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Die shape optimisation in forging of aerofoil sections

机译:翼型件锻造中的模具形状优化

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Dimensional tolerances are among the most important manufacturing criteria in the forging of aerofoil blades for aeroengine applications. A die shape optimisation system under development for the net-shape forging of aerofoil blades is outlined in this paper. In forging simulation using finite elements (FEs), a compensation approach was used in order to eliminate the aerofoil thickness errors due to die-elasticity. The optimised die shape is obtained by modifying the nominal die shape with a fraction of the die-elastic deflections through an introduced weighting factor While forging simulation enables the evaluation of material flow, mechanical behaviour and die deflections, the compensation approach provides an effective means to minimise aerofoil thickness errors with only a small number of forging simulation iterations, suggesting substantial computing cost savings.
机译:尺寸公差是航空发动机应用的机翼叶片锻造中最重要的制造标准之一。本文概述了正在开发的用于翼型叶片净形锻造的模具形状优化系统。在使用有限元(FE)进行锻造模拟时,为了消除由于模具弹性引起的翼型厚度误差,使用了一种补偿方法。通过使用引入的权重系数以一部分模具弹性挠度修改名义模具形状来获得最佳模具形状,而锻造仿真可以评估材料流动,机械性能和模具挠度,而补偿方法则提供了一种有效的方法来仅通过少量的锻造仿真迭代就可以最大程度地减小翼型厚度误差,这表明可以节省大量计算成本。

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