留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

碳纤维/酚醛树脂体系Z-pin加捻拉挤工艺及其性能

张向阳 李勇 褚奇奕 李吻

张向阳, 李勇, 褚奇奕, 李吻. 碳纤维/酚醛树脂体系Z-pin加捻拉挤工艺及其性能[J]. 航空动力学报, 2015, 30(7): 1638-1644. doi: 10.13224/j.cnki.jasp.2015.07.015
引用本文: 张向阳, 李勇, 褚奇奕, 李吻. 碳纤维/酚醛树脂体系Z-pin加捻拉挤工艺及其性能[J]. 航空动力学报, 2015, 30(7): 1638-1644. doi: 10.13224/j.cnki.jasp.2015.07.015
ZHANG Xiang-yang, LI Yong, CHU Qi-yi, LI Wen. Pultrusion and properties of the twisted carbon fiber/phenolic resin Z-pin[J]. Journal of Aerospace Power, 2015, 30(7): 1638-1644. doi: 10.13224/j.cnki.jasp.2015.07.015
Citation: ZHANG Xiang-yang, LI Yong, CHU Qi-yi, LI Wen. Pultrusion and properties of the twisted carbon fiber/phenolic resin Z-pin[J]. Journal of Aerospace Power, 2015, 30(7): 1638-1644. doi: 10.13224/j.cnki.jasp.2015.07.015

碳纤维/酚醛树脂体系Z-pin加捻拉挤工艺及其性能

doi: 10.13224/j.cnki.jasp.2015.07.015
详细信息
    作者简介:

    张向阳(1987-),女,河北唐山人,博士生,主要从事复合材料三维增强技术研究.

  • 中图分类号: V258;TB332

Pultrusion and properties of the twisted carbon fiber/phenolic resin Z-pin

  • 摘要: 为了解决碳纤维/酚醛树脂体系Z-pin拉挤制品中的孔隙缺陷,实现耐烧蚀复合材料三维增强体的制备,在分析孔隙的形成与酚醛树脂的固化过程基础上,利用纤维加捻提高酚醛树脂固化压力进而改善Z-pin中的孔隙缺陷.研究表明:一定范围内,随着纤维捻度的增加,孔隙缺陷的尺寸与数量明显减少,Z-pin中树脂质量分数及可植入深度逐渐降低,而Z-pin抗压性能先提高后降低;碳纤维捻度为80捻/m时,Z-pin制品质量较好,树脂质量分数约为32%,可满足后续超声植入,常温下最大植入深度可达10mm.

     

  • [1] Mouritz A P.Review of Z-pinned composite laminates[J].Composites Part A:Applied Science and Manufacturing,2007,38(12):2383-2397.
    [2] Cartie D D R.Effect of Z-fibers TM on the delamination behavior of carbon fiber/epoxy laminates[D].Cranfield:Cranfield University,2000.
    [3] 孙先念,郑长良.层合复合材料Z-pinning增强技术的力学进展[J].航空学报,2006,27(6):1194-1202. SUN Xiannian,ZHENG Changliang.Advances on modeling through-the-thickness reinforcement of laminated composite by Z-pinning[J].Acta Aeronautica et Astronautica Sinica,2006,27(6):1194-1202.(in Chinese)
    [4] Toral V J,Castanié B,Barrau J J,et al.Multi-level analysis of low-cost Z-pinned composite joints:Part 2 joint behavior[J].Composites Part A:Applied Science and Manufacturing,2011,42(12):2082-2092.
    [5] Byrd L W,Birman V.The estimate of the effect of Z-pins on the strain release rate,fracture and fatigue in a composite co-cured Z-pinned double cantilever beam[J].Composite Structures,2005,68(1):53-63.
    [6] Walker S P,Sullivan B J.Sharp refractory composite leading edges on hypersonic vehicles[R].AIAA 2003-6915,2003.
    [7] 李仲平.防热复合材料发展与展望[J].复合材料学报,2011,28(2):1-9. LI Zhongping.Major advancement and development trends of TPS composites[J].Acta Material Composite Sinica,2011,28(2):1-9.(in Chinese)
    [8] 赵梦熊.载人飞船返回舱的烧蚀防热[J].气动实验与测量控制,1996,10(3):1-9. ZHAO Mengxiong.Ablative thermal protection of capsule type re-entry vehicle[J].Aerodynamic Experiment and Measurement and Control,1996,10(3):1-9.(in Chinese)
    [9] 袁海根,曾金芳,杨杰,等.防热抗烧蚀复合材料研究进展[J].化学推进剂与高分子材料,2006,4(1):21-25. YUAN Haigen,ZENG Jinmei,YANG Jie,et al.Research progress of high temperature themoprotective and ablation resistant composite materials[J].Chemical Propellants and Polymeric Materials,2006,4(1):21-25.(in Chinese)
    [10] 李宁.Z-pin增强酚醛层合板制备工艺及性能研究[D].南京:南京航空航天大学,2012. LI Ning.Research on preparation process and mechanical properties of Z-pinned phenolic composite laminates[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2012.(in Chinese)
    [11] Kardos J L,Dudukovi Dc' M P,Dave R.Void growth and resin transport during processing of thermosetting-matrix composites[M].Berlin:Springer,1986.
    [12] 郭昕昕,刘永琪.拉挤用酚醛树脂固化过程的研究[J].纤维复合材料,1999,16(4):39-42. GUO Xinxin,LIU Yongqi.Research on the curing process of phenolic resin for pultrusion[J].Fiber Composites,1999,16(4):39-42.(in Chinese)
    [13] 顾平,管辛.粘胶长丝加捻线的形态特征与数学模型[J].纺织学报,2005,26(2):33-36. GU Ping,GUAN Xin.Morphology features and mathematical model of viscose twisted filament threads[J].Journal of Textile Research,2005,26(2):33-36.(in Chinese)
    [14] Partridge I K,Cartie D D R,Bonnington T.Manufacture and performance of Z-pinned composites[M]//Shonaike G,Advani S.Advanced Polymeric Composites.Florida:CRC Press,2003.
    [15] 王晓旭,陈利.复合材料Z-pin的压缩试验研究[J].航空材料学报,2011,31(4):90-95. WANG Xiaoxu,CHEN Li.Experimental studies on compressive properties of composite Z-pins[J].Journal of Aeronautical Materials,2011,31(4):90-95.(in Chinese)
    [16] Whitney J M.Geometrical effects of filament twist on the modulus and strength of graphite fiber-reinforced composites[J].Textile Research Journal,1966,36(9):765-770.
    [17] Rugg K L,Cox B N,Ward K E,et al.Damage mechanisms for angled through-thickness rod reinforcement in carbon-epoxy laminates[J].Composites Part A:Applied Science and Manufacturing,1998,29(12):1603-1613.
  • 加载中
计量
  • 文章访问数:  1170
  • HTML浏览量:  117
  • PDF量:  660
  • 被引次数: 0
出版历程
  • 收稿日期:  2014-01-20
  • 刊出日期:  2015-07-28

目录

    /

    返回文章
    返回