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| 形状记忆合金驱动的折叠弹翼的结构设计 | |
| 引用本文： | 张玲,张世武,孟建新.形状记忆合金驱动的折叠弹翼的结构设计[J].航空兵器,2012(3):8-10. |
| 作者姓名： | 张玲 张世武 孟建新 |
| 作者单位： | 1. 中国空空导弹研究院,河南洛阳,471009 2. 中国科学技术大学,合肥,230000 3. 中国空空导弹研究院,河南洛阳471009／航空制导武器航空科技重点实验室,河南洛阳471009 |
| 摘 要： | 对于机载制导武器，翼面相对于导弹直径，在横向尺寸中占有很大的比例，因此采用翼面折叠的方式可以大大减小导弹横向尺寸。在弹翼展开机构中，展开驱动方式设计至关重要，本文提出了一种基于形状记忆合金的折叠弹翼展开机构的驱动方式。 |
| 关 键 词： | 导弹 折叠弹翼 记忆合金 |
The Structural Design of Folding Wing Actuated by Shape Memory Alloys |
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| ZHANG Ling,ZHANG Shi-wu,MENG Jian-xin.The Structural Design of Folding Wing Actuated by Shape Memory Alloys[J].Aero Weaponry,2012(3):8-10. | |
| Authors: | ZHANG Ling ZHANG Shi-wu MENG Jian-xin |
| Affiliation: | 1. China Airborne Missile Academy, Luoyang 471009, China ; 2. University of Science and Technology of China, Hefei 230000, China; 3. Aviation Key Laboratory of Science and Technology on Airborne Guided Weapons, Luoyang 471009, China) |
| Abstract: | Relative to the missile diameter, the wing has a large proportion in the horizontal dimen- sion of missile, therefore, using the way of wing folding can greatly reduce the horizontal size of missile. How to expand the wing is the key design. This paper presents a drive mode of folding wing deployment mechanism based on the shape memory alloy. |
| Keywords: | missile folding wing shape memory alloy |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ | |