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高强铝合金-PTFE纺织复合材料的摩擦磨损性能

Friction and Wear Properties of a High Strength Al Alloy-PTFE Fabric Composite

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【作者】 舒伟才向定汉

【Author】 Shu Weicai Xiang Dinghan (College of Materials Science and Technology,Nanjing University of Aeronautics and Astronautics,Nanjing Jiangsu 210016,China)

【机构】 南京航空航天大学材料科学与技术学院南京航空航天大学材料科学与技术学院 江苏南京210016江苏南京210016

【摘要】 将PTFE纺织复合材料粘结到高强铝合金背衬上,制备成铝合金-PTFE纺织复合材料。选择航空工业常用的3层复合材料(DU)作对比实验。摩擦磨损实验在摆动实验机上完成,实验条件为:载荷为10~80MPa,摆动频率8次/min,摆角为±30°,相对湿度(70±5)%。实验结果证实铝合金-PTFE纺织复合材料的摩擦因数大约0.055,摆动磨损寿命大约2.5万次,均优于DU材料。可见,这种高比强的新型复合材料适用于航空航天工业。

【Abstract】 An Al alloy-PTFE fabric composite was prepared,which is composed of polytetrafluoroethylene (PTFE) fabric as the matrix,and adhesive resin as the binder,and is cohered onto a high strength Al alloy support.Another kind of steel-bronze-PTFE composite (DU) was selected as a comparative investigation.Friction and wear tests were carried out in an oscillating tribo-tester.Experimental conditions were normal pressure from 10 to 90 MPa,an oscillating frequentcy of 8 times per minute,oscillating angles of ±30° and relative humidity of (70±5)%.The result shows that the Al alloy-PTFE fabric composite exhibits a lower coefficient of friction and longer oscillating wear life of 25 000 times than DU.So it is feasible that the newly high specific strength composite is applied in aerospace.

【基金】 航空科学基金项目(04G52044)
  • 【文献出处】 润滑与密封 ,Lubrication Engineering , 编辑部邮箱 ,2007年03期
  • 【分类号】TB333
  • 【被引频次】4
  • 【下载频次】250
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