期刊文献+

碳纤维/环氧预浸料摩擦滑移特性测试及其变化规律 被引量:8

Measurement and evolution of frictional slipping behavior of carbon fiber/epoxy prepreg
原文传递
导出
摘要 带曲率的复合材料层合结构在制备过程中,预浸料铺层之间、预浸料铺层与模具之间会发生摩擦滑移行为,其滑移程度影响复合材料的制造质量。本文采用自行建立的预浸料摩擦滑移特性测试装置,针对碳纤维/环氧树脂预浸料体系,测试分析了不同工艺条件下,预浸料铺层与铺层之间,以及预浸料铺层与钢模具、铝模具和橡胶模具材料之间的摩擦滑移特性。实验结果表明,温度变化会改变预浸料铺层间的摩擦机制,而外压变化不改变预浸料铺层间的摩擦机制;较高的温度或较小的外加压力会减小预浸料铺层的摩擦阻力,有利于预浸料铺层的滑移运动;预浸料铺层与模具材料之间的摩擦滑移特性与模具材料的表面粗糙度有关,其摩擦阻力受温度影响更明显,而受外压影响变化较小。 During fabricating curved composite laminate, frictional slipping processes in prepreg stack and between prepreg and mold occur. The slipping degree has significant effect on the manufacturing quality of composite. In this paper, a testing device was established to evaluate the frictional slipping behavior of prepreg systems. By means of this equipment, the frictional resistances of carbon fiber/epoxy prepreg and prepreg and prepreg and tool materials, including steel, aluminum and rubber, under different processing parameters were analyzed. The experimeantal results indicate that the change of temperature can alter the frictional mechanism in prepreg stack, while the variation of exteral pressure does not change the frictional mechanism in prepreg stack. High temperature and low external pressure decrease the frictional resistance in prepreg stack, and further the slipping behavior. In addition, the surface roughness of tool material has great effect on the rictional slipping property between prepreg and tool, and the frictional resistance is influenced by the temperature rather than the external pressure.
出处 《复合材料学报》 EI CAS CSCD 北大核心 2014年第1期101-106,共6页 Acta Materiae Compositae Sinica
基金 国家商用飞机制造工程技术研究中心新基金(SAMC12-JS-15-010)
关键词 树脂基复合材料 碳纤维预浸料 模具 层间滑移 摩擦阻力 polymer matrix composite carbon fiber prepreg mold interply slippage frictional resistance
  • 相关文献

参考文献12

  • 1谢富原,王雪明,李敏,张佐光.T形加筋板热压罐成型过程压力分布与树脂流动实验研究[J].复合材料学报,2009,26(6):66-71. 被引量:16
  • 2张丽华,范玉青.复合材料在飞机上的应用评述[J].航空制造技术,2006,49(3):64-66. 被引量:45
  • 3Johnston A, Vaziri R, Poursartip A. A plane strain model for process- induced deformation of laminated composite structures [J]. Journal of Composite Materials, 2001, 35 (16), 1435-1469.
  • 4Mallon P J, O'Bratdaigh C M. Deveplopment of a pilot autoclave for polymeric diaphragm forming of continuous fiber reinforced thermoplactics [J]. Composite, 1988, 19(1): 37-47.
  • 5Twigg G, Poursatip A, Ferlund G. Tool-part interaction in composite processing. Part L. experimental investigation and analytical model [J]. Composite Part A, 2004, 35(1) : 121- 133.
  • 6Twigg G, Poursatip A, Ferlund G. Tool-part interaction in composite processing. Part Ⅱ: numerical modeling [J]. Composite Part A, 2004, 35(1), 135-141.
  • 7Martin C J, Seferis J C, Wilhelm M A. Frictional resistance of thermaset prepregs and its influence on honeycomb composite processing [J]. Composite Part A, 1996, 27(10): 943-951.
  • 8Fernlund G, Rahman N, Courdji R. Experimental and numerical study of the effect of cure cycle, tool surface, geometry, and lay-up on the dimentional fidelity of autoclave -processed composite parts [J]. Composite Part A, 2002, 33 (3) : 341-351.
  • 9Khoun L, Hubert P. Investigation of the dimensional stability of carbon epoxy cylinders manufactured by resin transfer moulding [J] . Composite Part A, 2010, 41(1) : 116-124.
  • 10Kaushik V, Raghavan J. Experimental study of tool- part interaction during autoclave processing of thermoset polymer composite structures [J]. Composite Part A, 2010, 41 (9) : 1210-1218.

二级参考文献4

共引文献59

同被引文献48

  • 1王晓洁,梁国正,张炜,尤丽虹,谢群炜.高性能碳纤维表面分析及其力学性能研究[J].航空材料学报,2006,26(4):119-122. 被引量:10
  • 2马立敏,张嘉振,岳广全,刘建光,薛佳.复合材料在新一代大型民用飞机中的应用[J].复合材料学报,2015,32(2):317-322. 被引量:210
  • 3元振毅,王永军,张跃,杨选宏,王俊彪,魏生民.基于材料性能时变特性的复合材料固化过程多场耦合数值模拟[J].复合材料学报,2015,32(1):167-175. 被引量:28
  • 4杜善义.先进复合材料与航空航天[J].复合材料学报,2007,24(1):1-12. 被引量:1019
  • 5Nyman P, Mki R, Olsson R, et al. Influence of surface to- pography on friction characteristics in wet clutch applica- tions[J]. Wear,2006,26] (1) ..46-52.
  • 6Ingram M,Spikes H ,Noles J ,et al. Contact properties of a wet clutch friction materialEJl. Tribology International, 2010,43(4) :815-821.
  • 7Kadiyala A K, Bijwe J. Surface lubrication of graphite fab- ric reinforced epoxy composites with nano-and micro sized hexagonal boron nitride[J]. Wear, 2013,301 (1) : 802-809.
  • 8Sharma M, Bijwe J, Mitsehang P. Wear perform-ance of PEEK-carbon fabric composites with strengthened fiber- matrix interface[J]. Wear,2011,271(9):2 261-2 268.
  • 9Fei J,Li H J,Fu Y W,et al. Effect of phenolic resin con- tent on performance of carbon fiber re-inforced paper- based friction material[J]. Wear,2010,269(7) ,534-540.
  • 10Liu Y, Jing X. Pyrolysis and structure of hyper-branched polyborate modified phenolic resins[J]. Carbon, 2007,45 (10):1 965 1 971.

引证文献8

二级引证文献34

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