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燃气射流载荷和风载荷对适配器分离影响研究

  • 殷鑫 ,
  • 宋双婧 ,
  • 于骐瑞 ,
  • 王新星 ,
  • 赵鑫 ,
  • 李军
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  • 1 南京理工大学机械工程学院, 南京 210094
    2 湖北江山重工有限责任公司, 湖北襄阳 441000
    3 中国兵器工业导航与控制技术研究所, 北京 100089

殷鑫(1993-),男,山东烟台人,硕士研究生,研究方向:火箭发射系统动力学分析与液压系统分析。

收稿日期: 2017-04-25

  网络出版日期: 2025-05-28

Study on the Influence of Gas Jet Load and Wind Load on Adapter Separation

  • YIN Xin ,
  • SONG Shuangjing ,
  • YU Qirui ,
  • WANG Xinxing ,
  • ZHAO Xin ,
  • LI Jun
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  • 1 School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing 210094, China
    2 Hubei Jiangshan Heavy Industries Co. Ltd, Hubei Xiangyang 441000, China
    3 Navigation and Control Technology Research Institute of China Ordnance Industries, Beijing 100089, China

Received date: 2017-04-25

  Online published: 2025-05-28

摘要

火箭炮利用适配器实现同时离轨发射是一种新技术。为了研究适配器落点范围及分离过程中适配器是否与火箭弹发生二次碰撞,依据真实燃气射流速度衰减规律,提出了一种简化燃气射流加载方法,并综合考虑不同衰减规律及不同风速、风向情况下各载荷对适配器运动规律的影响,运用ADAMS软件进行分析。结果表明,适配器能与火箭弹安全可靠的分离,不会发生二次碰撞,但在零度方向角发射时适配器会落在炮车上,存在安全隐患。

本文引用格式

殷鑫 , 宋双婧 , 于骐瑞 , 王新星 , 赵鑫 , 李军 . 燃气射流载荷和风载荷对适配器分离影响研究[J]. 弹箭与制导学报, 2018 , 38(2) : 7 -10,15 . DOI: 10.15892/j.cnki.djzdxb.2018.02.002

Abstract

Using adapter to make rocket artillery simultaneously deorbit when it is launched is a new technology. In order to analyze the landing range of the adapter and whether the second time collision between adapter and rocket would occur in the process of separation, according to the law of real gas jet velocity attenuation, this paper presents a simplified method for gas jet loading, the effects of each load under the conditions of different attenuation laws, different wind speeds and wind directions which influenced the movement of the adapter were considered, then we used ADAMS to analyze. The analysis results show that the adapter can be safely and reliably separated from the rocket, and the second time collision will not occur, but the adapter falls on the artillery truck under the zero launching angles, there are some security risks.

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参考文献

[1]
赵华, 王敏杰, 杨为,等. 箱式发射导弹适配器[J]. 战术导弹技术, 2007. 27(4): 42-50.
[2]
RUDD G E, MILER J F, SIMON J T. Shock Absorbing Missile Launch Pads: US 4734329 P. 1988-08-16.
[3]
秦丽, 陈国光. 有弹性适配器的火箭弹发射动力学研究[J]. 弹箭与制导学报, 1997, 17(2): 12-18.
[4]
董贵. 适配器强度有限元分析[J]. 战术导弹技术, 1995, 15(2): 61-64.
[5]
施俊凯. 垂直发射适配器分离过程虚拟实验研究[D]. 哈尔滨: 哈尔滨工业大学, 2014.
[6]
高强, 白静, 张平,等. 分离力作用点位置和风速大小对适配器分离影响研究[J]. 导弹与航天运载技术, 2013, 35(3): 23-26.
[7]
黄聪. 适配器结构外形和外界风载荷对适配器分离落点分布的影响[D]. 北京: 北京理工大学, 2016.
[8]
陈立平, 张云清, 任卫群,等. 机械系统动力学分析及ADAMS 应用教程[M]. 北京: 清华大学出版社, 2005: 33-50.
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