PDF下载 分享
[1]黄清伟,袁洪滨,李 海.弹箭星用电爆阀可靠性验证及评估[J].火箭推进,2015,41(06):51-54.
　HUANG Qingwei,YUAN Hongbin,LI Hai.Reliability validation and assessment of pyrovalve used in missile, rocket and satellite[J].Journal of Rocket Propulsion,2015,41(06):51-54.
点击复制

弹箭星用电爆阀可靠性验证及评估

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 41 期数: 2015年06期 页码: 51-54 栏目: 研究与设计 出版日期: 2015-12-31
Title:
Reliability validation and assessment of pyrovalve used in missile, rocket and satellite
作者:
黄清伟; 袁洪滨; 李 海
西安航天动力研究所，陕西 西安 710100
Author(s):
HUANG Qingwei;  YUAN Hongbin;  LI Hai
Xi’an Aerospace Propulsion Institute, Xi’an 710100, China
关键词:
电爆阀; 可靠性验证; 可靠性评估
Keywords:
pyrovalve;  reliability validation;  reliability assessment
分类号:
V431-34
文献标志码:
A
摘要:
针对电爆阀可靠性验证及评估难度大、所需试验样本数量多等问题，提出了一种强化试验的小子样可靠性评估及验证方法，对样本观测值利用数理统计方法计算产品的可靠性。经实际应用检验，本方法可以采用较少的试验样本获得较高的可靠性，降低了可靠性试验验证成本，使试验评定成为可能，满足了电爆阀可靠性评估及验证的工程需要。
Abstract:
Aiming at the difficulty of pyrovalve reliability validation and assessment, and requirement of large number of samples, a small sample reliability verification method of strenuous test is put forward. The product reliability is calculated with sample observation value by means of mathematical statistics method. Practical application proves that this method can obtain high reliability by using less test samples. It reduced the cost of reliability test, made the test evaluation possible and met the requirement of engineering reliability assessment of pyrovalve

参考文献/References:

[1]BEURTEY X. Reliability prediction on Ariane 5 pyrotech- nical devices using the hardened test method[C]// Proceedings of Probabilistic Safety Assessment and Manag-ement. Crete Greece: Springer London Ltd, 1997: 1687-1695.
[2][苏]卓洛托夫, 季托夫. 空间运载器的可靠性保证[M]. 潘绍珍, 译. 北京: 宇航出版社, 1996.
[3]邵德生. 关于火工装置的可靠性设计与验证问题[J]. 质量与可靠性, 2002, (增刊2): 34-36.
[4]胡昌寿. 航天可靠性设计手册[M]. 北京: 机械工业出

相似文献/References:

[1]张晓东,陈 健,唐妹芳,等.一种间接作用式常开电爆阀[J].火箭推进,2012,38(01):22.
　ZHANG Xiao-dong,CHEN Jian,TANG Mei-fang,et al.A new type of indirect normally open pyrovalve[J].Journal of Rocket Propulsion,2012,38(06):22.
[2]尤裕荣,杜大华,袁洪滨,等.电爆阀启动过程的响应特性与活塞撞击变形分析[J].火箭推进,2012,38(03):49.
　YOU Yu-rong,DU Da-hua,YUAN Hong-bin,et al.Analyses of response characteristics and piston impact deformation in process of pyro-valve start-up[J].Journal of Rocket Propulsion,2012,38(06):49.
[3]袁洪滨,胡攀,王志永,等.浅析国外电爆阀电爆机理研究进展[J].火箭推进,2016,42(02):86.
　YUAN Hongbin,HU Pan,WANG Zhiyong,et al.Analysis on research progress of mechanism of pyrotechnic valves abroad[J].Journal of Rocket Propulsion,2016,42(06):86.
[4]仵亮,赵飞,徐鸿翔,等.四刃交汇切刀的磨削工艺研究[J].火箭推进,2017,43(02):82.
　WU Liang,ZHAO Fei,XU Hongxiang,et al.Research on grinding technology of four-blade interactive cutter[J].Journal of Rocket Propulsion,2017,43(06):82.

备注/Memo

收稿日期：2015-01-15；修回日期：2015-03-20 基金项目：国家863项目（2008AA705313） 作者简介：黄清伟（1983—），男，工程师。研究领域为液体火箭推进系统阀门设计

更新日期/Last Update: 1900-01-01