弹箱滑移电液随动系统建模仿真与特性研究OA
Modeling,Simulation and Characteristics Study of the Electro-hydraulic Follow-up System for Ammunition Box Sliding
为减小箱式火箭炮发射过程中冲击力对发射架和弹箱的影响,提出了一种基于静液压执行器的弹箱滑移电液随动系统.介绍了弹箱滑移电液随动系统的结构组成、工作模式与工作原理,建立了弹箱滑移电液随动系统液压控制回路模型,研究了系统管道长度、管道直径、节流孔孔径等关键结构参数对随动时间、弹箱复位时间、接触冲击力等系统特性的影响规律.研究表明,节流孔孔径大小会影响弹箱与挡板之间的接触力,随着节流孔孔径的减小,接触力也会相应降低,同时随动时间会明显延长;当节流孔孔径增大到3.6 mm 时,接触力会产生 20%左右振荡,弹箱复位时间缩短.在弹箱滑移电液随动系统结构下,可根据火箭弹发射需要调节节流孔孔径以实现火箭炮发射过程随动特性调整.
To mitigate the impact of shock forces on the launch frame and ammunition box during the firing process,an electro-hydraulic servo system for ammunition box sliding,based on a hydrostatic actuator,is proposed.The system configuration,operational modes,and working principles of the electro-hydraulic follow-up system for container sliding are described.A hydraulic circuit model of the system is established,and the influences of structural parameters such as system pipeline length,pipeline diameter,and orifice diameter on performance metrics(including follow-up time,reset time,and contact impact force)are investigated.The results indicate that the orifice diameter affects the contact force between the ammunition box and the baffle.As the size of the orifice diameter decreases,the contact force reduces correspondingly,while the follow-up time increases significantly.When the orifice diameter increases to 3.6 mm,the contact force exhibits approximately 20%oscillation,and the reset time of the ammunition box decreases.Therefore,within the structure of the follow-up container sliding system,the orifice diameter can be adjusted according to the requirements of rocket launch to achieve the tailored follow-up characteristics during the launcher's operation.
雷军波;康彦群;黎寿平;宋韫峥;杨奎
中国兵器装备集团上海电控研究所,上海 200092中国兵器装备集团上海电控研究所,上海 200092中国兵器装备集团上海电控研究所,上海 200092中国兵器装备集团上海电控研究所,上海 200092中国兵器装备集团上海电控研究所,上海 200092
机械制造
随动系统弹箱滑移电液系统建模仿真
follow-up systemammunition boxes slidingelectro-hydraulic systemmodeling and simulation
《液压与气动》 2026 (4)
110-118,9
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