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重载负荷下的燃气作动筒内弹道推力特性研究

  • 吴宪举 ,
  • 吴豪 ,
  • 余威格 ,
  • 詹京松
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  • 台州学院航空工程学院, 浙江台州 318000

吴宪举(1980-),男,湖北襄阳人,高级工程师,硕士,研究方向:飞行器设计。

收稿日期: 2019-09-12

  网络出版日期: 2025-05-30

Study on the Internal Ballistic Thrust Characteristics of Gas Actuator under Heavy Load

  • WU Xianju ,
  • WU Hao ,
  • YU Weige ,
  • ZHAN Jingsong
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  • School of Aeronautical Engineering, Taizhou University, Zhejiang Taizhou 318000, China

Received date: 2019-09-12

  Online published: 2025-05-30

摘要

以某军工项目为研究背景,建立内弹道模型,对燃气作动筒加载一系列的负载进行推力特性的定性定量研究。该套带高压室喷管系统的燃气作动筒装置,基于高压室壅塞流动和非壅塞流动的数学模型,采用Matlab中的Simulink模块进行程序搭建,以实例进行内弹道仿真计算,得到该燃气作动筒的内弹道参数和推杆推力的数值解,并对其结果进行定性和定量分析,得到燃气作动筒推力特性的一般规律,为燃气作动筒的工程应用提供了借鉴。

本文引用格式

吴宪举 , 吴豪 , 余威格 , 詹京松 . 重载负荷下的燃气作动筒内弹道推力特性研究[J]. 弹箭与制导学报, 2020 , 40(4) : 34 -36 . DOI: 10.15892/j.cnki.djzdxb.2020.04.008

Abstract

Based on the research background of a military project, the internal ballistic model is established to study the thrust characteristics of a series of loads loaded onto the gas actuator. In this paper, a set of gas actuators with high pressure bunker nozzle system is designed. Based on the mathematical model of congestion flow and unchoked flow in high pressure bunker, the program is built by using Simulink module in MATLAB, and the internal trajectory is simulated with an example, the numerical solution of the interior ballistic parameter and push rod thrust of the gas actuator cylinder is obtained. The results are qualitatively and quantitatively analyzed, and the general rule of thrust characteristics of the gas actuator cylinder is obtained. It provides a reference to the engineering application of gas actuators.

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[1]
徐方舟, 张斌, 宋春雨. 基于油液阻尼的气动作动筒方案[J]. 科技创新与应用, 2018(20):125-126.

[2]
PEI W W, CHEN H P, HONG W U, et al. Study and analysis of a landing gear altuating cylinder inner-lock[J]. International Journal of Plant Engineering and Management, 2011(2):97-103.

[3]
马玉勇, 吴建军, 屠小昌, 等. 燃气作动筒弹翼展开负载模拟装置研究[J]. 航天制造技术, 2008(2):30-33.

[4]
杨敏鹏, 杨树彬, 屠小昌, 等. 弹翼展开燃气作动筒内弹道预估技术[J]. 火工品, 2016(2):29-32.

[5]
杨侃, 雷龙. 燃气作动筒驱动的弹翼旋转展开过程动力学分析计算[J]. 装备制造技术, 2016(8): 23-26.

[6]
姚小宁, 屠小昌, 黄运銮, 等. 弹翼展开机构中燃气作动筒的运动模型[J]. 弹箭与制导学报, 2012, 32(5):48-50.

DOI

[7]
谢建. 导弹发射技术[M]. 西安: 西北工业大学出版社, 2015:37-58.

[8]
谭大成. 弹射内弹道学[M]. 北京: 北京理工大学出版社, 2015:55-82.

[9]
张石玉, 唐金兰, 任华, 等. 燃气作动筒式折叠弹翼展开过程分析[J]. 固体火箭技术, 2010, 33(5):481-485.

[10]
HENRY J, SCHWARTZ D R, SOUKUP M A, et al. Design, construction,and testing of a folding-wing,tube-launced micro air vehicle:AIAA 2005-1451[R]. 2005.

[11]
李海军, 游坤. 航空弹药冷气弹射动力学特性研究[J]. 火力与指挥控制, 2018, 43(1): 113-116.

[12]
税朗泉, 郭姣姣. 某型三级作动筒气动弹射系统仿真研究[J]. 机械设计与制造, 2016(3):10-13.

[13]
游坤, 李海军. 单级作动筒冷气弹射装置动力学特性的数值计算[J]. 中北大学学报(自然科学版), 2017, 38(5):568-573.

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