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A Three-Dimensional Inverse Method based on Load Control for Radial Inflow Turbine Impeller

机译:一种基于径向流入汽轮机叶轮载荷控制的三维逆方法

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There are surprisingly a few inverse methods found in literature that are composed of clear and definite fluid flow physics. Within this paper one method is proposed to design three dimensional turbine blade shape of uniform thickness. Prescribed mean swirl distribution throughout the meridional flow path was used. Flow is considered inviscid and flow losses through blade passage are taken into account via entropy increase modeling. In order to avoid ambiguity in blade thickness distribution, uniform blade thickness is used to indicate its influence on the velocity field, which may be considerable accurate for impellers of radial inflow turbine. In order to obtain smooth mean swirl distribution, one Laplace equation is used to prescribe over the given flow path region. With given inlet and exit mean swirls of impeller together with possible slopes, mean swirl distribution along meridional surface can be varied freely which then provides further space to seek for optimized impeller geometry shaping. Method was used to design an impeller for a low speed radial inflow turbine as example to show its validity and feasibility.
机译:令人惊讶的是,文学中发现的一些反向方法是由清晰和明确的流体流物理组成的。在本文中,提出了一种方法来设计三维涡轮叶片的均匀厚度。使用整个子午线路径的规定的平均旋流分布。流动被认为是通过熵增加建模考虑通过刀片通道的刀片和流失。为了避免叶片厚度分布中的模糊性,使用均匀的叶片厚度来表示其对速度场的影响,这对于径向流入涡轮机的叶轮可能具有相当大的准确性。为了获得平滑的平均旋流分布,一个拉普拉斯方程用于规定给定的流路区域。通过给定的入口和出口平均叶轮旋转,可以与可能的斜面一起,可以自由地改变沿着子午面的平均旋流分布,然后提供进一步的空间以寻找优化的叶轮几何形状。方法用于设计用于低速径向流入涡轮机的叶轮,例如示例以显示其有效性和可行性。

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