Steam Turbine and Gas Turbine
GUAN Junjun, ZHANG Yi, ZHANG Yeping, BAO Amei, DAI Ren
In order to obtain higher cooling efficiency, the two-step method was used to optimize the geometry of fan-shaped film holes. In the first step, taking the leading edge length L1, trailing edge length L2, exit width H and cylinder segment length Lm as optimization variables, the first round Latin hypercube sample space was constructed, and the sensitivity of the objective function to each optimization variable was obtained based on parameter sensitivity analysis. In the second step, high sensitive parameters were selected to generate the second round of parameter sample space, and the Kriging surrogate model was constructed. Finally, multi-island genetic algorithm was used for optimization. Results show that L1, L2 and Lm would significantly affect surface average cooling efficiency with high sensitivity, while the sensitivity of H is the least. After reducing dimension of parameters by sensitivity analysis, the prediction accuracy of the surrogate model can be improved. Surface average cooling efficiency of the optimized hole obtained by two-step method is higher than that of one-step optimization, and the convergence of the optimization results can be improved.