基于神经网络的涡轮喷管叶栅叶间通道液滴运动模拟

IF 0.9 Q4 ENERGY & FUELS
V. A. Tishchenko, V. V. Popov, I. Yu. Gavrilov, V. G. Gribin, A. A. Tishchenko, K. A. Berdyugin, D. G. Sokolov, A. O. Smirnov
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引用次数: 0

摘要

研究了神经网络在涡轮叶片间通道液滴运动规律分析中的应用问题。对喷嘴叶栅中液滴的流动进行了广泛的蒸汽流型和液相条件下的数值研究。计算采用实验验证的液相流模型进行。叶栅后理论马赫数为0.4 ~ 0.9,液相相对密度为1800 ~ 5100,液滴直径为5 ~ 205µm,液滴初始滑移系数为0.1 ~ 0.9,蒸汽与液滴速度矢量的初始夹角为-15°~ +15°。揭示了不同参数对液滴在叶间通道内运动特性和液滴在叶片表面沉积特性的影响。数值模拟产生了大约100万个液滴的阵列,用于训练神经网络。在对这些数据进行分析的基础上,提出了一种利用神经网络预测涡轮叶栅初级液滴行为的算法。该算法包括两个神经网络:第一个解决二元分类问题,以确定液滴与叶片碰撞的概率;第二个神经网络预测液滴与叶片表面相互作用的特征。该算法针对一组未参与训练但在相同参数范围内的数据进行了测试。测试集包括三种流动模式和四种不同的液滴直径。测试数据集确定的液滴沉积点相对坐标的均方根误差为5.2%,碰撞能量无因次系数的均方根误差为1.5%。对模拟计算时间的估计表明,使用神经网络的算法运行速度比最接近的模拟快100倍以上。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Simulation of the Droplet Movement in the Interblade Channel of a Turbine Nozzle Cascade Using Neural Networks

The issue of application of neural networks for analyzing the regularities of droplet motion in the interblade channel of turbomachines is examined. The droplet flow in a nozzle cascade was numerically investigated in a wide range of steam flow regimes and liquid phase conditions. The calculations were performed using an experimentally verified model of the liquid phase flow. The theoretical Mach number behind the cascade varied from 0.4 to 0.9, the relative density of the liquid phase from 1800 to 5100, the droplet diameter from 5 to 205 µm, the initial slip coefficient of the droplets from 0.1 to 0.9, and the initial angle between the velocity vectors of steam and droplets from ‒15° to +15°. The effect of various parameters on the characteristics of droplet movement through the interblade channel and droplets deposition on the blade surface was revealed. The numerical simulations yielded an array of approximately 1 million droplets, which was used to train neural networks. Based on the analysis of these data, an algorithm for using neural networks to predict the behavior of primary droplets in a turbine cascade was developed. The algorithm includes two neural networks: the first solves the problem of binary classification to determine the probability of a droplet collision with a blade, and the second predicts the features of droplet interaction with the blade surface. This algorithm was tested against a set of data that had not been engaged in the training but were in the same range of parameters. The test set consisted of three flow patterns with four different droplet diameters. The root mean square error determined for the test data set was 5.2% for the relative coordinate of the droplet deposition point and 1.5% for the dimensionless coefficient of collision energy. Estimation of the calculation time for the simulation has revealed that the algorithm using neural networks runs more than 100 times faster than its closest analogue.

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来源期刊
CiteScore
1.30
自引率
20.00%
发文量
94
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