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一种高空飞艇螺旋桨结构多目标优化设计方法

程俊杰 王海峰 尚玲玲

程俊杰, 王海峰, 尚玲玲. 一种高空飞艇螺旋桨结构多目标优化设计方法[J]. 航空动力学报, 2021, 36(3): 584-591. doi: 10.13224/j.cnki.jasp.2021.03.014
引用本文: 程俊杰, 王海峰, 尚玲玲. 一种高空飞艇螺旋桨结构多目标优化设计方法[J]. 航空动力学报, 2021, 36(3): 584-591. doi: 10.13224/j.cnki.jasp.2021.03.014
CHENG Junjie, WANG Haifeng, SHANG Lingling. Multi-objective optimization design method for propeller structure of a high-altitude airship[J]. Journal of Aerospace Power, 2021, 36(3): 584-591. doi: 10.13224/j.cnki.jasp.2021.03.014
Citation: CHENG Junjie, WANG Haifeng, SHANG Lingling. Multi-objective optimization design method for propeller structure of a high-altitude airship[J]. Journal of Aerospace Power, 2021, 36(3): 584-591. doi: 10.13224/j.cnki.jasp.2021.03.014

一种高空飞艇螺旋桨结构多目标优化设计方法

doi: 10.13224/j.cnki.jasp.2021.03.014
基金项目: 国家自然科学基金(51675428)

Multi-objective optimization design method for propeller structure of a high-altitude airship

  • 摘要: 为了远离旋转激振力的影响避免桨叶共振,需要提高桨叶的弯曲频率,这不可避免的会增加质量。为了解决低质量与高频率之间的矛盾,提出了一种螺旋桨两目标优化方法。以桨叶最小质量和最大弯曲频率作为两个优化目标,以复合材料的铺层角度、铺层厚度和铺层区域作为设计变量,以最大应变、桨尖最大位移和桨叶50%、75%和85%剖面处的扭转角作为约束,使用非支配排序遗传算法(NSGA-Ⅱ)对螺旋桨进行优化设计,得到了关于质量和频率的Pareto解集。转速为520 r/min的两叶桨的转频为8.76 Hz,穿越频率为17.33 Hz,根据频率在Pareto解集上选取远离这两个点的方案。通过制造与测试,得到的实物桨叶频率为12.29 Hz,距离两个共振点都较远,有效的避免了桨叶共振。

     

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出版历程
  • 收稿日期:  2020-07-15
  • 刊出日期:  2021-03-28

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