基于Modelica的安全保险机构驱动装置系统仿真研究

武伟; 陈芷怡; 吕志超; 朱睿; 温雄飞

doi:10.15892/j.cnki.djzdxb.2025.06.005

弹箭与制导学报 >

2025 , Vol. 45 >Issue 6: 1002 - 1008

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2025.06.005

学术文章

基于Modelica的安全保险机构驱动装置系统仿真研究

武伟 ,
陈芷怡 ,
吕志超 ,
朱睿 ,
温雄飞

展开

上海航天动力技术研究所,上海 201109

武伟(1997—),男,助理工程师,硕士研究生。E-mail:2502159469@qq.com。

收稿日期: 2024-08-12

网络出版日期: 2026-01-24

收起

Simulation Study on the Driving Device System of Safety Igniter Based on Modelica

WU Wei ,
CHEN Zhiyi ,
LV Zhichao ,
ZHU Rui ,
WEN Xiongfei

Expand

Shanghai Space Propulsion Technology Research Institute,Shanghai,201109,China

Received date: 2024-08-12

Online published: 2026-01-24

Fold

摘要

本文基于多领域物理统一建模语言Modelica,通过研究固体火箭发动机安全保险机构驱动装置的工作原理,建立了包含伺服电机、齿轮传动机构、蜗轮蜗杆传动机构等组件的驱动装置系统仿真模型,并对模型进行了校核。以某型号使用的安全保险机构驱动装置为研究对象,应用建立的系统仿真模型计算了不同工况下驱动装置的转换时间、最大电流、平稳电流等参数,并与试验数据进行比较。结果表明,相同负载下,随着电压的增加,电机转速和蜗轮转速逐渐增大,转换时间减小。电机平稳电流、最大电流的仿真误差最大为0.7%和4.2%,转换时间的仿真误差范围为3.8%~8.7%,计算结果与试验结果吻合较好,模型能够正确地模拟驱动装置的运行规律。

关键词： 固体火箭发动机; 安全保险机构驱动装置; 系统仿真; 转换时间; Modelica

本文引用格式

武伟 , 陈芷怡 , 吕志超 , 朱睿 , 温雄飞 . 基于Modelica的安全保险机构驱动装置系统仿真研究[J]. 弹箭与制导学报, 2025 , 45(6) : 1002 -1008 . DOI: 10.15892/j.cnki.djzdxb.2025.06.005

Abstract

This paper is based on the multi-domain physical unified modeling language Modelica and focuses on studying the working principle of the drive device for the safety insurance agency of a solid rocket engine.Through this research,a simulation model of the drive device system has been established,which includes components such as servo motors,gear transmission mechanisms,worm gear transmission mechanisms,and others.Additionally,the model has been rigorously verified to ensure its accuracy.Taking the safety insurance agency drive device used in a specific model as the research object,the established system simulation model was applied to calculate parameters such as the conversion time,maximum current,and stable current of the drive device under different working conditions.These calculated parameters were then compared with experimental data to validate the model's effectiveness.The results indicate that under the same load,as the voltage increases,the motor speed and worm gear speed gradually increase,while the conversion time decreases.The maximum simulation errors for the steady current and maximum current of the motor are 0.7% and 4.2%,respectively.The simulation error range for the conversion time is 3.8%~8.7%.This research provides valuable insights into the design and performance evaluation of drive devices for safe igniters in solid rocket engines.By utilizing the established simulation model,engineers can effectively predict and analyze the behavior of the drive device under various conditions,thereby facilitating the optimization and improvement of its design.

Key words： Solid rocket motor; safety insurance agency drive device; system simulation; conversion time; Modelica

[an error occurred while processing this directive]

参考文献

原文顺序 | 文献年度倒序 | 文中引用次数倒序

[1]	姚洪志, 赵团, 纪向飞, 等. 电火工品电磁响应表征技术研究进展[J]. 火工品, 2023,(3):32-37. YAO H Z, ZHAO T, JI X F, et al. Research progress of electromagnetic response characterization technology for electro-explosive devices[J]. Initiators&Pyrotechnics, 2023,(3):32-37.

[2]	李金明, 安振涛, 罗兴柏, 等. 射频对电火工品的影响及防护措施[J]. 爆破器材, 2004,(5):17-19. LI J M, AN Z T, LUO X B, et al. The Effect of Radio Frequency to EED and Its Protection Measure[J]. Explosive Materials, 2004,(5):17-19.

[3]	邢永明, 康补晓, 朱红, 等. 固体发动机保险机构在高温高压下的实验研究[J]. 力学学报, 2000, 32(2):239-244. DOI XIN Y M, KANG B X, ZHU H, et al. An experimental analysis of thermal strain on solid motor safe device[J]. Acta Mechanica Sinica, 2000, 32(2):239-244.

[4]

张宸赫, 张蕊, 付东晓. 温湿度应力对火工品金属桥带温度场影响的仿真与试验研究[J]. 装备环境工程, 2022,(2):20-26.

ZHANG

C H

, ZHANG

, FU

D X

. Simulation and experimental research on the effect of temperature and humidity stress on temperature field of metal bridge belt of pyrotechnic product[J]. Equipment Environmental Engineering, 2022,(2):20-26.

[5]	丁跃伟, 丁茂元, 赵伶俐, 等. 半导体桥火工品静电响应特性研究[J]. 火工品, 2023,(4):19-23. DING Y W, DING M Y, ZHAO L L, et al. Research on electrostatic response characteristics of semiconductor bridge detonator[J]. Initiators & Pyrotechnics, 2023,(4):19-23.

[6]	魏光辉, 刘尚合, 徐义根. 静电放电对电点火管安全性的影响[J]. 火工品, 1996,(4):16-18. WEI G H, LIU S H, XU Y G. Effect of ESD on the safety of electroexplosive initiators[J]. Initiators & Pyrotechnics, 1996,(4):16-18.

[7]	于晓静. 关于钝感火工品中新技术、新含能材料研究[J]. 化工管理, 2018,(8):81. YU X J. Research on new technology and energetic material in insensitive pyrotechnic devices[J]. Chemical Enterprise Management, 2018,(8):81.

[8]	张超. 一种非电传爆安全点火装置研究[D]. 长沙: 国防科技大学, 2013. ZHANG C. A non electric detonation safety ignition device[D]. Changsha: National University of Defense Technology, 2013.

[9]	周章添. 一种高性能机电组合式触发引信[J]. 制导与引信, 2003,(1):8-10. ZHOU Z T. An Electromechanical Compound Contact Fuse of High-capacity[J]. GUIDANCE & FUZE, 2003,(1):8-10.

[10]	孙晓波, 曹旭平, 李世义, 等. 引信电子安全系统的发展[J]. 探测与控制学报, 2003,(2):46-49. SUN X B, CAO X P, LI S Y, et al. Development of the Electronic Safety and Arming Device[J]. Journal of Detection &Control, 2003,(2):46-49.

[11]	赵亚芹, 马存立, 肖承翩. 固体火箭发动机安全保险装置设计综述[J]. 图书情报导刊, 2009,(19):129-131. ZHAO Y Q, MA C L, XIAO C P. Review of designing the safe-and-arm device for solid rocket motor[J]. Sci-tech Information Development & Economy, 2009,(19):129-131.

[12]	华琦, 赵亮, 叶淑琴, 等. 一种带有安全保险机构的点火装置设计[J]. 火工品, 2013,(6):1-4. HUA Q, ZHAO L, YE S Q, et al. Design on a ignition device with safety & arm mechanism[J]. Initiators & Pyrotechnics, 2013,(6):1-4.

[13]	何锋彦, 王蕾, 杨正才, 等. 一种新型安全点火装置[J]. 火工品, 2019,(1):5-8. HE F Y, WANG L, YANG Z C, et al. A new type of safe ignition device[J]. Initiators & Pyrotechnics, 2019,(1):5-8.

[14]	赵建军, 丁建完, 周凡利, 等. Modelica语言及其多领域统一建模与仿真机理[J]. 系统仿真学报, 2006, 18(z2):570-573. ZHAO J J, DING J W, ZHOU F L, et al. Modelica and its mechanism of multi-domain unified modeling and simulation[J]. Journal of System Simulations, 2006, 18(z2):570-573.

[15]	WALL J. Modelling of Components for Conventional Car and Hybrid Electric Vehicle in Modelica[D]. Linköping: Linköping University, 2004.

[16]	William R.Binder, Christiaan J. J.Paredis, Humberto E. Garcia. Hybrid energy system modeling in Modelica[C]//Proceedings of the 10th International Modelica Conference. Lund:INL,2014:979-988.

[17]	陈琼忠, 孟光, 莫雨峰, 等. 开关磁阻电机的非线性解析模型及其在航空系统仿真中的应用[J]. 上海交通大学学报, 2008, 42(12):2041-2046. CHEN Q Z, MENG G, MO Y F, et al. An analytical nonlinear model of SRM and its application in the system-level simulation of aircraft power system[J]. Journal of Shanghai Jiaotong University, 2008, 42(12):2041-2046.

[18]	张旭阳, 张鲲羽, 刘忠诚, 等. 基于Modelica/Mworks的船用射汽抽气器图形化建模与仿真[J]. 机电设备, 2022, 39(5):30-36. ZHANG X Y, ZHANG K Y, LIU Z C, et al. Graphic modeling and simulation of marine steam jet air ejector based on modelica/Mworks[J]. Mechanical and Electrical Equipment, 2022, 39(5):30-36.

[19]	李运洲. 基于Modelica的无刷直流电机设计与仿真[D]. 武汉: 华中科技大学, 2017. LI Y Z. Design and simulation of brushless DC motor based on modelica[D]. Wuhan: Huazhong University of Science and Technology, 2017.

[20]	刘翠玲, 孙晓荣, 于家斌, 等. 电机与拖动[M]. 北京: 北京理工大学出版社, 2016. LIU C L, SUN X R, YU J B, et al. Motor and Drive[M]. Beijing: Beijing Institute of Technology Press, 2016.

Options

文章导航