C/C复合材料与石墨材料干态摩擦磨损行为

TRIBOLOGY PROPERTIES OF C/C COMPOSITES AND GRAPHITE AT NON-LUBRICATION WEAR ENVIRONMENT

  • 摘要: 在M-2000型摩擦磨损实验机上,以GCr15钢为配副,对石墨材料和C/C复合材料在干态条件下的滑动摩擦进行研究。结果表明:C/C复合材料的摩擦系数和体积磨损均比石墨材料的低。具有光滑层炭结构 (SL) 的C/C复合材料的摩擦系数和体积磨损量比具有粗糙层结构 (RL) 的C/C复合材料低;低密度石墨的摩擦系数和体积磨损量比高密度石墨材料高。随时间延长,RL结构的C/C复合材料摩擦系数在60、80、200 N时有小幅度的增长,另三种则下降; SL结构的C/C复合材料摩擦系数除60 N外基本保持平稳;石墨材料的摩擦系数随时间延长表现出增长趋势。SEM观察表明: RL结构的C/C复合材料摩擦表面随载荷增加而趋向完整,SL结构的C/C复合材料的摩擦表面随载荷增加变化不大。而高密度石墨摩擦表面比密度低的石墨完整。C/C复合材料比石墨更适宜用作航空发动机轴间密封材料。

     

    Abstract: Using the M-2000 tribology machine, without lubrication, the tribology properties of two kinds of graphite and two kinds of C/C composites were studied with GCr15 steel as couple. The results show that C/C composites own the lower friction coefficient and bulk worn loss than the graphite. Both the friction coefficient and bulk worn loss of C/C composites with the smooth lamination(SL) carbon matrix structure are lower than the two of C/C composites with rough lamination (RL) structure. The low density graphite gets higher friction coefficient and bulk worn loss than the high density graphite. With time prolonging, the friction coefficient of RL C/C composites increased under 60 N,80 N and 200 N while others decreased. But the friction coefficient of SL C/C composites decreased except 60 N and changed a little, and that of two kinds of graphite increased. The SEM show that the friction film of RL C/C composites becomes more integrate with increasing load, while that changes only a little of SL C/C composites. The friction film of high density graphite is more integrate than the low density graphite. C/C composites have advantage over graphite used as the seal ring of the main axis of turbine engine for airplane.

     

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