• 中国科技核心期刊
  • Scopus收录期刊
  • DOAJ收录期刊
  • JST收录期刊
  • Euro Pub收录期刊
WANG Hong-rui, CAO Xiao-juan, YIN Shao-ping, ZHANG Zhi-min, SHAN Zhi-xiong. Analysis on the Factors Influencing Structural Transfer Characteristic of Torpedo Vibration Test System[J]. Journal of Unmanned Undersea Systems, 2019, 27(5): 574-579. doi: 10.11993/j.issn.2096-3920.2019.05.014
Citation: WANG Hong-rui, CAO Xiao-juan, YIN Shao-ping, ZHANG Zhi-min, SHAN Zhi-xiong. Analysis on the Factors Influencing Structural Transfer Characteristic of Torpedo Vibration Test System[J]. Journal of Unmanned Undersea Systems, 2019, 27(5): 574-579. doi: 10.11993/j.issn.2096-3920.2019.05.014

Analysis on the Factors Influencing Structural Transfer Characteristic of Torpedo Vibration Test System

doi: 10.11993/j.issn.2096-3920.2019.05.014
  • Received Date: 2019-03-01
  • Rev Recd Date: 2019-04-06
  • Publish Date: 2019-10-31
  • The transfer characteristic of the torpedo vibration test system is crucial to the confidence level of vibration environment simulation. Therefore, constructing a test system that can accurately transmit vibration test conditions is the basis for conducting test and simulation of structural transfer characteristic. In this paper, based on different boundary conditions, finite element simulation analysis of transfer characteristic of system under random load excitation is carried out for the cabin vibration test system, and the factors influencing structural transfer characteristic of the test system are determined. Conclusions are drawn as follows: 1) bolt preload, clamp support spacing, and intermediate layer material’s properties are the main factors affecting the transfer characteristic of the system; 2) within a certain range, as the bolt preload increases, the transfer characteristic of the system tends to increase, but when the tightening torque is greater than 40 N·m, the transfer characteristic tends to be stable; 3) the torpedo cabin with a slenderness ratio of 2 to 4 has better system transfer characteristic when the support ratio is from 50% to 66.67%; and 4) when the intermediate layer uses a material with small thickness, large friction coefficient and relatively large damping ratio, the system can achieve higher resonance frequency and better transfer characteristic.

     

  • loading
  • [1]
    许江文. 影响振动环境试验的若干关键技术要点解析[J]. 环境试验, 2015(3): 10-13.

    Xu Jiang-wen. Analysis on Some Key Technologies of Impact Vibration Environment Test[J]. Environmental Testing, 2015(3): 10-13.
    [2]
    王涌泉, 雷平森, 冯睿. 力学环境试验技术[M]. 西安: 西北工业大学出版社, 2003.
    [3]
    郑勇斌, 林丽.弹体振动传递函数测试及其数据应用[J]. 现代防御技术, 2009, 37(4): 50-54.

    Zheng Yong-bin, Lin Li. Transfer Function Test of Missile Vibration and Data Application[J]. Modern Defence Technology, 2009, 37(4): 50-54.
    [4]
    王亚斌, 刘明杰, 谭惠民.弹引系统传递函数系统辨识[J]. 机械工程学报, 2008, 44(3): 200-204.

    Wang Ya-bin, Liu Ming-jie, Tan Hui-min. System Identification of the Bullet-fuze System Transfer Function[J]. Chinese Journal of Mechanical Engineering, 2008, 44(3): 200-204.
    [5]
    张琳, 邓长华, 谭永华, 等. 随机振动试验仿真技术研究[J]. 机械强度, 2011, 33(6): 927-931.

    Zhang Lin, Deng Chang-hua, Tan Yong-hua, et al. Research on the Simulation of Random Virbation Testing[J]. Journal of Mechanical Strength, 2011, 33(6): 927-931.
    [6]
    陈颖, 田光明, 钟继根. 典型细长体结构的两点激励振动试验设计[J]. 航天器环境工程, 2013, 30(1): 68-71.

    Chen Ying, Tian Guang-ming, Zhong Ji-gen. Dual-exciter Vibration Test Design for a Typical Slender Structure[J]. Spacecraft Environment Engineering, 2013, 30(1): 68-71.
    [7]
    马兴瑞, 于登云, 韩增尧, 等. 星箭力学环境分析与试验技术研究进展[J]. 字航学报, 2006, 27(3): 323-331.

    Ma Xing-rui, Yu Deng-yun, Han Zeng-yao, et al. Research Evolution on the Satellite-Rocket Mechanical Environment Analysis & Test Technology[J]. Journal of Astronautics, 2006, 27(3): 323-331.
    [8]
    刘青林, 陈颖, 田光明, 等. 导弹飞行振动环境地面模拟试验方法[J]. 装备环境工程, 2016, 13(5): 68-75.

    Liu Qing-lin, Chen Ying, Tian Guang-ming, et al. Laboratory Test Methods of Vibration Environment for the Flighting Missiles[J]. Equipment Environment Engineering, 2016, 13(5): 68-75.
    [9]
    苏华昌, 丁富海, 吴家驹. 战术导弹多台并激振动试验技术研究[J]. 强度与环境, 2016, 43(3): 39-46.

    Su Hua-chang, Ding Fu-hai, Wu Jia-ju. Vibration Test Technology Study of Tactical Missile with Multi-shaker Synchronization[J]. Structure & Environment Engineering, 2016, 43(3): 39-46.
    [10]
    王磊, 王飞, 王海东, 等.细长型飞行器双台随机振动试验虚拟试验技术研究[J]. 上海航天, 2014, 31(1): 56-62.

    Wang Lei, Wang Fei, Wang Hai-dong, et al. Research on Virtual Vibration Test of Dual-Exciter Random Vibration Test for Slender Aerocraft[J]. Aerospace Shanghai, 2014, 31(1): 56-62.
    [11]
    Singiresu S Rao. 机械振动[M].第5版. 北京: 清华大学出版社, 2016.
    [12]
    刘鸿文. 材料力学[M].第5版. 北京: 高等教育出版社, 2011.
    [13]
    舒歌群, 赵文龙, 梁兴雨, 等. 约束阻尼结构的振动分析及结构参数优化研究[J]. 西安交通大学学报, 2014, 48(3): 108-114.

    Shu Ge-qun, Zhao Wen-long, Liang Xing-yu, et al. Vibration Analysis and Optimization of Composite Structure with Constrained-Layer Damping Treatment[J]. Journal of Xi’an Jiaotong University, 2014, 48(3): 108-114.
    [14]
    黄微波, 李华阳, 张志超, 等. 约束阻尼结构板振动性能实验研究[J]. 科学技术与工程, 2018, 18(2): 199-203.

    Huang Wei-bo, Li Hua-yang, Zhang Zhi-chao, et al. Experimental Study on Vibration Performance of Constrained Damped Structural Plates[J]. Science Technology and Engi-neering, 2018, 18(2): 199-203.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article Views(429) PDF Downloads(302) Cited by()
    Proportional views
    Related
    Service
    Subscribe

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return