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Two-Zone Modeling Prediction Method of Centrifugal Compressor Performance

机译:离心压缩机性能的两区建模预测方法

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In an effort to produce an effective performance prediction method of centrifugal compressor, based on the test data completed with current test facilities in turbocharger, theory of two-zone modeling performance prediction and its simulation method have been studied. The results demonstrate: 1) For twozone modeling method, although the details of diffusion and loss processes have been actually considered, as well as the basic viscous flow processes under the influence of adverse pressure gradients, its simulation method is rather simply and practical, easier to apply in engineering design. 2)This method can effectively predict the performance of centrifugal compressor in turbocharger, including its surge boundary and choke boundary, and can effectively present its overall performance characteristics. 3) Cases provided in this article also indicate: comparing prediction value with test data, the difference of the total to total pressure ratio is less than 3%, the difference of adiabatic efficiency based on total to total pressure ratio is less than,one point, and the mass flow difference on surge line or choke line is less than 0.06 at transonic operation conditions.
机译:为了产生一种有效的离心压缩机性能预测方法,基于现有的涡轮增压器测试数据,对两区建模性能预测理论及其仿真方法进行了研究。结果表明:1)对于二区建模方法,尽管已经考虑了扩散和损失过程的细节,以及在不利的压力梯度影响下的基本粘性流动过程,但其模拟方法相当简单,实用,容易。应用于工程设计。 2)该方法可以有效地预测涡轮增压器中离心压缩机的性能,包括其喘振边界和节流边界,并可以有效地展现其整体性能特征。 3)本文提供的案例还表明:将预测值与测试数据进行比较,总压力与总压力之比的差异小于3%,基于总压力与总压力之比的绝热效率差异小于1分,在跨音速工况下,喘振线或扼流线上的质量流量差小于0.06。

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