| 导弹折叠翼展开机构的可靠性定性分析 |
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| 引用本文： | 倪健,陆凯,张铎.导弹折叠翼展开机构的可靠性定性分析[J].上海航天,2000,17(3):33-36. |
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| 作者姓名： | 倪健 陆凯 张铎 |
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| 作者单位： | 西北工业大学航天工程学院,陕西,西安,710072 |
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| 摘 要： | 通过对导弹折叠翼展开机构的分析得出了可靠性分析模型。针对某型飞航导弹的折叠翼展开过程，运用失效模式和影响分析（FMEA）的原理，对导弹折叠展开机的可靠性进行了较为全面的探讨和研究，得出了导弹折叠展开机构可靠性分析的各种故障模式，以便对全弹结构的可靠性进行定量分析。
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| 关 键 词： | 折叠翼 展开机构 可靠性分析 习航导弹 |
| 修稿时间： | ：1999－12－1 |
RELIABILITY QUALITATIVE ANALYSIS OF UNFOLDING MECHANISM OF MISSILE FOLDING-WING |
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| NI Jian,LU Kai,ZHANG Duo.RELIABILITY QUALITATIVE ANALYSIS OF UNFOLDING MECHANISM OF MISSILE FOLDING-WING[J].Aerospace Shanghai,2000,17(3):33-36. |
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| Authors: | NI Jian LU Kai ZHANG Duo |
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| Abstract: | In this thesis, the reliability analysis model is deduced by the study of the unfolding mechanism of missile fold wing. The failure mode and effect analysis method are used to analyze the reliability of the unfolding mechanism in detail. From this, all kinds of failure modes are gained so that whole missile's reliability will be analyzed quantitatively. |
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| Keywords: | Missile Fold wing Unfolding mechanism Reliability analysis |
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