滚转机构在0.6m跨超声速风洞中的应用研究

doi:10.3969/j.issn.1000-1093.2017.08.025

兵工学报 ›› 2017, Vol. 38 ›› Issue (8): 1658-1664.doi: 10.3969/j.issn.1000-1093.2017.08.025

• 研究简报 • 上一篇

滚转机构在0.6m跨超声速风洞中的应用研究

荣祥森，唐淋伟，王伟仲，李增军，蒲泓宇

（中国空气动力研究与发展中心高速空气动力研究所，四川北川 622762）

收稿日期:2016-11-28 修回日期:2016-11-28 上线日期:2017-10-10
作者简介:荣祥森（1978—），男，工程师。E-mail:874277349@qq.com
基金资助:
国家“973”计划项目（613240）；国家自然科学基金项目（11402286）

Application of Rolling Device in 0.6m×0.6m Transonic and Supersonic Wind Tunnel

RONG Xiang-sen, TANG Lin-wei, WANG Wei-zhong, LI Zeng-jun, PU Hong-yu

(High Speed Aerodynamics Institute, China Aerodynamics Research and Development Center, Beichuan 622762, Sichuan, China)

Received:2016-11-28 Revised:2016-11-28 Online:2017-10-10

摘要/Abstract

摘要： 为了实现0.6 m跨超声速风洞试验过程中模型可连续变滚转角，提升0.6 m量级风洞的试验效率和试验范围，研制了一种滚转机构。介绍了该滚转机构、中空内置力矩电机以及控制系统软硬件的设计，对涉及到的关键技术问题进行了分析和总结，给出了结论并进行了风洞试验验证。试验结果表明：分别采用滚转机构与常规测力中部支架作为模型的支撑机构时，试验数据重复性好；滚转机构控制精度高（滚转角≤±3′）；载荷、工程性、可靠性均满足风洞试验要求。

关键词: 飞行器试验技术, 风洞, 滚转机构, 力矩电机, 控制系统, 工程应用

Abstract: A rolling device is developed for the continuous change of model's rolling angle, the improvement of test efficiency and test range in the 0.6 m×0.6 m transonic and supersonic wind tunnel. The designs of rolling device, hollow built-in torque servomotor and the software and hardware of control system are introduced. The key technical problems are analyzed and summarized, and the conclusions are finally validated by a wind tunnel test. The test data shows that the rolling device and the central support of the normal force test, as model's supporting mechanisms, can be used to acquire better repeatable data. Meanwhile, the system has a high level control precision (rolling angle≤±3′), and the engineering reliability of the loads meets the wind tunnel test requirements. Key

Key words: experimentaltechnologyofaerocraft, windtunnel, rollingdevice, torqueservomotor, controllingsystem, engineeringapplication

中图分类号:

V211.72

荣祥森，唐淋伟，王伟仲，李增军，蒲泓宇. 滚转机构在0.6m跨超声速风洞中的应用研究[J]. 兵工学报, 2017, 38(8): 1658-1664.

RONG Xiang-sen, TANG Lin-wei, WANG Wei-zhong, LI Zeng-jun, PU Hong-yu. Application of Rolling Device in 0.6m×0.6m Transonic and Supersonic Wind Tunnel[J]. Acta Armamentarii, 2017, 38(8): 1658-1664.

参考文献

［1］熊健.FL-23风洞测控处系统改造方案论证[R].绵阳:中国空气动力研究与发展中心高速空气动力研究所,2003.
XIONG Jian. The project approachment of rebuilding control and measurement system in FL-23 wind tunnel[R]. Mianyang: High Speed Aerodynamics Institute , China Aerodynamics Research and Development Center, 2003. (in Chinese)
[2］高鹏,凌忠伟,高飞，等. 西门子802Cbl数控系统在FL-23风洞投放机构改造上的应用[C]∥空气动力测控技术五届五次测控学术交流会论文集.武汉:中国空气动力测控学会,2009:108-112.
GAO Peng, LING Zhong-wei, GAO Fei, et al. The application of SIEMENS 802C base line numerical control system to the reforming of drop-off device in FL-23 wind tunnel[C]∥Proceedings of Fifth Measurement and Control Conference on Aerodynamic Measurement and Control Technology. Wuhan: China Aerodynamics Measurement and Control Association, 2009:108-112. (in Chinese)
[3］唐淋伟, 荣祥森,王伟仲. FL-23风洞滚转机构研制项目总结报告[R]. 绵阳:中国空气动力研究与发展中心高速空气动力研究所，2015.
TANG Lin-wei, RONG Xiang-sen, WANG Wei-zhong. FL-23 wind tunnel roll institutions development project summary report[R]. Mianyang:High Speed Aerodynamics Institute, China Aerodynamics Research and Development Center, 2015. (in Chinese)
[4］冯明, 白本奇,曲亮.风洞滚转机构用高性能力矩电机的研制[J].实验流体力学, 2012, 26(6): 67-69.
FENG Ming, BAI Ben-qi, QU Liang. Development of high performance torque motor for wind tunnel rolling system[J]. Journal of Experiments in Fluid Mechanics, 2012, 26(6): 67-69. (in Chinese)
[5］ Feng M,Qu L.Torque performance analysis of HDD spindle motors based on geometrical interpretation[J]. IEEE Transactions on Magnetics, 2011, 47(7):1906-1910.
[6］ Feng M, Kenjo T, Qu L.A direct Ampere-Gauss analytical method for surface permanent magnet motor calculation [C]∥2010 International Conference on Electrical Machines and Systems. Incheon, South Korea: IEEE, 2010:984-989.
[7］高月波,王勉华,张国平,等.高性能高精度力矩电机伺服控制系统设计[J]. 微电机, 2012, 45(2): 53-55.
GAO Yue-bo, WANG Mian-hua, ZHANG Guo-ping, et al. High-precision servo control system design for torque motor[J]. Micromotors, 2012, 45(2): 53-55. (in Chinese)
[8］刘刚，白本奇，冯明. 一种滚转控制装置在高超声速风洞中的应用[J]. 兵工自动化，2013, 32(6): 4-6.
LIU Gang，BAI Ben-qi，FENG Ming. Application of rolling control device in hypersonic wind tunnel[J]. Ordnance Industry Automation,2013, 32(6): 4-6. (in Chinese)
[9］姚春德，刘小平. 基于模糊PID控制的可变配气相位控制系统仿真研究[J]. 兵工学报，2007, 28(9): 1026-1029.
YAO Chun-de，LIU Xiao-ping. Simulation of variable cam timing control system based on fuzzy-PID[J]. Acta Armamentarii, 2007, 28(9): 1026-1029. (in Chinese)

[10］ GJB 7658—2012飞行器全模测力高速风洞试验方法[S].北京:中国人民解放军总装备部,2012.
GJB 7658—2012 Test method for aerodynamic force measurement of aircraft full model in high speed wind tunnel[S].Beijing: General Armament Department of PLA,2012.(in Chinese)
[11］范洁川. 风洞实验手册[M]. 北京:航空工业出版社，2002:281-283.
FAN Jie-chuan. Handbook of wind tunnel test[M]. Beijing: Aviation Industry Press,2002:281-283. (in Chinese)
[12］恽起麟. 风洞试验[M]. 北京:国防工业出版社，2000:236-237.
YUN Qi-lin. Wind tunnel test[M]. Beijing: National Defense Industry Press, 2000:236-237. (in Chinese)
[13］李周复. 风洞试验手册[M]. 北京:航空工业出版社，2015:336-337.
LI Zhou-fu. Handbook of wind tunnel test[M]. Beijing: Aviation Industry Press, 2015:336-337. (in Chinese)
[14］刘志勇,刘刚.基于5D机构组合模拟大侧滑角的方法[J].气动研究与发展,2011, 21(2): 35-38.
LIU Zhi-yong, LIU Gang. Amethod of joined-simulation of big side-angle on the 5D system [J].Aerodynamics Research and Development, 2011, 21(2): 35-38. (in Chinese)



下5篇留版

第38卷
第8期2017 年8月兵工学报ACTA
ARMAMENTARIIVol.38No.8Aug.2017

[1]	王武，付小强，卢青山，薛鹏，岳小东. 某型火箭炮运弹车自动调平控制系统的设计与实现[J]. 兵工学报, 2022, 43(S1): 82-87.
[2]	李景奎，林文杰，江秀红，卢雨泽. 基于GO-Markov的飞机燃油闭环控制系统可靠性分析[J]. 兵工学报, 2022, 43(6): 1447-1455.
[3]	刘月, 刘铁林, 姜相争, 韩月明. 基于径向基函数和自组织映射的导弹控制系统健康状态评估[J]. 兵工学报, 2022, 43(4): 931-939.
[4]	周恩民，顾蕴松，程松，刘恺，张文，王仪田，熊波. 连续式跨声速风洞中压缩机一体化设计[J]. 兵工学报, 2021, 42(6): 1331-1338.
[5]	孙一博，孟秀云. 滑翔飞行器多投放条件下飞行性能优化[J]. 兵工学报, 2021, 42(4): 781-797.
[6]	叶建川，王江，梁熠，宋韬，吴则良，徐超. 四旋翼无人机前飞模态特性[J]. 兵工学报, 2021, 42(11): 2476-2490.
[7]	薛栋，刘金，王欢，尹晋涛，江春茂，袁先士. CG-01高速风洞弹箭模型动稳定性导数实验系统设计[J]. 兵工学报, 2021, 42(11): 2522-2530.
[8]	井安言，佘湖清. 基于神经网络观测器的水下拖体输出反馈姿态控制[J]. 兵工学报, 2020, 41(12): 2504-2513.
[9]	周磊，李忠新，杨海波，蔡红明. 一种新型灵巧枪弹的气动特性研究[J]. 兵工学报, 2019, 40(4): 744-752.
[10]	雷瑶，纪玉霞. 小型共轴旋翼自然来流下的抗风扰气动特性分析[J]. 兵工学报, 2018, 39(6): 1225-1232.
[11]	黄伟，徐建城，吴华兴，李俊兵. 基于非数据通信的导弹编队制导律算法[J]. 兵工学报, 2018, 39(5): 910-918.
[12]	贺云，张飞龙，徐志刚，刘哲. 一种基于风洞试验环境的轨迹捕获系统设计[J]. 兵工学报, 2018, 39(12): 2480-2487.
[13]	柳忠彬，肖守讷，王欢. 非爆破柔性气缸弹射器研究[J]. 兵工学报, 2017, 38(2): 389-395.
[14]	杨树兴. 陆军多管火箭武器的发展与思考[J]. 兵工学报, 2016, 37(7): 1299-1305.
[15]	张文，周恩民，刘恺，程松，刘烽. 连续式跨声速风洞动力系统运行安全研究[J]. 兵工学报, 2016, 37(7): 1330-1336.

滚转机构在0.6m跨超声速风洞中的应用研究

Application of Rolling Device in 0.6m×0.6m Transonic and Supersonic Wind Tunnel

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