Thermal synergistic effect on CFRP laminates with modified fiber/matrix systems for heat transfer applications

Carbon fiber reinforced polymer (CFRP) laminates are modified to enhance their suitability for various thermal applications. A synergistic approach utilizing the effect of various conductive and insulative modifiers with diglycidyl ethers of bisphenol A (DGEBA) epoxy resin and/carbon fiber (CF) is e...

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Main Authors: Aravind, J., Manu, M., Roy, K. E. Reby, Ali, M. Mubarak, Abu Hassan, Shukur, Rajalekshmi, S., Daniel, Desin S.
Format: Article
Published: John Wiley and Sons Inc 2023
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Online Access:http://eprints.utm.my/105252/
http://dx.doi.org/10.1002/macp.202200462
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spelling my.utm.1052522024-04-17T06:23:43Z http://eprints.utm.my/105252/ Thermal synergistic effect on CFRP laminates with modified fiber/matrix systems for heat transfer applications Aravind, J. Manu, M. Roy, K. E. Reby Ali, M. Mubarak Abu Hassan, Shukur Rajalekshmi, S. Daniel, Desin S. Q Science (General) TK Electrical engineering. Electronics Nuclear engineering Carbon fiber reinforced polymer (CFRP) laminates are modified to enhance their suitability for various thermal applications. A synergistic approach utilizing the effect of various conductive and insulative modifiers with diglycidyl ethers of bisphenol A (DGEBA) epoxy resin and/carbon fiber (CF) is explored. In CFRP laminates developed after modifications made in epoxy resin using a thermoplastic material, such as polycarbonate (PC) and/or acrylonitrile butadiene styrene (ABS), exhibit high thermal resistance (TR) of 77.1% compared to unmodified CFRP. In contrast, modifications made using conductive mediums like phosphonium (P), imidazolium (I), or silanized-graphene oxide (SGO) have lower TR of 25.7%, 30.5%, and 32.4%, respectively. A temperature gradient (TG) enhancement of 75% is reported for the 1.5 wt% PC/ABS modified CFRP laminates. On the contrary, modifications using 0.5 parts per hundred (phr)P, 0.5 phr I, and 1 g L−1 SGO in epoxy reduce the TG by 25%, 30%, and 32%, respectively. Thermogravimetric analysis (TGA) and differential scanning calorimetry (DSC) analyses are done to explore the thermal characteristics of each case of modification. Finally, scanning electron microscopy images confirm the distribution profile of the modifiers used. Based on the types of modifications performed, the current study can offer insightful information on the thermal performances of modified CFRP laminates. John Wiley and Sons Inc 2023-06 Article PeerReviewed Aravind, J. and Manu, M. and Roy, K. E. Reby and Ali, M. Mubarak and Abu Hassan, Shukur and Rajalekshmi, S. and Daniel, Desin S. (2023) Thermal synergistic effect on CFRP laminates with modified fiber/matrix systems for heat transfer applications. Macromolecular Chemistry and Physics, 224 (11). NA. ISSN 1022-1352 http://dx.doi.org/10.1002/macp.202200462 DOI:10.1002/macp.202200462
institution Universiti Teknologi Malaysia
building UTM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Malaysia
content_source UTM Institutional Repository
url_provider http://eprints.utm.my/
topic Q Science (General)
TK Electrical engineering. Electronics Nuclear engineering
spellingShingle Q Science (General)
TK Electrical engineering. Electronics Nuclear engineering
Aravind, J.
Manu, M.
Roy, K. E. Reby
Ali, M. Mubarak
Abu Hassan, Shukur
Rajalekshmi, S.
Daniel, Desin S.
Thermal synergistic effect on CFRP laminates with modified fiber/matrix systems for heat transfer applications
description Carbon fiber reinforced polymer (CFRP) laminates are modified to enhance their suitability for various thermal applications. A synergistic approach utilizing the effect of various conductive and insulative modifiers with diglycidyl ethers of bisphenol A (DGEBA) epoxy resin and/carbon fiber (CF) is explored. In CFRP laminates developed after modifications made in epoxy resin using a thermoplastic material, such as polycarbonate (PC) and/or acrylonitrile butadiene styrene (ABS), exhibit high thermal resistance (TR) of 77.1% compared to unmodified CFRP. In contrast, modifications made using conductive mediums like phosphonium (P), imidazolium (I), or silanized-graphene oxide (SGO) have lower TR of 25.7%, 30.5%, and 32.4%, respectively. A temperature gradient (TG) enhancement of 75% is reported for the 1.5 wt% PC/ABS modified CFRP laminates. On the contrary, modifications using 0.5 parts per hundred (phr)P, 0.5 phr I, and 1 g L−1 SGO in epoxy reduce the TG by 25%, 30%, and 32%, respectively. Thermogravimetric analysis (TGA) and differential scanning calorimetry (DSC) analyses are done to explore the thermal characteristics of each case of modification. Finally, scanning electron microscopy images confirm the distribution profile of the modifiers used. Based on the types of modifications performed, the current study can offer insightful information on the thermal performances of modified CFRP laminates.
format Article
author Aravind, J.
Manu, M.
Roy, K. E. Reby
Ali, M. Mubarak
Abu Hassan, Shukur
Rajalekshmi, S.
Daniel, Desin S.
author_facet Aravind, J.
Manu, M.
Roy, K. E. Reby
Ali, M. Mubarak
Abu Hassan, Shukur
Rajalekshmi, S.
Daniel, Desin S.
author_sort Aravind, J.
title Thermal synergistic effect on CFRP laminates with modified fiber/matrix systems for heat transfer applications
title_short Thermal synergistic effect on CFRP laminates with modified fiber/matrix systems for heat transfer applications
title_full Thermal synergistic effect on CFRP laminates with modified fiber/matrix systems for heat transfer applications
title_fullStr Thermal synergistic effect on CFRP laminates with modified fiber/matrix systems for heat transfer applications
title_full_unstemmed Thermal synergistic effect on CFRP laminates with modified fiber/matrix systems for heat transfer applications
title_sort thermal synergistic effect on cfrp laminates with modified fiber/matrix systems for heat transfer applications
publisher John Wiley and Sons Inc
publishDate 2023
url http://eprints.utm.my/105252/
http://dx.doi.org/10.1002/macp.202200462
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score 13.211869