件的轴承基座结构形式.全系统有限元建模分析表明,改进后的筒盖系统满足使用强度要求,并且分析结果与对应的测试数据基本一致.

     

    Abstract: Finite element dynamics models of the cover-U form frame system and the bearing support system are built respectively by using subsystem modeling method.Based on the finite element analysis of the subsystems,the force acted on the bearing support system is obtained and system structural faults appearing in experiment are replayed.By means of the static model,structure of the bearing support is modified,finally an optimum structure form of the bearing support which meets the need of the operation conditions is achieved.Modeling and analysis of the whole cover system show that the strength of the modified cover system is reasonable.In addition,analysis results agree with the testing data very well.

     

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