爆炸螺栓预紧力对冲击响应影响分析

黄含军,王军评,毛勇建,岳晓红,吕 剑

振动与冲击 ›› 2015, Vol. 34 ›› Issue (16) : 166-169.

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振动与冲击 ›› 2015, Vol. 34 ›› Issue (16) : 166-169.
论文

爆炸螺栓预紧力对冲击响应影响分析

  • 黄含军,王军评,毛勇建,岳晓红,吕  剑
作者信息 +

Influence analysis of pretightening force of explosive bolt on impulse response

  • HUANG Han-jun,WANG Jun-ping,MAO Yong-jian,YUE Xiao-hong,Lü Jian
Author information +
文章历史 +

摘要

爆炸分离冲击环境地面模拟试验中一般通过悬挂试验实现。试验中连接两分离部件爆炸螺栓预紧力可能会对分离冲击响应产生影响。爆炸螺栓预紧力由螺栓安装拧紧力矩与分离下件重量产生,通过分析该力矩及该重量变化研究预紧力对响应影响。通过数值模拟、试验研究,分别在时、频域对响应影响进行分析。结果表明,爆炸螺栓安装力矩及分离下件重量在一定范围内的变化对中远场冲击响应影响较小。

Abstract

The pyroshock simulation test on the ground is achieved through a hanging test. Two separation parts are connected by explosive bolts. The pretightening force of explosive bolts may have influence on impulse response during a pyroshock event.Considering the pretightening force is determined by the tightening torque and the weight of the lower separation part,the importance of these two factors is investigated in this research by applying a FE numerical simulation and a hanging test. Different tightening torque and separation part weight are considered. The experiment results are analyzed both in time and frequency domain. Both the simulation and experiment results indicate that the influence of thoses two factors is limited at mid-field and far-field from the explosive bolts.

关键词

爆炸螺栓 / 预紧力 / 爆炸分离冲击 / 冲击响应

Key words

explosive bolt / pretightening force / pyroshock / impulse response

引用本文

导出引用
黄含军,王军评,毛勇建,岳晓红,吕 剑. 爆炸螺栓预紧力对冲击响应影响分析[J]. 振动与冲击, 2015, 34(16): 166-169
HUANG Han-jun,WANG Jun-ping,MAO Yong-jian,YUE Xiao-hong,Lü Jian . Influence analysis of pretightening force of explosive bolt on impulse response[J]. Journal of Vibration and Shock, 2015, 34(16): 166-169

参考文献

[1] 张小达,夏益霖.爆炸分离冲击试验方法标准研究[J].航天标准化,2002(6):1-5.
   ZHANG Xiao-da,XIA Yi-lin. [J].Aerospace Standardization,2002(6):1-5.
[2] 张建华. 航天产品的爆炸冲击环境技术综述[J].导弹与航天运载技术,2005(3):30-36
    ZHANG Jian-hua. Pyroshock environment of missiles and launch vehicles[J]. Missiles and space vehicles, 2005(3): 30-36.
[3] NASA technical standard, Pyroshock test criteria[S]. NASA- STD-7003.NASA, 1999.
[4] Department of defense test method standard. Environmental engineering considerations and laboratory tests [S]. MIL- STD-810F. Department of Defense, USA, 2000: 517.1- 517.24.
[5] Moening C J. Views of the world pyrotechnic shock[J]. S&V Bul, 1986,56(3): 3-7.
[6] GJB150.27-2009,爆炸分离冲击试验[S].
[7] 韩晓健,焦安超,王睿.包带低冲击装置冲击试验及数据分析[J].航天器环境工程,2007,24(5):318-321.
    HAN Xiao-jian,JIAO An-chao,WANG Rui. Shock tests for low shock device of wrapping band and related data processing[J].Abstracts of the presentissue, 2007,24(5): 318- 321.
[8] 王军评,毛勇建,黄含军.点式火工分离装置冲击载荷作用机制的数值模拟研究[J].振动与冲击,2013,32(2):9-13.
    WANG Jun-ping,MAO Yong-jian,HUANG Han-jun. Numerical simulation for impulsively loading mechanism of a point pyrotechnic separation device[J].Journal of Vibration and Shock, ,2013,32(2):9-13.
[9] 金恂叔. 航天器爆炸冲击环境及其模拟试验技术[J].环境技术,1999(3):1-12.
    JIN Xun-shu.The spacecraft pyroshock environment and its simulation test techniques[J].Environmental Technology, 1999(3):1-12.
[10] 潘瑞琳,汪裕炳.空间系统爆炸分离冲击资料 第Ⅰ卷[J].强度与环境,1975(2):

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