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Abrasive Waterjet Contour Cutting of Thick Titanium/Graphite Laminates.

机译:厚钛/石墨层压板的磨料水刀轮廓切割。

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摘要

One of the primary focus in aerospace industry is the reduction of buy-to-fly ratio. Although TiGr laminates are molded/autoclaved to a near net shape, secondary machining such as drilling, peripheral machining and contouring is often unavoidable. Machining of composites alone poses a great challenge which becomes more challenging in a three phase material system---hybrid composites, where the non-homogeneity and anisotropy of composites together with the difference in the removal mechanism for all the three different phases aggravate the machining problem.;An investigation was conducted to evaluate the feasibility and machinability of contouring thick TiGr through Abrasive Waterjet (AWJ) in terms of kerf characteristics---taper ratio and surface quality. A cutting geometry with different profile curvatures was machined with conditions according to a response surface experimental design obtained using Design Expert software. The process variables included pump pressure, jet traverse speed, load ratio (by varying abrasive flow rate) and nozzle dimensions. Material removal mechanism was studied for three different phase material systems. Kerf taper ratio was investigated to qualitatively characterize superior and inferior quality cuts. Topological characteristics of the kerf were also studied with roughness evaluation of surfaces parallel (longitudinal) and orthogonal (transverse) to jet traverse direction. Analysis of Variance (ANOVA) was used to statistically characterize the effect of operating variables on kerf taper ratio. Predictive mathematical models were developed for taper ratio and transverse roughness R z, whereas semi-analytical model was developed to predict Average transverse roughness Ra. The AWJ process was characterized using Skewness-Kurtosis and Rq/Ra ratio of the kerf profile. Overall, machinability of thick TiGr laminates was evaluated as a function of kerf taper ratio and surface roughness and statistical optimization was done for machining with low taper and low roughness.
机译:航空航天业的主要关注点之一是降低购机率。尽管将TiGr层压板模制/高压灭菌成接近最终的形状,但通常不可避免地需要进行二次加工,例如钻孔,周边加工和轮廓加工。仅复合材料的加工就构成了巨大的挑战,这在三相材料系统中变得更加具有挑战性,即混合复合材料,复合材料的非均质性和各向异性以及所有三个不同相的去除机理的差异加剧了机械加工进行了一项研究,以从切缝特征-锥度比和表面质量的角度评估通过磨料水刀(AWJ)加工厚TiGr的可行性和可加工性。根据使用Design Expert软件获得的响应面实验设计,在一定条件下加工具有不同轮廓曲率的切削几何形状。工艺变量包括泵压力,喷射速度,负载比(通过改变磨料流速)和喷嘴尺寸。研究了三种不同相材料系统的材料去除机理。研究了Kerf锥度比,定性地表征了优质和劣质的切块。还通过对平行于(纵向)和与射流横向正交(横向)的表面进行粗糙度评估,研究了切缝的拓扑特性。方差分析(ANOVA)用于统计表征操作变量对切缝锥度比的影响。开发了锥度比和横向粗糙度R z的预测数学模型,而开发了半分析模型以预测平均横向粗糙度Ra。 AWJ过程的特征是通过偏度-峰度和切口轮廓的Rq / Ra比进行表征。总的来说,评估厚TiGr层压板的可加工性是切缝锥度比和表面粗糙度的函数,并针对低锥度和低粗糙度的加工进行了统计优化。

著录项

  • 作者

    Pahuja, Rishi.;

  • 作者单位

    University of Washington.;

  • 授予单位 University of Washington.;
  • 学科 Mechanical engineering.;Aerospace engineering.
  • 学位 Masters
  • 年度 2015
  • 页码 253 p.
  • 总页数 253
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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