| 用于导弹发射装置的平衡机 |
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| 引用本文： | 汪敬东,韩金良,冯大成.用于导弹发射装置的平衡机[J].上海航天,2006,23(3):32-35. |
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| 作者姓名： | 汪敬东 韩金良 冯大成 |
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| 作者单位： | 上海航天技术研究院研发中心,上海,200235 |
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| 摘 要： | 简述了导弹发射装置中弹簧式和扭杆式两种平衡机的特点及制造工艺。介绍了单发、多联装、箱式和舰用型等不同导弹发射装置中平衡机的结构布局,以及各自的特点,给出了平衡机设计的一般原则。
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| 关 键 词： | 导弹 发射装置 平衡机 弹簧式 扭杆式 结构布局 |
| 文章编号： | 1006-1630（2006）03-0032-04 |
| 收稿时间： | 2005-05-16 |
| 修稿时间： | 2005-07-21 |
Balancing Mechanism in the Missile Launcher |
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| WANG Jing-dong,HAN Jin-liang,FENG Da-cheng.Balancing Mechanism in the Missile Launcher[J].Aerospace Shanghai,2006,23(3):32-35. |
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| Authors: | WANG Jing-dong HAN Jin-liang FENG Da-cheng |
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| Abstract: | The characteristics of two main kinds of balancing mechanisms those were spring and torsion one for missile launcher were described briefly in this paper.The layout and characteristics of the balancing mechanisms in one-unit launcher,multi-unit launcher,box-style launcher and warship-type launcher were presented.The general principle in balancing mechanism design was given at last. |
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| Keywords: | Missile Launcher Balancing mechanism Spring Torsion Layout |
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