Dynamic analysis of clamp band joint system subjected to axial vibration

被引:36
作者
Qin, Z. Y. [1 ]
Yan, S. Z. [1 ]
Chu, F. L. [1 ]
机构
[1] Tsinghua Univ, Dept Precis Instruments & Mechanol, Beijing 100084, Peoples R China
关键词
VEHICLE; STRESS;
D O I
10.1016/j.jsv.2010.05.012
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
Clamp band joints are commonly used for connecting circular components together in industry. Some of the systems jointed by clamp band are subjected to dynamic load. However, very little research on the dynamic characteristics for this kind of joint can be found in the literature. In this paper, a dynamic model for clamp band joint system is developed. Contact and frictional slip between the components are accommodated in this model. Nonlinear finite element analysis is conducted to identify the model parameters. Then static experiments are carried out on a scaled model of the clamp band joint to validate the joint model. Finally, the model is adopted to study the dynamic characteristics of the clamp band joint system subjected to axial harmonic excitation and the effects of the wedge angle of the clamp band joint and the preload on the response. The model proposed in this paper can represent the nonlinearity of the clamp band joint and be used conveniently to investigate the effects of the structural and loading parameters on the dynamic characteristics of this type of joint system. (C) 2010 Elsevier Ltd. All rights reserved.
引用
收藏
页码:4486 / 4500
页数:15
相关论文
共 14 条
[1]  
[Anonymous], 2000, GDED2214 NASA GODD S
[2]   Investigation of space launch vehicle catastrophic failures [J].
Chang, IS .
JOURNAL OF SPACECRAFT AND ROCKETS, 1996, 33 (02) :198-205
[3]   Estimating the energy dissipated in a bolted spacecraft at resonance [J].
Crocombe, AD ;
Wang, R ;
Richardson, G ;
Underwood, CI .
COMPUTERS & STRUCTURES, 2006, 84 (5-6) :340-350
[4]   MODELING AND ANALYSIS OF NONLINEAR SLEEVE JOINTS OF LARGE SPACE STRUCTURES [J].
FERRI, AA .
JOURNAL OF SPACECRAFT AND ROCKETS, 1988, 25 (05) :354-360
[5]  
GAUL L, 1997, ACTA MECH, V125, P160
[6]  
HAYASHI C, 1964, NONLINEAR OSCIL, P128
[7]   Effect of smoothening functions on the frequency response of an oscillator with clearance non-linearity [J].
Kim, TC ;
Rook, TE ;
Singh, R .
JOURNAL OF SOUND AND VIBRATION, 2003, 263 (03) :665-678
[8]   Dynamic model for Global Positioning System Block IIR space vehicle [J].
Lin, CS ;
Cole, TR .
JOURNAL OF SPACECRAFT AND ROCKETS, 1997, 34 (03) :354-359
[9]  
[秦朝烨 QIN Zhao-ye], 2009, [宇航学报, Journal of Chinese Society of Astronautics], V30, P2080
[10]  
ROBERT DT, 1994, AIAA ASME ASCE AHS A, V1, P320