| 导弹折叠翼展开机构运动功能可靠性分析 |
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| 引用本文： | 倪健,陆凯,张铎.导弹折叠翼展开机构运动功能可靠性分析[J].上海航天,2001,18(5):1-5. |
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| 作者姓名： | 倪健 陆凯 张铎 |
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| 作者单位： | 西北工业大学航天学院 , |
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| 摘 要： | 通过建立等效动力模型得出导弹弹翼展开机构的运动规律，进而对弹翼展开机构进行动态静力分析。针对某型飞航导弹的折叠弹翼展开过程，对机构运动功能可靠性进行了较为全面的探讨和研究。该方法可用于 飞行器分离机构，展开机构和折叠机构等的可靠性分析。
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| 关 键 词： | 导弹折叠翼 展开机构 等效动力模型 可靠性 运动功能 可靠性分析 |
| 文章编号： | 1006-1630(2001)05-0001-05 |
| 修稿时间： | 2000年1月21日 |
Movement Function Reliability of Mechanism of Deployable Folded Wings of Missile |
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| NI Jian,LU Kai,ZHANG Duo.Movement Function Reliability of Mechanism of Deployable Folded Wings of Missile[J].Aerospace Shanghai,2001,18(5):1-5. |
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| Authors: | NI Jian LU Kai ZHANG Duo |
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| Abstract: | A movement law of deployable folded mechanism of missile wing is gained through setting up equivalent dynamical model. Moreover, deployable mechanism of missile wing is analysized dynamicolly. This paper discusses and studies the mechanism's movement function reliability for some cruise missile. This method can be used for reliability analysis of separated, deployable and folded mechanism of aerocraft. |
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| Keywords: | Missile folded wing Deployable mechanism Equivalent dynamical model Reliability Movement function reliability |
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