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航天器大型密封舱垂直进舱工装设计

赵璐 肖正懿 黄垒 曾婷 刘孟周

航天器环境工程2011,Vol.28Issue(6):620-624,5.
航天器环境工程2011,Vol.28Issue(6):620-624,5.DOI:10.3969/j.issn.1673-1379.2011.06.023

航天器大型密封舱垂直进舱工装设计

Design of support equipment for vertical access to spacecraft's large sealed cabin in ground assembly

赵璐 1肖正懿 1黄垒 1曾婷 2刘孟周1

作者信息

  • 1. 北京卫星环境工程研究所,北京100094
  • 2. 北京卫星制造厂,北京100190
  • 折叠

摘要

Abstract

To achieve the vertical access to a large sealed cabin during the spacecraft assembly process and in view of the large cabin's structure and layout features, this paper discusses the structural characteristics of three kinds of equipment for vertical access, I.e. The lifting basket, the segmented combination ladder, and the motor-driven device. By comparing the advantages and disadvantages of three schemes, an analysis is made with regard to the features of the outside cabin assembly platform, the applicability to the assembly environment, and the security and the effect of vertical access to the cabin. This paper provides some guidance on the design and the evaluation of vertical access equipment for large spacecraft assembly.

关键词

航天器总装/密封舱:垂直进舱/地面辅助设备

Key words

spacecraft assembly/ sealed cabin/ vertical access/ ground support equipment

分类

航空航天

引用本文复制引用

赵璐,肖正懿,黄垒,曾婷,刘孟周..航天器大型密封舱垂直进舱工装设计[J].航天器环境工程,2011,28(6):620-624,5.

基金项目

国家重大科技专项工程 ()

航天器环境工程

OACSTPCD

1673-1379

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