An Analytical Model of Thermal Conductivity for Carbon/Carbon Composites with Pitch-Based Matrix

The carbon/carbon (C/C) composites are composed of carbon fibers, carbon matrix, and pores and cracks, which have been successfully used in various aerospace applications. In this paper, nanoscale submodel is proposed to describe the thermal conductivity of the matrix based on its microscopic struct...

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Main Authors: Zhi-Hai Feng, Jia-Yun Zhi, Zhen Fan, Duo Sun, Chao Si, Xiao-Dong Wang
Format: Article
Language:English
Published: SAGE Publishing 2015-01-01
Series:Advances in Mechanical Engineering
Online Access:https://doi.org/10.1155/2014/242586
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spelling doaj-8319fa0462b7464ca434de5314f42e6b2020-11-25T03:43:29ZengSAGE PublishingAdvances in Mechanical Engineering1687-81322015-01-01710.1155/2014/24258610.1155_2014/242586An Analytical Model of Thermal Conductivity for Carbon/Carbon Composites with Pitch-Based MatrixZhi-Hai Feng0Jia-Yun Zhi1Zhen Fan2Duo Sun3Chao Si4Xiao-Dong Wang5 Key Laboratory of Advanced Functional Composite Materials, Aerospace Research Institute of Materials and Processing Technology, Beijing 100076, China Beijing Key Laboratory of Multiphase Flow and Heat Transfer for Low Grade Energy, North China Electric Power University, Beijing 102206, China Key Laboratory of Advanced Functional Composite Materials, Aerospace Research Institute of Materials and Processing Technology, Beijing 100076, China Beijing Key Laboratory of Multiphase Flow and Heat Transfer for Low Grade Energy, North China Electric Power University, Beijing 102206, China Beijing Key Laboratory of Multiphase Flow and Heat Transfer for Low Grade Energy, North China Electric Power University, Beijing 102206, China Beijing Key Laboratory of Multiphase Flow and Heat Transfer for Low Grade Energy, North China Electric Power University, Beijing 102206, ChinaThe carbon/carbon (C/C) composites are composed of carbon fibers, carbon matrix, and pores and cracks, which have been successfully used in various aerospace applications. In this paper, nanoscale submodel is proposed to describe the thermal conductivity of the matrix based on its microscopic structure, and then the submodel is incorporated into a microscale model to analytically predict the equivalent thermal conductivities of the composites by equivalent circuit approach. The results predicted by the present model agree well with those from the experimental measurements. Based on the model, the effects of the composite porosity as well as the thickness and porosity of the interface phase on the thermal performance of five composites are studied. It is found that the thermal conductivities show decreasing trends in responding to an increase in each of the three parameters. The composite porosity has a significant effect on the thermal conductivities both parallel and transverse to the fiber axis, while the thickness and the porosity of the interface phase remarkably affect the thermal conductivity only transverse to the fiber axis.https://doi.org/10.1155/2014/242586
collection DOAJ
language English
format Article
sources DOAJ
author Zhi-Hai Feng
Jia-Yun Zhi
Zhen Fan
Duo Sun
Chao Si
Xiao-Dong Wang
spellingShingle Zhi-Hai Feng
Jia-Yun Zhi
Zhen Fan
Duo Sun
Chao Si
Xiao-Dong Wang
An Analytical Model of Thermal Conductivity for Carbon/Carbon Composites with Pitch-Based Matrix
Advances in Mechanical Engineering
author_facet Zhi-Hai Feng
Jia-Yun Zhi
Zhen Fan
Duo Sun
Chao Si
Xiao-Dong Wang
author_sort Zhi-Hai Feng
title An Analytical Model of Thermal Conductivity for Carbon/Carbon Composites with Pitch-Based Matrix
title_short An Analytical Model of Thermal Conductivity for Carbon/Carbon Composites with Pitch-Based Matrix
title_full An Analytical Model of Thermal Conductivity for Carbon/Carbon Composites with Pitch-Based Matrix
title_fullStr An Analytical Model of Thermal Conductivity for Carbon/Carbon Composites with Pitch-Based Matrix
title_full_unstemmed An Analytical Model of Thermal Conductivity for Carbon/Carbon Composites with Pitch-Based Matrix
title_sort analytical model of thermal conductivity for carbon/carbon composites with pitch-based matrix
publisher SAGE Publishing
series Advances in Mechanical Engineering
issn 1687-8132
publishDate 2015-01-01
description The carbon/carbon (C/C) composites are composed of carbon fibers, carbon matrix, and pores and cracks, which have been successfully used in various aerospace applications. In this paper, nanoscale submodel is proposed to describe the thermal conductivity of the matrix based on its microscopic structure, and then the submodel is incorporated into a microscale model to analytically predict the equivalent thermal conductivities of the composites by equivalent circuit approach. The results predicted by the present model agree well with those from the experimental measurements. Based on the model, the effects of the composite porosity as well as the thickness and porosity of the interface phase on the thermal performance of five composites are studied. It is found that the thermal conductivities show decreasing trends in responding to an increase in each of the three parameters. The composite porosity has a significant effect on the thermal conductivities both parallel and transverse to the fiber axis, while the thickness and the porosity of the interface phase remarkably affect the thermal conductivity only transverse to the fiber axis.
url https://doi.org/10.1155/2014/242586
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