Transient thermoelastic analysis of carbon/carbon composite multidisc brake using finite element method

被引:2
|
作者
Ghashochi-Bargh, Hadi [1 ]
Goodarzila, Mohammad-Saeed [1 ]
Karimi, Masoud [2 ]
Salamat-Talab, Mazaher [3 ]
机构
[1] Buein Zahra Tech Univ, Dept Ind Mech & Aerosp Engn, Buein Zahra, Qazvin, Iran
[2] Amirkabir Univ Technol, Dept Aerosp Engn, Tehran, Iran
[3] Arak Univ Technol, Dept Mech Engn, Arak, Iran
来源
关键词
thermoelastic; C/C composite brake system; finite element method; THERMAL-ANALYSIS; AIRCRAFT BRAKING; DISC; TEMPERATURE; BEHAVIOR; STRESSES;
D O I
10.12989/aas.2020.7.2.135
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In the current paper, a generalization of the results of Zhao et al. (2008) on a new design of C/C composite multidisc brake system is presented. The purpose of this paper is to study the effect of thermal sensitivity of Carbon/Carbon (C/C) composite material on the temperature distributions, deformation, and stress during braking. In this regard, a transient temperature-displacement coupled analysis for C/C composite brake discs with frictional heat generation under simulated operating conditions is performed. An axisymmetric model for brake system is used for the finite element analysis according to the them of energy transformation and transportation. The transient temperature distributions on the friction surfaces, deformation, and stress are obtained. To check the validity, the results are corroborated with other solutions available in the literature, wherever possible. The current study could be used as a guide in the initial design of a high performance multidisc brake system.
引用
收藏
页码:135 / 149
页数:15
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