| 摘要: |
| 针对跨声速风扇动叶中掠、弯结合叶片基于控制点的B样条曲线对积叠线进行参数化,以掠、弯为设计自由度,应用实验设计、三维粘性流场求解、响应面模型及遗传算法对Rotor 67以近尖峰效率工况点为设计点对风扇转子进行了气动优化设计,得到了前掠与弯向旋转方向的复合设计叶片,其总压比有较明显提高。但由于优化是在单一工况点下进行的,其变工况性能不佳。 |
| 关键词: 涡轮机械 转子叶片 实验设计 响应面模型+ 优化设计 |
| DOI： |
| 分类号:V231.3 |
| 基金项目: |
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| Dynamic optimization design of a fan rotor based on design of experiment and response surface model |
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XUE Liang1, HAN Wan-jin1, HUANG Jia-hua2, LI Guo-zhong2
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1.School of Energy Science and Engineering,Harbin Inst.of Technology,Harbin 150001,China;2.The Second Artillery Representative office in 31st Research Inst.,Beijing 100074,China
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| Abstract: |
| The B-spline was used to parameterize the rotor stacking line,considering of the freedom of sweeping and bowing using the dynamic optimization design method and response surface model,3D viscosity N-S solver and genetic algorithm to optimize the flow field of Rotor 67 under high efficiency operating point.The results show that by using the forward-swept and bowed blade,the total pressure was significantly improved.However,optimization was done under a single operation point and its off-design performance is not good. |
| Key words: Turbomachinery Rotor blade Experiment design Response surface model+ Optimum design |
