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首页> 外文期刊>The International Journal of Advanced Manufacturing Technology >Tool wear and surface quality in milling of a gamma-TiAl intermetallic
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Tool wear and surface quality in milling of a gamma-TiAl intermetallic

机译:γ-TiAl金属间化合物铣削中的刀具磨损和表面质量

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Advanced structural materials for high-temperature applications are often required in aerospace and automotive fields. Gamma titanium aluminides, intermetallic alloys that contain less than 60 wt.% of Ti, around 30-35 wt.% of aluminum, and other alloy elements, can be used as an alternative to more traditional materials for thermally and mechanically stressed components in aerospace and automotive engines, since they show an attractive combination of favorable strength-to-weight ratio, refractoriness, oxidation resistance, high elastic modulus, and strength retention at elevated temperatures, together with good creep resistance properties. Unfortunately such properties, along with high hardness and brittleness at room temperature, surface damage, and short and unpredictable tool life, undermine their machinability, so that gamma-TiAl are regarded as difficult to cut materials. A deeper knowledge of their machinability is therefore still required. In this context the paper presents the results of an experimental campaign aimed at investigating the machinability of a gamma titanium aluminide, of aeronautic interest, fabricated via electron beam melting and then thermally treated. Milling experiments have been conducted with varying cutting speed, feed, and lubrication conditions (dry, wet, and minimum quantity lubrication). The results are presented in terms of correlation between cutting parameters and lubrication condition with tool wear, surface hardness and roughness, and chip morphology. Tool life, surface roughness, and chirp morphology showed dependence on the cutting parameters. Lubrication conditions were observed to heavily affect tool wear, and minimum quantity lubrication was shown to be by far the method that allows to extend tool life.
机译:航空航天和汽车领域经常需要用于高温应用的高级结构材料。 γ-钛铝化物,含少于60%(重量)的Ti,约30-35%(重量)的铝和其他合金元素的金属间合金可用作航空航天中受热和机械应力的传统材料的替代品以及汽车发动机,因为它们具有良好的强度重量比,耐火度,抗氧化性,高弹性模量和高温下的强度保持性以及良好的抗蠕变性,具有吸引人的组合。不幸的是,这些性能以及在室温下的高硬度和脆性,表面损伤以及短而不可预测的工具寿命破坏了它们的可机械加工性,因此γ-TiAl被认为是难以切割的材料。因此仍然需要对它们的可加工性有更深的了解。在这种情况下,本文提出了一项实验研究的结果,旨在研究通过电子束熔化然后进行热处理的,具有航空意义的γ-铝化钛的可加工性。铣削实验是在不同的切削速度,进给和润滑条件(干,湿和最小量润滑)下进行的。结果以切削参数和润滑条件与工具磨损,表面硬度和粗糙度以及切屑形态之间的相关性表示。刀具寿命,表面粗糙度和chi形貌显示出对切削参数的依赖性。观察到润滑条件会严重影响工具的磨损,到目前为止,证明最小量的润滑是可以延长工具寿命的方法。

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