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Milling surface roughness for 7050 aluminum alloy cavity influenced by nozzle position of nanofluid minimum quantity lubrication

机译:7050铝合金型腔的铣削表面粗糙度受纳米流体喷嘴位置影响的最小量润滑

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In nanofluid minimum quantity lubrication (NMQL) milling of aviation aluminum alloy, it is the bottleneck problem to adjust the position parameters (target distance, incidence angle, and elevation angle) of the nozzle to improve the surface roughness of milling, which has large and uncontrollable errors. In this paper, the influence law of milling cutter speed, helical angle, and cavity shape on the flow field around the milling cutter was studied, and the optimal nozzle profile parameters were obtained. Using 7050 aluminum alloy as the workpiece material, the milling experiment of the NMQL cavity was conducted by utilizing cottonseed oil-based Al2O3 nanofluid. Results show that the high velocity of the surrounding air flow field and the strong gas barrier could be attributed to high rotating velocities of the milling cutter. The incidence angle of the nozzle was consistent with the helical angle of the milling cutter, the target distance was appropriate at 25–30 mm, and the elevation angle was suitable at 60°–65°. The range and variance analyses of the signal-to-noise ratio of milling force and roughness were performed, and the chip morphology was observed and analyzed. The results show that the optimal combination of nozzle position parameters was the target distance of 30 mm, the incidence angle of 35°, and the elevation angle of 60°. Among these parameters, target distance had the largest impact on cutting performance with a contribution rate of more than 55, followed by incidence angle and elevation contribution rate. Analysis by orthogonal experiment revealed that the nozzle position parameters were appropriate, and Ra (0.087 μm) was reduced by 30.4 from the maximum value (0.125 μm). Moreover, Rsm (0.05 mm) was minimum, which was 36 lower than that of the seventh group (Rsm = 0.078 mm).
机译:在航空铝合金的纳米流体微量润滑(NMQL)铣削中,调整喷嘴的位置参数(目标距离、入射角和仰角)以提高铣削表面粗糙度是瓶颈问题,存在较大且不可控的误差。本文研究了铣刀转速、螺旋角和型腔形状对铣刀周围流场的影响规律,得到了最佳喷嘴轮廓参数。以7050铝合金为工件材料,利用棉籽油基Al2O3纳米流体对NMQL型腔进行了铣削实验。结果表明:周围气流场的高转速和较强的气体阻隔可归因于铣刀的高转速。喷嘴的入射角与铣刀的螺旋角一致,目标距离适宜在25-30 mm,仰角适宜于60°-65°。对铣削力和粗糙度的信噪比进行了范围和方差分析,并观察和分析了切屑的形貌。结果表明:喷嘴位置参数的最优组合为目标距离30 mm、入射角35°、仰角60°;在这些参数中,目标距离对切削性能的影响最大,贡献率超过55%,其次是入射角和仰角贡献率。正交实验分析表明,喷嘴位置参数合适,Ra(0.087 μm)较最大值(0.125 μm)降低了30.4%。此外,Rsm (0.05 mm) 最小,比第七组 (Rsm = 0.078 mm) 低 36%。

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