SIMULATION OF FINAL DIRECT EXTRUSION STAGE FOR LARGE RODS WITH LOW EXTRUSION RATIO

V. Kargin, A. Y. Deryabin
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Abstract

The direct extrusion of large 7075 alloy bars 188, 214, 252, 283, 326, 560 mm in diameter was simulated with 0 and 0,5 friction coefficients, 80° and 90° die cone angles from the 800 mm diameter container at the 200 MN press using the DEFORM-2D software package. It provided the distribution of metal flow radial velocities on the dummy block working surface versus the contact friction value, die cone angle and extrusion ratio factor at the main and final stages of extrusion. Butt-end height at the beginning of back-end extrusion defect formation was taken equal to a distance between the dummy block plane and the plane of extruded metal feeding into flat or cone die openings. The joint effect of the extrusion ratio factor, friction coefficient and die cone angle on the butt-end height, extrusion force, deformation and stress intensity factors, and die opening edge temperature was studied. Numerical experiments were performed based on the 23 complete factorial design for the following parameter variability intervals: Х1 = 3÷9, Х2 = 0÷0,5, Х3 = 80÷90°. Friction between the tool and the blank at the final extrusion stage has a negative effect due to a noticeable radial velocity reduction. This leads to the earlier initiation of central back-end extrusion defect formation. Extrusion into the conical die and increasing the extrusion ratio factor, on the contrary, speeds up radial flow velocity and ensures that the back-end extrusion defect starts forming later. The main factor that determines butt-end height is the extrusion ratio factor. A mathematical model is proposed to select the butt-end thickness for specific conditions of extruding large bars with low extrusion ratios.
低挤压比大棒材最终直接挤压阶段的模拟
利用DEFORM-2D软件包,对直径为188,214,252,283,326,560 mm的7075合金棒材在200 MN压力机上,以0和0.5摩擦系数,80°和90°的模锥角从直径为800 mm的容器中直接挤压进行了模拟。给出了在挤压主、末阶段金属流径向速度与接触摩擦值、模锥角、挤压比系数的关系。后端挤压缺陷形成开始时的对端高度等于虚拟块平面与挤压金属进入平模或锥模开口的平面之间的距离。研究了挤压比系数、摩擦系数和模锥角对对端高度、挤压力、变形和应力强度因素以及开模边缘温度的联合影响。数值试验采用23全因子设计,参数变异区间为Х1 = 3÷9, Х2 = 0÷0,5, Х3 = 80÷90°。在最后的挤压阶段,由于径向速度明显降低,工具和毛坯之间的摩擦产生了负面影响。这导致中心后端挤压缺陷形成较早。挤压进锥形模具,增大挤压比系数,反而加快了径向流动速度,保证了后端挤压缺陷开始成形较晚。决定顶端高度的主要因素是挤压比因素。针对低挤压比大棒材挤压的具体情况,提出了选择顶端厚度的数学模型。
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