Vibration Frequency Analysis of Beam-Ring Structure for Circular Deployable Truss Antenna

被引:23
作者
Wu, R. Q. [1 ]
Zhang, W. [1 ]
Behdinan, K. [2 ]
机构
[1] Beijing Univ Technol, Coll Mech Engn, Beijing Key Lab Nonlinear Vibrat & Strength Mech, Beijing 100124, Peoples R China
[2] Univ Toronto, Dept Mech & Ind Engn, Adv Res Lab Multifunct Light Weight Struct, 5 Kings Coll Rd, Toronto, ON M5S 3G8, Canada
基金
中国国家自然科学基金;
关键词
Circular deployable truss antenna; beam-ring structure; the governing equations of motion; linear frequency; BREATHING VIBRATIONS; BOUNDARY-CONDITIONS; CYLINDRICAL-SHELL; CHAOTIC DYNAMICS; GALERKIN METHOD; RESPONSES; MODEL;
D O I
10.1142/S0219455419500123
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
The circular truss antenna of the large aperture is considered to be a flexible structure which may cause vibration in space and may affect its performance. The frequency analysis of the circular truss antenna is an important problem for understanding its vibration mechanism. In this paper, we investigate the frequency characteristics of a beam-ring structure which is proposed for the first time to model the circular truss antenna in the case of the antenna expended and locked. Based on describing the displacements of the beam-ring system in detail, the kinetic energy and potential energy are calculated. The partial differential governing equations of motion and boundary conditions for the beam-ring structure are derived by Hamilton principle. From the linear parts of the governing equations of motion and the corresponding boundary conditions, the linear frequencies of the beam-ring structure are theoretically obtained. The effects of the physical parameters on the frequency characteristics of the beam-ring structure are studied, which are further verified by the numerical results. The finding phenomena of this paper are helpful for designing and controlling the beam-ring structure such as the circular truss antenna.
引用
收藏
页数:20
相关论文
共 42 条
[1]   Nonlinear nonplanar dynamics of parametrically excited cantilever beams [J].
Arafat, HN ;
Nayfeh, AH ;
Chin, CM .
NONLINEAR DYNAMICS, 1998, 15 (01) :31-61
[2]  
Balachandran B., 1991, NONLINEAR DYNAM, V2, P77, DOI DOI 10.1007/BF00053831
[3]  
Balachandran B., 1990, NONLINEAR DYNAM, V1, P36
[4]   Study of pure transverse motion in free cylinders and plates in flexural vibration by Ritz's method [J].
Bayon, A. ;
Gascon, F. ;
Medina, R. ;
Nieves, F. J. ;
Salazar, E. .
EUROPEAN JOURNAL OF MECHANICS A-SOLIDS, 2011, 30 (03) :423-431
[5]   Frequency analysis of a uniform ring perturbed by point masses and springs [J].
Behbahani, Amir H. ;
M'Closkey, Robert T. .
JOURNAL OF SOUND AND VIBRATION, 2017, 397 :204-221
[6]   Nature of stationarity of the natural frequencies at the natural modes in the Rayleigh-Ritz method [J].
Bhat, RB .
JOURNAL OF SOUND AND VIBRATION, 1997, 203 (02) :251-263
[7]   Analytical and experimental studies on nonlinear characteristics of an L-shape beam structure [J].
Cao, Dong-Xing ;
Zhang, Wei ;
Yao, Ming-Hui .
ACTA MECHANICA SINICA, 2010, 26 (06) :967-976
[8]   Rayleigh-Ritz analysis for localized buckling of a strut on a softening foundation by Hermite functions [J].
Chen, G ;
Baker, G .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2003, 40 (26) :7463-7474
[9]   Structural optimization and model fabrication of a double-ring deployable antenna truss [J].
Dai, Lu ;
Guan, Fuling ;
Guest, James K. .
ACTA ASTRONAUTICA, 2014, 94 (02) :843-851
[10]  
DASILVA MRM, 1991, APPL MECH REV, V44, pS51