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虚拟环境下导弹舱段连接精度预分析
引用本文:熊珍琦,宁汝新,刘检华,刘伟东.虚拟环境下导弹舱段连接精度预分析[J].兵工学报,2008,29(8):950-955.
作者姓名:熊珍琦  宁汝新  刘检华  刘伟东
作者单位:北京理工大学机械与车辆工程学院,北京,100081;北京理工大学机械与车辆工程学院,北京,100081;北京理工大学机械与车辆工程学院,北京,100081;北京理工大学机械与车辆工程学院,北京,100081
摘    要:针对导弹舱段连接精度问题,提出一种虚拟环境下装配精度分析、优化的方法。定义了产品装配精度预分析的概念,并对其在实际生产中不同阶段的应用进行阐述。根据导弹舱段不同连接方法引起的各种装配误差对导弹最终飞行性能的影响,建立了产品装配公差模型,并在各个作用尺寸传递系数和加工难易程度的指导下进行装配精度的优化。以计算某导弹各个舱段连接偏差造成导弹头顶点偏移量为例验证导弹舱段连接精度预分析方法。

关 键 词:机械设计  虚拟环境  精度预分析  公差分析  公差优化

Pre-analysis of Connecting Precision of Missile Sections in Virtual Environment
XIONG Zhen-qi,NING Ru-xin,LIU Jian-hua,LIU Wei-dong.Pre-analysis of Connecting Precision of Missile Sections in Virtual Environment[J].Acta Armamentarii,2008,29(8):950-955.
Authors:XIONG Zhen-qi  NING Ru-xin  LIU Jian-hua  LIU Wei-dong
Affiliation:School of Mechanical and Vehicular Engineering, Beijing Institute of Technology, Beijing 100081, China
Abstract:An analysis and optimization method of assembly precision in virtual environment was pro?posed for the connecting precision of missile sections. A concept of product assemoly precision pre-anal?ysis was defined, and its application in different phases of actual production was described. According to the effect of all kinds of assembly errors caused by the different connecting methods of missile sec?tions on the flight performance of missile, a product assembly tolerance model was established.The as?sembly precision was optimized based on the transfer coefficients of dimensions and the machining diffi?culty coefiicients of dimensions. The pre-analysis method of connecting precision of missile sections was verified by calculating the missile vertex offset caused with the section connecting deflection through taking a certain missile as example.
Keywords:machinery design    virtual environment    pre-analysis of precision    tolerance analysis    tol?erance optimization  
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