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Analysis and optimization of temperature distribution in carbon fiber reinforced composite materials during microwave curing process

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TLDR
In this paper, the influence of ply orientation and thickness on through-thickness temperature distribution of carbon fiber reinforced composite laminates was investigated in two different types of epoxy systems.
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This article is published in Journal of Materials Processing Technology.The article was published on 2014-03-01 and is currently open access. It has received 65 citations till now. The article focuses on the topics: Epoxy & Microwave.

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Citations
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Journal ArticleDOI

Vacuum-assisted microwave curing of epoxy/carbon fiber composite: An attempt for defect reduction in processing

TL;DR: In this article, the authors focused on the manufacturing challenges during microwave curing of carbon fiber reinforced epoxy composite (CFREC) with 10% reinforcement by weight with or without assistance of vacuum pressure.
Journal ArticleDOI

Tooling materials compatible with carbon fibre composites in a microwave environment

TL;DR: In this article, an alternative tooling material in carbon fiber reinforced plastic (CFRP) was successfully used to cure CFRP panels in laboratory and industrial microwaves, and the conductive carbon fibres in the tool facilitated the fast heat transfer across the part.
Journal ArticleDOI

Carbon fiber/epoxy composite materials cured thermally and with microwave irradiation

TL;DR: In this paper, composite materials of short carbon fibers (CFs) and a thermosetting epoxy were prepared in three different ways: without curing, thermal curing, and thermal curing followed by micro...
Journal ArticleDOI

Investigation of strain history in fast and conventional curing epoxy matrix composites by FBGs

TL;DR: In this paper, the authors measured the strain history of fast and conventional curing epoxy matrix composite laminates by fiber Bragg grating (FBG) sensors and found that the peak temperature due to curing exothermal reaction was 133.7°C in both the 1st and the 5th ply in the fast curing composite when cure temperature profile settled at 80°C, which was 27.4°C higher than that in the conventional curing composite.
Journal ArticleDOI

Indirect Microwave Curing Process Design for Manufacturing Thick Multidirectional Carbon Fiber Reinforced Thermoset Composite Materials

TL;DR: In this paper, a multiphysics model was constructed to reflect the composite curing behavior in a cost-effective manner, which agreed well with the experimental results, and a new indirect microwave curing cycle was designed, and relevant process parameters were determined.
References
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Journal ArticleDOI

Fiber Bragg grating technology fundamentals and overview

TL;DR: Fiber Bragg grating (FBG) technology has been extensively studied in the literature as mentioned in this paper, where the basic techniques for fiber grating fabrication, their characteristics, and the fundamental properties of fiber gratings are described.
Journal ArticleDOI

Microwave processing: fundamentals and applications

TL;DR: In this paper, the fundamentals of electromagnetic theory, dielectric response, and applications of microwave heating to materials processing, especially fiber composites, are reviewed in this article, and a knowledge of electromagnetic theories and dielectrics is essential to optimize the processing of materials through microwave heating.
Journal ArticleDOI

Process-Induced Stress and Deformation in Thick-Section Thermoset Composite Laminates:

TL;DR: In this paper, a study of process-induced stress and deformation in thick-section thermosetting composite laminates is presented, and a methodology is proposed for predict ing the evolution of residual stress develop...
BookDOI

Optical Fiber Sensor Technology

TL;DR: In this article, the authors present an overview of the development of optical fiber sensor technology and its application in the field of temperature measurement and current measurement, as well as other applications.
Journal ArticleDOI

Effect of laminate configuration and feed rate on cutting performance when drilling holes in carbon fibre reinforced plastic composites

TL;DR: In this paper, the results of twist drilling 1.5 mm diameter holes in 3 mm thick carbon fiber reinforced plastics laminate using tungsten carbide (WC) stepped drills were presented.
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Frequently Asked Questions (15)
Q1. What contributions have the authors mentioned in the paper "Analysis and optimization of temperature distribution in carbon fiber reinforced composite materials during microwave curing process" ?

Two different types of epoxy systems have been studied. The maximum temperature difference of the samples formed using themodified microwave curing technologies in this research could be reduced by 79 % to 2. 1 °C. 

Future studies will be carried out to identify the relationship between several physical mechanisms in microwave curing to get a better temperature distribution and establish the standard process specifications. 

The physical mechanism of microwave curing includes the natural heat convection of air inthe microwave oven, heat conduction inside the composite material and the directly heating action of microwave. 

Using the vacuum pressure technology and ceramic tooling, the composite samples achieved lower cost in manufacturing and better performance. 

Bogetti and Gillespie (1992) reported that the complex gradients of temperature in thickness direction of composite laminates may cause serious process-induced residual stress and deformation. 

Under the action of an electromagnetic field, the temperature at the surface of carbon fiberreinforced composites is lower than the target temperature, no matter for what kinds of composite laminates. 

Boey and Yap (2001) reported that microwave curing was more effective than conventional heating in enhancing the reaction rates during cross-linking by testing different curing agents in curing. 

The condition to be satisfied to get such a Bragg reflected wavelength is known as Bragg condition and is given by Grattan and Meggitt (1997) as: 2B nD (1) 

The thickness values of composite laminates are 4.5, 7.5 and 22.5mm, corresponding to sample #1, sample #2 and sample #3 respectively. 

The most important dwell stages were studied to analysis the temperature distribution influenced by ply orientation and thickness. 

A periodic perturbation of the refractive index can be formed along the fiber length through the change of reflection wavelength influenced by the physical or mechanical characteristics of the grating area. 

Based on the analysis, in order to uniform the temperature distribution of compositelaminates, different solutions need to be applied. 

For the above reason, alternative processing technologies, such as microwave curingtechnologies have been developed to form composite structures and provide a uniform temperature distribution. 

Considering the previous work, the 0.09Mpa vacuum pressure was provided when heating from 100 °C or 90 °C to the end of heat preservation. 

The composite laminates were laid up on a ceramic tooling coated with release agent and the edge areas were covered by sealant tapes.