Active control of thermal buckling and vibration for a sandwich composite laminated plate with piezoelectric fiber-reinforced composite actuator facesheets

被引:24
作者
Li, Jinqiang [1 ]
Li, Fengming [1 ]
Narita, Yoshihiro [2 ]
机构
[1] Harbin Engn Univ, Coll Aerosp & Civil Engn, Harbin 150001, Heilongjiang, Peoples R China
[2] Hokkaido Univ, Fac Engn, Sapporo, Hokkaido, Japan
基金
中国国家自然科学基金;
关键词
Active control; sandwich plates; temperature feedback; thermal buckling; buckling control; POSTBUCKLING ANALYSIS; FGM PLATES; SUPPRESSION; PANELS;
D O I
10.1177/1099636218783168
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The present paper is concerned with the active control of thermal buckling and vibration of a sandwich composite laminated plate with piezoelectric fiber-reinforced composite actuator facesheets in a thermal environment. An active temperature feedback control strategy is proposed for the thermal buckling of the composite sandwich plate. The results of numerical simulations show that the piezoelectric actuator can significantly improve the thermal buckling characteristics of the composite plates. The influence of the active thermal buckling control gain on the damping ratio and natural frequency of the structure is also investigated. From the numerical results it is observed that the active thermal buckling control with temperature feedback gain can not only enlarge the critical buckling temperature but can also reduce the resonant amplitude of the structure. Furthermore, the optimization problem is studied and it is found that the critical buckling temperature can be optimized by varying the fiber orientation in the piezoelectric fiber-reinforced composite layer. The active thermal buckling control method presented in this paper working in combination with the vibration control strategy can significantly improve the stability of the laminated composite plates. The present study will be useful for designing laminated composite structures used in the thermal environment.
引用
收藏
页码:2563 / 2581
页数:19
相关论文
共 33 条
[1]   Thermal buckling behavior of cross-ply hybrid composite laminates with inclined crack [J].
Avci, Ahmet ;
Sahin, Omer Sinan ;
Ataberk, Necati .
COMPOSITES SCIENCE AND TECHNOLOGY, 2006, 66 (15) :2965-2970
[3]   Buckling and post-buckling analysis of delaminated piezo-composite material under electro-mechanical loading [J].
Chitsaz, Nasim ;
Ovesy, Hamid R. ;
Kharazi, Mahsa .
JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 2016, 27 (13) :1780-1791
[4]   TRANSVERSE VIBRATION OF SYMMETRICALLY LAMINATED RECTANGULAR COMPOSITE PLATES [J].
CHOW, ST ;
LIEW, KM ;
LAM, KY .
COMPOSITE STRUCTURES, 1992, 20 (04) :213-226
[5]   Thermal buckling of composite plates with spatial varying fiber orientations [J].
Duran, A. V. ;
Fasanella, N. A. ;
Sundararaghavan, V. ;
Waas, A. M. .
COMPOSITE STRUCTURES, 2015, 124 :228-235
[6]   Nonlinear free and forced vibration of simply supported shear deformable laminated plates with piezoelectric actuators [J].
Huang, XL ;
Shen, HS .
INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2005, 47 (02) :187-208
[7]   Thermal buckling analysis of porous circular plate with piezoelectric actuators based on first order shear deformation theory [J].
Jabbari, M. ;
Joubaneh, E. Farzaneh ;
Mojahedin, A. .
INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2014, 83 :57-64
[8]   Thermal buckling of uniformly heated unidirectional and symmetric cross-ply laminated fiber-reinforced composite uniaxial in-plane restrained simply supported rectangular plates [J].
Jones, RM .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2005, 36 (10) :1355-1367
[9]   Thermal buckling and postbuckling analysis of a laminated composite beam with embedded SMA actuators [J].
Lee, JJ ;
Choi, S .
COMPOSITE STRUCTURES, 1999, 47 (1-4) :695-703
[10]   Vibration suppression for laminated composite plates with arbitrary boundary conditions [J].
Li, J. ;
Narita, Y. .
MECHANICS OF COMPOSITE MATERIALS, 2013, 49 (05) :519-530