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A novel continuous carbon nanotube fiber/carbon composite by electrified preform heating chemical vapor infiltration
被引:24
|作者:
Feng, Lei
[1
,3
]
Fu, Qiangang
[2
]
Song, Qiang
[2
]
Yang, Yanling
[1
]
Zuo, Yu
[1
]
Suo, Guoquan
[1
]
Hou, Xiaojiang
[1
]
Zhang, Li
[1
]
Ye, Xiaohui
[1
]
机构:
[1] Shaanxi Univ Sci & Technol, Sch Mat Sci & Engn, Shaanxi Key Lab Green Preparat & Functionalizat I, Xian 710021, Shaanxi, Peoples R China
[2] Northwestern Polytech Univ, State Key Lab Solidificat Proc, Xian 710072, Shaanxi, Peoples R China
[3] Tianjin Univ, Sch Mat Sci & Engn, Tianjin 300073, Peoples R China
来源:
基金:
中国国家自然科学基金;
关键词:
PYROLYTIC CARBON;
CARBON/CARBON COMPOSITES;
ALIGNED CARBON;
MECHANICAL-PROPERTIES;
FIBERS;
DEPOSITION;
STRENGTH;
MICROSTRUCTURE;
CONDUCTIVITY;
DENSIFICATION;
D O I:
10.1016/j.carbon.2019.11.009
中图分类号:
O64 [物理化学(理论化学)、化学物理学];
学科分类号:
070304 ;
081704 ;
摘要:
The extraordinary mechanical and physical properties of carbon nanotubes (CNTs) have provided the impetus in developing a new promising CNT/carbon (CNT/C) composite, which may effectively alleviate the shortcomings of sharp-angle and thin-walled C/C components in mechanical performance. Present researches on preparing CNT/C composites focus on infiltrating pyrocarbon into CNT assemblies such as array, block, sheet, film, and buckypaper using complicated and time-consuming methods. Here, we report a facile and efficient strategy for preparing CNT fiber/C composites via electrified preform heating chemical vapor infiltration. Densification process is identified as continual deposition of pyrocarbon around CNTs (called coaxial structure) and further deposition among them, which can be accomplished in short time. Small-diameter (below 500 nm) coaxial structures give composites high deformability; larger ones coupled with bridging action of pyrocarbon among them result in better load transfer and more conductive pathways. Optimized CNT fiber/C composites demonstrate impressive tensile strength (205 MPa) and excellent conductivity (431 S/cm), which are comparable to the previously reported C/C and CNT/C composites. Moreover, such composites exhibit lightweight (1.21 g/cm(3)), good deformability and high fracture strain. Our work could open up a general strategy for efficiently fabricating various high-performance CNT/C composites that could be used in high-temperature aerospace fields. (C) 2019 Elsevier Ltd. All rights reserved.
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页码:640 / 648
页数:9
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