A study of the interply strengthening of CF/PA6 composites using micro-size core-shell particles
Thermoplastic composites have become increasingly popular due to their numerous benefits. To enhance the performance of fiber-reinforced thermoplastic composites, many research efforts have been made using various types of fillers. However, the high melting temperature and viscosity of thermoplastic...
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sg-ntu-dr.10356-1811872024-11-23T16:48:58Z A study of the interply strengthening of CF/PA6 composites using micro-size core-shell particles Sharma, Anurag Joshi, Sunil Chandrakant School of Mechanical and Aerospace Engineering Engineering Interply strengthening Carbon fiber Thermoplastic composites Core-shell particles Flexural strength ILSS Compression strength Thermoplastic composites have become increasingly popular due to their numerous benefits. To enhance the performance of fiber-reinforced thermoplastic composites, many research efforts have been made using various types of fillers. However, the high melting temperature and viscosity of thermoplastic polymer melt present a primary challenge in achieving uniform filler dispersion. Interply strengthening is one of the simplest and most cost-effective techniques for addressing this challenge. This study utilized micro-size core-shell particles that were dispersed using a sieve. The particles were carefully sprinkled onto the sieve, facilitating their controlled dispersion at the ply interface, after which fabric and thermoplastic films were laid on top. The resulting stacked arrangement was then processed using a hot consolidation cycle via compression molding to produce composite laminate. The impact of incorporating core-shell particles on the mechanical performance of carbon fiber-reinforced polyamide 6 (CF/PA6) laminates was investigated. Results showed that adding 4 wt% core-shell particles led to a maximum improvement of 58.99%, 25.62%, 41.56%, and 47.83% in flexural strength and modulus, interply shear strength, and compression strength, respectively, compared to the pristine composites. Stress-strain curves confirmed that the core-shell particles delayed matrix and interlaminar crack propagation. Furthermore, micrographic images indicated improved interaction of CSPs at the ply interfaces. These findings can improve the interply strength of thermoplastic composites and assist designers in achieving higher performance. Published version This research received no external funding. 2024-11-18T02:55:06Z 2024-11-18T02:55:06Z 2024 Journal Article Sharma, A. & Joshi, S. C. (2024). A study of the interply strengthening of CF/PA6 composites using micro-size core-shell particles. Journal of Composites Science, 8(11), 447-. https://dx.doi.org/10.3390/jcs8110447 2504-477X https://hdl.handle.net/10356/181187 10.3390/jcs8110447 11 8 447 en Journal of Composites Science © 2024 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https:// creativecommons.org/licenses/by/ 4.0/). application/pdf |
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Engineering Interply strengthening Carbon fiber Thermoplastic composites Core-shell particles Flexural strength ILSS Compression strength Sharma, Anurag Joshi, Sunil Chandrakant A study of the interply strengthening of CF/PA6 composites using micro-size core-shell particles |
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Thermoplastic composites have become increasingly popular due to their numerous benefits. To enhance the performance of fiber-reinforced thermoplastic composites, many research efforts have been made using various types of fillers. However, the high melting temperature and viscosity of thermoplastic polymer melt present a primary challenge in achieving uniform filler dispersion. Interply strengthening is one of the simplest and most cost-effective techniques for addressing this challenge. This study utilized micro-size core-shell particles that were dispersed using a sieve. The particles were carefully sprinkled onto the sieve, facilitating their controlled dispersion at the ply interface, after which fabric and thermoplastic films were laid on top. The resulting stacked arrangement was then processed using a hot consolidation cycle via compression molding to produce composite laminate. The impact of incorporating core-shell particles on the mechanical performance of carbon fiber-reinforced polyamide 6 (CF/PA6) laminates was investigated. Results showed that adding 4 wt% core-shell particles led to a maximum improvement of 58.99%, 25.62%, 41.56%, and 47.83% in flexural strength and modulus, interply shear strength, and compression strength, respectively, compared to the pristine composites. Stress-strain curves confirmed that the core-shell particles delayed matrix and interlaminar crack propagation. Furthermore, micrographic images indicated improved interaction of CSPs at the ply interfaces. These findings can improve the interply strength of thermoplastic composites and assist designers in achieving higher performance. |
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School of Mechanical and Aerospace Engineering |
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School of Mechanical and Aerospace Engineering Sharma, Anurag Joshi, Sunil Chandrakant |
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Article |
author |
Sharma, Anurag Joshi, Sunil Chandrakant |
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Sharma, Anurag |
title |
A study of the interply strengthening of CF/PA6 composites using micro-size core-shell particles |
title_short |
A study of the interply strengthening of CF/PA6 composites using micro-size core-shell particles |
title_full |
A study of the interply strengthening of CF/PA6 composites using micro-size core-shell particles |
title_fullStr |
A study of the interply strengthening of CF/PA6 composites using micro-size core-shell particles |
title_full_unstemmed |
A study of the interply strengthening of CF/PA6 composites using micro-size core-shell particles |
title_sort |
study of the interply strengthening of cf/pa6 composites using micro-size core-shell particles |
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2024 |
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https://hdl.handle.net/10356/181187 |
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1816859023308226560 |