| 火箭橇试验减振系统力学仿真研究 |
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| 引用本文： | 丁春全,周昊,冯志杰,周俊明.火箭橇试验减振系统力学仿真研究[J].舰船电子工程,2012,32(8):87-89,112. |
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| 作者姓名： | 丁春全 周昊 冯志杰 周俊明 |
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| 作者单位： | 1. 襄阳市157信箱,襄阳,441003
2. 航宇救生装备有限公司,襄阳,441003 |
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| 摘 要： | 文章以火箭橇试验减振系统为研究对象,针对试验减振效果符合预期和减振系统出现异常的工作模式,建立减振系统数值仿真模型,通过数值仿真分析,分析减振失效的原因,提出对系统进行改进设计的建议,并对改进方案进行仿真评估。
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| 关 键 词： | 火箭橇 减振 仿真分析 |
Studies on Mechanics Simulation of a Rocket Pulley Reduce-oscillation System |
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| DING Chunquan,ZHOU Hao,FENG Zhijie,ZHOU Junming.Studies on Mechanics Simulation of a Rocket Pulley Reduce-oscillation System[J].Ship Electronic Engineering,2012,32(8):87-89,112. |
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| Authors: | DING Chunquan ZHOU Hao FENG Zhijie ZHOU Junming |
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| Institution: | 1.P.O.Box 157,Xiangyang 441003)(2.AVIC Aerospace LifeSupport Industries,LTD,Xiangyang 441003) |
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| Abstract: | With the research objects concentrated on the infrared rocket pulley reduceoscillation system,it’s aimed to the reduceoscillation effect according to anticipation in the second test,but not in the third test.Based on numerical simulation model,it analysed the reason of invalidation,and some ideas which would been provided for further improvement. |
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| Keywords: | rocket pulley reduceoscillation numerical simulation |
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