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DESIGN OPTIMIZATION OF A CENTRIFUGAL COMPRESSOR IMPELLER USING RADIAL BASIS NEURAL NETWORK METHOD

机译:基于径向基神经网络的离心压缩机叶轮设计优化

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This paper presents a procedure for design optimization of a centrifugal compressor. The centrifugal compressor consists of a centrifugal impeller, vaneless diffuser and volute. And, optimization techniques based on radial basis neural network method are used to optimize the impeller of the centrifugal compressor. Latin hypercube sampling of design of experiments is used to generate thirty design points within design spaces. Three-dimensional Reynolds-averaged Navier-Stokes equations with shear stress transport turbulence model are discretized by using finite volume approximations and solved on hexahedral grids to evaluate the objective function of an isentropic efficiency. Four variables defining impeller hub and shroud contours are selected as design variables in this optimization. The results of optimization show that the isentropic efficiency of the optimized shape at the design flow coefficient is enhanced by 1.0% and the efficiencies at the off-design points are also improved significantly by the design optimization.
机译:本文提出了一种用于离心压缩机设计优化的程序。离心压缩机由离心叶轮,无叶片扩压器和蜗壳组成。并且,基于径向基神经网络方法的优化技术被用于优化离心压缩机的叶轮。实验设计的拉丁超立方体采样用于在设计空间内生成三十个设计点。利用有限体积近似将具有切应力传输湍流模型的三维雷诺平均Navier-Stokes方程离散化,并在六面体网格上求解以评估等熵效率的目标函数。在此优化中,选择了四个定义叶轮轮毂和护罩轮廓的变量作为设计变量。优化结果表明,通过设计优化,优化形状在设计流量系数时的等熵效率提高了1.0%,并且在非设计点的效率也得到了显着提高。

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