首页> 外文OA文献 >The effect of chisel length and associated pilot hole on delamination when drilling composite materials
【2h】

The effect of chisel length and associated pilot hole on delamination when drilling composite materials

机译:复合材料钻孔时凿子长度和相关的导向孔对分层的影响

摘要

[[abstract]]Drilling-induced delamination often occurs both at the entrance and the exit of the workpiece during drilling of composite material. Investigators have studied analytically and experimentally that delamination in drilling can be correlated to the thrust force of the drill. With a pre-drilled pilot hole, the delamination can be reduced significantly. Early reference reported models of drilling-induced delamination, however, the effect of chisel edge length and pilot hole diameter on delamination is rarely discussed. The optimal range of chisel edge length with respect to drill diameter is derived in this paper. © 2003 Elsevier Ltd. All rights reserved.
机译:[[摘要]]在复合材料的钻孔过程中,钻孔引起的分层经常发生在工件的入口和出口。研究人员已经进行了分析和实验研究,认为钻削时的分层可能与钻头的推力有关。通过预钻的导向孔,可以大大减少分层。早期的参考文献报道了钻孔引起的分层的模型,但是,很少讨论凿刃长度和导向孔直径对分层的影响。本文推导了刀刃长度相对于钻头直径的最佳范围。 ©2003 ElsevierLtd。保留所有权利。

著录项

  • 作者

    Tsao C.C.;

  • 作者单位
  • 年度 2010
  • 总页数
  • 原文格式 PDF
  • 正文语种 [[iso]]en
  • 中图分类

相似文献

  • 外文文献
  • 中文文献
  • 专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号