| 一体化、轻量化卫星承力筒的研究 |
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| 引用本文： | 姚骏,谭时芳,李明珠,韩宇.一体化、轻量化卫星承力筒的研究[J].航天返回与遥感,2010,31(1):55-63. |
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| 作者姓名： | 姚骏 谭时芳 李明珠 韩宇 |
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| 作者单位： | 1. 上海卫星工程研究所,上海,200240
2. 北京空间机电研究所,北京,100076 |
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| 摘 要： | 承力筒是卫星结构的关键部件。文章首先介绍了一种轻量化的蜂窝夹层结构承力筒,一体化设计了柱段和锥段,优选了蒙皮铺层;随后详细阐述了承力筒的主要工艺流程,给出了制造结果;在通过模态试验、振动试验等验证后,该承力筒成功地应用于某卫星上。最后,文章给出了该承力筒研制成功的重要意义。
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| 关 键 词： | 承力筒 蜂窝夹层结构 设计 分析 制造 试验 卫星 |
Study on the Combined and Light Satellite Cylinder |
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| Yao Jun Tan Shifang Li Mingzhu Han Yu.Study on the Combined and Light Satellite Cylinder[J].Spacecraft Recovery & Remote Sensing,2010,31(1):55-63. |
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| Authors: | Yao Jun Tan Shifang Li Mingzhu Han Yu |
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| Institution: | Yao Jun Tan Shifang Li Mingzhu Han Yu(1 Shanghai Institute of Satellite Engineering,Shanghai 200240,China)(2 Beijing Institute of Space Mechanics ＆ Electricity,Beijing 100076,China) |
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| Abstract: | The cylinder was a key part for satellite structure.Firstly,the light cylinder of honeycomb sandwich was introduced briefly,whose column and taper were combined,and the cylinder panel was optimized reasonably.Secondly,the technical flowchart was described detailedly,and the production result was listed minutely.After the model and vibrate test,the cylinder was used in the satellite successfully.Finally,the important meaning was pointed out constructively. |
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| Keywords: | Cylinder Honeycomb sandwich Design Analysis Production Test Satellite |
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