| 固体火箭发动机衬层粘接技术综述 |
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| 引用本文： | 诸毓武,詹国柱,黄洪勇.固体火箭发动机衬层粘接技术综述[J].上海航天,2012,29(2):31-35,54. |
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| 作者姓名： | 诸毓武 詹国柱 黄洪勇 |
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| 作者单位： | 1. 中国人民解放军海军驻上海地区航天系统军事代表室,上海,201109
2. 上海航天动力技术研究所,浙江湖州,313000 |
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| 摘 要： | 综述了固体火箭发动机衬层粘接技术。介绍了衬层材料选择原则,分析了刷涂、喷涂、抛涂、离心和拉涂等成型工艺,讨论了界面粘接及其影响因素与改善途径,给出了前人的研究方法,阐述了衬层关键技术的发展趋势。
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| 关 键 词： | 固体火箭发动机 衬层 成型工艺 界面粘接 |
Progress in Liner Bonding Technology of Solid Rocket Motor |
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| ZHU Yu-wu,ZHAN Guo-zhu,HUANG Hong-yong.Progress in Liner Bonding Technology of Solid Rocket Motor[J].Aerospace Shanghai,2012,29(2):31-35,54. |
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| Authors: | ZHU Yu-wu ZHAN Guo-zhu HUANG Hong-yong |
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| Institution: | 1.The CPLA Navy Representative Office of Aerospace System in Shanghai,Shanghai 201109,China; 2.Shanghai Space Propulsion Technology Research Institute,Huzhou 313000,Zhejiang,China) |
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| Abstract: | The liner bonding technology of solid rocket motor was summarized in this paper.The design of liner formula was introduced.The forming technologies such as brush coating,spray coating,cast coating,centrifugal coating and pull coating were analyzed.The characterization of liner bonded interface and influencing factors of bonding property as well as the improving strategies were discussed.The study methods of the formers were given out.The developing trends of liner were also briefly introduced. |
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| Keywords: | Solid rocket motor Liner Forming technology Bonding property |
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