首页> 外文会议>International Symposium on Eco-Materials Processing and Design(ISEPD-8); 20070111-13; Kitakyushu(JP) >The Influence of Microstructure on the Friction Properties of Carbon/ Carbon Composites
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The Influence of Microstructure on the Friction Properties of Carbon/ Carbon Composites

机译:微观结构对碳/碳复合材料摩擦性能的影响

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Carbon/carbon (C/C) composites with smooth laminar texture pyrocarbon (SL), rough laminar texture pyrocarbon (RL) and RL pyrocarbon adding particle resin carbon were prepared, respectively. The open porosities of the composites were measured by Archimedes principle, and their mechanical and thermophysical properties were tested. The friction properties of the braking disc prepared from the three types C/C composites were tested at stimulating airplane braking conditions. The friction coefficient of the SL C/C composites with is 0.26 under normal landing condition. For the RL C/C composites with open porosity of 13%, the friction coefficients are 0.35, 0.24, 0.29 under normal landing (NL), rejected take-off (RTO), damp landing (DL) conditions, respectively. The friction coefficients of C/C composites with RL pyrocarbon adding particle resin carbon (open porosity is 8%) are 0.36, 0.31, 0.36 under NL, RTO, DL conditions, respectively. The results show that the RL pyrocarbon increases the friction coefficients of the C/C. The addition of particle resin carbon in the C/C increases the braking efficiency of C/C composites under high energy landing. Low porosity C/C has better braking efficiency under DL condition.
机译:分别制备了具有光滑层状热解碳(SL),粗糙层状热解碳(RL)和RL热解碳添加颗粒树脂碳的碳/碳(C / C)复合材料。通过阿基米德原理测量复合材料的开孔率,并测试其力学性能和热物理性能。在刺激的飞机制动条件下测试了由三种C / C复合材料制成的制动盘的摩擦性能。在正常着陆条件下,SL C / C复合材料的摩擦系数为0.26。对于开孔率为13%的RL C / C复合材料,在正常着陆(NL),拒收起飞(RTO)和潮湿着陆(DL)的条件下,摩擦系数分别为0.35、0.24、0.29。在NL,RTO和DL条件下,添加RL焦碳的颗粒树脂碳(开孔率为8%)的C / C复合材料的摩擦系数分别为0.36、0.31、0.36。结果表明,RL裂解碳增加了C / C的摩擦系数。在C / C中添加颗粒树脂碳可以提高C / C复合材料在高能着陆下的制动效率。低孔隙度C / C在DL条件下具有更好的制动效率。

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