首页> 外文会议>SAE AeroTech Congress Exhibition >Fail Safe Drilling of CFRP/Titanium and /Aluminium Stack with H8 Quality for Aerospace Applications
【24h】

Fail Safe Drilling of CFRP/Titanium and /Aluminium Stack with H8 Quality for Aerospace Applications

机译:用于航空航天应用的H8质量的CFRP /钛和/铝堆栈的防止安全钻孔

获取原文

摘要

Ever since the advent of fiber reinforced polymer materials in the field of Aerospace, Metal-FRP stacks started to gain importance due to their superior fatigue performance, phenomenal low weight and good specific strength. However the machining, specially drilling these multi stack materials has always proved to be a challenge for the field of manufacturing and assembly. Drilling holes in only metal with a drill (metal drill), the material removal is through a process of clear shearing since the tool is much harder and sharper than the base material. The tools hence wears at a much slower and gradual rate, also the malleable properties of the machined metal compensate to the reduced cutting capability of the worn out drill. These properties of the machined metal act like a ‘FAIL SAFE’ mechanism during the machining process assuring a trouble free fail safe environment during the drilling process. However, drilling FRP composites is altogether a different story. The very properties that make the FRP composite superior make it a challenge for machining. The mechanism of machining viewed here is more or less fracturing and breakage of the fibers present in the system. This breakage of fiber also induces fractures in the tool resulting in accelerated tool wear. These characteristics render the process unreliable. Also the temperature during the machining of composites is higher than while machining a metal due to the lower thermal conductive properties of the composite. When two such extremely different elements are brought together in the form of a FRP-Metal stack, various challenges are faced to achieve required hole size, quality, tool life and most of all a FAIL SAFE Process. This article elaborates about methods to achieve a FAIL SAFE process during the drilling of CFRP/Titanium and Aluminum stacks just by adding and optimizing certain geometric features to the drill. The article also goes through simplified theoretic models which show how CFRP/Titanium stacks should be machined “Fail Safe”, inside the required Cpk tolerance, without scratches and burn marks even when the drill is during its last stages its life. The concept of Micro Reamer Technology (patented by MAPAL) is discussed and the application of this technology to achieve the required hole quality, burr and other important parameters is elaborated. The only apparent indicator for the end of tool life would be a linear increase in the burr height.
机译:自从航空航天领域的纤维增强聚合物材料的出现以来,由于其卓越的疲劳性能,高重量和良好的特异性强度,金属FRP堆栈开始升高。然而,采用电加工,特别钻孔这些多堆材料一直被证明是制造领域的挑战。仅使用钻头(金属钻)的金属钻孔(金属钻),材料去除是通过透明剪切的过程,因为该工具比基材更难以且更清晰。因此,工具以较慢且逐渐速度的速度磨损,也是加工金属的可延伸性能补偿了磨损钻头的减小的切割能力。在加工过程中,加工金属的这些性能起到“故障安全”机制,确保在钻井过程中无故障防止安全环境。但是,钻井FRP复合材料完全是不同的故事。使FRP复合材料优越的性质使其成为加工的挑战。这里观察的加工机理或多或少地是系统中存在的纤维的压裂和破裂。这种纤维的破裂也诱导工具中的骨折导致加速的工具磨损。这些特性使过程不可靠。同样在复合材料加工过程中的温度高于加工由于复合材料的较低的导热性能而加工金属。当两个这样极不同的元素以FRP金属堆叠的形式聚集在一起时,面临各种挑战以实现所需的孔尺寸,质量,刀具寿命,以及所有故障安全过程中的大部分。本文阐述了通过添加和优化钻头的某些几何特征来实现CFRP /钛和铝合金堆栈期间实现无CFRP /钛和铝堆的方法的方法。本文还通过了简化的理论模型,该模型显示了CFRP /钛堆栈应该如何加工“失败安全”,即使钻头在其最后阶段期间,也没有划痕和烧伤标记。讨论了微铰刀技术(Mapal专利)的概念,并阐述了该技术的应用来实现所需的孔质量,毛刺和其他重要参数。刀具寿命结束的唯一明显的指示器将是毛刺高度的线性增加。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

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