刘龙涛,张保刚,张兴勇,于喆,俞刘建,安庆升.基于性能参数的某发射箱前盖可靠性评估[J].装备环境工程,2020,17(6):122-125. LIU Long-tao,ZHANG Bao-gang,ZHANG Xing-yong,YU Zhe,YU Liu-jian,AN Qing-sheng.Reliability Assessment for Frangible Cover of a Launch Canister Based on Performance Parameters[J].Equipment Environmental Engineering,2020,17(6):122-125.
基于性能参数的某发射箱前盖可靠性评估
Reliability Assessment for Frangible Cover of a Launch Canister Based on Performance Parameters
投稿时间:2019-11-16  修订日期:2019-12-26
DOI:10.7643/issn.1672-9242.2020.06.019
中文关键词:  性能参数  可靠性评估  成败型  小子样
英文关键词:performance parameter  reliability assessment  success-or-failure pattern  small sample
基金项目:
作者单位
刘龙涛 上海机电工程研究所,上海 201109 
张保刚 上海机电工程研究所,上海 201109 
张兴勇 上海机电工程研究所,上海 201109 
于喆 上海机电工程研究所,上海 201109 
俞刘建 上海机电工程研究所,上海 201109 
安庆升 上海机电工程研究所,上海 201109 
AuthorInstitution
LIU Long-tao Shanghai Electro-Mechanical Engineering Institute, Shanghai 201109, China 
ZHANG Bao-gang Shanghai Electro-Mechanical Engineering Institute, Shanghai 201109, China 
ZHANG Xing-yong Shanghai Electro-Mechanical Engineering Institute, Shanghai 201109, China 
YU Zhe Shanghai Electro-Mechanical Engineering Institute, Shanghai 201109, China 
YU Liu-jian Shanghai Electro-Mechanical Engineering Institute, Shanghai 201109, China 
AN Qing-sheng Shanghai Electro-Mechanical Engineering Institute, Shanghai 201109, China 
摘要点击次数:
全文下载次数:
中文摘要:
      目的 有效评估某发射箱前盖发射任务的可靠性。方法 采用特征量为性能参数的可靠性验证试验和评估方法。结果 通过开展前盖可靠性验证试验,结合开盖压力参数进行可靠性评估,发射任务的可靠度满足要求。结论 基于性能参数的可靠性评估方法适用于高可靠性指标要求的成败型航天机械产品小子样评估。
英文摘要:
      To effectively evaluate the reliability of frangible cover for a launch canister, the method of reliability verification test and assessment was carried out based on the characteristic variables of performance parameters. The results of reliability versification test of the frangible cover in combination with the reliability assessment based on the parameters of opening pressure showed that the reliability of frangible cover meet the requirement. The reliability assessment method based on performance parameters is suitable for small sample assessment of success-or-failure aerospace machinery products with high reliability requirement.
查看全文  查看/发表评论  下载PDF阅读器
关闭

关于我们 | 联系我们 | 投诉建议 | 隐私保护 | 用户协议

您是第12773129位访问者    渝ICP备15012534号-5

版权所有:《装备环境工程》编辑部 2014 All Rights Reserved

邮编:400039     电话:023-68792835    Email: zbhjgc@163.com

视频号 公众号