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Reduction in post forging errors for aerofoil forging using finite element simulation and optimization

机译:使用有限元模拟和优化减少翼型锻件的锻后误差

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This paper reports on recent work in the development of a finite element (FE) based forging optimization methodology. It utilizes the commercial FE package ABAQUS and the optimization code VisualDOC. Taking into account the effect of die and press elastic deflections and thermal distortion in cooling, a direct compensation approach and optimized weighting factor method are used to achieve the optimized die shape for improved dimensional accuracy of forged aerofoil blades. The significant predicted reduction in aerofoil shape errors using a single 2D section from a forged nickel-based blade demonstrates the efficiency and potential for applying this approach to more complex, realistic and industrially relevant 3D forging problems.
机译:本文报告了基于有限元(FE)的锻造优化方法开发的最新工作。它利用了商业有限元软件包ABAQUS和优化代码VisualDOC。考虑到模具和压力机的弹性变形和冷却中的热变形的影响,采用直接补偿方法和优化的加权因子方法来获得优化的模具形状,从而提高了锻造翼型叶片的尺寸精度。使用锻造的镍基叶片的单个2D截面可以显着地预测机翼形状误差的减少,这表明将这种方法应用于更复杂,现实和工业相关的3D锻造问题的效率和潜力。

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