| 战术导弹全弹FMECA方法研究 |
| |
| 引用本文： | 陈万创,张绍伟.战术导弹全弹FMECA方法研究[J].上海航天,2005,22(1):57-61,64. |
| |
| 作者姓名： | 陈万创 张绍伟 |
| |
| 作者单位： | 上海机电工程研究所,上海,200233 |
| |
| 摘 要： | 论述了故障模式影响及危害性分析(FMECA)的目的和意义，尤其强调了战术导弹全弹FMECA对提高导弹可靠性的作用。讨论了导弹详细设计阶段硬件的FMECA方法，包括自下而上综合方法、约定层次划分、故障严酷度分类等问题。最后，结合工程实践，给出了导弹全弹FMECA的部分应用实例。
|
| 关 键 词： | 战术导弹 全弹故障模式影响及危害性分析 自下而上法 约定层次划分 故障严酷度 |
| 文章编号： | 1006-1630(2005)01-0057-05 |
Failure Mode Effect and Criticality Analysis for Whole Tactical Missile |
| |
| CHEN Wan-chuang,ZHANG Shao-wei.Failure Mode Effect and Criticality Analysis for Whole Tactical Missile[J].Aerospace Shanghai,2005,22(1):57-61,64. |
| |
| Authors: | CHEN Wan-chuang ZHANG Shao-wei |
| |
| Abstract: | The purpose and mean of failure mode effect and criticality analysis (FMECA) were presented in this paper, and the function of FMECA for whole tactical missile to improve the missile reliability was stressed. The FMECA of hardware in the detailed design period and relative issues such as from-low-to-up integrated method, conventional layer classification, classification of fault criticality were discussed. At last, an application example of whole missile FMECA for some tactical missile was given. |
| |
| Keywords: | Tactical missile Failure mode effect and criticality analysis for whole missile From-low-to-up method Conventional layer classification Fault criticality |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
