期刊文献+

聚酯纤维布增强环氧树脂基复合材料的拉伸和摩擦学性能 被引量:5

Tensile and Tribological Properties of Polyester Fiber Reinforced Epoxy Resin Composites
下载PDF
导出
摘要 采用层压法制备了四种聚酯纤维布增强环氧树脂基复合材料,研究了不同填充物(纳米Al2O3颗粒和PTFE)对不同织物取向复合材料拉伸性能和摩擦磨损性能的影响,分析了拉伸断口和摩损表面的形貌。结果表明:加入PTFE使复合材料的经向和纬向的拉伸强度和弹性模量分别提高了1.4%,11.2%和31.5%,22.1%,纳米Al2O3颗粒的加入使复合材料的经向和纬向的拉伸强度和弹性模量分别提高了4.2%,14.2%和34.9%,26.3%;PTFE和纳米Al2O3均能提高复合材料的耐磨损性能,PTFE的加入使复合材料的摩擦因数降低了22.5%、磨损率减少了78.1%,Al2O3的加入使复合材料的摩擦因数增加了21.3%、磨损率减少了94.1%。 Four fiber reinforced epoxy resin composites were prepared by laminating method. The influence of different fillers of nano-particles and PTFE on the tensile and tribological properties of the composites with different fabric orientations was studied. The mierographs of tensile fracture and friction surfaces of the composites were also analyzed. The retults show that the tensile strength and modulus in warp and weft directions of the composites with the addition of PTFE increased 1. 4%, 11. 2% and 31. 5%, 22. 1% respectively. While the same properties increased 4. 2%, 14. 2% and 34. 9%, 26. 3% with the addition of Al2O3 nano-particles respectively. The tribological properties of the composites could be improved. The friction coefficient was reduced by 22. 5% by filling PTFE whereas the same property of Al2O3-filled composite was increased by 21.3%. The wear rate was reduced by 78. 1% by filling PTFE and the same property was reduced by 94. 1% by filling Al2O3.
出处 《机械工程材料》 CAS CSCD 北大核心 2010年第3期61-65,69,共6页 Materials For Mechanical Engineering
基金 上海市科学技术发展基金资助项目(072012027)
关键词 聚酯纤维 环氧树脂基复合材料 拉伸性能 摩擦学性能 polyester fiber epoxy resin composite tensile property tribological property
  • 相关文献

参考文献13

  • 1ZHENG L Y, ZHAO L X, ZHANG J J, et al. Frietion and wear properties of three-dimensionally braided carbon fabric- reinforced nylon eomposites[J]. Carbon, 2006,44 : 158-193. 被引量:1
  • 2CALLUS P J, MOURITZ A P, BANNISTER M K, et al. Tensile properties and failure mechanisms of 3D woven GRP composites[J]. Compos Part A, 1999,30:1277-1287. 被引量:1
  • 3FUJII T, AMIJIMA S, OKUBO K. Microscopic fatigure process in plain weave glass fibre composites[J]. Comp Sci Tech, 1993,49 (4) : 327-333. 被引量:1
  • 4RODRIGUEZ J, CHOCRON IS, MARTINEZ MA, et al. High strain rate properties of aramid and polyethylene woven fabric composites[J]. Compos Part B, 1996,27:147-154. 被引量:1
  • 5NAIK R A. Failure analysis of woven and braided fabric rein- forced composites [J].Compos Mater, 1995, 29 ( 17 ) : 2334- 2363. 被引量:1
  • 6MUNIKENCHE G T, NAIDU A C B, CHHAYA R. Some mechanical properties of untreated jute fabric-reinforced polyester composites[J].Compos Part A, 1999,30 : 277-284. 被引量:1
  • 7RATTAN R, BIJWE J, FAHIM M. Influence of weave of carbon fabric on low amplitude ozeillating wear performance of Polyetherimide eomposites[J]. Wear, 2007,262 : 727-735. 被引量:1
  • 8BUWE, INDUMATHI J, GHOSH A K. Influence of weave of glass fabric on the oscillating wear performance of polyetherimide (PEI) composites[J]. Wear, 2002,253 : 803-812. 被引量:1
  • 9BIJWE J, INDUMATHI J, GHOSH A K. Influence of orientation and volume fraction of aramid fabric on abrasive wear performance of polyethersulfone composites[J]. Wear, 2006, 260:401-411. 被引量:1
  • 10BURRIS D L, SAWYER W G. Improved wear resistance in alumina-PTFE nanocomposites with irregular shaped nanoparticles[J]. Wear, 2006,260 : 915-918. 被引量:1

二级参考文献6

共引文献7

同被引文献41

  • 1程起有,姚磊江,童小燕,吕胜利.补片尺寸对复合材料胶接修理性能的影响[J].飞机设计,2004,24(3):31-33. 被引量:22
  • 2ZHENG L Y, ZHAO L X, ZHANG J J,et al. Friction and wear properties of three-dimensionally braided carbon fabric reinforced nylon eomposites[J]. Carbon, 2006,44 : 158-193. 被引量:1
  • 3NAIK R A. Failure analysis of woven and braided fabric reinforced composites [J]. Compos Mater, 1995, 29 ( 17 ): 2334- 2363. 被引量:1
  • 4BIJWE J, INDUMATHI J, GHOSH A K. Influence of orientation and volume fraction of Aramid fabric on abrasive wear performance of polyethersulfone composites [J]. Wear, 2006, 260:401-411. 被引量:1
  • 5GB3357-1982.单向纤维增强塑料层间剪切强度试验方法[S].[S].,.. 被引量:2
  • 6JONES J S, GRAVES S R. Repair technique for Celion/LARC- 160 graphite/polyimide composite structures[M]. Washington D C: National Aeronautics and Space Administration, Scientif ic and Technical Information Branch, 1984. 被引量:1
  • 7OKAFOR C A, SINGH N, ENEMUOH U E, et al. Design analysis and performance of adhesively bonded composite patch repair of cracked aluminum aircraft panels [J]. Composite Structures, 2005,71 (2) : 258-270. 被引量:1
  • 8OUINASD, HEBBARA, BACHIR, etal. Numerical analysis of the stress intensity factors for repaired cracks from a notch with bonded composite semicircular patch [J]. Composites, 2009,40 (6) : 804-810. 被引量:1
  • 9OUDAD W, BOUIADJRA B B, BELHOUARI M, et al. A- nalysis of the plastic zone size ahead of repaired cracks with bonded composite patch of metallic aircraft structures [J]. Computational Materials Science, 2009,46 (5) : 950-954. 被引量:1
  • 10曲建俊,曲焱炎,肖殿东.超声马达各向异性摩擦材料性能的试验研究[J].润滑与密封,2007,32(11):133-136. 被引量:15

引证文献5

二级引证文献12

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部