徐波涛,刘玉刚,方志开,吕景辉,喻新发.运输包装箱的多载荷减振设计研究[J].装备环境工程,2020,17(8):45-50. XU Bo-tao,LIU Yu-gang,FANG Zhi-kai,LYU Jing-hui,YU Xin-fa.Vibration Damping Design for Multi-load Cargo Container[J].Equipment Environmental Engineering,2020,17(8):45-50.
运输包装箱的多载荷减振设计研究
Vibration Damping Design for Multi-load Cargo Container
投稿时间:2019-11-10  修订日期:2019-12-16
DOI:10.7643/issn.1672-9242.2020.08.007
中文关键词:  运输  包装箱  减振设计  兼容性
英文关键词:transportation  container  vibration damping  compatibility
基金项目:国防基础科研项目(JCKY2018203B009)
作者单位
徐波涛 北京卫星环境工程研究所,北京 100094;北京市航天产品智能装配技术与装备工程技术研究中心,北京 100094 
刘玉刚 北京卫星环境工程研究所,北京 100094;北京市航天产品智能装配技术与装备工程技术研究中心,北京 100094 
方志开 北京卫星环境工程研究所,北京 100094;北京市航天产品智能装配技术与装备工程技术研究中心,北京 100094 
吕景辉 北京卫星环境工程研究所,北京 100094;北京市航天产品智能装配技术与装备工程技术研究中心,北京 100094 
喻新发 北京卫星环境工程研究所,北京 100094 
AuthorInstitution
XU Bo-tao Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China;Beijing Engineering Research Center of the Intelligent Assembly Technology and Equipment for Aerospace Product, Beijing 100094, China 
LIU Yu-gang Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China;Beijing Engineering Research Center of the Intelligent Assembly Technology and Equipment for Aerospace Product, Beijing 100094, China 
FANG Zhi-kai Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China;Beijing Engineering Research Center of the Intelligent Assembly Technology and Equipment for Aerospace Product, Beijing 100094, China 
LYU Jing-hui Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China;Beijing Engineering Research Center of the Intelligent Assembly Technology and Equipment for Aerospace Product, Beijing 100094, China 
YU Xin-fa Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China 
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中文摘要:
      目的 考虑降低成本,提高效率,面向卫星产品型谱的通用式包装箱设计势在必行。如何确定和选用一种适应于不同载荷特性的减振方案,成为航天器运输减振设计的关键点和技术难点。方法 针对这一问题,分析了目标产品的尺寸接口和质量特性,对卫星不同舱段运输工况进行了振动特性分析和试验。结果 在此基础上设计了一种适用于3种卫星舱体、4种运输状态通用的包装箱减振分系统,并对装载尺寸参数进行了优化。系统一阶垂向频率不高于5.8 Hz。结论 运输试验数据表明新型减振系统对航天产品的减振效果满足要求。
英文摘要:
      The work aims to design a kind of general container for satellite product to reduce cost and improve efficiency in view of how to determine and select a damping scheme suitable for different load characteristics has become the key point and technical difficulty in spacecraft transportation vibration damping design. Aiming at this problem, the size interface and weight of the target products were analyzed, and the vibration feature of different transporting conditions of the satellite was investigated and tested. On basis of this, a general shock absorption subsystem for three kinds of satellites and four kinds of transportation conditions was designed, and the loading size parameters were optimized. The first-order vertical fundamental frequency of the system was less than 5.8 Hz. The transportation test data show that the vibration damping effect of the new vibration damping system for aerospace products meets the requirements.
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