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Creating model stages of centrifugal compressor based on experimental data

机译:基于实验数据创建离心压缩机的模型阶段

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The gas-dynamic characteristics of nine single-stage centrifugal compressors of turbo-expander units are approximated with great accuracy by the equations of the new version of the mathematical model of the Universal Modeling Method and are included in the database of model stages. The universal set of empirical coefficients of the model is somewhat modified for each of the compressors, whose dimensionless gas-dynamic characteristics lie within a fairly wide range. The families of characteristics are calculated by varying the similarity criteria for compressibility. The influence of the surface roughness was investigated. The database and computer programs of the Universal Modeling Method make it possible to use the characteristics of model stages for designing compressors by approximate gas-dynamic similarity.
机译:涡轮扩展器单元的九个单级离心压缩机的气体动力学特性通过通用建模方法的数学模型的新版本的等式来近似,并包含在模型阶段的数据库中。对于每个压缩机,模型的通用经验系数集是稍微改进的,其压缩机的无量纲气体动态特性位于相当宽的范围内。通过改变对压缩性的相似标准来计算特性的家庭。研究了表面粗糙度的影响。通用建模方法的数据库和计算机程序使得可以通过近似气体动态相似性来使用模型阶段的特性来设计压缩机。

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