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[1]徐登伟,尤裕荣,袁洪滨,等.基于AMESim的先导膜片式电磁阀动态特性仿真[J].火箭推进,2017,43(04):41-45.
　XU Dengwei,YOU Yurong,YUAN Hongbin,et al.AMESim-based simulation analysis on dynamic characteristics of pilot-operated diaphragm solenoid valve[J].Journal of Rocket Propulsion,2017,43(04):41-45.
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基于AMESim的先导膜片式电磁阀动态特性仿真

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 43 期数: 2017年04期 页码: 41-45 栏目: 研究与设计 出版日期: 2017-10-01
Title:
AMESim-based simulation analysis on dynamic characteristics of pilot-operated diaphragm solenoid valve
作者:
徐登伟; 尤裕荣; 袁洪滨; 赵双龙
西安航天动力研究所, 陕西 西安 710100
Author(s):
XU Dengwei;  YOU Yurong;  YUAN Hongbin;  ZHAO Shuanglong
Xi’an Aerospace Propulsion Institute, Xi’an 710100, China
关键词:
先导膜片式电磁阀; 动态特性; AMESim; 仿真
Keywords:
pilot-operated diaphragm solenoid valve;  dynamic characteristic;  AMESim;  simulation
分类号:
V434-34
文献标志码:
A
摘要:
介绍了先导膜片式电磁阀的结构及工作原理，建立了其多物理过程耦合的数学模型，利用AMESim软件建立了先导式电磁阀动态仿真模型，研究了节流孔、工作压力、弹簧刚度及弹簧力对先导膜片式电磁阀动态响应的影响。结果表明：节流孔对响应时间的影响因素较大，随着节流孔的增大，阀门的打开响应时间越长，关闭响应时间越短。该分析方法可应用于先导式电磁阀的设计和分析，具有一定的工程应用价值。
Abstract:
The mechanical structure and working principle of a pilot-operated diaphragm solenoid valve are introduced. A mathematical model for coupling of multi-physical processes is set up. The AMESim-based dynamic simulation model of the pilot-operated solenoid valve is built. The influences of throttling orifice, work pressure, spring stiffness and spring force on the dynamic response characteristics of the pilot-operated diaphragm solenoid valve are analyzed. The results show that throttling orifice has a great influence on the response time of the pilot-operated diaphragm solenoid valve, and the opening response time prolongs and the close response time decreases with increase of the throttling orifice. The method in this paper can be applied to the design and analysis of pilot-operated solenoid valve, and has a certain value in engineering application.

参考文献/References:

[1] WALLER J M, ROTH T E. Causes and mitigation of fuel valve pilot seal extrusion in space shuttle orbiter primary RCS thrusters. AIAA2004-4149[R]. Fort Lauderdale, Florida: AIAA, 2004.
[2]王宝龄. 电磁电器设计基础[M]. 北京: 国防工业出版社，1989.
[3]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.
[4]陈亮, 梁国柱. 基于AMESim的电磁阀工作过程动态特性建模与仿真[J]. 导弹与航天运载技术, 2014(3): 49- 54.
[5]戴佳, 黄敏超, 余勇, 等. 电磁阀动态响应特性仿真研究[J]. 火箭推进, 2007, 33(1): 41-48.
DAI Jia, HUANG Minchao,YU Yong, et al. Simulation on the dynamic response characteristics of solenoid valve[J].Journal of rocket propulsion, 2007, 33(1): 41-48.
[6]朱宁昌. 液体火箭发动机设计（下）[M]. 北京: 中国宇航出版社, 1994.
[7]袁洪滨, 张民庆, 孙彦堂. 基于AMESim的直动式电磁阀动态特性仿真研究[J]. 火箭推进, 2011, 37(5): 30-35.
YUAN Hongbin, ZHANG Minqing, SUN Yantang. AMESim-based simulation analysis of dynamic character- istics of direct-acting solenoid valve[J]. Journal of rocket propulsion, 2011, 37(5): 30-35.
[8]王秋霞, 樊丁, 彭凯. AMESim仿真技术在高速电磁阀中的应用[J]. 航空动力学报, 2014, 29(3): 702-707.

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备注/Memo

收稿日期：2015-09-15；修回日期：2015-10-11 基金项目：基础科研项目（JCKY2016203C050） 作者简介：徐登伟（1985—），男，工程师，研究领域为液体火箭发动机阀门设计

更新日期/Last Update: 1900-01-01