“一字型”折叠翼展开试验与仿真验证分析

中国机械工程 ›› 2015, Vol. 26 ›› Issue (13): 1801-1805.

“一字型”折叠翼展开试验与仿真验证分析

胡明1;章斌1;陈文华1;田芳菲1;张虹2;周小红2

1.浙江理工大学机电产品可靠性技术研究浙江省重点实验室，杭州，310018
2.北京机电工程研究所，北京，100074

出版日期:2015-07-10 发布日期:2015-07-08
基金资助:
国家自然科学基金资助项目(51375458)；教育部高等学校博士学科点专项科研基金资助项目（20123318130001）;浙江省自然科学基金资助项目(LZ12E05004)

Expand Performance and Simulation Verification of Line-styled Folding-wing

Hu Ming1;Zhang Bin1;Chen Wenhua1;Tian Fangfei1;Zhang Hong2;Zhou Xiaohong2

1.Zhejiang Province's Key Laboratory of Reliability Technology for Mechanical and Electrical Products,Zhejiang Sci-Tech University，Hangzhou，310018
2.Beijing Research Institute of Mechanical & Electrical Engineering，Beijing，100074

Online:2015-07-10 Published:2015-07-08
Supported by:
National Natural Science Foundation of China（No. 51375458）;Research Fund for the Doctoral Program of Higher Education of the Ministry of Education（No. 20123318130001）;Zhejiang Provincial Natural Science Foundation of China（No. LZ12E05004）

摘要/Abstract

摘要：

以某“一字型”折叠翼展开机构为研究对象，应用研制的折叠翼展开试验装置，进行了不同转矩下的展开试验，得到了其关键性能参数变化规律。参照“一字型”折叠翼展开机构原理样机的实际几何参数、物理特性及约束条件，在ADAMS中建立其虚拟样机模型，通过仿真分析得到了对应驱动力下折叠翼的运动参数和展开性能参数的变化规律。对比分析仿真与试验结果可知：弹翼能及时展开到位，准确定位、可靠锁定，且展开过程中各部件之间无干涉，满足设计要求。

关键词: 折叠翼, 展开机构, 展开试验, ADAMS仿真

Abstract:

Aiming at researching deployable mechanism of line-styled folding-wing, a spreading experimental device was designed, multiple spreading experiments were carried out in different torques, and the key performance parameter regulations were researched. A virtual prototype model of the folding-wing was established in ADAMS based on the actual geometric parameters, physical characteristics and constraints of the line-styled folding-wing. The simulation were used to study the folding-wing under different driving force of motion parameters and performance parameters regulations. Comparing simulation results with the test data, both of the dynamic simulation results and the group test data show that the folding-wing can unfurl to the appointed place quickly, can be located accurately and locked reliably. There are no interferences among each parts during the deployment process of folding-wing.

Key words: folding-wing, unfolding mechanism, spreading experiment, ADAMS simulation

中图分类号:

TJ760.3

胡明, 章斌, 陈文华, 田芳菲, 张虹, 周小红 . “一字型”折叠翼展开试验与仿真验证分析[J]. 中国机械工程, 2015, 26(13): 1801-1805.

Hu Ming, Zhang Bin, Chen Wenhua, Tian Fangfei, Zhang Hong, Zhou Xiaohong. Expand Performance and Simulation Verification of Line-styled Folding-wing[J]. China Mechanical Engineering, 2015, 26(13): 1801-1805.

参考文献

[1]李莉，吴斌. 折叠翼展开性能仿真研究与实验[D]. 西安：西北工业大学，2005.
[2]Wang H，Yu T X，Pang H，et al. Reliability Simulation Analysis for Complex Mechanism Based on Support Vector Machine[C]//2011 International Conference on Consumer Electronics，Communications and Networks. Las Vegas：2011：546-550.
[3]Venanzi S，Parenti-Castelli V. A New Technique for Clearance Influence Analysis in Spatial Mechanisms[J]. Journal of Mechanical Design，Transactions of the ASME，2005，127(3)：446-455.
[4]Guilaume M，Mandanis G，Pfiffner I，et al. The Swiss F/A-18 Full Scale Fatigue Test-Modern and Efficient Testing[C]//AIAA 4th Aviation Technology，Integration and Operations (ATIO) Forum. Chicago，2004：1-27.
[5]Hudson L，Stephens C. X-37 C/SiC Ruddervator Subcomponent Test Program[C]//NASA/Fundamental Aeronautics Program Annual Meeting. Atlanta，2009：20090037113.
[6]赵育善，余旭东，马彩霞，等. 折叠翼展开过程仿真研究[J]. 弹箭与制导学报,1997,17(2):19-23.
Zhao Yushan，Yu Xudong，Ma Caixia，et al. The Research on Unfolding Process Simulation of Folding-wing[J]. Journal of Projectiles，Rockets，Missiles and Guidance，1997,17(2)：19-23.
[7]马彩霞, 余旭东, 王焘. 导弹折叠翼展开运动试验[J]. 弹箭与制导学报,1996,16(2):63-65.
Ma Caixia, Yu Xudong, Wang Tao. Expand Motion Performance and Simulation of Missile Folding-wing[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 1996,16(2):63-65.
[8]谭湘霞, 吴斌, 余旭东, 等. 导弹折叠翼的机构弹性动力学分析与仿真研究[J]. 弹箭与制导学报，1999,19(1):17-21.
Tan Xiangxia, Wu Bin, Yu Xudong, et al. The Research on Mechanism Simulation and Elastic Dynamics of Missile Folding-wing[J]. Journal of Projectiles，Rockets，Missiles and Guidance，1999，19(1)：17-21.
[9]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，2011，31(3)：164-166.
Wu Junquan，Sun Haiwen，Zhang Xiaomin. The Research on Unfolding Test and Dynamic Model of Folding-wing[J]. Journal of Projectiles，Rockets，Missiles and Guidance，2011，31(3)：164-166.
[10]赵俊峰，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 (4)：155-157.
Zhao Junfeng，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 (4)：155-157.
[11]郑旸，吴斌，杨森. 折叠翼机构加载展开试验系统设计和仿真研究[J]. 装备环境工程，2013，10(2)：38-43.
Zheng Yang，Wu Bin，Yang Sen. Design and Simulation of Folding Wings Loading and Spreading Experimental Device[J]. Equipment Environmental Engineering，2013，10(2)：38-43.