| 筒式发射器圆柱凸轮机构设计 |
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| 引用本文： | 郭三学.筒式发射器圆柱凸轮机构设计[J].重型机械,2011(5):50-52. |
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| 作者姓名： | 郭三学 |
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| 作者单位： | 武警工程大学装备运输系,陕西西安,710086 |
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| 基金项目： | 武警部队科研项目(WXK2009-01) |
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| 摘 要： | 针对火箭抛锚器的应用特点，采用筒式发射器的结构形式，设计了圆柱凸轮控制机构，通过等速推杆运动规律实现对火帽的准确击发，确定了凸轮轮廓曲线，圆柱凸轮机构经使用能安全可靠的击发火箭抛锚体。
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| 关 键 词： | 发射器 凸轮机构 设计 |
Design of cylindrical cam mechanism in cylindrical launcher |
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| GUO San-xue.Design of cylindrical cam mechanism in cylindrical launcher[J].Heavy Machinery,2011(5):50-52. |
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| Authors: | GUO San-xue |
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| Affiliation: | GUO San-xue (Department of Ordnance and Transportation,Engineering College ofCAPF,Xi'an 710086,China) |
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| Abstract: | The structure of the cylindrical launcher is adopted to design the cylindrical cam control mechanism according to the feature of the rocket anchor projectile.The precise percussion is realized by means of the constant velocity motion pattern The cam contour curve was confirmed.The practice indicates that the cylindrical cam mechanism can launch the rocket anchor projectile safely and reliably. |
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| Keywords: | launcher cam mechanism design |
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