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气膜冷却作为当代燃机高温透平中必需的冷却手段,其冷却性能在多种参数的影响下表现复杂。采用BP神经网络模型对多种几何、流动参数变化下的气膜冷却系统的绝热气膜冷却效率进行预测。选择气膜冷却系统的吹风比、密度比、主流湍流度、面积比和长径比作为神经网络的输入参数,以燃气轮机透平叶片气膜冷却的实际运行工况为范围建立数据库。计算结果表明,采用贝叶斯归一化法训练后建立的气膜冷却神经网络模型在预测精度上要优于经验公式法,而且参数适用范围更广,具有良好的发展应用前景。

Film cooling is necessary for modern gas turbine.Its cooling effectiveness is sophisticated influenced by multi parameters.The BP neural network is applied to predict the adiabatic film cooling effectiveness of the cooling system with multi geometry and flow parameters.The input parameters of neural network are chosen as blowing ratio,density ratio,free stream turbulence intensity,area ratio and length ratio.A database covering the real operation range is build up.Prediction from the neural network trained by Bayesian Regulation backpropagation is compared to an existing correlation.The result shows a good accuracy and wide application range of the neural network model.It implicates that the developed model is promising to be applied on the film cooling system.

参考文献

[1] Aleksander I.;Morton H.B. .General neural unit: retrieval performance[J].Electronics Letters,1991(19):1776-1778.
[2] M. Gritsch;A. Schulz;S. Wittig .Adiabatic wall effectiveness measurements of film-cooling holes with expanded exits[J].Journal of turbomachinery,1998(3):549-556.
[3] E. Lutum;B. V. Johnson .Influence of the hole length-to-diameter ratio on film cooling with cylindrical holes[J].Journal of turbomachinery,1999(2):209-216.
[4] Michael Gritsch;Will Colban;Heinz Schaer;Klaus Doebbeling .Effect of Hole Geometry on the Thermal Performance of Fan-Shaped Film Cooling Holes[J].Journal of turbomachinery,2005(4):718-725.
[5] 李佳,韩昌,任静,蒋洪德.基于压敏漆的带横槽气膜冷却实验与数值研究[J].工程热物理学报,2010(02):239-242.
[6] R. J. Goldstein;P. Jin;R. L. Olson .Film cooling effectiveness and mass/heat transfer coefficient downstream of one row of discrete holes[J].Journal of turbomachinery,1999(2):225-232.
[7] Christian Saumweber;Achmed Schulz;Sigmar Wittig .Free-Stream Turbulence Effects on Film Cooling With Shaped Holes[J].Journal of Turbomachinery,2003(1):65-73.
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