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飞船检漏间气密性检测系统研制与应用
引用本文:王学忠,胡永刚. 飞船检漏间气密性检测系统研制与应用[J]. 装备指挥技术学院学报, 2007, 18(1): 109-112. DOI: 10.3783/j.issn.1673-0127.2007.01.026
作者姓名:王学忠  胡永刚
作者单位:1. 装备指挥技术学院,航天装备系,北京,101416;中国酒泉卫星发射中心,甘肃,酒泉,732750
2. 装备指挥技术学院,航天装备系,北京,101416
摘    要:飞船检漏间气密性检测系统研制的目的是对气密性检测过程和结果进行分析,确保飞船气密性测试的安全、准确、可靠。该系统采用现代计算机及自动控制等技术,解决了泄漏量测量的建模和系统配置问题。采用电荷耦合、提高放大倍数、降低量程等误差修正技术,提高了系统抗干扰能力和温度、压力测量数据的精度;实现了测量数据计算和结果适时显示、判定等功能。实际使用结果表明,该系统的检测结果满足飞船检漏气密性指标及试验任务要求。

关 键 词:气密性  密封  泄漏  温度  压力
文章编号:1673-0127(2007)01-0109-04
收稿时间:2006-04-17
修稿时间:2006-04-17

Development and Application of the Leakage Examination System for a Spacecraft-airproof-checking Room
WANG Xuezhong,HU Yonggang. Development and Application of the Leakage Examination System for a Spacecraft-airproof-checking Room[J]. Journal of the Academy of Equipment Command & Technology, 2007, 18(1): 109-112. DOI: 10.3783/j.issn.1673-0127.2007.01.026
Authors:WANG Xuezhong  HU Yonggang
Abstract:The leakage examination systems for a spacecraft-airproof-checking room is developed in order to assure the airproof of a spacecraft is safe and trustiness through the analysis result of the airproof checking.The technology of the modern computer and auto control are used in this system,and some problem about the leakage measure,configure system is solved.The robustness of system,the precise of temperature and pressure are observably improved as charge coupled,increase the amplification constant,decrease measure scope,etc.the method of correction error are adopted in the system.The actual results presented to verify this system can suffice the requirement of leakage examination.
Keywords:leakage  airproof  leak out  temperature  pressure  
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