导弹折叠翼展开过程的动力学仿真及试验研究

doi:10.3969/j.issn.1000-1093.2016.08.010

兵工学报 ›› 2016, Vol. 37 ›› Issue (8): 1409-1414.doi: 10.3969/j.issn.1000-1093.2016.08.010

导弹折叠翼展开过程的动力学仿真及试验研究

甄文强，姬永强，石运国

(中国工程物理研究院总体工程研究所，四川绵阳 621000)

收稿日期:2016-01-06 修回日期:2016-01-06 上线日期:2016-09-30
通讯作者: 甄文强 E-mail:413zhenwq@caep.cn
作者简介:甄文强（1989—），男，工程师
基金资助:
中国工程物理研究院总体工程研究所创新与发展基金项目(15CXJ13)

Dynamic Simulation and Experimental Study of Deployment Process of Missile Folding-wing

ZHEN Wen-qiang, JI Yong-qiang, SHI Yun-guo

(Institute of Systems Engineering, China Academy of Engineering Physics, Mianyang 621000, Sichuan, China)

Received:2016-01-06 Revised:2016-01-06 Online:2016-09-30
Contact: ZHEN Wen-qiang E-mail:413zhenwq@caep.cn

摘要/Abstract

摘要： 对导弹中常用的横向折叠翼展开过程进行研究，考虑折叠翼展开过程中气动阻力和摩擦力的作用，建立了导弹发射及地面试验时折叠翼展开过程的数学模型，使用动力学仿真软件建立相应动力学仿真模型，设计并制作了折叠翼，使用高速摄影获取折叠翼展开过程图像，开展地面试验研究。研究结果表明，试验结果与数学模型及动力学仿真模型结果的一致性较好，验证了折叠翼展开过程数学及动力学仿真模型的正确性。根据试验结果给出摩擦力矩的具体取值范围，为折叠翼的工程设计和应用提供了参考。

关键词: 兵器科学与技术, 折叠翼, 展开, 动力学仿真, 试验

Abstract: The deployment process of transverse folding-wings of missiles is studied. The mathematical model and dynamic simulation model of deployment process of folding-wing in missile launching and ground tests are both established, in which the influences of friction and aerodynamic force are considered. The folding-wing were designed and manufactured. The images of deployment process of folding-wings are obtained using the high speed photography during ground test. The research results show that the test results are in good agreement with those of mathematic and dynamic simulation models. A value range of friction moment is also provided from the test results, which can support the design and application of folding-wing.

Key words: ordnance science and technology, folding-wing, deployment, dynamic simulation, experiment

中图分类号:

TJ760.13

甄文强，姬永强，石运国. 导弹折叠翼展开过程的动力学仿真及试验研究[J]. 兵工学报, 2016, 37(8): 1409-1414.

ZHEN Wen-qiang, JI Yong-qiang, SHI Yun-guo. Dynamic Simulation and Experimental Study of Deployment Process of Missile Folding-wing[J]. Acta Armamentarii, 2016, 37(8): 1409-1414.

参考文献

［1］余旭东, 葛金玉, 段德高, 等. 导弹现代结构设计［M］. 北京:国防工业出版社, 2007.
YU Xu-dong，GE Jin-yu，DUAN De-gao, et al. Modern structure design of missiles［M］. Beijing:National Defense Industry Press, 2007.(in Chinese)
［2］ Kroyer R．Wing mechanism analysis［J］． Computers and Structures, 1999, 72(2): 253-265．
［3］ Henry J I, Schwartz D R, Soukup M A. Design construction and testing of a folding-wing tube-launched micro air vehicle［C］∥43rd AIAA Aerospace Sciences Meeting and Exhibit. Reno，Nevada:AIAA, 2005:2005-1451．
［4］李莉, 任茶仙, 张铎. 折叠翼机构展开动力学仿真及优化［J］. 强度与环境, 2007, 34(1):17-21.
LI Li，REN Cha-xian，ZHANG Duo. Dynamic simulation and optimization design of deployment of folding-wing［J］. Structure & Environment Engineering, 2007, 34(1):17-21.(in Chinese)
［5］崔二巍, 于存贵, 李猛, 等. 某导弹折叠弹翼展开过程的仿真分析［J］. 兵工自动化, 2013, 32(12):12-14.
CUI Er-wei, YU Cun-gui, LI Meng, et al. Simulation analysis of a missile folding wing deployment process［J］. Ordnance Industry Automation, 2013, 32(12):12-14.(in Chinese)
［6］赵俊锋, 刘莉, 杨武, 等. 折叠弹翼展开动力学仿真及优化［J］. 弹箭与制导学报, 2012, 32(2):155-157.
ZHAO Jun-feng, LIU Li, YANG Wu, et al. Dynamic simulation and optimization design of folding wing deployment［J］. Journal of Projectiles, Rockets, Missiles and Guidance, 2012, 32(2):155-157. (in Chinese)
［7］吴俊全, 孙海文, 张晓旻. 折叠翼展开试验与动力学仿真研究［J］. 弹箭与制导学报, 2011, 32(3):164-166.
WU Jun-quan，SUN Hai-wen，ZHANG Xiao-min. The research on unfolding test and dynamic model of folding-wing［J］. Journal of Projectiles, Rockets, Missiles and Guidance, 2011, 32(3):164-166. (in Chinese)
［8］张钦, 聂宏, 张明, 等. 无人机折叠翼展开动力学分析［J］. 机械设计与制造工程, 2015, 44(2):12-16.
ZHANG Qin，NIE Hong，ZHANG Ming，et al. Dynamic analysis of UAV folding wing depolyment process［J］. Machine Design and Manufacturing Engineering Technology, 2015, 44(2):12-16. (in Chinese)
［9］胡文华, 张伟, 曹东兴. 折叠翼的理论建模与实验研究［J］. 动力学与控制学报, 2015, 13(3):230-234.
HU Wen-hua，ZHANG Wei, CAO Dong-xing. Research on theoretical model and experiments of folding wings［J］. Journal of Dynamics and Control, 2015，13(3):230-234.(in Chinese)
［10］雷歌, 邓飞, 刘权, 等. 水下航行器折叠翼展开机构设计与动力学仿真［J］. 鱼雷技术, 2013, 21(2):81-85.
LEI Ge，DENG Fei，LIU Quan，et al. Design and dynamic simulation of folding wing expansion mechanism of underwater vehicle［J］. Torpedo Technology, 2013, 21(2):81-85. (in Chinese)
［11］秦永明, 蔡琛芳, 董金刚. 机载导弹折叠舵展开气动特性试验研究［J］. 航空兵器, 2013(5):3-6.
QIN Yong-ming，CAI Chen-fang，DONG Jin-gang. Experimental study on aerodynamics of airborne missile folding rudder［J］. Aero Weaponry, 2013(5):3-6.(in Chinese)
［12］贾毅. 战术导弹折叠翼两种展开方法及测试结果比较［J］. 流体力学实验与测量, 2003, 17(2):70-73.
JIA Yi. The comparison between two deploying methods and results of folding wings for some tactical missiles［J］. Experiments and Measurements in Fluid Mechanics, 2003, 17(2):70-73.(in Chinese)
［13］李真, 董玉立, 冯成良, 等. 基于CFD-FASTRN的导弹折叠弹翼展开过程模拟［J］. 弹箭与制导学报, 2015, 35(2):5-8.
LI Zhen, DONG Yu-li, FENG Cheng-liang, et al. Simulation of deployment of missile folded wings based on CFD-FASTRAN［J］. Journal of Projectiles, Rocekets, Missiles and Guidance, 2015, 35(2):5-8.(in Chinese)

[1]	张震东，王雪琴，任杰，刘峥，高原，王玺. 连续碳纤维增强环氧树脂复合材料圆管多胞结构的准静态压缩响应[J]. 兵工学报, 2022, 43(5): 1185-1193.
[2]	纪明，卜珺珺，马聪. 最大熵试验法对航天作动器输出可靠性的评估[J]. 兵工学报, 2022, 43(4): 919-923.
[3]	李宜果，王聪，武雨嫣，曹伟，卢佳兴，何乾坤. 跨介质航行体高速入水空泡壁面运动特性[J]. 兵工学报, 2022, 43(3): 574-585.
[4]	徐干成，袁伟泽，陈林恒，李成学，颉旭虎，聂梦琪. NFB700高强钢板抗震塌性能[J]. 兵工学报, 2022, 43(2): 391-400.
[5]	吕映庆，陈南勋，武海军，赵宏远，张雪岩. 弹体高速侵彻超高性能混凝土靶机理[J]. 兵工学报, 2022, 43(1): 37-47.
[6]	路宽，饶翔，王花梅，张倩. 不同形式锚泊系统对海洋资料浮标水动力性能的影响[J]. 兵工学报, 2022, 43(1): 120-130.
[7]	李军宁，王倩，韩卡，陈武阁. 坦克炮发射角对炮塔座圈动力学行为及其润滑性能的影响[J]. 兵工学报, 2021, 42(9): 1819-1828.
[8]	闫银坡，于福杰，陈原. 开架式水下机器人水动力系数计算与动力学建模[J]. 兵工学报, 2021, 42(9): 1972-1986.
[9]	刘安民，高峰，张青斌，袁天保，张国斌. 基于多项式混沌展开方法的翼伞飞行不确定性[J]. 兵工学报, 2021, 42(7): 1392-1399.
[10]	李淑睿，段卓平，郑保辉，罗观，黄风雷. 24-二硝基苯甲醚基熔铸含铝炸药圆筒试验及爆轰产物状态方程[J]. 兵工学报, 2021, 42(7): 1424-1430.
[11]	司骥跃，庞兆君，由锰，冯广斌，杜忠华. 空间绳网结构设计及优化方法[J]. 兵工学报, 2021, 42(5): 1065-1073.
[12]	鄢阿敏，皮爱国，王健，黄风雷，王晓锋. 基于薄层单元模型的弹体与引信系统螺纹连接参数确定方法[J]. 兵工学报, 2021, 42(4): 743-754.
[13]	祝昊，靳栓宝，王东，王公宝，魏应三，胡鹏飞，武星宇，何升阳，胡风革. 无轴泵喷推进器敞水特性[J]. 兵工学报, 2021, 42(4): 835-841.
[14]	宁小磊，吴颖霞，赵新. 融合仿真数据的小子样圆概率误差评估[J]. 兵工学报, 2021, 42(2): 388-398.
[15]	胡听春，孙宇锋，赵广燕. 武器装备可靠性设计保证系数取值方法[J]. 兵工学报, 2021, 42(12): 2753-2761.

导弹折叠翼展开过程的动力学仿真及试验研究

Dynamic Simulation and Experimental Study of Deployment Process of Missile Folding-wing

PDF

可视化

被引次数

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 15

编辑推荐

Metrics

本文评价