The Application of Mathematical Models for Industrial Centrifugal Compressor Optimal Design

Y. Galerkin, K. Soldatova, A. Drozdov
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引用次数: 14

Abstract

The authors present the design approach aiming to reach maximum possible efficiency of an industrial centrifugal compressor. To reach the goal the flow coefficient of stages must lie within the range where velocity at an impeller inlet are not more than 0,7 of blade speed. Flow path channels must not be less than 0,05 of an impeller diameter. A loading factor must vary between 0,4 and 0,5. Design limitations are important too. The Universal Modeling Method of effective design and reliable calculation is shortly described. The original two-zone model is being processed by implemented in PC programs to optimize basic dimensions of a flow path and to calculate gas dynamic performances. Q3D calculations are applied to optimize 2D and 3D blade cascades. CFD calculations are used as a finishing operation. Two samples of high effective compressors developed in cooperation with PAO SMPO (Sumy city, Ukraine) are presented. 16 MW booster compressor demonstrated efficiency close to 88% due to proper choice of number of stages'. 32 MW single-stage compressor design was based on most effective scheme and parameters offered by PAO SMPO. The Industrial partner designed, manufactured and tested 1:2 scale model. The tests have verified the project gas dynamic performances with high accuracy. Polytropic efficiency of 90% was reached for the first time in the Authors' design practice.
数学模型在工业离心压缩机优化设计中的应用
作者提出了一种旨在使工业离心压缩机达到最大效率的设计方法。为了达到这一目的,各级的流量系数必须在叶轮入口速度不大于叶片速度0.7的范围内。流道通道不得小于叶轮直径的0.05。负载因子必须在0,4和0,5之间变化。设计限制也很重要。简要介绍了有效设计和可靠计算的通用建模方法。原始的两区模型正在PC程序中进行处理,以优化流道的基本尺寸并计算气体的动态性能。Q3D计算应用于优化二维和三维叶片叶栅。CFD计算被用作收尾操作。介绍了与PAO SMPO(乌克兰苏梅市)合作开发的两种高效压缩机样品。通过对级数的合理选择,16mw增压压缩机的效率接近88%。32mw单级压缩机的设计是根据PAO SMPO提供的最有效方案和参数进行的。工业合作伙伴设计、制造和测试了1:2比例模型。试验验证了该工程的气体动力性能,具有较高的精度。在笔者的设计实践中,首次达到了90%的多向效率。
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