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Three-dimensional turbulent optimization of vaned diffusers for centrifugal compressors based on metamodel-assisted genetic algorithms

机译:基于元模型辅助遗传算法的离心压缩机叶片扩压器三维湍流优化

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摘要

In this work, the performance of an automotive turbocharger centrifugal compressor, to be used in a microturbine for combined heat and power applications, have been improved through a design optimization procedure for vaned diffusers. This methodology couples a genetic algorithm with a three-dimensional turbulent computational fluid dynamics code. The computational costs have been reduced by using a Kriging metamodel to assist the genetic algorithm. The simulations have been performed by considering both the impeller and vaned diffuser, in order to account for the turbulent, three-dimensional, and non-uniform flow conditions at the diffuser inlet. A multi-objective optimization problem has been solved by minimizing two objective functions, which depend on the compressor stage total-to-static pressure ratio and total-to-total isentropic efficiency. The design variables are the position and inclination of the diffuser vanes leading and trailing edges, the vane number, and the diffuser outlet radius. Three optimized geometries extrapolated from the Pareto front exhibit higher static pressure recovery than the vaneless diffuser, but only one has better efficiency. Nevertheless, the performance of the current compressor can be improved by substituting the vaneless diffuser with a vaned one.
机译:在这项工作中,通过叶片式扩散器的设计优化程序,改进了用于微型涡轮机中用于热电联产的汽车涡轮增压器离心压缩机的性能。这种方法将遗传算法与三维湍流计算流体动力学代码结合在一起。通过使用Kriging元模型来辅助遗传算法,降低了计算成本。为了考虑到扩压器进口处的湍流,三维和非均匀流动情况,已通过同时考虑叶轮和叶片扩压器进行了模拟。通过最小化两个目标函数来解决多目标优化问题,这两个目标函数取决于压缩机级的总静压力比和总总等熵效率。设计变量是扩散器叶片前缘和后缘的位置和倾斜度,叶片数量和扩散器出口半径。从帕累托(Pareto)前端推断出的三种优化几何形状比无叶扩压器具有更高的静压恢复能力,但只有一种具有更高的效率。然而,通过用无叶片扩压器代替无叶片扩压器可以改善当前压缩机的性能。

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