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Cutting Forces Modeling in Finish Turning of Inconel 718 Alloy with Round Inserts

机译:带圆刀片的Inconel 718合金精车削中的切削力建模

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摘要

In turning, the applied forces have to be known as accurately as possible, especially in the case of difficult-to-cut materials for aircraft workpieces finishing operations. Traditionally, edge discretisation methodology based on local cutting laws is used to determine the cutting forces and results are usually considered suitable. Nevertheless, only the rake face is considered in most of studies and the cutting relations are determined by direct identification with a straight edge. This study deals with finishing operations of Inconel 718 alloy with one type of round insert. The main objective is to formulate a novel cutting forces model, taking into account the clearance face. First, a generic model based on a geometrical description using homogeneous matrix transformation is presented. Then, cutting coefficients are identified by inverse identification from experimental measurements distributed with an orthogonal design experiment including tool wear. Finally, modeling and experimental values of the cutting forces are compared and the identified model is analysed.
机译:在转弯时,必须尽可能准确地知道所施加的力,尤其是在用于飞机工件精加工操作的难切削材料的情况下。传统上,基于局部切削定律的边缘离散化方法用于确定切削力,通常认为结果合适。然而,在大多数研究中仅考虑前刀面,并且通过直接识别直边来确定切削关系。这项研究涉及一种类型的圆刀片的Inconel 718合金的精加工操作。主要目的是在考虑间隙面的基础上,制定一种新颖的切削力模型。首先,提出了一种基于几何描述并使用齐次矩阵变换的通用模型。然后,通过从带有正交设计实验(包括刀具磨损)的分布的实验测量值中进行逆向识别,可以确定切削系数。最后,比较切削力的模型和实验值,并对识别出的模型进行分析。

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