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Parametric analysis of the Ultimate Tensile Strength in dry machining of UNS A97075 Alloy

机译:UNS A97075合金干加工极限抗拉强度的参数分析。

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Aluminium alloys (mainly 2XXX and 7XXX series) have been traditionally used in the industry in the manufacture of structural parts in aircrafts, due to their excellent ratio density-mechanical properties. Machining is commonly used in the manufacture of these parts. In addition, the actual trend is machining in dry, due to environmental and economic reasons. Under these conditions, surface integrity becomes one of the most important quality requirements applicable to machined parts. The micro and macro-geometrical properties analysis of the dry machined surface as a function of the cutting parameters is widely studied. Notwithstanding, there is a lack of research in the field dedicated to the physicochemical properties. In this paper the feed influence on the ultimate tensile strength for UNS A97075 (Al-Zn) alloy turned in dry is presented, as a first approximation to the study of the influence of the cutting parameters on this mechanical property.
机译:铝合金(主要是2XXX和7XXX系列)由于其优异的比率密度-机械性能而一直在工业上用于制造飞机的结构部件。这些零件的制造中通常使用机加工。另外,由于环境和经济原因,实际趋势是在干燥状态下加工。在这些条件下,表面完整性成为适用于机加工零件的最重要的质量要求之一。广泛研究了干加工表面作为切削参数的函数的微观和宏观几何特性分析。尽管如此,在该领域中缺乏针对物理化学性质的研究。本文提出了进料对干燥后的UNS A97075(Al-Zn)合金极限抗拉强度的影响,作为研究切削参数对该机械性能影响的第一近似方法。

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