首页 | 本学科首页   官方微博 | 高级检索  
     检索      

适配器支撑飞行器/发射箱组合几何特性研究
引用本文:孟偲,王田苗,王家顺,王庆竹.适配器支撑飞行器/发射箱组合几何特性研究[J].北京航空航天大学学报,2002,28(4):428-431.
作者姓名:孟偲  王田苗  王家顺  王庆竹
作者单位:1. 北京航空航天大学机械工程及自动化学院;2. 中国航天三院
摘    要:基于先进的适配器支撑箱式发射技术,讨论了飞行器/适配器/发射箱一体化组合的几何特性,利用二维平面组合装配的数学模型,分析了飞行器、适配器、发射箱的相关形位和尺寸公差对间隙的影响,基于飞行器与发射箱组合基本公差配合特性,对三维几何模型进行了相应的参数设计.利用仿真分析系统分析干扰对间隙和通过性的影响,仿真结果表明可以作为为设计、装配和调整提供必要的理论依据.

关 键 词:箱式发射  装配  协调  飞行器系统  尺度分析
文章编号:1001-5965(2002)04-0428-04
收稿时间:2000-11-15
修稿时间:2000年11月15日

Research on Geometrical Features of Assembly of Aerocraft and Container
MENG Cai,WANG Tian-miao,WANG Jia-shun,WANG Qing-zhu.Research on Geometrical Features of Assembly of Aerocraft and Container[J].Journal of Beijing University of Aeronautics and Astronautics,2002,28(4):428-431.
Authors:MENG Cai  WANG Tian-miao  WANG Jia-shun  WANG Qing-zhu
Institution:Beijing University of Aeronautics and Astronautics, School of Mechanical Engineering and Automation
Abstract:Based on the advanced adapter-based container launching technology, the geometrical features of the assembly of aerocraft & container are studied. Taking advantage of the planar assembly model, the tolerances to fit clearances are analyzed, which have effects on size, shape, location of areocraft and etc. Furthermore, the parameter design of three-dimensional model is tried. Meanwhile, the effects that interferences have on fit clearances and steering ability is analyzed by emulator. The results indicates that it can provide essential theory references for design, assembly and coordination.
Keywords:container launching  assembling  coordination  aerocraft systems  dimensional analysis  
本文献已被 CNKI 维普 万方数据 等数据库收录!
点击此处可从《北京航空航天大学学报》浏览原始摘要信息
点击此处可从《北京航空航天大学学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号