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

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  • Sponsored by: China Association for Science and Technology (CAST)

    Editor-In-Chief: Xu Yida

    ISSN 1000-1093

    　

  • Hosted By: China Ordnance Society

    Published By: Acta Armamentarii

    CN 11-2176/TJ

Acta Armamentarii, a Chinese monthly journal, was first published in 1979. The journal is supervised by China Association for Science and Technology, sponsored by China Ordnance Society，and edited and published by Editorial Board of Acta Armamentarii. The Journal is included in all important domestic databases，and also collected by Engineering Index (EI, USA), Chemical Abstracts (CA, USA), Science Abstracts (SA, UK）, Abstract Journal (AJ, Russia), and Current Bibliography on Science and Technology(CBST).Acta Armamentarii has been selected into the journal Of Ordnance Science and Technology (Weapons Industry) Field Of High Quality Scientific and Technological Periodical Classification Catalogue (2022 edition), ranking T1, and the journal of Automotive Engineering Field of High Quality Scientific and technological Periodical classification Catalogue, ranking T2.
Acta Armamentarii ›› 2017, Vol. 38 ›› Issue (8) : 1658-1664. DOI: 10.3969/j.issn.1000-1093.2017.08.025
Research Notes

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
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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

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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. Acta Armamentarii. 2017, 38(8): 1658-1664 https://doi.org/10.3969/j.issn.1000-1093.2017.08.025

References



［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］FengM,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)


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