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。
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.
出处
《航空兵器》
2012年第3期8-10,共3页
Aero Weaponry
基金
航空科学基金资助项目(20100178001)
关键词
导弹
折叠弹翼
记忆合金
missile
folding wing
shape memory alloy
