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Experimental investigations on single-lip deep hole drilling of superalloy Inconel 718 with small diameters

机译:小直径Inconel 718合金单唇深孔钻削实验研究

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摘要

Recent trends in downsizing, as well as miniaturization of components, increase the importance of deep hole drilling with small diameters in various industrial applications. For the manufacturing of deep holes, many processes are used. In addition to mechanical cutting, processes based on thermal material removal mechanisms like electrical discharge machining (EDM), laser drilling and electron-beam drilling are established. Whereas non-mechanical processes can be used for the machining of extremely hard and high-strength materials, substantial disadvantages are the restrictions in the realizable hole diameter and depth dimensions, the long production times, the requirement for special-purpose machinery, as well as the limited bore hole quality. In the aerospace industry, where nickel-based superalloys are widespread, high requirements lie on the surface integrity due to high stress loads during operation. Hence, the major drawback of these non-mechanical processes is the alteration of the subsurface zone, which could affect the part safety. In contrast, the mechanical machining of nickel-based superalloys is extremely difficult due to material properties such as high strength, high tendency to work hardening and low thermal conductivity which results in increased mechanical tool loads and heavy abrasive and adhesive tool wear. An additional challenge is constituted by the chip removal and the unfavorable ratio of cutting edge rounding and undeformed chip thickness caused by the limitation in the feed rates, if deep hole drilling with small diameters and high-length-to-diameter ratios of difficult-to-cut materials like nickel-based superalloys is required. Up to now, the use of standard tool geometries in small diameter single-lip deep hole drilling of Inconel 718 has not been productive and leads to limited process stability and drilling lengths as well as insufficient bore hole quality. Concerning this matter, this paper presents a process adaption using a tailored cutting edge design to accomplish the predominant challenges. Substantial analysis on gun drilling in Inconel 718 regarding mechanical tool loads, chip formation, the tool wear, as well as bore hole quality will be presented.
机译:小型化以及组件小型化的最新趋势增加了在各种工业应用中进行小直径深孔钻削的重要性。为了制造深孔,使用了许多工艺。除了机械切割之外,还建立了基于热材料去除机制的工艺,例如放电加工(EDM),激光钻孔和电子束钻孔。非机械工艺可用于加工极硬和高强度的材料,但最大的缺点是可实现的孔径和深度尺寸受限,生产时间长,对专用机械的需求以及有限的钻孔质量。在广泛使用镍基高温合金的航空航天工业中,由于操作过程中的高应力负荷,对表面完整性有很高的要求。因此,这些非机械过程的主要缺点是改变了地下区域,这可能会影响零件的安全性。相反,由于诸如高强度,高加工硬化倾向和低导热率的材料特性,对镍基高温合金的机械加工极为困难,这导致机械工具负荷增加以及严重的磨料和粘合工具磨损。另一个挑战是,如果直径较小,长径比大而难以加工的情况下,由于进给速度的限制而引起的切屑去除,切削刃倒圆率和切屑厚度不佳的不利影响,将带来挑战。需要诸如镍基高温合金之类的切削材料。到目前为止,在Inconel 718的小直径单唇深孔钻削中使用标准刀具几何形状一直没有取得成功,并且导致了有限的工艺稳定性和钻削长度以及不足的钻孔质量。关于此问题,本文提出了使用量身定制的尖端设计来完成主要挑战的过程调整。将对Inconel 718中的枪钻进行大量的机械工具载荷,切屑形成,工具磨损以及钻孔质量的分析。

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