|Table of Contents|

Fast-response solenoid valve based on resistance and capacitance(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2019年04期
Page:
58-62
Research Field:
研究与设计
Publishing date:

Info

Title:
Fast-response solenoid valve based on resistance and capacitance
Author(s):
ZOU Jia1LIU Fei2ZHU Jianguo2ZHOU Xuefeng2
(1.Naval Equipment Department,Xi’an 710065,China;2.Xi’an Aerospace Propulsion Institute,Xi’an 710100,China)
Keywords:
solenoid valve fast-response drive circuit resistance-capacitance
PACS:
V432
DOI:
-
Abstract:
In order to find a simple and convenient driving circuit and realize the solenoid valve with high voltage starting and low voltage sustaining rapid responsive mode,which full use of the electrical components function that the capacitance can charge and discharge and the resistance can share voltage,the driving circuit principle that the solenoid valve coil connected with resistance and capacitance which were parallel connected was designed.Through the AMESim simulation software, the simulation model of solenoid valve and driving circuit was establish,and the influence of the resistance and capacitance on the coil current and response was analyzed.Also it was evaluated by test that the solenoid valve can start rapidly at high voltage and maitain at low voltage,which meets the rapid response requirement.In response to the contrast testing data,a parameter of the capacitance to control current peak and rate-of-climb when opening can be selected,and a parameter of the resistance to control maintenance current can be also selected.The driving circuit technology can be extended and applied in the design of fast solenoid valve,with simple structure and easy to operate.

References:

[1] 周汉申.单组元液体火箭发动机设计与研究[M].北京:中国宇航出版社,2009.
[2] HODGEK F,ALLEN K A,HEMMINGS B.Development and test of the ASAT bipropellant attitude control system(ACS)engine:AIAA1993-2587[R].USA:AIAA,1993.
[3] EDWAR D,BUSHWAY I,ELMER N.Design and development of lightweight integrated valve/injectors for the THAAD program:AIAA1994-3383[R].USA:AIAA,1994.
[4] HUFTALEN R L,PLATT A L,PARKER J M,et al.Minimum impulse thruster valve design and development:AIAA2003-4930[R].USA:AIAA,2003.
[5] 宋军,李书泽,李孝禄,等.高速电磁阀驱动电路设计及试验分析[J].汽车工程,2005,27(5):546-549.
[6] CORY J,FARRELL W.Internally vented bipropellant va lves for divert and ACS missile control:AIAA 1996-3267[R].USA:AIAA,1996.
[7] WICHMANM H.High performance miniature flightweight pilot operated valves:AIAA1995-3100[R].USA:AIAA,1995.
[8] COCHRAN M.Modular injection systems for miniature engines:AIAA1992-3253[R].USA:AIAA,1992.
[9] 宋会玲,王春民,王云岩,等.集成控制双绕组高速电磁阀的设计与仿真分析[J].火箭推进,2012,38(6):16-19.SONG H L,WANG C M,WANG Y Y,et al.Design and simulation analysis of bi-coil high-speed solenoid valve with integrated control[J].Journal of Rocket Propulsion,2012,38(6):16-19.
[10] 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.
[11] 付永领,祁晓野.LMS Imagine.Lab AMESim系统建模和仿真参考手册[M].北京:北京航空航天大学出版社,2011.
[12] 朱建国,魏学峰,孙亮.某减压阀高压冲击超调问题仿真分析与试验研究[J].火箭推进,2015,41(5):72-76.ZHU J G,WEI X F,SUN L.Simulation and experiment research on high-pressure shock overshoot phenomenon of pressure reducing valve[J].Journal of Rocket Propulsion,2015,41(5):72-76.
[13] 刘忠,刘卫萍,何谦.高速开关电磁阀动态响应建模与仿真[J].湖南师范大学自然科学学报,2009,32(3):53-57.
[14] 杨玉涛,张小栋.高速电磁阀模型建立及响应特性研究[J].测控技术,2008,27(6):86-89.
[15] 汪志刚,张敬国,陈勤学.电控柴油机用高速电磁阀的仿真研究[J].机电设备,2003,20(4):22-26.
[16] 阮晓芳,孔晓武,尹学松.高速开关阀驱动电路的仿真与试验研究[J].机电工程,2011,28(2):209-211.

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Last Update: 2019-08-31