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首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers, Part B. Journal of engineering manufacture >Hole quality and tool wear when dry drilling of a new developed metal/composite co-cured material
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Hole quality and tool wear when dry drilling of a new developed metal/composite co-cured material

机译:孔质量和工具磨损在干燥钻孔新型发发的金属/复合材料共固化材料时

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摘要

The new developed metal/composite co-cured material composed of carbon fiber-reinforced plastic and Al phases has been increasingly applied for manufacturing of attitude control flywheel in aerospace industry. However, drilling of co-cured material is still a challenging task to produce holes with high quality and low cost in the assembly chain and dynamic balance debugging of attitude control flywheel. In other words, the relevant mechanisms and experimental findings involved in the drilling process of carbon fiber-reinforced plastic/Al co-cured material is not clearly defined, which impedes the progress of attitude control flywheel production. To this end, this article specially addresses the experimental studies on the drilling process of carbon fiber-reinforced plastic/Al co-cured material with standard TiAlN-coated cemented carbide twist drill. The significance of this work aims to reveal the regardful cutting responses of the hole characteristics and tool wear modes during the practical drilling process of co-cured material. A full factorial experiment including three levels of feed rate and four levels of cutting speed was performed. The hole diameter shows different values in different positions while it indicates consistent pattern regardless of the cutting variables: the largest in the Al phase, followed by the upper and lower carbon fiber-reinforced plastic phases, respectively. Grooves and matrix degradation are the major machining defects for carbon fiber-reinforced plastic layers, while a great chip debris adhered to the machined surface is the case for Al layer. Subsequent wear analysis showed that abrasion was mainly maintained at the vicinity of major/minor cutting edges and drill edge corner, followed by chip adhesion on the chisel edge region. Carbide substrate of drill flank face is exposed, and thereafter cavities are formed under the strong mechanical abrasion. These results could provide several implications for industrial manufacturers during the attitude control flywheel production.
机译:由碳纤维增强塑料和AL阶段组成的新型开发的金属/复合共固化材料越来越多地应用于航空航天工业中的态度控制飞轮的制造。然而,共固化材料的钻井仍然是一个具有挑战性的任务,可以在装配链和动态平衡调试中生产具有高质量和低成本的孔,而动态平衡调试的姿态控制飞轮。换句话说,涉及碳纤维增强塑料/ Al共固化材料的钻井过程中涉及的相关机制和实验结果并没有明确定义,这阻碍了态度控制飞轮生产的进展。为此,本文特别地解决了碳纤维增强塑料/ Al共固化材料的钻井过程的实验研究,具有标准的TiAln涂层硬质合金扭曲钻。该工作的重要性旨在揭示在共固化材料的实际钻井过程中揭示孔特性和刀具磨损模式的视线。进行全部阶乘实验,包括三种水平的进料速率和四个级别的切削速度。孔直径在不同位置表示不同的值,同时表示不论切割变量如何:Al相中最大,其次是上部和下碳纤维增强塑料相。凹槽和矩阵劣化是碳纤维增强塑料层的主要加工缺陷,而粘附到加工表面的碎片是Al层的壳体。随后的磨损分析表明,磨损主要保持在主要/次要切削刃和钻头角附近,然后在凿边区域上进行芯片粘附。钻孔侧面的碳化物基板暴露,然后在强机械磨损下形成腔。这些结果可以在态度控制飞轮生产中为工业制造商提供若干影响。

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