材料工程与机械制造

超磁致伸缩执行器驱动的射流伺服阀参数优化

  • 李跃松 ,
  • 朱玉川 ,
  • 吴洪涛 ,
  • 田一松 ,
  • 牛世勇
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  • 1. 南京航空航天大学 机电学院, 江苏 南京 210016;
    2. 西安飞行自动控制研究所, 陕西 西安 710065
李跃松(1985- ) 男,博士研究生。主要研究方向:流体传动与控制,机电控制及自动化。 E-mail: liyaosong707@163.com 朱玉川(1974- ) 男,博士,副教授。主要研究方向:流体传动与控制,机电控制及自动化。 Tel: 025-84892503 E-mail: meeyczhu@nuaa.edu.cn 吴洪涛(1962- ) 男,博士,教授,博士生导师。主要研究方向:机电控制及自动化,多体系统动力学。 E-mail: meehtwu@nuaa.edu.cn

收稿日期: 2010-11-08

  修回日期: 2011-01-04

  网络出版日期: 2011-07-23

基金资助

国家自然科学基金(50805080);航空科学基金(20090752008);南京航空航天大学基本科研业务费专项科研项目(NS2010150)

Parameter Optimization of Jet-pipe Servovalve Driven by Giant Magnetostrictive Actuator

  • LI Yuesong ,
  • ZHU Yuchuan ,
  • WU Hongtao ,
  • TIAN Yisong ,
  • NIU Shiyong
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  • 1. College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
    2. Flight Automatic Control Research Institute, Xi’an 710065, China

Received date: 2010-11-08

  Revised date: 2011-01-04

  Online published: 2011-07-23

摘要

为提高射流伺服阀的性能,提出了一种超磁致伸缩执行器驱动的直动式射流伺服阀。采用磁场有限元分析的方法,建立了超磁致伸缩执行器输出电流与输出位移的关系,分析了线圈结构对其输出位移的影响,并给出了所设计执行器的实验曲线。结合所设计的射流伺服阀的特点,以能量传递效率最大为优化目标,建立了射流结构与射流效率的关系方程,求出了所设计射流伺服阀的最佳射流结构参数,并利用流场分析软件分析了其静态特性,其零位无因次压力增益为1.7 mm-1,零位无因次流量增益为1.9 mm-1

本文引用格式

李跃松 , 朱玉川 , 吴洪涛 , 田一松 , 牛世勇 . 超磁致伸缩执行器驱动的射流伺服阀参数优化[J]. 航空学报, 2011 , 32(7) : 1336 -1344 . DOI: CNKI:11-1929/V.20110303.1352.001

Abstract

In order to improve the performance of a jet-pipe servovalve, a novel direct drive jet-pipe servovalve driven by a giant magnetostrictive actuator is proposed in this paper. By means of magnetic field finite element analysis, a model of the giant magnetostrictive actuator is established. The influence of coil structure on actuator displacement is analyzed and the experimental curves of the designed actuator are given. On the basis of the designed jet-pipe servovalve and taking the maximum energy transfer efficiency as the optimization objective, an equation is built between the jet parameters and jet efficiency. The best jet structure parameters of the designed servovalve are worked out, and its static characteristics are analyzed with the help of a flow field analysis software. The results show that its null dimensionless pressure gain is 1.7 mm-1, and the null dimensionless flow gain is 1.9 mm-1.

参考文献

[1] 李跃松, 朱玉川, 吴洪涛, 等. 射流伺服阀用超磁致伸缩执行器磁场建模与分析[J]. 兵工学报, 2010, 31(12): 1587-1592. Li Yuesong, Zhu Yuchuan, Wu Hongtao, et al. The magnetic field modeling and analysis of giant magntostrictive actuator for jet servovalve[J]. Acta Armamentarii, 2010, 31(12): 1587-1592. (in Chinese)



[2] Henri P D, Hollerbach J M, Nahvi A. An analytical and experimental investigation of a jet pipe controlled electro pneumatic actuator[J]. IEEE Transactions on Robotics and Automation, 1998, 14(6): 601-610.



[3] 章敏莹, 方群, 金瑶兰. 射流管伺服阀在航空航天领域的应用//第五届全国流体传动与控制学术会议. 北京: 北京航空航天大学, 2008: 810-812. Zhang Minying, Fang Qun, Jin Yaolan. Application of a jet pipe servovalve in aerospace//5th Fluid Power Transmiss & Conference of China. Beijing: Beihang University, 2008: 810-812. (in Chinese)



[4] 王传礼. 基于GMM转换器喷嘴挡板阀伺服阀的研究. 杭州: 浙江大学机械与能源工程学院, 2005. Wang Chuanli. Research on the nozzle flapper servo valve driven by GMM actuator . Hangzhou: College of Mechanical and Energy Engineering, Zhejiang University, 2005. (in Chinese)



[5] Karunanidhi S. Design, analysis and simulation of magnetostrictive actuator and its application to highdynamic servovalve[J]. Sensors and Actuators A: Physical, 2010, 157(11): 185-197.



[6] 王春行. 液压控制系统[M]. 北京: 机械工业出版社, 1999: 36-37. Wang Chunhang. Hydraulic control systems[M]. Beijing: China Machine Press, 1999: 36-37. (in Chinese)



[7] Grunwald A, Olabi A G. Design of a magnetostrictive (MS) actuator[J]. Sensors and Actuators A:Physical, 2008, 144(1): 161-175.



[8] The performance curves of the 8mm product of TbDyFe magnetostrictive alloys. . http: //www. tzjgre. com/en/tbdyfeprod. html.



[9] 陆君安, 尚涛, 谢进. 偏微分方程的 MATLAB 的解法[M]. 武汉: 武汉大学出版社, 2001: 53-61. Lu Jun’an, Shang Tao, Xie Jin. Use MATALAB to solve partial differential equation[M]. Wuhan: Wuhan University Press, 2001: 53-61. (in Chinese)



[10] 王兆铭, 渠立鹏, 金瑶兰. 射流电液伺服阀在压力控制中的应用[J]. 液压与机床, 2009, 37(11): 22-26. Wang Zhaoming, Qu Lipeng, Jin Yaolan. Application of jet-pipe electro hydraulic servovalve to pressure control[J]. Machine Tool & Hydraulics, 2009, 37(11): 22-26. (in Chinese)



[11] 成大先. 机械设计手册:液压控制[M]. 北京:化学工业出版社, 2004: 69-71. Cheng Daxian. Mechanical design handbook:hydraulic control[M]. Beijing: Chemical Industry Press, 2004: 69-71. (in Chinese)



[12] Somashekhar S H. Mathematical modeling and simulation of a jet pipe electrohydraulic flow control servovalve[J]. Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering, 2007, 221(3): 365-382.



[13] 杨月花. 伺服阀前置级射流流场分析及实验研究. 哈尔滨: 哈尔滨工业大学机电工程学院, 2006. Yang Yuehua. Analysis and experimental research of prestage jet flow field in hydraulic servovalve. Harbin: School of Mechanical and Electrical Engineering, Harbin Institute of Technology, 2006. (in Chinese)



[14] 冀宏, 魏列江. 射流管伺服阀射流管放大器的流场解析[J]. 机床与液压, 2008, 36(10): 119-121. Ji Hong, Wei Liejiang. Investigation to the flow of the jet-pipe amplifier in a servo valve[J]. Machine Tool & Hydraulics, 2008, 36(10): 119-121. (in Chinese)



[15] Hiremath S, Singaperumal M, Krishnakumar R. FE approach electro-mechanical-fluid modelling of jet pipe electrohydraulic servovalve//Power transmission and motion control PTMC 2003. London: Professional Engineering Publishing, 2003: 200-210.

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