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Optimized Design of a Novel Hydraulic Propeller Turbine for Low Heads

机译:低头新型液压螺旋桨汽轮机的优化设计

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In the present paper, an optimized design procedure capable of providing the geometry of a high efficiency compact hydraulic propeller turbine for low head is proposed and developed. The turbine preliminary design is based on fundamental turbomachinery mean-line equations and on the employment of statistical correlations, which relate the main geometrical parameters to the fundamental design parameters. The first obtained geometry represents the starting point of an automated aerodynamic single point optimization procedure based on a genetic algorithm generating and updating a wide database of turbine geometries. The approach employs a three-dimensional (3D) Reynolds averaged Navier–Stokes (RANS) solver for the construction of the corresponding database of performance. A meta-model, such as an artificial neural network (ANN), is used to speed up the design optimization process. The procedure has been applied on the practical case of a novel simplified hydraulic propeller turbine prototype for very low heads. The adopted design optimization procedure is able to modify the turbine blade and vane geometries in order to achieve automatically the targeted net head and the maximum for the total to total internal efficiency once diameter, mass flow rate, and rotational speed are assigned.
机译:在本文中,提出了一种优化的设计过程,其能够为低头提供高效率紧凑型液压螺旋桨涡轮机的几何形状。涡轮机初步设计基于基础涡轮机械均值线条方程和统计相关的就业,这将主要的几何参数与基本设计参数相关联。第一获得的几何形状表示基于生成和更新涡轮几何形状的宽数据库的遗传算法的自动空气动力单点优化过程的起点。该方法采用三维(3D)Reynolds平均Navier-Stokes(RANS)求解器,用于构建相应的性能数据库。 META模型,例如人工神经网络(ANN),用于加速设计优化过程。该程序已经应用于一种用于非常低头的新型简化液压螺旋桨式原型的实际情况。采用的设计优化程序能够修改涡轮叶片和叶片几何形状,以便自动地实现目标网头,并为总,对总内部效率进行一次直径,质量流量和转速。

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