[1]帅 超,廖贵超,张阳新,等.高压空气抛射角反射器过程内弹道研究[J].南京理工大学学报(自然科学版),2017,41(02):152.[doi:10.14177/j.cnki.32-1397n.2017.41.02.003]
 Shuai Chao,Liao Guichao,Zhang Yangxin,et al.Interior ballistic process for high-pressure air oflaunching corner reflector[J].Journal of Nanjing University of Science and Technology,2017,41(02):152.[doi:10.14177/j.cnki.32-1397n.2017.41.02.003]
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高压空气抛射角反射器过程内弹道研究()
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《南京理工大学学报》(自然科学版)[ISSN:1005-9830/CN:32-1397/N]

卷:
41卷
期数:
2017年02期
页码:
152
栏目:
出版日期:
2017-04-30

文章信息/Info

Title:
Interior ballistic process for high-pressure air oflaunching corner reflector
文章编号:
1005-9830(2017)02-0152-07
作者:
帅 超廖贵超张阳新董士崔文 海郭盛雨
中船重工第七一〇研究所,湖北 宜昌 443000
Author(s):
Shuai Chao1Liao GuichaoZhang YangxinDong ShicuiWen HaiGuo Shengyu
Yichang Testing Technique Research Institue,Yichang 443000,China
关键词:
舰船 角反射器 高压空气 抛射 内弹道
Keywords:
ships corner reflectors high-pressure air launch interior ballistic
分类号:
TJ716.7
DOI:
10.14177/j.cnki.32-1397n.2017.41.02.003
摘要:
充气式角反射器是舰船重要的雷达干扰和诱饵器材,将其从舰船上快速抛出是应用中至关重要的一步。该文搭建了充气式角反射器高压空气抛射试验平台,测试了角反射器的抛射效果,并建立了气瓶中高压空气喷射过程与抛射筒内角反射器运动过程的联合数学模型。利用测试结果验证了模型的合理性,分析了各相关因素对抛射过程内弹道的影响。结果表明,在计算范围内,增大气瓶体积、填充压力和气瓶出口直径会缩短抛射时间,提高抛射出口速度; 适当增加抛射筒的初始自由容积对抛射过程有利; 摩擦系数和预紧力变化对内弹道影响不明显; 角反射器质量增加会明显提高后坐力,但对抛射时间和出口速度影响较小。
Abstract:
The inflatable corner reflector is an important ship equipment for radar jamming and decoying,and its launching from the ship is the first step for usage.The experimental apparatus of the launching inflatable corner reflector is set up in this paper,the launching performance of the inflatable corner reflector is tested,and the combined models of the air flow from gas bottles and the interior ballistic process of the inflatable corner reflector are obtained.The suitability of the models are verified using the experimental data,and then the influences of several factors on the interior ballistic process characteristics are studied comprehensively.The results show that,with the increase of the volume,the pressure and the exit diameter of the gas bottles,the launch time is shortened; the proper increase of the initial free volume of the tube is benefit for launching; the friction coefficient and the pretightening force have little effect on the interior ballistic process; the increase of the corner reflector mass significantly increases the recoil but has little effects on the launch time and the outlet velocity.

参考文献/References:

[1] 赵国庆.雷达对抗原理[M].西安:西安电子科技大学出版社,1999.
[2]孙建中.舰载武器[M].北京:航空工业出版社,2010.
[3]韩朝,赵国志.动力型微型角反射器研究[J].南京理工大学学报,2006,30(3):269-272.
Han Chao,Zhao Guozhi.Energetic mini corner reflector[J].Journal of Nanjing University of Science and Technology,2006,30(3):269-272.
[4]柴刚,陆益敏,陈骁明.角反射器在海军中的战术使用[J].舰船电子对抗,2006,29(5):11-14.
Chai Gang,Lu Yimin,Chen Xiaoming.Tactical usage of corner reflector in navy[J].Shipboard Electronic Countermeasure,2006,29(5):11-14.
[5]祝寄徐,裴志斌,屈绍波,等.一种旋转型的角反射器的设计[J].现代电子技术,2013,36(11):1-4.Zhu Jixu,Pei Zhibin,Qu Shaobo,et al.Design of rotary-type corner reflector[J].Modern Electronics Technique,2013,36(11):1-4.
[6]李海林,刘国栋,柴华,等.某新型角反射器快速展开设计[J].四川兵工学报,2009,30(4):96-98.
Li Hailin,liu Guodong,Chai Hua,et al.The Rapid spread of a new corner reflector[J].Journal of Sichuan Ordnance,2009,30(4):96-98.
[7]陶如意,孙继兵,黄明,等.高低压室平衡炮内弹道数值模拟及试验研究[J].南京理工大学学报,2006,30(4):478-485.
Tao Ruyi,Sun Jibing,Huang Ming,et al.Interior ballistics numerical simulation and experiment on balance gun with low and high pressure chamber[J].Journal of Nanjing University of Science and Technology,2006,30(4):478-485.
[8]王珊珊,王浩,阮文俊,等.单兵火箭平衡发射系统内弹道数值模拟[J].南京理工大学学报,2011,35(3):343-346.
Wang Shanshan,Wang Hao,Ruan Wenjun,et al.Numerical simulation on interior ballistic of individual rocket balance launching system[J].Journal of Nanjing University of Science and Technology,2011,35(3):343-346.
[9]陶如意,叶涛,李鹏,等.小型物体冷气发射系统内弹道过程分析[J].弹道学报,2012,24(4):82-85.
Tao Ruyi,Ye Tao,Li Peng,et al.Interior ballistic process for cool-gas launch system of minitype object[J].Journal of Ballistics,2012,24(4):82-85.
[10]赵俊利,高跃飞.气体炮实用内弹道技术研究[J].太原理工大学学报,2003,34(3):288-290.
Zhao Junli,Gao Yuefei.Study on the interior ballistics of the gas gun[J].Journal of Taiyuan University of Technology,2003,34(3):288-290.
[11]赵俊利,曹锋.气体炮实用内弹道方程及应用[J].火炮发射与控制学报,2003(3):48-51.
Zhao Junli,Cao Feng.Practical interior ballistic equation of the gas-gun and its application[J].Gun Launch & Control Journal,2003(3):48-51.
[12]赵希欣,高元楼.一种气体炮的建模与分析[J].液压气动与密封,2012,32(10):43-44.
Zhao Xixin,Gao Yuanlou.Modeling and analysis of a gas gun[J].Hydraulics Pneumatics & Seals,2012,32(10):43-44.
[13]鲍鹏,岳建伟.流体力学[M].郑州:黄河水利出版社,2006.
[14]沈维道,蒋智敏,童钧耕.工程热力学[M].北京:高等教育出版社,2000.

相似文献/References:

[1]韩 朝.动力型微型角反射器研究[J].南京理工大学学报(自然科学版),2006,(03):269.
 HAN Chao,ZHAO Guo-zhi.Energetic Mini Corner Reflector[J].Journal of Nanjing University of Science and Technology,2006,(02):269.

备注/Memo

备注/Memo:
收稿日期:2016-10-31 修回日期:2017-03-15
作者简介:帅超(1988-),男,博士,工程师,主要研究方向:舰载舷外电子对抗技术,E-mail:shuaichao710@163.com。
引文格式:帅超,廖贵超,张阳新,等.高压空气抛射角反射器过程内弹道研究[J].南京理工大学学报,2017,41(2):152-158.
投稿网址:http://zrxuebao.njust.edu.cn
更新日期/Last Update: 2017-04-30