Morphing characteristics and damage analysis of 3D printing variable stiffness bistable laminates based on continuous fiber thermosetting composites

被引:25
作者
Zhang, Zheng [1 ,2 ]
Xu, Jiaze [1 ]
Ma, Yonglong [1 ]
Sun, Min [1 ,2 ]
Pan, Baisong [1 ,2 ]
Chai, Hao [3 ]
Zhang, Guang [1 ,2 ]
Jiang, Shaofei [1 ,2 ]
机构
[1] Zhejiang Univ Technol, Coll Mech Engn, Hangzhou 310014, Peoples R China
[2] Zhejiang Univ Technol, Key Lab Special Purpose Equipment & Adv Proc Techn, Minist Educ & Zhejiang Prov, Hangzhou 310014, Peoples R China
[3] Zhejiang Univ Technol, Zhijiang Coll, Shaoxing 312030, Peoples R China
关键词
Morphing characteristics; Damage analysis; 3D printing; Variable stiffness bistable laminate; Curvilinear fiber; Thermosetting resin; DESIGN; BEHAVIOR; SHAPE;
D O I
10.1016/j.compstruct.2023.117026
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The morphing characteristics and damage analysis of variable stiffness bistable laminate fabricated by continuous fiber 3D printing technology are systematically studied. Conventionally, bistable structures used in morphing applications are achieved with straight fibers. With the application of fiber placement technology, it is now possible to prepare variable stiffness laminates with different directions and layup angles of fibers. Moreover, the structure will be damaged with the increase in deformation times. How to effectively suppress the failure of laminates is also a highlight for this composite structure. In this paper, three curvilinear fiber paths are designed and compared. And a semi-analytical model based on the Rayleigh-Ritz method is used to predict the curvature of stable configuration. In particular, continuous fiber thermosetting resin matrix composites 3D printing technology is proposed for preparing variable stiffness laminates, which has several advantages compared to other traditional preparation methods of variable stiffness laminates. The corresponding finite element model is also developed to investigate the bistable behavior and damage analysis. In addition, the influence of different angle parameters and fiber paths on the stable configuration and the snap-load are also discussed. Finally, the damage evolution and mechanical properties of straight-fiber laminates and variable stiffness laminates in tension and compression are carried out based on the Hashin failure criteria.
引用
收藏
页数:15
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