首页> 外文OA文献 >Drilling thick fabric woven CFRP laminates with double point angle drills
【2h】

Drilling thick fabric woven CFRP laminates with double point angle drills

机译:用双点角钻钻孔加工厚织物编织CFRP层压板

代理获取
本网站仅为用户提供外文OA文献查询和代理获取服务,本网站没有原文。下单后我们将采用程序或人工为您竭诚获取高质量的原文,但由于OA文献来源多样且变更频繁,仍可能出现获取不到、文献不完整或与标题不符等情况,如果获取不到我们将提供退款服务。请知悉。

摘要

Carbon fiber reinforced plastics (CFRPs) have many desirable properties, including high strength-to-weight ratio, high stiffness-to-weight ratio, high corrosion resistance, and low thermal expansion. These properties make CFRP suitable for use in structural components for aerospace applications. Drilling is the most common machining process applied to CFRP laminates, and it is difficult due to the extremely abrasive nature of the carbon fibers and low thermal conductivity of CFRP. It is a challenge for manufacturers to drill CFRP materials without causing any delamination on the work part while also considering the economics of the process. The subject of this study is the drilling of fabric woven type CFRP laminates which are known to be more resistant to delamination than unidirectional type CFRP laminates. The objective of this study is to investigate the influence of double point angle drill geometry on drilling performance through an experimental approach. An uncoated carbide and two diamond coated carbide drills with different drill tip angles are employed in drilling experiments of aerospace quality thick fabric woven CFRP laminates. Force and torque measurements are used to investigate appropriate drilling conditions based on drill geometry and ideal drilling parameters are determined. Tool life tests of the drills were conducted and the condition of the diamond coating is examined as a function of drilling operational parameters. High feed rate drilling experiments are observed to be favorable in terms of drill wear. Feed is observed to be more important than speed, and the upper limit of feed is dictated by the drill design and the rigidity of the machine drill. Hole diameter variation due to drill wear is monitored to determine drill life. At high feeds, hole diameter tolerance is observed to be more critical than hole exit delamination during drilling of fabric woven CFRP laminates. © 2012 Elsevier B.V.
机译:碳纤维增强塑料(CFRP)具有许多理想的特性,包括高强度重量比,高刚度重量比,高耐腐蚀性和低热膨胀性。这些特性使CFRP适用于航空航天应用的结构部件。钻孔是应用于CFRP层压板的最常见的机加工工艺,由于碳纤维的极具磨蚀性和CFRP的低导热性,很难进行钻孔。对于制造商而言,在不考虑工件经济性的前提下钻出CFRP材料而又不会在工件上产生任何分层是一个挑战。这项研究的主题是织物编织型CFRP层压板的钻孔,该层压板比单向CFRP层压板更耐分层。本研究的目的是通过实验方法研究双点角钻头几何形状对钻削性能的影响。在航空航天质量的厚织物编织CFRP层压板的钻孔实验中,使用了未涂覆的硬质合金钻头和两个具有不同钻尖角的金刚石涂覆的硬质合金钻头。力和扭矩测量用于根据钻头几何形状研究合适的钻削条件,并确定理想的钻削参数。进行了钻头的刀具寿命测试,并检查了金刚石涂层的状况与钻削操作参数的关系。观察到高进给速度的钻探实验在钻头磨损方面是有利的。观察到进给比速度更重要,进给的上限由钻头的设计和机械钻的刚度决定。监测由于钻头磨损引起的孔径变化,以确定钻头寿命。在高进给率下,观察到孔直径公差比在机织CFRP层压板钻孔时孔出口分层更为关键。 ©2012 Elsevier B.V.

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
代理获取

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