Journal of Textile Research ›› 2020, Vol. 41 ›› Issue (06): 27-35.doi: 10.13475/j.fzxb.20190101809

• Fiber Materials • Previous Articles     Next Articles

Finite element simulation on wear resistance of copper-plated carbon fiber tows

DAI Xin1,2,3, LI Jing1,2,3(), CHEN Chen1,4   

  1. 1. School of Mechanical and Electrical Engineering, Xi'an Polytechnic University, Xi'an, Shaanxi 710048, China
    2. Xi'an Key Laboratory of Modern Intelligent Textile Equipment, Xi'an, Shaanxi 710048, China
    3. Manufacturing Management Department of Jiangsu Yonggang Group Co., Ltd., Zhangjiagang, Jiangsu 215628, China
    4. Shaoxing Keqiao West-Tex Textile Industry Innovative Institute, Shaoxing, Zhejiang 312065, China
  • Received:2019-01-10 Revised:2020-03-14 Online:2020-06-15 Published:2020-06-28
  • Contact: LI Jing E-mail:ljing62@126.com

Abstract:

In order to improve the abrasion resistance of carbon fiber tow, copper plating on the surface of carbon fiber tow was proposed. Firstly, a mesoscopic model for resin-based carbon fiber tow was established in Solidworks, and the sliding friction damage between a carbon fiber tow and a copper-plated heald wire eye during shedding was simulated using ABAQUS, and the progressive damage failure model of fiber composite was used for the damage evolution analysis. Then the resin-based carbon fiber tow was changed to copper-plated carbon fiber tow, and the feasibility of the model was verified by simulation of tensile loading. The wear resistance of copper-plated carbon fiber tow was simulated by Archard model. Finally, the stiffness of the fiber tow was simulated using ABAQUS. The results show that when the thickness of copper plating layer is 1.0 μm, the wear resistance predicted by the simulation of a copper-plated carbon fiber tow is about twice that of a carbon fiber tow with a sizing rate of 0.32% and a slurry mass fraction of 3%. Carbon fiber tow plated with 0.5-1 μm copper layer demonstrates optimal weavability.

Key words: carbon fiber, weaving, opening damage, copper-plated carbon fiber fabric, wear resistance, finite element analysis

CLC Number: 

  • TS155

Fig.1

Three-dimensional model of copper-plated heald eye and copper-plated carbon fiber bundle"

Fig.2

Coppe-plated wire bundle mesoscopic model"

Tab.1

Geometric parameters of copper-plated wire bundlesμm"

长度
L
宽度
W
高度
H
镀铜厚度
d1 d2 d3 d4
75.0 20.8~36.0 5.2~9.0 0.1 0.5 1.0 2.0

Fig.3

Tensile verification stress cloud diagram of filament model"

Fig.4

Structure of progressive damage model"

Fig.5

Pre-processing result of finite element. (a) Setting of model constraints;(b) Grid generation"

Fig.6

Finite element stress cloud diagram. (a) Damage stress cloud map at initial acceleration;(b) Damage stress cloud map during deceleration; (c) Stress cloud diagram of resin-based carbon fiber composites after injury; (d) Damage stress cloud diagram of carbon fiber after wear"

Fig.7

Progressive damage of carbon fiber. (a) Stress convergence of damage points perpendicular to fiber direction;(b) Strain curve at same damage point perpendicular to fiber direction;(c) Stress curve at same damage point perpendicular to fiber direction"

Fig.8

Schematic diagram of intersection of carbon fiber bundles during opening motion"

Fig.9

Copper-plated wire bundle mesh generation model"

Fig.10

Setting of model boundary conditions"

Fig.11

Copper die wear area"

Fig.12

Finite element simulation flow chart of wear"

Fig.13

Wear stress cloud diagram. (a) Stress cloud map of initial position during wear;(b) Stress clouds at end of wear"

Fig.14

Relationship between copper plating thickness and wear resistance"

Fig.15

Comparison on flexibility of various fiber monofilaments. (a) Copper coated carbon fiber of 0.1 μm;(b) Copper coated carbon fiber of 0.5 μm;(c) Copper coated carbon fiber of 1.0 μm;(d) Copper coated carbon fiber of 2.0 μm; (e)ZylonHM fiber; (f)Sized carbon fiber"

Fig.16

Relationship between apex bending displacement and load of various fiber monofilaments"

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