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首页> 外文期刊>International Journal of Computer Integrated Manufacturing >High-speed ball nose end milling of burn-resistant titanium (BuRTi) alloy
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High-speed ball nose end milling of burn-resistant titanium (BuRTi) alloy

机译:耐火钛(BuRTi)合金的高速球头立铣

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摘要

Following a brief introduction to aero-engine materials and the development of BuRTi alloy (Ti-25V-15Cr-2Al-0.2C), the paper details a statistically designed machinability experiment involving high-speed ball end milling. Testing utilised 8 mm diameter AlTiN-coated carbide ball nose end mills in a Taguchi L8 fractional factorial design with six factors, each at two levels. Output measures related to tool life/wear, cutting forces, workpiece surface roughness, microstructure and microhardness. Main effect plots, tabulated ANOVA data, percentage contribution ratio (PCR) values together with graphical and SEM data are presented. Use of the lowest material removal rate, high-pressure (70 bar) cutting fluid and a workpiece orientation of 45° resulted in the longest tool life with a machining time of ~60 min; however, surface roughness was poor, and there was smeared/adhered material to a depth of 20 μm. Additionally, carbide fracture/pull-out was observed near the workpiece surfaces whereas microhardness depth profiles from sectioned, mounted and polished samples showed a moderate increase in surface hardness of ~80HK0.25 above the bulk value.
机译:在简要介绍了航空发动机材料和BuRTi合金(Ti-25V-15Cr-2Al-0.2C)的发展后,本文详细介绍了统计设计的可加工性实验,其中涉及高速球头铣削。测试在Taguchi L8分数阶乘设计中使用了8毫米直径的AlTiN涂层硬质合金球头立铣刀,具有六个因子,每个因子有两个等级。输出量度与刀具寿命/磨损,切削力,工件表面粗糙度,显微组织和显微硬度有关。介绍了主要效果图,列表化的方差分析数据,百分比贡献率(PCR)值以及图形和SEM数据。使用最低的材料去除率,高压(70 bar)切削液和45°的工件定向可实现最长的刀具寿命,加工时间约为60分钟;然而,表面粗糙度差,并且涂污/粘附的材料的深度为20μm。此外,在工件表面附近观察到碳化物断裂/拉出,而切片,安装和抛光样品的显微硬度深度分布表明,表面硬度在整体值之上适度增加了〜80HK0.25。

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