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Numerical Optimization of Cooling Process of the Gas Turbine Blade

Numerical Optimization of Cooling Process of the Gas Turbine Blade
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摘要 The paper presents a scheme of optimization of the cooling process of the gas turbine blade. As an optimization criterion has been taken into account on the outer surface temperature of the blade. Inverse problem is solved for stationary heat conduction in which beside the optimization criterion of the heat transfer coefficient on the outer surface of the blade the temperature distribution is known, and the values sought are the heat transfer coefficients and surface temperature of the cooling channels. This problem was solved by the boundary element method using SVD algorithm and Tikhonov regularization. The temperature and heat transfer coefficient of cooling channels obtained from the inverse problem was oscillating in nature. This solution is nonphysical, so the heat transfer coefficients on the surface of cooling channels were averaged. Then the problem was solved simply with averaged coefficients of heat transfer on the surface of the cooling channels and the known distribution on the outer surface of blade. The temperature distribution obtained from the solution of direct problem with averaged values of heat transfer coefficient was compared with the criterion of optimization.The calculation results obtained using the SVD algorithm gave the temperature distribution on the external wall of the blade closer to the criterion of optimization.
机构地区 Thermal Engineering
出处 《Journal of Chemistry and Chemical Engineering》 2011年第4期355-357,共3页 化学与化工(英文版)
关键词 Inverse problem SVD algorithm Tikhonov regularization 燃气涡轮叶片 数值优化 Tikhonov正则化方法 冷却过程 外表面温度 传热系数 SVD算法 冷却通道
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参考文献5

  • 1G. Nowak, W. Wr6 blewski, T. Chmielniak, Optimization of cooling passages within a turbine vane, in: Proceedings ofASME TurboExpo 2005, Paper GT 344 2005-68552, pp 1-8.
  • 2L.D. Hylton, M.S. Mihelc, E.R. Turner, DA. Nealy, RE York, Analytical and Experimental Evaluation of the Heat Transfer Distribution Over the Surfaces of Turbine Vanes, NASA CR-168015 DDA EDR 11209, 1983.
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