TY - JOUR
T1 - Multichannel hollow carbon fibers
T2 - Processing, structure, and properties
AU - Shirolkar, Narayan
AU - Maffe, Adam
AU - DiLoreto, Edward
AU - Arias-Monje, Pedro J.
AU - Lu, Mingxuan
AU - Ramachandran, Jyotsna
AU - Gulgunje, Prabhakar
AU - Gupta, Kishor
AU - Park, Jin Gyu
AU - Shih, Kuo Chih
AU - Kirmani, Mohammad Hamza
AU - Sharits, Andrew
AU - Nepal, Dhriti
AU - Nieh, Mu Ping
AU - Liang, Richard
AU - Tsotsis, Thomas
AU - Kumar, Satish
N1 - Publisher Copyright:
© 2020 Elsevier Ltd
PY - 2021/4/15
Y1 - 2021/4/15
N2 - Multifilament continuous hollow carbon fiber tows with a honeycomb cross-section have been produced using a gel-spun bicomponent islands-in-a-sea precursor with polyacrylonitrile (PAN) as the sea component and polymethylmethacrylate (PMMA) as the sacrificial island component. The density of the hollow carbon fibers is 1.15 g/cm3, more than 30% lower compared to commercial carbon fibers. The tensile strength of these fibers is in the range of 2.3–3.0 GPa and tensile modulus between 202 and 234 GPa. The tensile strength is over 80% higher than the 1.6 GPa strength value reported earlier for hollow carbon fibers. The specific tensile strength is 30% higher than T300 carbon fibers. The specific tensile modulus is 60% higher than T300 carbon fibers and 20% higher than aerospace grade IM7 carbon fibers. The manufacturing was successfully scaled up from a single filament to 740 filament tow without affecting the carbon fiber structural parameters. The tensile strength is limited by the size of the largest defects present, estimated to be in the range of 40–65 nm for the hollow carbon fibers.
AB - Multifilament continuous hollow carbon fiber tows with a honeycomb cross-section have been produced using a gel-spun bicomponent islands-in-a-sea precursor with polyacrylonitrile (PAN) as the sea component and polymethylmethacrylate (PMMA) as the sacrificial island component. The density of the hollow carbon fibers is 1.15 g/cm3, more than 30% lower compared to commercial carbon fibers. The tensile strength of these fibers is in the range of 2.3–3.0 GPa and tensile modulus between 202 and 234 GPa. The tensile strength is over 80% higher than the 1.6 GPa strength value reported earlier for hollow carbon fibers. The specific tensile strength is 30% higher than T300 carbon fibers. The specific tensile modulus is 60% higher than T300 carbon fibers and 20% higher than aerospace grade IM7 carbon fibers. The manufacturing was successfully scaled up from a single filament to 740 filament tow without affecting the carbon fiber structural parameters. The tensile strength is limited by the size of the largest defects present, estimated to be in the range of 40–65 nm for the hollow carbon fibers.
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U2 - 10.1016/j.carbon.2020.11.077
DO - 10.1016/j.carbon.2020.11.077
M3 - Research Article
AN - SCOPUS:85099347704
SN - 0008-6223
VL - 174
SP - 730
EP - 740
JO - Carbon
JF - Carbon
ER -