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A 3D rigid-viscoplastic FEM simulation of the isothermal precision forging of a blade with a damper platform

机译:带阻尼平台的叶片等温精密锻造的3D刚粘塑性有限元模拟

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摘要

A blade with a damper platform, with excellent anti-vibration characteristics and high efficiency, has become one of the most important new types of blade being developed in the aeronautical engine. However, the blade is complicated in shape, and the material used for its manufacture is difficult to deform. Therefore, it is important to undertake research on the blade-oriented precision forging process using three-dimensional finite on such research has been scant. In this paper, based on the rigid-viscoplastic principle, three-dimensional finite element simulation is reported for the isothermal precision forging of the blade using the penalty function, and eight-node hexahedral isoparameteric elements for discretizing the deforming workpiece and triangular elements for discretizing the die cavity. The method of contracting from the boundary to the interior, proposed by the authors, is used for remeshing a distorted mesh system, and the method of modifying the position of nodes touching the die according to its original normal, also proposed by the authors, is used to avoid the "dead lock" problem due to the normal uncontinuity of scatted die meshes, to enable he simulation to be successful. Friction is considered for the die-workpiece interface boundary condition, and an arc is considered for the tenon-body joint, and a damper platform-body joint on the blade die cavity, respectively, which make it possible for the simulation to approach the practical forging process of a blade with a damper platform. 3D FEM simulation results have been obtained for the initial and deformed configurations, the deformed meshes of typical cross-sections, the distribution of effective strain at the final stage, load-displacement curves, in this way the deformation law of the forging of a blade with a damper platform being revealed. The achievements of this research serve as a significant guide to the optimization of design for the relevant process and dies. The method used is also of general significance to the forging process of other type of blades and other complicated massive deformation process.
机译:具有减震平台的叶片具有出色的抗振动特性和高效率,已成为航空发动机中开发的最重要的新型叶片之一。然而,叶片的形状复杂,并且用于其制造的材料难以变形。因此,重要的是,对利用三维有限元进行的叶片定向精密锻造工艺的研究很少。本文基于刚粘塑性原理,利用惩罚函数对叶片的等温精密锻造进行了三维有限元模拟,对变形工件进行离散化的是八节点六面体等参元素,对离散化采用了三角形元素。模腔。作者提出了一种从边界到内部的收缩方法,用于对变形的网格系统进行重新网格化,作者还提出了根据其原始法线修改接触模具的节点的位置的方法。用于避免由于分散的模具网格的正常不连续性而导致的“死锁”问题,从而使模拟成功。模具-工件界面边界条件考虑了摩擦,并且叶片模腔上的榫-本体接头和阻尼器平台-本体接头分别考虑了电弧,这使得仿真有可能接近实际带有阻尼器平台的叶片的锻造过程。获得了初始和变形构型,典型截面的变形网格,最终阶段的有效应变分布,载荷-位移曲线的3D FEM仿真结果,通过这种方式,叶片锻件的变形定律带有阻尼器平台。这项研究的成果为优化相关工艺和模具的设计提供了重要指导。所使用的方法对于其他类型叶片的锻造过程以及其他复杂的大规模变形过程也具有普遍意义。

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