Journal of Textile Research ›› 2022, Vol. 43 ›› Issue (11): 68-74.doi: 10.13475/j.fzxb.20210902107

• Textile Engineering • Previous Articles     Next Articles

Fabrication and thermal-activated recovery properties of shape memory composite braided circular tubes

ZHANG Wei, JIANG Zhe, XU Qi, SUN Baozhong()   

  1. College of Textiles, Donghua University, Shanghai 201620, China
  • Received:2021-09-08 Revised:2022-04-30 Online:2022-11-15 Published:2022-12-26
  • Contact: SUN Baozhong E-mail:sunbz@dhu.edu.cn

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Abstract:

To investigate the effects of braiding angle and recovery temperature on mechanical properties and shape recovery performances of braided circular tube composites, continuous carbon fiber/shape memory polyurethane composite filament was prepared using the modified twin-screw extrusion technique, and the braided circular tubes with different braiding angles were obtained by 2-D braiding. The braiding angles included 15°, 30°, 45°, 60° and 75°, and the radial strength and shape recovery performances of braided circular tubes were compared. The results show that continuous carbon fiber is evenly coated by shape memory polyurethane and in the center of composite filament. Radial force of the circular tube is proportional to the braiding angle and the closer the braiding angle is to 45°, the higher the shape recovery ratio will be. Recovery temperature has the effect on shape memory properties. As the recovery temperature increases, recovery rate and recovery ratio are both enhanced. The braided circular tube structure demonstrated a shape recovery ratio of up to 96%.

Key words: braided circular tube, shape memory, composite filament, thermal-activated, braiding angle

CLC Number: 

  • TS101.2

Fig.1

Experimental setup for preparation of CCF/SMPU composite filament"

Fig.2

diamond braiding structure (a) and cross-sectional view (b)"

Tab.1

Braiding parameters"

编织角度/(°) 锭子角速度/(rad·s-1) 芯轴牵引速度/(mm·s-1)
15 0.32 8.96
30 0.32 4.16
45 0.32 2.40
60 0.32 1.38
75 0.32 0.64

Fig.3

Braided circular tube specimens with different braiding angles"

Fig.4

Model diagram of shape memory properties testing"

Fig.5

Cross sectional morphology of CCF/SMPU composite filament(×200)"

Fig.6

Thermal gravimetric analysis of CCF/SMPU composite filament"

Fig.7

Mechanical tensile test of shape memory filaments. (a) Load-displacement curves; (b) Stress-strain curves"

Fig.8

Radial compression load-displacement curves of CCF/SMPU braided circular tubes"

Fig.9

Shape recovery process for thermal driven at 60 ℃"

Fig.10

Relationship between shape recovery ratio and time, braiding angle and temperature. (a) 60 ℃; (b)70 ℃; (c) 80 ℃; (d) Effect of braiding angle and temperature on shape recovery ratio"

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