首页> 外文会议>International Conference on Metal Cutting and High Speed Machining >HIGH SPEED BALL NOSE END MILLING OF INCONEL 718 WITH VARIABLE TOOL GEOMETRY-EXPERIMENTAL AND FINITE ELEMENT ANALYSIS
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HIGH SPEED BALL NOSE END MILLING OF INCONEL 718 WITH VARIABLE TOOL GEOMETRY-EXPERIMENTAL AND FINITE ELEMENT ANALYSIS

机译:具有可变工具几何实验和有限元分析的高速球鼻鼻铣铣刀inconel718

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The longest cut length (approx 200 m) was achieved using the medium' radial rake angle and 'high' primary relief angle. Higher cut lengths were achieved when using tool geometries which did not lead to chatter. Cutting forces (Fx, Fy and Fz) were generally in the range 100-250 N and forces tended to be lower in magnitude where chatter did not occur. Workpiece surface roughness values of <1 mu m Ra were achieved in all tests with both new and worn cutting tools. Values as low as 0.4 mu m Ra were possible. Machined surfaces had tensile residual stresses (typically 200-1000 MPa), however, subsequent work has resulted in the production of surfaces with highly compressive stresses. 2D FE modelling of the process indicated similar trends to the force signatures obtained in the experimental work. Industrial pre-production trials on a combustion chamber outer casing have proved that high-speed ball nose end milling is a feasible process for aerospace components.
机译:使用介质的径向前角和“高”初级浮雕角度实现最长的切割长度(约200μm)。使用工具几何形状时,实现了更高的切割长度,这不会导致颤动。切割力(FX,FY和FZ)通常在100-250 n的范围内,并且力倾向于较低的尺寸下降,其中没有发生颤动。在新的和磨损的切削刀具中的所有测试中实现了<1μmra的工件表面粗糙度值。值低至0.4μm的值。机加工表面具有拉伸残余应力(通常为200-1000MPa),然而,随后的工作导致具有高压缩应力的表面的产生。该过程的2D FE建模表明了在实验工作中获得的力签名的类似趋势。在燃烧室外壳上的工业预生产试验证明,高速球鼻端铣削是航空航天部件的可行过程。

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