Manufacturing and Performance Evaluation of Carbon Fiber–Reinforced Honeycombs

In this work, the manufacturing characteristics and a performance evaluation of carbon fiber⁻reinforced epoxy honeycombs are reported. The vacuum-assisted resin transfer molding process, using a central injection point, is used to infuse a unidirectional dry slit tape with the epoxy resin...

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Main Authors: Sanjeev Rao, Jimmy Thomas, Alia Aziz, Wesley Cantwell
Format: Article
Language:English
Published: MDPI AG 2019-01-01
Series:Journal of Composites Science
Subjects:
Online Access:https://www.mdpi.com/2504-477X/3/1/13
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spelling doaj-ad664cef020d45cba493548ed1e356a72020-11-24T23:56:42ZengMDPI AGJournal of Composites Science2504-477X2019-01-01311310.3390/jcs3010013jcs3010013Manufacturing and Performance Evaluation of Carbon Fiber–Reinforced HoneycombsSanjeev Rao0Jimmy Thomas1Alia Aziz2Wesley Cantwell3Aerospace Research and Innovation Centre, Khalifa University of Science and Technology, PO Box 127788, Abu Dhabi, UAEDepartment of Mechanical Engineering, Khalifa University of Science and Technology, PO Box 127788, Abu Dhabi, UAEAerospace Research and Innovation Centre, Khalifa University of Science and Technology, PO Box 127788, Abu Dhabi, UAEAerospace Research and Innovation Centre, Khalifa University of Science and Technology, PO Box 127788, Abu Dhabi, UAEIn this work, the manufacturing characteristics and a performance evaluation of carbon fiber&#8315;reinforced epoxy honeycombs are reported. The vacuum-assisted resin transfer molding process, using a central injection point, is used to infuse a unidirectional dry slit tape with the epoxy resin system Prime 20 LV in a wax mold. The compression behavior of the manufactured honeycomb structure was evaluated by subjecting samples to quasi-static compression loading. Failure criteria for the reinforced honeycombs were developed and failure maps were constructed. These maps can be used to evaluate the reliability of the core for a prescribed loading condition. Improvements in the load-carrying capacity for the reinforced samples, as compared with unreinforced specimens, are discussed and the theoretical predictions are compared with the experimental data. The compression test results highlight a load-carrying capacity up to 26 kN (~143 MPa) for a single hexagonal cell (unit cell) and 160 kN (~170 MPa) for cores consisting of 2.5 &#215; 3.5 cells. The failure map indicates buckling to be the predominant mode of failure at low relative densities, shifting to cell wall fracture at relative densities closer to a value of 10<sup>&#8722;1</sup>. The resulting energy absorption diagram shows a monotonic increase in energy absorption with the increasing <i>t/l</i> ratio of the honeycomb core cell walls.https://www.mdpi.com/2504-477X/3/1/13honeycombscarbon fiberslit tapefiber-reinforced cores
collection DOAJ
language English
format Article
sources DOAJ
author Sanjeev Rao
Jimmy Thomas
Alia Aziz
Wesley Cantwell
spellingShingle Sanjeev Rao
Jimmy Thomas
Alia Aziz
Wesley Cantwell
Manufacturing and Performance Evaluation of Carbon Fiber–Reinforced Honeycombs
Journal of Composites Science
honeycombs
carbon fiber
slit tape
fiber-reinforced cores
author_facet Sanjeev Rao
Jimmy Thomas
Alia Aziz
Wesley Cantwell
author_sort Sanjeev Rao
title Manufacturing and Performance Evaluation of Carbon Fiber–Reinforced Honeycombs
title_short Manufacturing and Performance Evaluation of Carbon Fiber–Reinforced Honeycombs
title_full Manufacturing and Performance Evaluation of Carbon Fiber–Reinforced Honeycombs
title_fullStr Manufacturing and Performance Evaluation of Carbon Fiber–Reinforced Honeycombs
title_full_unstemmed Manufacturing and Performance Evaluation of Carbon Fiber–Reinforced Honeycombs
title_sort manufacturing and performance evaluation of carbon fiber–reinforced honeycombs
publisher MDPI AG
series Journal of Composites Science
issn 2504-477X
publishDate 2019-01-01
description In this work, the manufacturing characteristics and a performance evaluation of carbon fiber&#8315;reinforced epoxy honeycombs are reported. The vacuum-assisted resin transfer molding process, using a central injection point, is used to infuse a unidirectional dry slit tape with the epoxy resin system Prime 20 LV in a wax mold. The compression behavior of the manufactured honeycomb structure was evaluated by subjecting samples to quasi-static compression loading. Failure criteria for the reinforced honeycombs were developed and failure maps were constructed. These maps can be used to evaluate the reliability of the core for a prescribed loading condition. Improvements in the load-carrying capacity for the reinforced samples, as compared with unreinforced specimens, are discussed and the theoretical predictions are compared with the experimental data. The compression test results highlight a load-carrying capacity up to 26 kN (~143 MPa) for a single hexagonal cell (unit cell) and 160 kN (~170 MPa) for cores consisting of 2.5 &#215; 3.5 cells. The failure map indicates buckling to be the predominant mode of failure at low relative densities, shifting to cell wall fracture at relative densities closer to a value of 10<sup>&#8722;1</sup>. The resulting energy absorption diagram shows a monotonic increase in energy absorption with the increasing <i>t/l</i> ratio of the honeycomb core cell walls.
topic honeycombs
carbon fiber
slit tape
fiber-reinforced cores
url https://www.mdpi.com/2504-477X/3/1/13
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AT jimmythomas manufacturingandperformanceevaluationofcarbonfiberreinforcedhoneycombs
AT aliaaziz manufacturingandperformanceevaluationofcarbonfiberreinforcedhoneycombs
AT wesleycantwell manufacturingandperformanceevaluationofcarbonfiberreinforcedhoneycombs
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