基本信息:
- 专利标题： 一种基于当地流动特征剪裁的超声速六边形切角空气舵
- 专利标题（英）：Supersonic hexagon corner cut airvane based on local characteristic that flows is tailor
- 申请号：CN201620319826.9 申请日：2016-04-15
- 公开(公告)号：CN205593435U 公开(公告)日：2016-09-21
- 发明人： 陈新民 , 尹立中 , 陈世立 , 陈皓 , 温玉芬 , 马友林 , 高庆 , 朱辰 , 陈松 , 卢鑫 , 高晶晶 , 范晶晶 , 陈星星 , 谢晓阳 , 雷延花 , 宋少倩 , 韩英宏 , 李新田 , 刘珺怡 , 洪东跑 , 李翔
- 申请人： 中国运载火箭技术研究院
- 申请人地址： 北京市丰台区北京9200信箱38分箱
- 专利权人： 中国运载火箭技术研究院
- 当前专利权人： 中国运载火箭技术研究院
- 当前专利权人地址： 北京市丰台区北京9200信箱38分箱
- 代理机构： 中国航天科技专利中心
- 代理人： 庞静
- 主分类号： F42B10/04
- IPC分类号： F42B10/04
The utility model discloses a supersonic hexagon corner cut airvane based on local characteristic that flows is tailor, this airvane rudder face is protruding hexagon, its area is confirmed according to guided missile operation stability parameter, the leading edge sweep angle, the leading edge corner cut, the tip angle of osculation, the trailing edge corner cut is confirmed according to the mobile characteristic of rudder face, make the rudder face be supersonic flow, the rudder face is the most most opened up long definitely according to rudder face area and aspect ratio, the best value range of aspect ratio is 1.5~3, the leading edge, trailing edge corner cut position is confirmed according to local boundary layer thickness apart from root string perpendicular distance. Under the long -pending condition of equal airvane every detail, the rudder face control moment of hexagon corner cut airvane is excellent, and the rudder face is pressed and is felt concerned about several change volumes and obviously reduce, and comprehensive properties has apparent promotion, has reduced the guided missile design degree of difficulty.
IPC结构图谱:
| F | 机械工程；照明；加热；武器；爆破 |
| --F42 | 弹药；爆破 |
| ----F42B | 爆炸装药，例如用于爆破；烟火；弹药 |
| ------F42B10/00 | 效应装置，例如改进弹丸或发射物的空气动力学性质；弹丸或发射物的稳定、控制、降低射程、增加射程或减速降落用的装置 |
| --------F42B10/02 | .稳定装置 |
| ----------F42B10/04 | ..用固定翼 |