期刊
COMPOSITES SCIENCE AND TECHNOLOGY
卷 71, 期 16, 页码 1944-1952出版社
ELSEVIER SCI LTD
DOI: 10.1016/j.compscitech.2011.09.011
关键词
Composite material; Carbon fiber; Polymer; Epoxy; Thermal conductivity; Carbon black; Carbon nanotube; Polymer-matrix composites (PMCs); Structural composites; Thermal properties
The low through-thickness thermal conductivity limits heat dissipation from continuous carbon fiber polymer-matrix composites. This conductivity is increased by up to 60% by raising the curing pressure from 0.1 to 2.0 MPa and up to 33% by incorporation of a filler (<= 1.5 vol.%) at the interlaminar interface. The 7-mu m-diameter 7-W/m K-thermal-conductivity continuous fiber volume fraction is increased by the curing pressure increase, but is essentially unaffected by filler incorporation. The thermal resistivity is dominated by the lamina resistivity (which is contributed substantially by the intralaminar fiber-fiber interfacial resistivity), with the interlaminar interface thermal resistivity being unexpectedly negligible. The lamina resistivity and intralaminar fiber-fiber interfacial resistivity are decreased by up to 56% by raising the curing pressure and up to 36% by filler incorporation. The curing pressure increase does not affect the effectiveness of 1-mm-long 10-mu m-diameter 900-1000-W/m K-thermal-conductivity K-1100 carbon fiber or single-walled carbon nanotube (SWCNT) as fillers for enhancing the conductivity, but hinders the effectiveness of carbon black (CB, low-cost), which is less effective than K-1100 or SWCNT at the higher curing pressure, but is almost as effective as K-1100 and SWCNT at the lower curing pressure. The effectiveness for enhancing the flexural modulus/strength/ductility decreases in the order: SWCNT, CB, K-1100. (C) 2011 Elsevier Ltd. All rights reserved.
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