电磁阀用自锁电磁铁吸力与电压关系研究

推进技术 ›› 2016, Vol. 37 ›› Issue (7): 1372-1379.

电磁阀用自锁电磁铁吸力与电压关系研究

任志彬,王宗伟,常志鹏,石里男,董耀军

空间物理重点实验室，北京 100076,空间物理重点实验室，北京 100076,空间物理重点实验室，北京 100076,空间物理重点实验室，北京 100076,空间物理重点实验室，北京 100076

发布日期:2021-08-15
作者简介:任志彬，男，硕士，工程师，研究领域为飞行器动力系统。

Research on Solenoid-Force-Voltage Relationship of Latching Solenoid for Solenoid Valves

Science and Technology on Space Physics Laboratory，Beijing 100076，China,Science and Technology on Space Physics Laboratory，Beijing 100076，China,Science and Technology on Space Physics Laboratory，Beijing 100076，China,Science and Technology on Space Physics Laboratory，Beijing 100076，China and Science and Technology on Space Physics Laboratory，Beijing 100076，China

Published:2021-08-15

摘要/Abstract

摘要： 为了解释自锁电磁铁进行吸力试验时出现的电磁吸力随电压非单调变化的现象，利用ANSYS软件进行仿真计算，并开展理论分析。仿真和分析得到了与试验相同的电磁吸力变化趋势。根据仿真和分析的结果确定:主要因素为导磁材料饱和，导致电磁吸力停止增大；次要因素为磁钢工作点变化，导致电磁吸力出现下降趋势。

关键词: 自锁电磁铁；电磁吸力；非单调；导磁材料饱和；磁钢工作点；ANSYS

Abstract: It is discovered during the experiments of latching solenoids that the solenoid forces change non-monotonically along with the voltages. In order to explain this phenomenon，the solenoid forces are simulated based on ANSYS，and are analysed theoretically. The results of the simulation and the analysis show the same tendency as the experiments. It is concluded that the saturation of the magnetic material is the primary factor，which makes the solenoid force stop increasing. And the variation of the working point of the permanent magnet is the secondary factor，which leads to the solenoid force decreasing.

Key words: Latching solenoid；Solenoid force；Non-monotonic；Magnetic material saturation；Permanent magnet working point；ANSYS

任志彬,王宗伟,常志鹏,石里男,董耀军. 电磁阀用自锁电磁铁吸力与电压关系研究[J]. 推进技术, 2016, 37(7): 1372-1379.

REN Zhi-bin,WANG Zong-wei,CHANG Zhi-peng,SHI Li-nan,DONG Yao-jun. Research on Solenoid-Force-Voltage Relationship of Latching Solenoid for Solenoid Valves[J]. Journal of Propulsion Technology, 2016, 37(7): 1372-1379.

参考文献

[1] 廖少英. 液体火箭推进增压输送系统[M]. 北京:国防工业出版社, 2007.
[2] 朱宁昌, 刘国球, 章本立, 等.液体火箭发动机设计(下)[M].北京:中国宇航出版社, 1994.
[3] 王心清, 李兴泉, 吴德隆, 等.结构设计[M]. 北京:宇航出版社, 1994.
[4] Reinicke R H, Harris S A. BiLatch Isolation Valve for Spacecraft Propulsion Systems[R]. AIAA 95-3098.
[5] Lynch R A. Common Valve Design for Space Shuttle Payload Propulsion System Applications[R]. AIAA 80-1296.
[6] Pond G T, Wichmann H. Development of a Bipropellant Titanium Latch Valve[R]. AIAA 87-2115.
[7] Morash D H, Barbarits J K. Propellant Valve Assembly for the Upper Stage of the Ariane 5 Launch Vehicle[R]. AIAA 95-3095.
[8] Hinckel J, T-Airoldi V, Corat E, et al. Propulsion Subsystem Component Development Program for the MECB RSS Satellite[R]. AIAA 91-1836.
[9] Li Q, Li W, D F, et al. A Novel Design for an Electromagnetic Valve Actuator for High Pressure Applications[J]. Smart Materials and Structures, 2012, 21 (107001): 1-4.
[10] Kim J, Lieu D K. Designs for a New, Quick-Response, Latching Electromagnetic Valve[C]. San Antonio: IEEE International Conference on Electric Machines and Drives, 2005.
[11] Belli Z, Mekideche M R. Dynamic Optimization of an Axisymmetric Linear Electromagnetic Valve Actuator[C]. Monte Carlo: Eighth International Conference and Exhibition on Ecological Vehicles and Renewable Energies, 2013.
[12] Yang Y P, Liu J J, Ye D H, et al. Multiobjective Optimal Design and Soft Landing Control of an Electromagnetic Valve Actuator for a Camless Engine[J]. IEEE/ASME Transactions on Mechatronics, 2013, 18(3): 963-972.
[13] Zhang C, Dan S, Ding X. Permanent Magnet Acts on the Dynamic Characteristic of Single-Stable Permanent Magnet Actuator[C]. Shanghai: Power and Energy Engineering Conference, APPEEC, Asia-Pacific, 2012.
[14] 王宝龄. 电磁电器设计基础(修订本)[M]. 北京:国防工业出版社, 1989.
[15] 林莘. 永磁机构与真空断路器[M]. 北京:机械工业出版社, 2002.
[16] 潘英朋, 高汉平, 刘刚. 磁性双位自锁电磁阀磁路设计与分析[J]. 液压气动与密封, 2010, (1): 29-34.
[17] 游一民, 郑军, 罗文科. 永磁机构及其发展动态[J]. 高压电器, 2001, 37(1): 44-47.
[18] 张冠生, 陆俭国. 电磁铁与自动电磁元件[M]. 北京:机械工业出版社, 1982.
[19] 娄路亮, 王海洲. 电磁阀设计中电磁力的工程计算方法[J]. 导弹与航天运载技术, 2007, 1: 40-45.
[20] 郭凤英, 何洪庆, 黄应坤, 等. 电动气活门的可靠性设计[J]. 推进技术, 1997, 18(5): 87-90. (GUO Feng-ying, HE Hong-qing, HUANG Ying-kun, et al. The Reliability Design of Electro-Pneumatic Valve[J]. Journal of Propulsion Technology, 1997, 18(5): 87-90.)
[21] 沈赤兵, 陈新华, 陈启智. 电动气阀动态特性及反力因素的影响[J]. 推进技术, 1996, 17(6): 64-68. (SHEN Chi-bing, CHEN Xin-hua, CHEN Qi-zhi. The Influence of Reaction Factors on the Dynamic Characteristics of Electropneumatic Valves[J]. Journal of Propulsion Technology, 1996, 17(6): 64-68.)
[22] 陶玉静, 范才智, 田章福, 等. 两位五通电动气阀动态特性研究[J]. 推进技术, 2006, 27(6): 542-545. (TAO Yu-jing, FAN Cai-zhi, TIAN Zhang-fu, et al. Study on the Dynamic Characteristic of the Electropneumatic Valve[J]. Journal of Propulsion Technology, 2006, 27(6): 542-545.)
[23] 刘潜峰, 薄涵亮, 秦本科. 直动电磁阀磁场特性分析[J]. 核科学与工程, 2009, 29(2): 103-107.
[24] 申卫兵, 周静, 李永振. 基于ANSYS的电磁阀仿真与分析[J]. 流体传动与控制, 2010, 5: 4-5.
[25] Wang S M, Miyano T, Hubbard M. Electromagnetic Field Analysis and Dynamic Simulation of a Two-Valve Solenoid Actuator[J]. IEEE Transactions on Magnetics, 1993, 29 (2): 1741-1746.
[26] Lee G S, Sung H J, Kim H C. Multiphysics Analysis of a Linear Control Solenoid Valve[J]. Journal of Fluids Engineering, 2013, 135: 1-10.
[27] 左全璋. 双稳态电磁机构计算方法的特点[J]. 机电元件, 1987, 7(1): 1-6.
[28] 张莹. 电磁铁用软磁合金系列的研究[J]. 上海钢研, 2002, (4): 3-9.(编辑:史亚红) 　　　　　　　　　　　　　*　收稿日期:2015-03-18；修订日期:2015-05-12。作者简介:任志彬,男,硕士,工程师,研究领域为飞行器动力系统。E-mail: jensjeremies@163.com