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Three-dimensional Design Optimization for Fir-tree Root of Turbine Blade with Finite Element Method

机译:有限元法的汽轮叶片枞树根的三维设计优化

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Fir-tree root is widely used inblades of gas turbine and large power steam turbine. The structure of root and rim affects the security of the entire blade to a certain extent. Based on the parametric design language APDL, the fir-tree root and rim with complex three-dimensional contact stress, are numerical studied and optimized with multi-variable using the finite element software ANSYS. The zero-order optimization algorithm and the first-order optimization algorithm are combined in the optimization process to enhance the credibility of results. A novel structure of the turbine blade fir-tree root and rim is then obtained. Moreover, numerical results show that equivalent stress has a reduction after the multi-variable optimization when the maximum equivalent stress of root is set as the objective function. Compared with the results of the initial design, the maximum equivalent stress of the root of the optimized design reduces by 4.56%, and the maximum equivalent stress of the rim reduces by 4.40%. Relevant results are expected to support the design of turbine blade in theory and then improve the operation reliability of turbo-machinery to some extent.
机译:杉木树根广泛应用于燃气轮机和大型电力汽轮机的燃气轮机。根和边缘的​​结构影响整个刀片的安全性到一定程度。基于参数化设计语言APDL,FIR-TREE根和具有复杂的三维接触应力的轮辋,是使用有限元软件ANSYS的多变量进行数值研究,并优化了多变量。零阶优化算法和一阶优化算法在优化过程中组合以增强结果的可信度。然后获得涡轮叶片枞树根和边缘的​​新颖结构。此外,数值结果表明,当根的最大等效应力被设定为目标函数时,在多变量优化之后的等效应力具有减少。与初始设计的结果相比,优化设计根部的最大等效应力降低了4.56%,并且轮辋的最大当量应力降低了4.40%。预计相关结果将支持理论上的涡轮叶片设计,然后在一定程度上提高涡轮机的运行可靠性。

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