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活塞式微作动器结构设计与仿真
引用本文:严楠,王刚,耿万钧,张良.活塞式微作动器结构设计与仿真[J].含能材料,2014,22(5):688-692.
作者姓名:严楠  王刚  耿万钧  张良
作者单位:1. 北京理工大学机电学院爆炸科学与技术国家重点实验 室,北京,100081
2. 北京理工大学机电学院爆炸科学与技术国家重点实验 室,北京 100081; 中国航天科工集团 8511研究 所,江苏南京210007
3. 西安近代化学研究所,陕西 西安,710065
基金项目:国家自然科学基金资助(11172042)
摘    要:为满足小口径弹药引信安全系统用微作动器结构和性能要求,利用ANSYS/LS-DYNA动力学有限元软件模拟分析了活塞式作动器的结构,研究了结构形式和尺寸参数对其性能的影响,并设计改进一种活塞式作功器,测试了不同结构参数的止推力和止退力,得到了不同装药量下活塞式微作动器的输出推力与推程的关系曲线和表达式。结果表明,台阶高度为0.03 mm时,止推力为142 N,止退力为38.5 N;推程为2.0 mm时,最小推力不小于20 N。试验结果与模拟结果比较吻合,偏差在15%以内,说明该数值方法可用于微作动器作用过程研究。

关 键 词:火工品  火工装置  作动器  数值模拟  推力
收稿时间:2013/8/27 0:00:00
修稿时间:2014/2/25 0:00:00

Structural Design and Numerical Simulation on the Piston Micro-actuator
YAN Nan,WANG Gang,GENG Wan-jun and ZHANG Liang.Structural Design and Numerical Simulation on the Piston Micro-actuator[J].Chinese Journal of Energetic Materials,2014,22(5):688-692.
Authors:YAN Nan  WANG Gang  GENG Wan-jun and ZHANG Liang
Abstract:In order to meet the piston micro-actuator used in the small-caliber Ammunition Fuze Safety System structural and functional requirements, ANSYS/LS-DYNA finite element software was applied to analyze the structure design of the piston micro-actuator, and the structure and size parameters which affect its performance were determined. The anti-thrust force and setback force of different structural size parameters piston micro-actuators was obtained through the piston micro-actuator performance experimental test. With step height of 0.03 mm, anti-thrust force is 142 N, and the setback force was 38.5 N. The fitting curve and expression of the piston micro-actuator and thrust distance were got under different charges. With thrust distance of 2.0 mm, the minimum thrust is greater than 20 N. Results show that the deviation of the numerical simulation results with experiment values with 15%, indicating that the numerical simulation method can be applied to research micro-actuator function process.
Keywords:pyrotechnics  pyrotechnics device  actuator  numerical simulation  thrust
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