节点文献

某航天代谢模拟装置的系统可靠性综合评估

Integrated Evaluation on System Reliability of a Space Metabolism Simulation Device

  • 推荐 CAJ下载
  • PDF下载
  • 不支持迅雷等下载工具,请取消加速工具后下载。

【作者】 杜振华陈金盾赵宇王立东

【Author】 DU Zhen hua,CHEN Jin dun,ZHAO Yu,WANG Li dong.Reliability Engineering Institute,Beijing University of Aeronau tics and Astronautics,Beijing 1 0 0 0 83,China

【机构】 北京航空航天大学可靠性工程研究所航天医学工程研究所航天医学工程研究所 北京100083北京100094北京100083北京100094

【摘要】 目的利用某航天代谢模拟装置组成单元的研制期间试验数据 ,给出该装置系统可靠性置信下限值。方法依据AMSAA模型给出了一种确定时间环境折合系数的新方法 ,进而得到各单元MTBF点估计和置信下限 ,最后利用L -M法给出该装置系统可靠度置信下限值。结果该装置在置信度为 0 .8下的系统可靠度置信下限值为 0 .92 81 ,与依据经典的系统可靠性评估方法得到的结果相接近。结论应用该方法进行系统可靠性综合评估可以较好地满足工程上的需求。

【Abstract】 Objective To define the lower confidence limit of the system reliability of the space metabolism simulation device by using the test data of the comprising units in their development phases. Method A new method for defining the environmental conversion factors of failure times has been given basing on the AMSAA model, and the MTBF point evaluated values and lower confidence limits of the units were defined, at last, the lower confidence limit of the system reliability was obtained using L M method. Result The lower confidence limit of the system reliability under confidence level of 0.8 is 0.9281, which is consistent with the result obtained by the classic system reliability evaluation method. Conclusion Integrated system reliability evaluation using the proposed method can well satisfy the need in engineering.

  • 【文献出处】 航天医学与医学工程 ,Space Medicine & Medical Engineering , 编辑部邮箱 ,2003年04期
  • 【分类号】V416
  • 【被引频次】3
  • 【下载频次】135
节点文献中: 

本文链接的文献网络图示:

本文的引文网络