Design and Simulation Analysis of Rocket Sled Vibration Reduction

被引:0
|
作者
Wang, Xinchao [1 ]
Wang, Ke [1 ]
Yu, Yuanyuan [2 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Inst Vibrat Engn, Nanjing, Jiangsu, Peoples R China
[2] Aerosp Lifesaving Equipment Co Ltd AVIC, Xiangyang, Hubei, Peoples R China
关键词
rocket sled; metal rubber; damper; FEM;
D O I
10.1109/icmae.2019.8880968
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Metal rubber (MR) devices, also called wire mesh dampers, are a new type of material made by pressing coiled thin metal wires into various shapes, and a damper is a nonlinear damping device with dry friction hysteresis, which can reduce the vibration in a wide frequency band. In this paper, according to the structural characteristics of the rocket sled, an improved scheme of the rocket sled with vibration reduction function is designed. Based on studying the mechanical characteristics and parameter model of the metal rubber devices, the dynamic finite element model of rocket sled structure was established. Through simulation analysis, the static and dynamic characteristics of rocket sled structure are studied, and the dynamic response under spectral excitation is estimated emphatically. The response changes before and after the vibration reduction measures are compared, and the effectiveness of the vibration reduction design scheme is preliminarily proved, which provides conditions for the implementation of the rocket sled's test.
引用
收藏
页码:459 / 463
页数:5
相关论文
共 50 条
  • [41] Vibration reduction analysis and design of friction ring damper in blisk
    Wen W.
    Qi W.
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2020, 35 (04): : 777 - 782
  • [42] Design and analysis of rocket nozzle
    Harikrishnan, R.
    Lokavarapu, Bhaskara Rao
    MATERIALS TODAY-PROCEEDINGS, 2021, 38 : 3365 - 3371
  • [43] Aerodynamic design optimization of a hypersonic rocket sled deflector using the free-form deformation technique
    Dang, Tianjiao
    Li, Bingfei
    Hu, Dike
    Sun, Yachuan
    Liu, Zhen
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2021, 235 (15) : 2240 - 2248
  • [44] Dynamic coupling analysis of rocket propelled sled using multibody-finite element method
    Zhang, J. (zhangjianh@chd.edu.cn), 1600, Transport and Telecommunication Institute, Lomonosova street 1, Riga, LV-1019, Latvia (18):
  • [45] Analysis of Magneto-inductive System for Rocket Sled Velocity Measurement Beyond Mach 1.5
    Khosla, P. K.
    Khanna, Rajesh
    Sood, Sanjay P.
    DEFENCE SCIENCE JOURNAL, 2014, 64 (02) : 143 - 151
  • [46] Vibration Isolation Design for the Micro-X Rocket Payload
    Danowski, M. E.
    Heine, S. N. T.
    Figueroa-Feliciano, E.
    Goldfinger, D.
    Wikus, P.
    McCammon, D.
    Oakley, P.
    JOURNAL OF LOW TEMPERATURE PHYSICS, 2016, 184 (3-4) : 597 - 603
  • [47] Evaluation of Thermomechanical Damage of a Slipper and Rail in a Rocket Sled System
    Yeo, Chang-Dong
    Palazotto, Anthony
    Song, Jingan
    Buentello, Rodolfo
    JOURNAL OF TESTING AND EVALUATION, 2016, 44 (04) : 1443 - 1453
  • [48] Adaptive notch filter design for bending vibration of a sounding rocket
    Choi, HD
    Kim, J
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2001, 215 (G1) : 13 - 23
  • [49] Design of vibration control of launcher for Multiple launch rocket System
    Zhan, Zhi-Huan
    Rui, Xiao-Ting
    Rong, Bao
    Yang, Fu-Feng
    Wang, Guo-Ping
    Zhendong Gongcheng Xuebao/Journal of Vibration Engineering, 2011, 24 (03): : 327 - 332
  • [50] Vibration Isolation Design for the Micro-X Rocket Payload
    Heine, S. N. T.
    Figueroa-Feliciano, E.
    Rutherford, J. M.
    Wikus, P.
    Oakley, P.
    Porter, F. S.
    McCammon, D.
    JOURNAL OF LOW TEMPERATURE PHYSICS, 2014, 176 (5-6) : 1082 - 1088