Systematic analysis of bistable anti-symmetric composite cylindrical shells and variable stiffness composite structures in hygrothermal environment

被引:24
作者
Chai, Hao [1 ]
Li, Yang [2 ]
Zhang, Zheng [2 ]
Sun, Min [2 ]
Wu, Huaping [2 ]
Jiang, Shaofei [2 ]
机构
[1] Zhejiang Univ Technol, Zhijiang Coll, Shaoxing 312030, Peoples R China
[2] Zhejiang Univ Technol, Key Lab E&M, Minist Educ & Zhejiang Prov, Hangzhou 310014, Peoples R China
基金
中国国家自然科学基金;
关键词
Hygrothermal environment; Bistable composite; Anti-symmetric cylindrical shells; Curvature control; Variable stiffness; FREE-VIBRATION CHARACTERISTICS; THIN-WALLED BEAM; SNAP-THROUGH; SLIT TUBES; TEMPERATURE; BEHAVIOR; RESIN; MOISTURE; DRIVEN; LOAD;
D O I
10.1007/s00170-019-04887-5
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper systematically studies the effect of temperature and moisture on bistable anti-symmetric composite cylindrical shells and variable stiffness composite structures in the hygrothermal environment. Based on the classical laminate theory, together with the principle of minimum potential energy, an analytical model is developed to predict the bistable behavior of those bistable anti-symmetric composite cylindrical shells in the hygrothermal environment. Finite element simulates the change of curvature of bistable anti-symmetric composite cylindrical shells. An experiment of temperature and moisture was presented to measure the principal curvatures and twisting curvatures in the hygrothermal environment. The numerical and experimental methods are employed for predicting and verifying the theoretical results. The temperature and moisture have prominent effects on the bistable anti-symmetric composite cylindrical shells. In order to optimize shell's shape for being used in some particular situations, a novel approach that may control the bistable shell's curvatures by adjusting the temperature or moisture are presented. For the moisture variation take a long time to affect the structure curvature, the twisting curvature is eliminated by adjusting the temperature to the given value. Finally, the change of variable stiffness composite structures in the process of moisture absorption is discussed, and the load-displacement test of variable stiffness composite structures is carried out at the maximum saturation value.
引用
收藏
页码:1091 / 1107
页数:17
相关论文
共 63 条
[1]   The combined effects of load, moisture and temperature on the properties of E-glass/epoxy composites [J].
Abdel-Magid, B ;
Ziaee, S ;
Gass, K ;
Schneider, M .
COMPOSITE STRUCTURES, 2005, 71 (3-4) :320-326
[2]   Passive load alleviation aerofoil concept with variable stiffness multi-stable composites [J].
Arrieta, Andres F. ;
Kuder, Izabela K. ;
Rist, Mathias ;
Waeber, Tobias ;
Ermanni, Paolo .
COMPOSITE STRUCTURES, 2014, 116 :235-242
[3]   Variable stiffness characteristics of embeddable multi-stable composites [J].
Arrieta, Andres F. ;
Kuder, Izabela K. ;
Waeber, Tobias ;
Ermanni, Paolo .
COMPOSITES SCIENCE AND TECHNOLOGY, 2014, 97 :12-18
[4]   TEMPERATURE-DEPENDENCE OF ELASTIC-CONSTANTS OF CFRP [J].
BARKER, AJ ;
VANGERKO, H .
COMPOSITES, 1983, 14 (01) :52-56
[5]   Hygrothermal effects in composites: Influence of geometry and determination of transverse coefficient of thermal expansion [J].
Cantera, M. A. ;
Romera, J. M. ;
Adarraga, I. ;
Mujika, F. .
JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 2012, 31 (19) :1270-1281
[6]   Hygroscopic aspects of epoxy/carbon fiber composite laminates in aircraft environments [J].
Choi, HS ;
Ahn, KJ ;
Nam, JD ;
Chun, HJ .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2001, 32 (05) :709-720
[7]   A multi-stable lattice structure and its snap-through behavior among multiple states [J].
Dai, Fuhong ;
Li, Hao ;
Du, Shanyi .
COMPOSITE STRUCTURES, 2013, 97 :56-63
[8]   Thermally-induced deformation behavior of unsymmetric laminates [J].
Dano, ML ;
Hyer, MW .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 1998, 35 (17) :2101-2120
[9]  
Daton-Lovett A, 1996, UK: Patent Cooperation Treaty application, Patent No. [PCT/GB97/00839, 9700839]
[10]   A Morphing Composite Air Inlet with Multiple Stable Shapes [J].
Daynes, S. ;
Weaver, P. M. ;
Trevarthen, J. A. .
JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 2011, 22 (09) :961-973