宇航计测技术 ›› 2023, Vol. 43 ›› Issue (2): 88-91.doi: 10.12060/j.issn.1000-7202.2023.02.16

• 计量保障技术 • 上一篇    下一篇

运载火箭双维度极性检查方法与应用

董余红1，韦康2，李茂1，黄辉1，刘秉1   

  1. 1.北京宇航系统工程研究所，北京 100076；2.中国文昌航天发射场，文昌 571333
  • 出版日期:2023-04-21 发布日期:2023-06-21
  • 作者简介:董余红（1979-），男，高级工程师，硕士，主要研究方向：运载火箭电气系统总体设计。

Double Dimensions Polarity Checking Method and Application for Launch-vehicle Systems

DONG Yu-hong1,WEI Kang2，LI Mao1，HUANG Hui1，LIU Bing1   

  1. 1.Beijing System Engineering Department，Beijing 100076,China;
     2.China Wenchang Spacecraft Launch Site,Wenchang 571333,China
  • Online:2023-04-21 Published:2023-06-21

PDF (PC)

102

摘要： 运载火箭接口极性设计及安装的正确性关系到型号的飞行成败，为确保运载火箭在设计及生产制造过程中的极性正确性，提出了一种对设计极性和安装极性进行双维度闭环检查确认的方法。本方法已在新一代大型运载火箭中实现了全箭接口极性全流程闭环检查确认，加强了极性设计状态和产品安装实现的闭环管控，确保了接口极性设计的正确和匹配。

关键词: 运载火箭, 设计极性, 安装极性, 闭环管控

Abstract: The design and assembly correctness of launch-vehicle’s interface polarity concern the flight success or failure.To make sure the polarity is correct during the launch-vehicle’s designing and production-manufacturing process,a method that can be used in a closed-loop double dimensions way for checking the correctness of design polarity and assembly polarity is presented.The method was used to check and confirm the new generation large scale launch-vehicle’s interface polarity in a closed-loop way,which strengthens the closed-loop management and control both of the polarity designing states and of the product’s assembly process,and which makes sure of the designing correctness and adaptability of the interface polarity.

Key words: Launch-vehicle, Design polarity, Assembly polarity, Closed-loop management and control

中图分类号: 

京ICP备09048426号-4　 京公网安备 11010602060144号　版权所有 © 《宇航计测技术》编辑部