CFRP/Al叠层结构制孔缺陷的有限元仿真
详细信息    查看全文 | 推荐本文 |
  • 英文篇名:Finite Element Analysis on Drilling Defects of Carbon Fiber Reinforced Plastic and Aluminum Stacks
  • 作者:黄树涛 ; 王浩涛 ; 张攀
  • 英文作者:HUANG Shutao;WANG Haotao;ZHANG Pan;School of Automobile and Traffic,Shenyang Ligong University;
  • 关键词:碳纤维复合材料 ; CFRP/Al叠层结构 ; 钻削仿真模型 ; 制孔缺陷
  • 英文关键词:carbon fiber reinforced plastic;;CFRP/Al Stacks;;drilling simulation model;;drilling defectss
  • 中文刊名:CLKX
  • 英文刊名:Journal of Materials Science and Engineering
  • 机构:沈阳理工大学汽车与交通学院;
  • 出版日期:2019-06-20
  • 出版单位:材料科学与工程学报
  • 年:2019
  • 期:v.37;No.179
  • 基金:沈阳航空航天大学国防重点学科实验室开放基金资助项目(SHSYS2016007);; 国家自然科学基金资助项目(51775356)
  • 语种:中文;
  • 页:CLKX201903027
  • 页数:9
  • CN:03
  • ISSN:33-1307/T
  • 分类号:155-162+166
摘要
应用Abaqus有限元仿真软件,建立了CFRP/Al钻削有限元仿真模型,对CFRP/Al钻孔过程中碳纤维复合材料的撕裂、分层损伤及毛刺的特征和形成机理进行了仿真研究,并进一步分析了切削速度、进给量对CFRP/Al叠层结构制孔缺陷的影响规律。结果表明:麻花钻横刃对碳纤维的拉伸作用是造成撕裂的主要原因;毛刺主要产生在纤维被切削时处于拉伸状态的区域,铝合金切屑对CFRP的划伤也是毛刺形成的原因之一;在CFRP/Al叠层结构制孔缺陷中分层损伤最显著,进给量和切削速度对出入口分层损伤成正相关且对入口处分层影响更大;在这种叠层结构中,铝合金板的支撑作用有效减小了碳纤维复合材料层出口的分层损伤。
        Building drilling CFRP/Al finite element simulation,which applied the finite element analysis software ABAQUS,had simulated the avulsion,delamination,characteristics of the burr and formation mechanism of carbon fiber reinforced plastic in the process of drilling CFRP/Al,and analyzed the influence which the cutting speed and feed had imposed on the drilling defects of CFRP/Al laminated construction.The results show that the tension effect caused by the chisel edge of twist drill is the main reason to cause avulsion of carbon fiber;the burr is mainly generated by cutting fibers in the area of tensile state,and the scratch of CFRP caused by aluminum alloy chips is also one of the reason of generating burr;the delamination damage is most obvious in the drilling defects of CFRP/Al laminated construction,and the cutting speed and feed have a positive correlation with the delamination damage of entrance and exit,and especially on the entrance;the support of aluminum alloy plate effectively reduces the delamination damage in the exit of carbon fiber composite material in this laminated construction.
引文
[1]郭玉琴,孙民航,杨艳,等.不同态碳纤维复合材料冲裁断裂行为[J].材料科学与工程学报,2015,33(3):362~367.
    [2]王帅,王隆宇,李多,等.碳纤维复合材料在汽车上的应用和发展[J].汽车实用技术,2017(15):170~172.
    [3]陈燕,葛恩德,傅玉灿,等.碳纤维增强树脂基复合材料制孔技术研究现状与展望[J].复合材料学报,2015,32(2):301~316.
    [4]Zitoune R,Krishnaraj V,Collombet F.Study of drilling of composite material and aluminium stack[J].Composite Structures,2010,92(5):1246~1255.
    [5]樊芊,张谦.CFRP/Al制孔分层临界轴向力研究[J].航空精密制造技术,2015(3):20~25.
    [6]温泉,郭东明,高航,等.基于划痕试验的碳纤维/环氧树脂复合材料制孔毛刺与撕裂缺陷形成机制[J].复合材料学报,2014,31(1):9~17.
    [7]Isbilir O,Ghassemieh E.Numerical investigation of the effects of drill geometry on drilling induced delamination of carbon fiber reinforced composites[J].Composite Structures,2013,105(8):126~133.
    [8]Isbilir O,Ghassemieh E.Finite Element Analysis of Drilling of Carbon Fibre Reinforced Composites[J].Applied Composite Materials,2012,19(3~4):637~656.
    [9]Phadnis V A,Makhdum F,Roy A,et al.Drilling in carbon/epoxy composites:Experimental investigations and finite element implementation[J].Composites Part A Applied Science and Manufacturing,2013,47(1):41~51.
    [10]金晓波,康万军,曹军,等.碳纤维复合材料/钛合金叠层板钻孔有限元仿真研究[J].工具技术,2015,49(1):24~28.
    [11]Giasin K,Hodzic A,Phadnis V,et al.Assessment of cutting forces and hole quality in drilling Al2024 aluminium alloy:experimental and finite element study[J].International Journal of Advanced Manufacturing Technology,2016,87(5~8):2041~2061.
    [12]NAN X H,XIE L J,ZHAO W X.On the application of 3Dfinite element modeling for small-diameter hole drilling of AISI1045 steel[J].The International Journal of Advanced Manufacturing Technology,2016,84(9~12):1927~1939.
    [13]Hillerborg A,M.Modéer,Petersson P E.Analysis of crack formation and crack growth in concrete by means of fracture mechanics and finite elements[J].Cement and Concrete Research,1976,6(6):773~781.

© 2004-2018 中国地质图书馆版权所有 京ICP备05064691号 京公网安备11010802017129号

地址:北京市海淀区学院路29号 邮编:100083

电话:办公室:(+86 10)66554848;文献借阅、咨询服务、科技查新:66554700