Fiber reinforced shape-memory polymer composite and its application in a deployable hinge

被引:417
作者
Lan, Xin [1 ]
Liu, Yanju [2 ]
Lv, Haibao [1 ]
Wang, Xiaohua [1 ]
Leng, Jinsong [1 ]
Du, Shanyi [1 ]
机构
[1] Harbin Inst Technol, Ctr Composite Mat & Struct, Harbin, Peoples R China
[2] Harbin Inst Technol, Dept Aerosp Sci & Mech, Harbin, Peoples R China
关键词
MOISTURE;
D O I
10.1088/0964-1726/18/2/024002
中图分类号
TH7 [仪器、仪表];
学科分类号
0804 ; 080401 ; 081102 ;
摘要
This paper investigates the shape recovery behavior of thermoset styrene-based shape-memory polymer composite (SMPC) reinforced by carbon fiber fabrics, and demonstrates the feasibility of using an SMPC hinge as a deployable structure. The major advantages of shape-memory polymers (SMPs) are their extremely high recovery strain, low density and low cost. However, relatively low modulus and low strength are their intrinsic drawbacks. A fiber reinforced SMPC which may overcome the above-mentioned disadvantages is studied here. The investigation was conducted by three types of test, namely dynamic mechanical analysis (DMA), a shape recovery test, and optical microscopic observations of the deformation mechanism for an SMPC specimen. Results reveal that the SMPC exhibits a higher storage modulus than that of a pure SMP. At/above T-g, the shape recovery ratio of the SMPC upon bending is above 90%. The shape recovery properties of the SMPC become relatively stable after some packaging/deployment cycles. Additionally, fiber microbuckling is the primary mechanism for obtaining a large strain in the bending of the SMPC. Moreover, an SMPC hinge has been fabricated, and a prototype of a solar array actuated by the SMPC hinge has been successfully deployed.
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页数:6
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