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Optimization of the forging of aerofoil blade using the finite element method and fuzzy-Pareto based genetic algorithm

机译:基于有限元和遗传算法的机翼叶片锻造优化

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摘要

In this research non-isothermal forging process of an aerofoil blade was simulated using 3-dimentional finite element method. Then an optimization approach integrated with the finite element method has been applied to optimize the blade forging process. Preform shape and angular position of the die parting line were optimized in order to minimize the flash volume, strain non-uniformity and lateral forces generated during the forging operation. The optimization method includes the finite element approach and the response surface method for the formulation of the objective functions. Using the multi-objective genetic algorithm, Pareto front of global optimal solutions was generated. Then a fuzzy-based membership value assignment method was used to select the best compromise solution. The simulation of the blade forging process was verified by experimental test. Results show that the numerical results and experimental tests have a good agreement. Waste material and lateral forces generated during the forging operation is decreased with optimization method significantly. Therefore the proposed approach is an appropriate method for multi-objective optimization of the forging process of aerofoil blades.
机译:在这项研究中,使用三维有限元方法模拟了翼型叶片的非等温锻造过程。然后应用了与有限元方法相集成的优化方法来优化叶片锻造工艺。优化了模具分型线的预成型件形状和角位置,以最大程度地减少毛边量,应变不均匀性和锻造过程中产生的侧向力。优化方法包括有限元法和响应面法,用于制定目标函数。使用多目标遗传算法,生成了全局最优解的Pareto前沿。然后基于模糊的隶属度值分配方法来选择最佳折衷解决方案。通过实验测试验证了叶片锻造过程的仿真。结果表明,数值结果与试验结果吻合良好。采用优化方法,可大大减少锻造过程中产生的废料和侧向力。因此,所提出的方法是一种多目标优化翼型叶片锻造工艺的方法。

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