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Journal of ZheJiang University (Engineering Science)  2020, Vol. 54 Issue (7): 1341-1346    DOI: 10.3785/j.issn.1008-973X.2020.07.012
    
Design and performance analysis of variable stiffness multi-stable composite laminate structure
Zheng ZHANG1(),Hao ZHANG1,Hao CHAI2,Hua-ping WU1,Shao-fei JIANG1
1. College of Mechanical Engineering, Zhejiang University of Technology, Hangzhou 310014, China
2. College of Mechanical Engineering, Zhijiang College of Zhejiang University of Technology, Shaoxing 312030, China
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Abstract  

Two variable stiffness multi-stable composite laminate structures were designed by analyzing the relationship between the theoretical model of regional fiber angle change and the stiffness change of composite structures. The variable stiffness multi-stable composite structure was modeled, and the stable configuration of the multi-stable composite structures with variable stiffness was obtained by solving different equilibrium equations with Matlab. The experimental specimens were prepared to measure the mechanical properties with different stable transformation. The cooling process were simulated by finite element software Abaqus, and the numerical results of equilibrium stable configuration were obtained. The stable configuration, the stable transformation maximum load and the load-displacement curvatures were analyzed by combining with the theoretical, numerical and experimental results.



Key wordsvariable stiffness      multi-stable composite structure      classical laminate theory      finite element analysis     
Received: 09 March 2019      Published: 05 July 2020
CLC:  TB 332  
Cite this article:

Zheng ZHANG,Hao ZHANG,Hao CHAI,Hua-ping WU,Shao-fei JIANG. Design and performance analysis of variable stiffness multi-stable composite laminate structure. Journal of ZheJiang University (Engineering Science), 2020, 54(7): 1341-1346.

URL:

http://www.zjujournals.com/eng/10.3785/j.issn.1008-973X.2020.07.012     OR     http://www.zjujournals.com/eng/Y2020/V54/I7/1341


变刚度多稳态复合材料结构设计与性能分析

通过研究复合材料层合板结构局部纤维角变化的理论模型与刚度变化的关系,设计2种变刚度多稳态复合材料层合板结构. 对变刚度多稳态复合材料结构进行建模,运用Matlab求出不同的平衡方程解,得到变刚度多稳态复合材料结构的稳态构型. 制备相应的实验试件,测量变刚度多稳态复合材料结构不同稳态转变时的力学性能,通过有限元软件Abaqus模拟变刚度多稳态复合材料结构的降温冷却过程,得到平衡稳定状态的数值解. 结合理论、数值与试验,分析变刚度多稳态复合材料结构的稳态构型、稳态转变最大载荷及载荷-位移曲线的变化规律.


关键词: 变刚度,  多稳态复合材料,  经典层合板理论,  有限元分析 
参数 数值
E11/GPa 186
E22/GPa 88
v12 0.3
G12/GPa 7.1
ɑ11/(10?6°C?1 0.345
ɑ22/(10?6°C?1 15.3
Tab.1 Material properties of carbon fibre laminates
Fig.1 Schematic diagram of fiber direction of variable stiffness multi-stable composite laminate structures
Fig.2 Processing equipment with constant temperature and pressure
Fig.3 Stable diagram of specimen 1
Fig.4 Stable diagram of specimen 2
Fig.5 Experiment of stable state transformation
Fig.6 Indenter and fixture
Fig.7 Load-displacement curvatures of two specimens
Fig.8 Comparison of second stable configuration of theoretical and simulation results for specimen 1
Fig.9 Two different stable configurations of specimen 1 in simulation and experiment specimen
Fig.10 Two different stable configurations of specimen 2 in simulation and experiment specimen
Fig.11 Comparison of load-displacement with experiment and simulation for specimen 2
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